LAA Technical Leaflet TL 3.17 Specific type Mod Title Description Engine Engine model Reg number manufacturer ACRODUSTER 2 14500 FUEL SYSTEM CHANGE . LYCOMING IO-360-A1A BLES ACRODUSTER 2 14646 2 PLACE CANOPY FACTORY-SUPPLIED 2-PLACE SLIDE-AND-LIFT CANOPY INSTALLED. SUPPLEMENTAL ENGAGEMENT LYCOMING IO-360-A1A BLES POINTS HAVE BEEN ADDED: TWO ON THE COAMING BETWEEN THE TWO SEATS (WITH ADDITIONAL STIFFENERS) AND ONE TO THE REAR OF THE P1 POSITION. PINS ATTACHED TO THE CANOPY ENGAGE IN THESE RECEPTACLES, PROVIDING LOAD PATHS TO THE FOR VERTICAL LOAD COMPONENTS.

MECHANISMS ARE PROVIDED TO ENABLE THE CANOPY TO BE OPENED FROM EITHER SEAT POSITION AND FROM OUTSIDE THE . ACRODUSTER TOO SA750 14241 CHANGE TO SENSENICH PROPELLER CHANGE TO W76HM8-54 76" X 54" PROPELLER. LYCOMING IO-360-A1B6 CEZK W76HM8-54 ACROSPORT 1 14069 PROPELLER CHANGE TO HERCULES INSTALLATION OF HERCULES 7255458-S 72 INCH DIAMETER X 55 INCH PITCH PROPELLER. LYCOMING O-290-D BTWI 7255458-S ACROSPORT 1 14552 MAIN UNDERCARRIAGE SUSPENSION INSTALLATION OF M-222-100 SPRING TYPE MAIN UNDERCARRIAGE SHOCK IN DIRECT LYCOMING O-290-D BTWI SHOCK STRUTS INSTALLATION REPLACEMENT OF BUNGEE SHOCK STRUTS. ACROSPORT 2 11962 INVERTED FUEL AND OIL SYSTEM FIT PART 1 - RAVEN INVERTED OIL SYSTEM INSTALLATION. ECI TITAN EXP O-360- BKCV PART 2 - ELLISON EFS4-5 BODY INJECTION SYSTEM INSTALLATION. D1A1N

NOTE: G-BKCV APPROVED FOR PART 1 ONLY. ACROSPORT 2 13363 END BOLT CHANGE STEEL DOUBLE-THREADED THREAD REDUCTION INSERT USED IN STANDARD 'THICK WALLED' LYCOMING O-360-A1A CGAK CRANKSHAFT END TO ENABLE USE OF 180HP GEAR WHEEL. INSERT CONVERTS INNER THREAD (MODIFIED) FROM 1/2" UNF TO 5/16" UNF. INSERT IS LOCKED IN PACE WITH A 1/16" STEEL PIN. ACROSPORT 2 13172 PITOT TUBE RELOCATION PITOT TUBE RELOCATED FROM BETWEEN RIBS 6&7 ON LOWER RIGHTHAND WING TO BETWEEN LYCOMING O-360-A1D DAGF RIBS 6&7 ON UPPER RIGHTHAND WING. TUBING ROUTED AND SECURED ACCORDINGLY.

ACROSPORT 2 13173 TWO PLACE CANOPY FITMENT OF PITTS S2 CANOPY IN ACCORDANCE WITH THE PITTS DRAWINGS/INSTRUCTIONS. LYCOMING O-360-A1D DAGF ALUMININIUM ALLOY BAND ADDED TO EXISTING WINDSHIELD TO PROVIDE DRAUGHT-PROOF JOINT BETWEEN WINDSHIELD AND CANOPY. ACROSPORT 2 13174 P-MAGS EMAG P114 PMAG UNITS INSTALLED IN ACCORDANCE WITH MANUFACTURER'S INSTRUCTIONS, TO LYCOMING O-360-A1D DAGF REPLACE STANDARD MAGNETO IGNITION. ACROSPORT 2 14627 ENGINE CHANGE TO LYCOMING 0-360- LYCOMING O-360-A4A FITTED WITH DUAL P-MAG IGNITION UNITS. PROPELLER INSTALLED IS A LYCOMING O-360-A1D DAGF A4A SENSENICH 76EM8-0-56. ACROSPORT 2 13720 REAR COCKPIT CANOPY REAR COCKPIT FITTED WITH PITTS S2 STYLE SLIDING CANOPY. LYCOMING O-360-A3A VCIO ACROSPORT 2 13472 PITTS S2 FULL CANOPY ADDED PITTS S2 CANOPY FITTED ENCLOSING BOTH COCKPITS, USING CUSTOM FIT SLIDER AND LATCH LYCOMING O-360-A4M CCFX RETROSPECTIVELY ARRANGEMENTS ADAPTED FROM PITTS S2 DESIGN (MODIFIED) ACROSPORT 2 14459 PRINCE P-TIP 76" X 58" PROPELLER INSTALLATION OF PRINCE P-TIP 76" X 58" PROPELLER LYCOMING O-360-A4M CCFX INSTALLATION (MODIFIED) AERONCA 0-58B 13319 REPLACEMENT OF WAR TIME WING REPLACEMENT OF WAR TIME STRUTS BY OVERSIZE 4130N TUBE 3.372" x 1.429" x 0.049" PER CONTINENTAL A65-8F BRHP STRUTS APPLICANT DRAWING AERONCA 0-58B 13378 AIRWOLF REMOTE SPIN-ON OIL FILTER INSTALLATION OF AIRWOLF SPIN-ON OIL FILTER ADAPTOR MOUNTED TO FRONT OF FIREWALL VIA CONTINENTAL A65-8F BRHP ADAPTOR FABRICATED L-SHAPED BRACKET. CHAMPION CH48108-1 FILTER INSTALLED AND SECURED BY LOCK- WIRE ATTACHED TO JUBILEE CLIP TIGHTENED AROUND FILTER BODY. AERONCA 0-58B 11795 Remote Spin-On Oil Filter CONTINENTAL A65-8F BRHP AERONCA 0-58B 15202 INSTALLATION OF BATTERY, TRAY & INSTALLATION OF EARTHX ETX680C LITHIUM IRON PHOSPHATE BATTERY IN BATTERY BOX ON CONTINENTAL A65-8F BRPR FRONT OF FIREWALL TO POWER AVIONICS. INCLUDES ASSOCIATED WIRING, SWITCHING AND CIRCUIT PROTECTION. AERONCA 0-58B 13319 REPLACEMENT OF WAR TIME WING REPLACEMENT OF WAR TIME STRUTS BY OVERSIZE 4130N TUBE 3.372" x 1.429" x 0.049" PER CONTINENTAL A65-8F BRPR STRUTS APPLICANT DRAWING

Prototype mods that have been approved since 1/1/2008 Page 1 30/11/20 LAA Technical Leaflet TL 3.17 AERONCA 100 14685 HERCULES LA.10-HP PROPELLER INSTALLATION OF A HERCULES LA.10-HP 66 INCH DIAMETER X 28 INCH PITCH REPLICA OF A LANG J.A.P. J.99 AEXD INSTALLATION LA.10 PROPELLER WHICH WAS SUITABLE FOR USE ON THE J.A.P. J99 ENGINE WITH A MAXIMUM RPM OF 2400. AERONCA 11AC 13759 PROPELLER CHANGE TO HERCULES INSTALLATION OF HERCULES 7245412-S 72 INCH DIAMETER X 45 INCH PITCH PROPELLER. CONTINENTAL A65-8 BTSR 7245412-S AERONCA 11AC 12819 PROPELLER CHANGE TO LODGE CJL 100 PROPELLER CHANGE TO LODGE CJL 100 72" DIAMETER X 47" PITCH. CONTINENTAL A65-8 IIAC 72" X 47" AERONCA 65C 14218 ENGINE CHANGE TO VERNER SCARLET 7H VERNER SCARLET 7HI INSTALLED, HERCULES PROPELLER VERNER SCARLET 7HI BTRG AND PROPELLER CHANGE TO HERCULES

AERONCA 65C 14334 REPLACE ORIGINAL DRUM & . VERNER SCARLET 7HI BTRG WHEELS WITH DISK BRAKES AND TUNDRA TYRES AERONCA 7AC 14316 HERCULES 7245412-S PROPELLER INSTALLATION OF HERCULES 7245412-S 72 INCH DIAMETER X 45 INCH PITCH PROPELLER. CONTINENTAL A65-8 BRER INSTALLATION AERONCA 7AC 14634 HERCULES 7242245-S PROPELLER INSTALLATION OF HERCULES 7242245-S 72 INCH DIAMETER X 42 INCH PITCH PROPELLER CONTINENTAL A65-8 OTOE INSTALLATION AERONCA 7AC 12790 PROPELLER CHANGE TO SENSENICH PROPELLER CHANGE TO SENSENICH W72CK-42 72 INCH DIAMETER X 42 INCH PITCH. CONTINENTAL A65-8F AVDT W72CK-42 AERONCA 7AC 13530 HERCULES 7042350-S 70" X 42" INSTALLATION OF HERCULES 7042350-S 70 INCH DIAMETER X 42 INCH PITCH PROPELLER. CONTINENTAL C85-12 TECC PROPELLER INSTALLATION PROPELLER PREVIOUSLY DESCRIBED AS A 7042350-C IN ERROR. AERONCA 7AC CHAMPION 15188 FUEL VALVE REPLACED REPLACEMENT FUEL TAP INSTALLED, BURLS AIRCRAFT P/N BAR-1-2403, IN ACCORDANCE WITH FAA CONTINENTAL A65-8 BRWA STC SA02370AK. AERONCA 7AC CHAMPION 12465 OIL FILTER ADAPTER FOR SPIN ON OIL OIL FILTER ADAPTOR TO DRAWING M12465-A 10-02-09 AND CHAMPION C138 OR BLUE PRINT CONTINENTAL A65-8 BRXG FILTER ADT32109 AUTOMOTIVE OIL FILTER FITTED. WESTACH OIL TEMPERATURE GAUGE FITTED, POWERED FROM LEFT MAGNETO. AERONCA 7AC CHAMPION 13903 PROPELLER CHANGE TO HERCULES HERCULES 7245412-S PROPELLER SUBSTITUTED CONTINENTAL A65-8 BRXG 7245412-S AERONCA 7AC CHAMPION 12696 PROPELLER CHANGE TO NEWTON TYPE PROPELLER CHANGE TO NEWTON TYPE 44R, 70 INCH DIAMETER X 44 INCH PITCH CONTINENTAL A65-8F AKTR 44R 70" X 44" AERONCA 7AC CHAMPION 13737 PROPELLER CHANGE TO HERCULES HERCULES PROPELLER FITTED CONTINENTAL A75-8 ATHK 6942402-S AERONCA 7AC CHAMPION 14734 MIXTURE CONTROL OPERATING CABLE INSTALLATION OF A PLUNGER TYPE BOWDEN CABLE MIXTURE CONTROL TO FRONT COCKPIT CONTINENTAL A75-8 ATHK INSTALLATION INSTRUMENT PANEL TO OPERATE EXISTING MIXTURE CONTROL LEVER ON STROMBERG NA-S3A1 CARBURETTOR. AERONCA 7AC CHAMPION 14785 LEFT & RIGHT AUXILIARY FUEL TANKS AUXILIARY FUEL TANKS INSTALLED IN WINGS IN ACCORDANCE WITH FAA STC SA19SO EXCEPT THAT CONTINENTAL A75-8 ATHK FLEXIBLE FUEL HOSES COMPATIBLE WITH MOGAS HAVE BEEN INSTALLED BETWEEN THE AUXILIARY TANKS AND THE MAIN TANK AND GLASS FUEL FILTERS HAVE BEEN INSTALLED ON EACH COCKPIT UPRIGHT TO ENABLE FLOW OF FUEL TO BE MONITORED. AERONCA 7AC CHAMPION 14908 STC CHANGE AIR FILTER FROM FOAM TO CP1150 CHALLENGER AIR FILTER INSTALLED IN ACCORDANCE WITH FAA STC SA01669CH. CONTINENTAL A75-8 ATHK K & N COTTON FILTER AERONCA 7AC CHAMPION 15045 FITTING A TOW BAR & RELEASE TOW BAR AND RELEASE MECHANISM FITTED TO ALLOW RIBBON TOWING. CONTINENTAL A75-8 ATHK CLEARLY VISIBLE COCKPIT PLACARD TO BE FITTED STATING AIRCRAFT NOT CLEARED FOR GLIDER OR BANNER TOWING. CLEARLY VISIBLE COCKPIT PLACARD TO BE FITTED STATING MAXIMUM AIRSPEED FOR RIBBON TOWING 85 KNOTS. BASE OF ALSO OF MODIFIED TRUNCATED DESIGN, AS FOUND AT TIME OF IMPORT AERONCA 7BCM (CONV) 12401 PROPELLER CHANGE TO NEWTON TYPE CHANGE OF PROPELLER TO NEWTON TYPE 44R 72 INCH DIAMETER X 48 INCH PITCH. PROPELLER CONTINENTAL C85-8F DHAH CHAMPION 44R 72" X 48" BASED ON SENSENICH W72G-48 (STANDARD). AERONCA 7BCM (CONV) 13160 UNDERCARRIAGE GEOMETRY CHANGE UNDERCARRIAGE TRACK INCREASED TO IMPROVE GROUND HANDLING CONTINENTAL C85-8F DHAH CHAMPION Prototype mods that have been approved since 1/1/2008 Page 2 30/11/20 LAA Technical Leaflet TL 3.17 AERONCA 7BCM (CONV) 13857 FRONT STICK CONTROL MOD CRANKED FRONT SEAT CONTROL COLUMN REPLACED WITH STRAIGHT CONTROL COLUMN OF THE CONTINENTAL C85-8F DHAH CHAMPION SAME MATERIAL TO ALLOW FULL CONTROL COLUMN MOVEMENT RANGE FOR SHORTER PILOTS.

AERONCA 7BCM (CONV) 14602 SPIN-ON OIL FILTER ADAPTER INSTALLATION OF A JPM AVIATION 79001002 SPIN-ON OIL FILTER ADAPTER ONTO CONTINENTAL CONTINENTAL C85-8F DHAH CHAMPION INSTALLATION C85-8F ENGINE AND FITTED WITH A BLUEPRINT ADT32109 OIL FILTER.

ISSUE 2 RAISED TO INCLUDE CONTINENTAL A65-8F ENGINE. ISSUE 3 RAISED TO INCLUDE CONTINENTAL C90-8F ENGINE. AERONCA C3 12664 PROPELLER CHANGE TO LODGE 63" X PROPELLER CHANGE TO LODGE 63" X 32.4", COPY OF AIRSCREW MANUFACTURING Z5930 5.25 J.A.P. J.99 AEFT 32.4", COPY OF AIRSCREW Z5930 FEET DIAMETER X 2.7 FEET PITCH. AERONCA C3 14383 HERCULES LA.10-HP 66" X 28" LANG INSTALLATION OF A HERCULES LA.10-HP 66 INCH DIAMETER X 28 INCH PITCH REPLICA OF A LANG J.A.P. J.99 AEFT LA.10 REPLICA PROPELLER INSTALLATION LA.10 PROPELLER WHICH WAS SUITABLE FOR USE ON THE J.A.P. J99 ENGINE WITH A MAXIMUM RPM OF 2400. AEROPRAKT A22 FOXBAT 12378 PROP CHANGE TO KIEV 263/1700 X 40 CHANGE OF PROPELLER TO KIEV 263/1700 X 40 DEGREES PITCH AT 34CM RADIUS 912-ULS FBAT DEG AT 34CM RAD AEROPRAKT A22 FOXBAT 14194 WARP DRIVE RPM 3 BLADE 70" INSTALLATION OF WARP DRIVE RPM 3 BLADE 70" DIAMETER X 13.5 DEGREES AT TIP PROPELLER. -ULS FOXB DIAMETER PROPELLER INSTALLATION AEROPRAKT A22 FOXBAT 14281 VARLEY Li-5 LiFePO4 LITHIUM IRON INSTALLATION OF A VARLEY Li-5 LiFePO4 LITHIUM IRON PHOSPHATE BATTERY IN PLACE OF A LEAD ROTAX 912-ULS FOXB PHOSPHATE BATTERY INSTALLATION ACID BATTERY. BATTERY MOUNTING TRAY ADAPTED WITH ADDITIONAL BRACKET TO ACCOMMODATE BATTERY'S SMALLER SIZE. AEROPRAKT A22 FOXBAT 13384 CATEGORY CHANGE TO GROUP A AIRCRAFT RECONFIGURED AS SEP AEROPLANE BY LOCKING FLAPPERON FUNCTION TO OPERATE AS ROTAX 912-ULS CWTD ONLY, IN NEUTRAL POSITION USING FIXED ALUMINIUM ANGLE LINK FITTED TO FLAP SYSTEM IN CABIN ROOF INSTEAD OF STANDARD SLOTTED GATE AND FLAP LEVER. FLAP LEVER COVER RETAINED TO PROTECT MECHANISM IN HEAD STRIKE AREA AEROPRAKT A22 FOXBAT 14151 CATEGORY CHANGE TO MICROLIGHT FLAPPERON FUNCTION RESTORED TO ALLOW STALL SPEED TO QUALIFY AS MICROLIGHT ROTAX 912-ULS CWTD AEROPRAKT A22 FOXBAT 13021 INVERT OIL COOLER OIL COOLER INVERTED TO BRING PIPEWORK OUT AT TOP RATHER THAN AT BOTTOM, PER ROTAX ROTAX 912-ULS GFOX RECOMMENDATIONS AEROPRAKT A22-L FOXBAT 14162 TRIM SPRING BIAS TRIM SYSTEM FITTED TO AILERON CONTROL SYSTEM ROTAX 912-ULS PHOX AEROPRAKT A22-L FOXBAT 13542 CATEGORY CHANGE TO MICROLIGHT NOISE CERTIFICATE ISSUED, RE-WEIGH AND PLACARD. MAX PERMITTED EMPTY WEIGHT AS ROTAX 912-ULS CESI MICROLIGHT 285 KG. AEROPRAKT A22-L FOXBAT 13021 INVERT OIL COOLER OIL COOLER INVERTED TO BRING PIPEWORK OUT AT TOP RATHER THAN AT BOTTOM, PER ROTAX ROTAX 912-ULS CEOP RECOMMENDATIONS AEROPRAKT A22-L FOXBAT 13310 RUDDER ANTI BALANCE TAB PUSH ROD RUDDER ANTI BALANCE TAB OPERATING CABLE REPLACED BY OPERATING PUSHROD AND ROTAX 912-ULS CEWR SUPPLIED BY DRAGON AVIATION ALTERNATIVE ATTACHMENT BRACKET. TAB HINGE ATTACHMENT DOUBLERS ADDED. INSTALL IN CONJUNCTION WITH DRAGON AVIATION INSTRUCTIONS 'FITTING INSTRUCTIONS RUDDER ANTI BALANCE TAB'. AEROPRAKT A22-L FOXBAT 12305 SOFT START MODULE INSTALLATION OF CON-AIR SPORTS SOFT START MODULE TO ROTAX 912-ULS ENGINE IN ROTAX 912-ULS FBTT ACCORDANCE WITH CON-AIR SPORTS INSTRUCTIONS AND SM12305 LEAFLET. AEROPRAKT A22-L FOXBAT 12683 FITTING OF FUEL FLOW METER ELECTRONICS INTERNATIONAL FT-60 FUEL FLOW TRANSDUCER FITTED TO FUEL SYSTEM, ROTAX 912-ULS EOID CONNECTED TO A DYNON FLIGHTDEK D180 EFIS UNIT. AEROPRAKT A22-L FOXBAT 15207 FUEL TANKS SLOSHING COMPOSITE FUEL TANKS COATED INTERNALLY WITH RUSTBUSTER TANK SEAL. TANKS COATED ROTAX 912-ULS EOID EXTERNALLY WITH EPOXY PAINT. REPLACEMENT FUEL OUTLET AND STRAINER INSTALLED. ADDITIONAL IN-LINE FUEL FILTERS ADDED. AEROPRAKT A22-L FOXBAT 13665 INSTALLATION OF MGL FF-1 FUEL INSTALLATION OF MGL FF-1 FUEL FLOW COMPUTER UTILISING PLASTIC FUEL FLOW TRANSDUCER, ROTAX 912-ULS OFGC MANAGEMENT COMPUTER WITH RESTRICTOR JET, DRILLED OUT TO 2.8 MM DIAMETER, FITTED DOWNSTREAM OF FUEL FILTER SITUATED BEHIND PASSENGER SEAT. AEROPRAKT A22-L FOXBAT 13075 FUEL FLOW SENSOR FLOSCAN 201A-6 FUEL FLOW SENSOR INSTALLED IN FUEL SYSTEM. SENSOR LOCATED ON ROTAX 912-ULS CGSX STARBOARD COCKPIT WALL ADJACENT TO RUDDER PEDAL ATTACHMENT BRACKET; BETWEEN FUEL FILTER AND MECHANICAL FUEL PUMP.

Prototype mods that have been approved since 1/1/2008 Page 3 30/11/20 LAA Technical Leaflet TL 3.17 AEROPRAKT A22-L FOXBAT 13149 SPRING SOLUTION TO PROVIDE RUDDER DELETION OF RUDDER ANTI-BALANCE TAB AND INSTALLATION OF RUDDER CABLE SPRING DEVICES, ROTAX 912-ULS CGSX PEDAL FORCE FEEDBACK CLAMPING ON TO THE RUDDER CONTROL CABLE AFT OF THE CROSS-MEMBER BEHIND THE SEAT.

AEROPRAKT A22-L FOXBAT 13311 RUDDER CENTERING SPRINGS FITTED TO RUDDER CENTERING SPRINGS FITTED AS PER DOCUMENT 'RUDDER CONTROL CIRCUIT ROTAX 912-ULS CGSX RUDDER CABLES IN COCKPIT MODIFICATION' REVISION 4.1 DATED 23.2.12.

RUDDER ANTI BALANCE TAB REMOVED INCLUDING HINGES, OPERATING CABLE AND CABLE ATTACHMENT BRACKET. AEROPRAKT A22-LS FOXBAT 13920 DYNON DUAL AXIS AUTO-PILOT 2 AXIS AUTO-PILOT INSTALLED USING FACTORY DESIGNED INSTALLATION KIT INCLUDING DYNON ROTAX 912-ULS FOXV INSTALLATION SV32 (PITCH) AND SV42 (ROLL) SERVOS. CONTROLLED BY DYNON SKYVIEW UNIT.

AT ISSUE 2 INCLUDES THE PROVISION FOR THE SKYVIEW UNIT TO PROVIDE PITCH TRIM CONTROL, INCLUDING AUTOTRIM WHEN THE IS ENGAGED. AEROPRAKT A22-LS FOXBAT 14836 REMOVABLE RUDDER PEDALS MANUALLY REMOVABLE RUDDER PEDALS FITTED, REMOVED BY UNDOING THROUGH-BOLTS ROTAX 912-ULS FOXV AEROPRAKT A22-LS FOXBAT 14839 CENTER ARMREST ARMREST CONSTRUCTED FROM ALLOY SHEETS LOCATED OVER THE CENTRE CONSOLE. INCLUDES ROTAX 912-ULS FOXV SMALL STOWAGE COMPARTMENT VIA A LOCKABLE HINGED COVER. AEROPRAKT A22-LS FOXBAT 14615 FUEL FLOW METER INSTALLATION OF MGL FUEL FLOW SENDER IN ACCORDANCE WITH MANUFACTURER'S ROTAX 912-ULS MILR INSTRUCTIONS. SENDER IS LOCATED BEHIND P2 SEAT AFTER A FILTER. SENDER IS CONNECTED TO AN MGL FF-1 FUEL COMPUTER. AEROPRAKT A22-LS FOXBAT 13920 DYNON DUAL AXIS AUTO-PILOT 2 AXIS AUTO-PILOT INSTALLED USING FACTORY DESIGNED INSTALLATION KIT INCLUDING DYNON ROTAX 912-iS FXBA INSTALLATION SV32 (PITCH) AND SV42 (ROLL) SERVOS. CONTROLLED BY DYNON SKYVIEW UNIT.

AT ISSUE 2 INCLUDES THE PROVISION FOR THE SKYVIEW UNIT TO PROVIDE PITCH TRIM CONTROL, INCLUDING AUTOTRIM WHEN THE AUTOPILOT IS ENGAGED. AEROPRAKT A32 VIXXEN 15175 SEAT ADJUSTMENT . ROTAX 912-ULS CLEH AEROTECHNIK EV-97 EUROSTAR 13123 CATEGORY CHANGE TO MICROLIGHT . ROTAX 912-UL CBWG

AEROTECHNIK EV-97 EUROSTAR 12661 CATEGORY CHANGE TO GROUP A ADDITIONAL FUEL PUMP FITTED ROTAX 912-UL PROW

AEROTECHNIK EV-97 EUROSTAR 13193 CATEGORY CHANGE TO MICROLIGHT . ROTAX 912-UL PROW

AEROTECHNIK EV-97 EUROSTAR 15129 WOODCOMP PROPULS AE174 1740MM INSTALLATION OF WOODCOMP PROPULS AE174 1740MM DIAMETER PROPELLER. ROTAX 912-UL DSKI DIAMETER PROPELLER INSTALLATION

AEROTECHNIK EV-97 EUROSTAR 14943 CATEGORY CHANGE TO MICROLIGHT . ROTAX 912-UL CCMP

AEROTECHNIK EV-97 EUROSTAR 13164 CATEGORY CHANGE TO MICROLIGHT . ROTAX 912-UL CCMO

AEROTECHNIK EV-97 EUROSTAR 13305 CATEGORY CHANGE TO GROUP A ELECTRIC FUEL PUMP MUST BE FITTED, MTWA INCRESED TO480 KG, PLACARDS AND WEIGHT ROTAX 912-UL CCMO SCHEDULE AMENDED AEROTECHNIK EV-97 EUROSTAR 13394 CATEGORY CHANGE TO MICROLIGHT NO PHYSICAL CHANGE REQUIRED EXCEPT TO PLACARDS AND WEIGHT SCHEDULE, NOISE ROTAX 912-UL CCMO CERTIFICATE. NEW PERMIT WITH DESIGNATION CHANGED TO EV-97 REQUIRED

Prototype mods that have been approved since 1/1/2008 Page 4 30/11/20 LAA Technical Leaflet TL 3.17 AEROTECHNIK EV-97 EUROSTAR 15437 IGNITECH IGNITION MODULES (SMD) TWIN IGNITECH IGNITION MODULES INSTALLED TO REPLACE ROTAX MODULES ROTAX 912-UL CCMO

MODULES INSTALLED ON COCKPIT SIDE OF FIREWALL ON A CUSTOM TRAY MADE FROM FOLDED ALUMINIUM SHEET THE TRAY IS STOOD OFF FROM THE FIREWALL, AND INSULATED USING FIBERFRAX, TO PROTECT THE MODULES IN CASE OF ENGINE FIRE THE WIRING LOOMS ARE PROTECTED USING AN AUTOMOTIVE HEAT-RESISTANT SHEATH

MODULES ALSO 12V DC POWERED WHEN MOTOR ENGAGED

NOTE: UPPER SECTION OF FIREWALL ALSO INSULATED USING FIBERFRAX (PROTECTED FROM DAMAGE USING AN AUTOMOTIVE ALUMINIUM-COATED HEAT-RESISTANT MAT) AEROTECHNIK EV-97 EUROSTAR 14711 CATEGORY CHANGE FROM GROUP A TO REVERT TO MICROLIGHT CONFIGURATION AND 450 KG MTWA ROTAX 912-UL DODG MICROLIGHT MICROLIGHT NOISE CERTIFICATE ALREADY EXISTS DESIGNATION EV-97 RATHER THAN EV-97A AEROTECHNIK EV-97 EUROSTAR 13873 CATEGORY CHANGE TO MICROLIGHT TRANSFER TO MICROLIGHT CATEGORY ROTAX 912-UL CDCC

AEROTECHNIK EV-97 EUROSTAR 14717 PROP CHANGE TO PROPULS AE174 WOODCOMP PROPULS AE174 1740 MM DIAMETER X 16 DEGREES PITCH AT 50 MM FROM TIP ROTAX 912-UL VORN INSTALLED ON ROTAX 912-UL. AEROTECHNIK EV-97 EUROSTAR 14986 CKT EXHAUST SYSTEM STANDARD EVEKTOR EXHAUST SYSTEM REPLACED WITH CKT SYSTEM COMPRISING 4 HEADERS, 1 ROTAX 912-UL VORN SILENCER, 1 TAILPIPE AND SPRINGS. AEROTECHNIK EV-97 EUROSTAR 13791 MOUNTING OF STROBES AND INSTALLATION OF TWO SKYBEACON STROBE UNITS, ONE CENTRALLY ON THE TURTLE DECK 0.5M ROTAX 912-UL CDOZ TRANSPONDER AERIAL AFT OF CANOPY, ONE ON UNDERSIDE BETWEEN THE FLAPS. INSTALLATION OF TRANSPONDER ANTENNA ADJACENT TO THE LOWER STROBE UNIT. BOTH STROBES AND TRANSPONDER ANTENNA MOUNTING AREAS REINFORCED WITH 100 X 100MM DOUBLER RIVETED IN PLACE. AEROTECHNIK EV-97 EUROSTAR 15505 IGNITECH IGNITION MODULES TWIN IGNITECH IGNITION MODULES INSTALLED TO REPLACE ROTAX MODULES ROTAX 912-UL CECY IGNITECH LOOM MADE FROM FRNC (FLAME RESISTANT NON CORROSIVE) WIRING

MODULES INSTALLED ON COCKPIT SIDE OF FIREWALL BEHIND INSTRUMENT PANEL FIBERFRAX INSULATION BETWEEN FIREWALL AND MODULES

MODULES ALSO 12V DC POWERED WHEN STARTER MOTOR ENGAGED AEROTECHNIK EV-97 EUROSTAR 13088 CATEGORY CHANGE TO GROUP A STANDARD CHANGE OF FUEL PUMP PER REQUIREMENT FOR GROUP A VERSION ROTAX 912-UL CDVD

AEROTECHNIK EV-97 EUROSTAR 14332 CATEGORY CHANGE TO MICROLIGHT CATEGORY CHANGE TO MICROLIGHT PER EXISTING ACCEPTED CONFIGURATION ROTAX 912-UL CDVD

AEROTECHNIK EV-97 EUROSTAR 14283 TWIN FUEL PUMPS EXPERIMENTAL TWIN ELECTRIC FUEL PUMP INSTALLATION, ALLOWING DELETION OF ENGINE ROTAX 912-UL ZZAC DRIVEN PUMP TO PREVENT POSSIBLE VAPOUR LOCK AND OTHER PROBLEMS WITH EDP. AEROTECHNIK EV-97 EUROSTAR 15244 CATEGORY CHANGE TO GROUP A CHANGE OF CATEGORY TO GROUP A WITH INCREASE IN MAXIMUM TOTAL WEIGHT AUTHORISED ROTAX 912-UL ZZAC TO 480 KGS AEROTECHNIK EV-97 EUROSTAR 15280 CATEGORY CHANGE TO MICROLIGHT AIRCRAFT CONVERTED TO EV-97 MICROLIGHT MODEL ROTAX 912-UL ORAU

AEROTECHNIK EV-97 EUROSTAR 14781 CATEGORY CHANGE TO GROUP A Category Change ROTAX 912-UL CFLL

AEROTECHNIK EV-97 EUROSTAR 14499 INSTAL 1 PAIR OF MINATURE LED 2 OFF LED LIGHTS AND ASSOCIATED WIRING, SWITCH AND FUSE INSTALLED. LIGHTS MOUNTED IN ROTAX 912-UL CFTZ LANDING LAMPS FRONT FACE OF LOWER ENGINE COWLING. AEROTECHNIK EV-97 EUROSTAR 14082 CATEGORY CHANGE TO MICROLIGHT CATEGORY CHANGE TO MICROLIGHT AND MAX GROSS WEIGHT REDUCED TO 450 Kg. OPTIONAL ROTAX 912-UL CGOG ELECTRIC FUEL PUMP REMAINS IN PLACE AND FUNCTIONING

Prototype mods that have been approved since 1/1/2008 Page 5 30/11/20 LAA Technical Leaflet TL 3.17 AEROTECHNIK EV-97 EUROSTAR 12813 ENGINE CHANGE TO ROTAX 914UL -UL FITTED BUT WITH TURBO ECU REPLACED WITH OVER-PRESSURE VALVE SET TO 1220 ROTAX 912-ULS RMPY DERATED TO 100 BHP MILLIBARS ACTING AS AUTOMATIC WASTEGATE, LIMITING POWER OUTPUT TO A AMXAMUM OF 100 BHP AT SEA LEVEL STANDARD DAY CONDITIONS AEROTECHNIK EV-97 EUROSTAR 12988 INSTALLATION OF RBA 300 BATTERY RBA 300 BATTERY INSTALLED IN EXISTING BATERY BOX WITH HARD FOAM PACKING TO FILL ROTAX 912-ULS RMPY UNWANTED SPACE. NO CHANGE TO ELECTRICAL INSTALLATION REQUIRED AEROTECHNIK EV-97 EUROSTAR 13351 ENGINE CHANGE TO ROTAX 912iS ROTAX 912-iS INSTALLED PER FACTORY INSTALLATION REQUIREMENTS ROTAX 912-ULS RMPY

AEROTECHNIK EV-97 EUROSTAR 14366 CATEGORY CHANGE FROM GROUP A TO ENGINE ROTAX 912-ULS WITH WOODCOMP KLASSIC 170/3 R PROPELLER ROTAX 912-ULS RMPY MICROLIGHT AEROTECHNIK EV-97 EUROSTAR 13142 WOODCOMP KLASSIC 170/2/R INSTALLATION OF WOODCOMP KLASSIC 170/2/R 1700MM DIAMETER 2 BLADED GROUND ROTAX 912-UL CGTT SL ADJUSTABLE PROPELLER. AEROTECHNIK EV-97 EUROSTAR 13707 REPLACEMENT OF SEAT HARNESSES AERO-TUFF SEAT BELTS SUBSTITUTED OF THE SAME PATTERN SUPPLIED WITH VANS RV KITS. ROTAX 912-UL CGTT SL STEPPED WASHERS FITTED TO INSTALL TO EXISTING MOUNTING BOLTS AEROTECHNIK EV-97 EUROSTAR 13886 ENGINE CHANGE TO ROTAX 912ULS AND ENGINE CHANGED TO ROTAX 912-ULS WITH WOODCOMP PROPELLER TYPE KLASSIC 170/3/R ROTAX 912-ULS EVPH SL PROPELLER CHANGE AEROTECHNIK EV-97 EUROSTAR 14661 WOODCOMP PROPULS AE 174, 1740 MM INSTALLATION OF A WOODCOMP PROPULS AE 174, 1740 MM DIAMETER GROUND ADJUSTABLE ROTAX 914-UL (MODIFIED) CHMW SL DIAMETER PROPELLER INSTALLATION PROPELLER.

AEROTECHNIK EV-97A 12854 CATEGORY CHANGE TO GROUP A . ROTAX 912-UL CBJR EUROSTAR AEROTECHNIK EV-97A 14499 INSTAL 1 PAIR OF MINATURE LED 2 OFF LED LIGHTS AND ASSOCIATED WIRING, SWITCH AND FUSE INSTALLED. LIGHTS MOUNTED IN ROTAX 912-UL CBJR EUROSTAR LANDING LAMPS FRONT FACE OF LOWER ENGINE COWLING. AEROTECHNIK EV-97A 14089 CATEGORY CHANGE TO GROUP A REQUIRED ELECTRIC FUEL PUMP ALREADY FITTED. ROTAX 912-UL OTUN EUROSTAR MAX GROSS WEIGHT INCREASED TO 480 Kg AEROTECHNIK EV-97A 13016 CATEGORY CHANGE TO GROUP A STANDARD RECONFIGURATION TO EV-97A ROTAX 912-UL CBRR EUROSTAR AEROTECHNIK EV-97A 13060 CATEGORY CHANGE FROM MICROLIGHT . ROTAX 912-UL CCCO EUROSTAR TO GROUP A AEROTECHNIK EV-97A 12504 CATEGORY CHANGE TO GROUP A AUXILLIARY FUEL PUMP ADDED AND PLACARDS REVISED TO BRING AIRCRAFT INTO COMPLIANCE ROTAX 912-UL CCKL EUROSTAR WITH AAN PFA-315-427 SUP 1 ISSUE 6 AEROTECHNIK EV-97A 12360 CATEGORY CHANGE FROM MICROLIGHT INSTALLATION OF ELECTRIC FUEL PUMP WITH COSMIK AVIATION SUPPLIED UPGRADE KIT TO ROTAX 912-UL CDIY EUROSTAR TO GROUP A ENABLE CATEGORY CHANGE FROM MICROLIGHT TO GROUP A. AEROTECHNIK EV-97A 14755 CATEGORY CHANGE TO GROUP A CATEGORY CHANGE TO SEP AIRCRAFT AS EV-97A ROTAX 912-UL EZZY EUROSTAR AEROTECHNIK EV-97A 14251 CATEGORY CHANGE TO GROUP A CATEGORY CHANGE TO GROUP A WITH 480 Kg MTWA ROTAX 912-UL CFEL EUROSTAR ELECTRIC FUEL BOOST PUMP ADDED NEW WEIGHT AND BALANCE REPORT AEROTECHNIK EV-97B 14039 AVEO POWERBURST AVEO POWERBURSTPLUS POSITION/NAV/STROBE LIGHTS BOLTED TO EACH USING 2 OFF ROTAX 912-ULS GVSL EUROSTAR SL STROBE/NAV/POSITION LIGHTS M3 STAINLESS BOLTS. LIGHTS WIRED TO AIRCRAFT ELECTRICAL SUPPLY VIA 20 AWG CABLES AND A 3A FUSE. A CABLE BETWEEN THE LIGHTS ENSURES SYCHRONISATION. AEROTECHNIK EV-97B 14059 FLOSCAN 201 FUEL FLOW TRANSDUCER FLOSCAN 201A-6 FUEL FLOW TRANSDUCER INSERTED IN FUEL LINE BETWEEN FILTER AND FUEL ROTAX 912-ULS GVSL EUROSTAR SL INSTALLATION PUMP. MOUNTED AFT OF THE FIREWALL IN ACCORDANCE WITH THE MANUFACTURER'S INSTRUCTIONS. AEROTECHNIK EV-97B 14747 KANARDIA DUAL AXIS AUTO-PILOT INSTALLATION OF KANARDIA DUAL AXIS AUTO-PILOT CONTROLLED VIA KANARDIA NESIS EFIS. ROTAX 912-ULS GVSL EUROSTAR SL INSTALLATION ROLL SERVO INSTALLED USING EVEKTOR MOUNTING BRACKET ATTACHED TO FLOOR UNDER CONTROL COLUMN AND LINKED TO AILERON PUSH-ROD AT . PITCH SERVO INSTALLED USING EVEKTOR MOUNTING BRACKET ATTACHED TO FLOOR ADJACENT TO ROLL SERVO AND CONNECTED VIA EVEKTOR BELLCRANK BONDED AND RIVETED TO PITCH TORQUE TUBE.

Prototype mods that have been approved since 1/1/2008 Page 6 30/11/20 LAA Technical Leaflet TL 3.17 ANDREASSON BA4B 13790 SMOKE SYSTEM INSTALLATION OF CUSTOM MADE SMOKE SYSTEM UTILISING A 10.5 LITRE TANK MOUNTED CONTINENTAL O-200-A YPSY UNDERNEATH THE MAIN AND PREVIOUSLY USED AS AN AUXILIARY FUEL TANK. OIL PUMP AND OPERATING SOLENOID VALVE MOUNTED TO REAR FACE OF FIREWALL. SMOKE OIL DELIVERY SET TO 2 LITRES/HOUR. ANDREASSON BA4B 12786 AMENDMENT TO MTWA MTWA INCREASE TO 480 Kg LYCOMING IO-320-B1A AYFV APPLICABLE ONLY TO CROSBY BUILT AIRCRAFT OF WHICH THIS IS THE SOLE SURVIVING EXAMPLE

ANDREASSON BA4B 13750 WEIGHT INCREASE TO 495KG, MAX INCREASE IN MAX GROSS WEIGHT TO 495 Kg LYCOMING IO-320-B1A AYFV AEROBATIC WEIGHT AND MLW OF 480 MAX LANDING WEIGHT AND AEROBATIC WEIGHT OF 480 KG INTRODUCED KG & REVISED G LIMITS REDUCED G LIMITS AT GROSS WEIGHTS OVER 480 KG ARROW ACTIVE 2 13919 DH GIPSY III DUE TO NON-AVAILABILITY OF ORIGINAL PARTS, REPLACEMENT FORGED ALUMINIUM ALLOY DE HAVILLAND GIPSY 3 ABVE ASSEMBLIES MANUFACTURED BY ROSS RACING PISTONS WITH MINOR VARIATIONS FROM ORIGINAL DESIGN ARV1 12761 ENGINE CHANGE TO JABIRU A2200 HEWLAND ENGINE REPLACED BY A FITTED USING CUSTOM MADE FOUR-LEG ENGINE JABIRU 2200A DEXP MOUNT, INCLUDING FITTING OF ADDITIONAL FUSELAGE HARD POINT TO ACCEPT FOUR-LEG MOUNT. ARV1 12961 PROPELLER CHANGE TO GT-2 157/100 INSTALLATION OF GT-2 157/100, 157 CM DIAMETER X 100 CM PITCH. JABIRU 2200A DEXP ARV1 SUPER 2 14903 ENGINE CHANGE TO ROTAX 912 ULS ENGINE CHANGED TO ROTAX 912-ULS WITH GSC TECH-III 68" DIAMETER PROPELLER USING HEWLAND AE75-D POOL SIMILAR INSTALLATION AS ALREADY APPROVED BY LAA ON G-OTAL/G-XARV AND G-BMWF AIRCRAFT ARV1 SUPER 2 13212 AUXILIARY FUEL TANK - RESTRICTED TO REMOVABLE AUXILLIARY FUEL TANK MOUNTED IN BAGGAGE COMPARTMENT PER APPLICANT'S ROTAX 914-F YARV 13 LITRES SUBMISSION. MANDATORY PLACARD MUST BE FITTED AS DESCRIBED IN FLIGHT MANUAL SUPPLEMENT REF LAA mod 13212. FLIGHT MANUAL SUPPLEMENT TO BE APPENDED TO POH ARV1 SUPER 2 (MODIFIED) 13510 FERRY TANK INSTALLATION TEMPORARY INSTALLATION OF 20 LITRE NATO JERRY CAN ON PASSENGER'S SEAT, USING SEAT BELT ROTAX 912-ULS OTAL AND ADDITIONAL STRAPPING TO SECURE IT, TO EXTEND RANGE. FUEL TRANSFERRED TO MAIN TANK USING FACET ELECTRIC FUEL PUMP THROUGH ADDITIONAL FUEL HOSE PLUMBED INTO MAIN FUEL SUPPLY LINE ADJACENT TO MAIN TANK OUTLET. FUEL TRANSFER LINE AND VENT LINE CONNECTED USING QUICK RELEASE COUPLINGS. AURORA 13346 PROPELLER CHANGE TO ARPLAST ARPLAST ECOPROP 1700L 130/3 PEOPELLER FITTED HKS 700E CBZS ECOPROP AUSTER 3 13271 NEWTON 48L01 6 FT 4 IN X 4 FT 7 IN INSTALLATION OF NEWTON 48L01 6 FEET 4 INCH DIAMETER X 4 FEET 7 INCH PITCH PROPELLER - DE HAVILLAND GIPSY MAJOR 1 AHLK PROPELLER INSTALLATION COPIED FROM DE HAVILLAND 5220/P PROPELLER. AUSTER 4 12682 ENGINE CHANGE TO LYCOMING O-290- ENGINE CHANGED TO LYCOMING O-290-D2 WITH HOFFMANN HO23B-190-112 PROPELLER. LYCOMING O-290-D2 AJXV D2 ENGINE MOUNT MODIFIED TO SUIT BOLT GEOMETRY. AUSTER 5 13170 GT-2/198/NO-FW133SRTC PROPELLER INSTALLATION OF GT-2/198/NO-FW133SRTC 198CM DIAMETER X 98CM PITCH PROPELLER. LYCOMING O-290-3 AKXP AUSTER 5 13055 PROPELLER CHANGE TO NEWTON 50R PROPELLER CHANGE TO NEWTON TYPE 50R 190CM X 112CM, COPIED FROM A HOFFMANN HO30- LYCOMING O-290-3 AJGJ 190CM X 112CM 190 112. THE USE OF THE NEWTON PROPELLER IS PERMITTED ONLY WHEN THE MAXIMUM NUMBER OF OCCUPANTS AUTHORISED IS TWO. AUSTER 5 13874 REPLACEMENT AIR FILTER FOR ENGINE ALTERNATIVE BRACKETT ENGINE INTAKE AIR FILTER TYPE BA-4106 WITH ASSOCIATED CUSTOM LYCOMING O-290-3 AJGJ ADAPTER PLATE AUSTER 5 14509 PROPELLER CHANGE TO HERCULES Z5600-HERCULES COPY OF Z5600 PROPELLER FITTED PREVIOUSLY EXCEPT MATERIAL CHANGED FROM LYCOMING O-290-3 ALBK HP 78" X 42" MAHOGANY TO BEECH AND HERCUTHANE INCORPORATED AUSTER 5 13875 INSTALLATION FOR ALTERNATOR FITTED IN PLACE OF STANDARD GENERATOR LYCOMING O-290-3 AJXC LYCOMING O-290-3 AUSTER 5 13876 REMOTE OIL FILTER INSTALLATION FOR REMOTE OIL FILTER FITTED LYCOMING O-290-3 AJXC LYCOMING O-290-3 AUSTER 5 13877 PROPELLER CHANGE TO MCCAULEY PROPELLER SUBSTITUTED AS ABOVE LYCOMING O-290-3 AJXC 1A170/DM 7647 Prototype mods that have been approved since 1/1/2008 Page 7 30/11/20 LAA Technical Leaflet TL 3.17 AUSTER 5D (MODIFIED) 13681 PROPELLER CHANGE TO HERCULES INSTALLATION OF HERCULES 7859280-ST 78 INCH DIAMETER X 59 INCH PITCH PROPELLER. DE HAVILLAND GIPSY MAJOR 1C AKSZ 7859280-ST AUSTER 5D (MODIFIED) 14254 ENGINE CHANGE TO GIPSY MAJOR 1C ENGINE REPLACED WITH GIPSY MAJOR 1C DE HAVILLAND GIPSY MAJOR 1C AKSZ AUSTER 5J1 14496 FIT TURBO ALTERNATOR WIND DRIVEN ALTERNATOR BPE-14 FITTED TO LOWER FUSELAGE FORWARD OF . BLACKBURN CIRRUS MINOR 2 AHAO

AUSTER 5J1 14497 FIT NEW BATTERY ON FIREWALL FITMENT OF VARLEY LI-16 BATTERY TO FORWARD FACE OF FIREWALL USING VARLEY BATTERY BOX. BLACKBURN CIRRUS MINOR 2 AHAO

AUSTER 5J1 14498 FIT BEACON PSA TRIMCRAFT 8002ACB-R-12V BEACON MOUNTED TO UPPER FUSELAGE. INCLUDES ASSOCIATED BLACKBURN CIRRUS MINOR 2 AHAO WIRING, SWITCH AND CIRCUIT BREAKER. AUSTER 5J1 14299 REINSTATEMENT OF ORIGINAL REAR ORIGINAL SINGLE REAR SEAT RE-FITTED, REAR LAP STRAPS RE-FITTED, PLACARDS AND WEIGHT BLACKBURN CIRRUS MINOR 2A AIGD SEAT SCHEDULE AMENDED ACCORDINGLY. OPERATING LIMITATIONS SHEET UPDATED ACCORDINGLY

AUSTER 5J1 13290 ALAN JAMES AJ7249/AWC/CIRR 72" X 49" INSTALLATION OF ALAN JAMES AJ7249/AWC/CIRR 72 INCH DIAMETER X 49 INCH PITCH (6.0' X CIRRUS MINOR II AIZU PROPELLER 4.04') PROPELLER BASED ON PERMALLI Z5701 5.5' X 4.78' PROPELLER FROM AUSTER 5J1 G-AMTM.

AUSTER 5J1S 13008 HERCULES 7859277-S 78" X 59" INSTALLATION OF HERCULES 7859277-S 78 INCH DIAMETER X 59 INCH PITCH PROPELLER. DE HAVILLAND GIPSY MAJOR 10 MK AMKU PROPELLER 2-2 AUSTER 5J2 13329 ENGINE & PROPELLER CHANGE CONTINENTAL C85-12 ENGINE AND JAMES 72" x 36" PROPELLER FITTED CONTINENTAL C85-12 AJAM AUSTER 5J2 ARROW 13107 CONTINENTAL C90-12F (MODIFIED) WITH CHANGE OF ENGINE TO CONTINENTAL C90-12F (MODIFIED) WITH MCCAULEY 1A105/SCM 71 INCH CONTINENTAL C90-12F(MODIFIED) BEAH MCCAULEY 1A105/SCM7152 PROPELLER DIAMETER X 52 INCH PITCH PROPELLER.

AUSTER 5J4/100 14672 MT-V-1-F/175-08 PROPELLER INSTALLATION OF MT-V-1-F/175-08, 175CM DIAMETER ELECTRIC CONSTANT SPEED PROPELLER CONTINENTAL O-200-A AIJT INSTALLATION USING AN MT PCU-120 ELECTRONIC CONTROLLER. AUSTER 6A 13741 AUSTER MK6 FLIGHT CONTROL SYSTEM - REVERSION TO SINGLE PILOT CONTROLS, REMOVAL OF FRONT RIGHT HAND SEAT AND HARNESS, DE HAVILLAND GIPSY MAJOR 10 MK ARIH SINGLE PILOT CONTROL AND INSTALLATION OF AIR OBSERVATION POST EQUIPMENT INCLUDING FIRST AID BOX, 1-1 IDENTIFICATION LAMP, SPARE ID LAMP LENS BOX AND LENSES, CROW BAR (LIGHTWEIGHT REPLICA), SIGNAL PISTOL HOLDER SIGNAL, PISTOL CARTRIDGE HOLDER AND CARTRIDGES (REPLICAS), TRAILING AERIAL CABLE GUIDE (REPLICA) AND OVERHEAD REAR VIEW MIRROR.

AUSTER 6A 12809 FITTING OF DUAL CONTROLS DUAL CONTROLS FITTED RETROSPECTIVELY TO STANDARD AUSTER PATTERN DE HAVILLAND GIPSY MAJOR 10 MK APRO 1-1 AUSTER 6A 12968 PROPELLER CHANGE TO DH 5220/P25R INSTALLATION OF DE HAVILLAND 5220/P25R 6 FT 4 INCH DIAMETER X 4 FT 7 INCH PITCH DE HAVILLAND GIPSY MAJOR 10 MK APRO 6'4" X 4'7" PROPELLER. 1-1 AUSTER 6A 14991 RE-FIT MACWHYTE STAINLESS TAIL 4 OFF MACWHYTE AN704AC STAINLESS STEEL TAIL WIRES FITTED IN PLACE OF ORIGINALS. DE HAVILLAND GIPSY MAJOR 10 MK APRO WIRES 1-1 AUSTER 6A 15076 HERCULES 7859280-ST 78" x 59" INSTALLATION OF HERCULES 7859280-ST 78 INCH DIAMETER X 59 INCH PITCH PROPELLER. DE HAVILLAND GIPSY MAJOR 10 MK APRO PROPELLER INSTALLATION 1-1 AUSTER 6A (MODIFIED) 13760 GRP NOSE COWLING MANUFACTURE AND INSTALLATION OF NOSE COWLING MADE FROM GLASS REINFORCED PLASTIC DE HAVILLAND GIPSY MAJOR 10 MK ARXU (GRP) COMPRISING RA7725 BIDIRECTIONAL GLASSCLOTH, WEST SYSTEMS 105/206 EPOXY 1-1A PROTECTED WITH SCOTT BADER CRYSTIC FIREGUARD 75PA EXCEL PAINT. AUSTER AOP.9 14983 STARTER MOTOR INSTALLATION INSTALLATION OF ROTAX STARTER MOTOR PT. NO. C.0225, INCLUDING STARTER SOLENOID, BLACKBURN BOMBARDIER 20801 BKVK STARTER SWITCH, STARTER ISOLATOR SWITCH AND STARTER ENGAGED WARNING LIGHT. AUSTER AOP.9 13653 INTRODUCTION OF NEW WIRING ALL WIRING REPLACED PER APPLICANT'S DESCRIPTION BLACKBURN BOMBARDIER 20801 BURR

AUSTER AOP.9 13697 M AAB5 24 091 BOLT . BLACKBURN BOMBARDIER 20801 BURR

AUSTER AOP.9 13704 NAVIGATION AND STROBE LIGHTS PLUS NAVIGATION AND STROBE LIGHTS INTRODUCED, WITH ASSOCIATED WIRING BLACKBURN BOMBARDIER 20801 BURR ADDITIONAL WIRING AUSTER D4-108 14232 HERCULES 7140481-S PROPELLER INSTALLATION OF HERCULES 7140481-S 71 INCH DIAMETER X 40 INCH PITCH PROPELLER. LYCOMING O-235-C1 ARLG INSTALLATION

Prototype mods that have been approved since 1/1/2008 Page 8 30/11/20 LAA Technical Leaflet TL 3.17 AUSTER D6 SERIES 180 14212 MTV-12-B/188-59f PROPELLER INSTALLATION OF MTV-12-B/188-59f PROPELLER LYCOMING O-360-A1A ARCS INSTALLATION AUSTER J1N 13569 HERCULES 7859280-ST 78" X 59" INSTALLATION OF HERCULES 7859280-ST 78 INCH DIAMETER X 59 INCH PITCH PROPELLER DE HAVILLAND GIPSY MAJOR 1 AHHH PROPELLER INSTALLATION AUSTER J1N 13855 ORATEX 6000 FABRIC SYSTEM ON COVERING OF WINGS AND AILERONS WITH ORATEX 6000 FABRIC IN ACCORDANCE WITH ORATEX DE HAVILLAND GIPSY MAJOR 1 AJAE AUSTER J1N FITTING INSTRUCTIONS. AT ISSUE 2, FOLLOWING RE-COVERING OF G-AJAE THIS MOD IS AMENDED TO INCLUDE OPTION OF AND ELEVATORS AS WELL AS WINGS AND AILERONS BEING COVERED IN ORATEX 6000, OR ANY OF THESE SURFACES SINGLY. AUSTER J1N 13415 HERCULES 7856258-ST 78" X 56" INSTALLATION OF HERCULES 7856258-ST 78 INCH DIAMETER X 56 INCH PITCH PROPELLER DE HAVILLAND GIPSY MAJOR 1 AIGF PROPELLER INSTALLATION AUSTER J1N 12832 PROPELLER CHANGE TO HOFFMANN PROPELLER REPLACED WITH STANDARD HOFFMAN ALTERNATIE AS LISTED ON AAN FOR THE J1N DE HAVILLAND GIPSY MAJOR 1 AGXN HO21-198B-140LK AUSTER J1N 13296 HERCULES 7856258-ST 78" X 56" INSTALLATION OF HERCULES 7856258-ST 78 INCH DIAMETER X 56 INCH PITCH PROPELLER. DE HAVILLAND GIPSY MAJOR 1 AJAJ PROPELLER INSTALLATION AUSTER J1N 13855 ORATEX 6000 FABRIC SYSTEM ON COVERING OF WINGS AND AILERONS WITH ORATEX 6000 FABRIC IN ACCORDANCE WITH ORATEX DE HAVILLAND GIPSY MAJOR 1 AJAS AUSTER J1N FITTING INSTRUCTIONS. AT ISSUE 2, FOLLOWING RE-COVERING OF G-AJAE THIS MOD IS AMENDED TO INCLUDE OPTION OF TAILPLANE AND ELEVATORS AS WELL AS WINGS AND AILERONS BEING COVERED IN ORATEX 6000, OR ANY OF THESE SURFACES SINGLY. AUSTER J1N 14636 ENGINE CHANGE TO LYCOMING O-320- GIPSY MAJOR ENGINE SUBSTITUTED WITH LYCOMING 0-320-E2D WITH MCCAULEY 1A 175/GM 80" LYCOMING O-320-E2D AHSS E2D WITH MCAULEY 1A 175 PROP x 52" PROPELLER, USING AIREDALE ENGINE MOUNT AND CUSTOM COWLINGS. FIN NOT FITTED TO THIS AIRCRAFT AT CONVERSION. AUSTER J1U 13770 ENGINE CHANGE TO SUPERIOR XP-IO-360-INSTALLATION OF SUPERIOR XP-IO-360-B1AC2, ASSEMBLED BY SWIFTAIR MAINTENANCE LTD, SUPERIOR XP-IO-360-B1AC2 APMH B1AC2 LEICESTER, WITH MCCAULEY 2D36C14-BEG/78KM-4 74 INCH DIAMETER CONSTANT SPEED PROPELLER. AUSTER J1U 14585 REPLACEMENT EXHAUST STANDARD VANS OP-54 EXHAUST FITTED, AS NORMALLY SUPPLIED FOR RV TYPE AIRCRAFT SUPERIOR XP-IO-360-B1AC2 APMH AUSTER J1U 14968 MTV-12-B-183-59b PROPELLER INSTALLATION OF AN MTV-12-B-183-59b PROPELLER SUPERIOR XP-IO-360-B1AC2 APMH INSTALLATION AUSTER J5F 14609 AIRSCREW Z8014/5/C PROPELLER INSTALLATION OF AIRSCREW Z8014/5/C 6.84 FEET DIAMETER X 3.53 FEET PITCH PROPELLER. DE HAVILLAND GIPSY MAJOR 1 AMZT INSTALLATION AUSTER J5F 13751 PROPELLER CHANGE TO HERCULES INSTALLATION OF HERCULES 7859280-ST 78 INCH DIAMETER X 59 INCH PITCH PROPELLER. DE HAVILLAND GIPSY MAJOR 10 MK AMTA 7859280-ST 78" X 59" 1-3 AUSTER J5L 12647 CURTIS DRAIN VALVE MOD 3 OFF EXISTING BRASS DRAIN PLUGS DRILLED AND TAPPED TO ACCEPT CURTIS DRAIN VALVES. DE HAVILLAND GIPSY MAJOR 10 MK AMYD FITTED ONE TO EACH TANK AND TO THE GASCOLATOR. DOORS MODIFIED WITH CUT-OUT TO 2 ALLOW CLEARANCE. AVID AEROBAT (MODIFIED) 14071 INSTALL ROTEC E-IGNITION UPGRADE ROTEC E-IGNITION UNIT INSTALLED IN PLACE OF STARBOARD MAGNETO IN ACCORDANCE WITH JABIRU 2200A BUON 'ROTEC AEROSPORT - JABIRU ELECTRIC UPGRADE KITS - INSTALLATION GUIDE 21/11/2014 REV 1.10'. AIRCRAFT ELECTRICAL SYSTEM AS PER FIGURE 5.1 OF THAT MANUAL. MK4 (MODIFIED) 13896 ELECTRIC CARBURETTOR HEATERS INSTALLATION OF AIRCRAFT GRAPHIX ELECTRIC CARBURETTOR HEATER AND ELECTRONIC FREEZE- ROTAX 912-UL PILL ALERT THERMOMETER TO BOTH OF THE BING CARBURETTORS OF THE ROTAX 912-UL ENGINE.

AVID HAULER MK4 12449 ENGINE CHANGED TO JABIRU 2200A JABIRU 2200A ENGINE INSTALLED RETROSPECTIVELY PER AAN PFA 189-352 SUP 1 ISSUE 2 JABIRU 2200A BWRC AVID SPEED WING 12727 ALUMINIUM AVID FUEL TANK SUBSTITUTE FUEL TANKS MANUFACTURED TO DRAWINGS SUPPLIED AND PROOF PRESSURE TESTED BMW R100 BTRC IN ACCORDANCE WITH NORMAL AVIATION PRACTISE AVID SPEEDWING 12307 NOSE WHEEL UNDERCARRIAGE RETROFIT OF FACTORY OPTIONAL NOSEWHEEL UNDERCARRIAGE BVFO AVID SPEEDWING 12618 PROPELLER CHANGE TO GSC TECH III 66 PROPELLER CHANGE TO GSC TECH III 66 INCH DIAMETER GROUND ADJUSTABLE 2 BLADED. ROTAX 582 BVFO INCH DIA AVID SPEEDWING 12816 ROTAX GEARBOX CHANGE FROM TYPE B 3:1 RATIO C TYPE GEARBOX FITTED, PROPELLER PITCH ADJUSTED ACCORDINGLY ROTAX 582 BVFO TO TYPE C AVID SPEEDWING 12502 POWERFIN FL270T PROPELLER POWERFIN FL270T GROUND ADJUSTABLE TWO BLADED PROPELLER USED WITH 2.58:1 B TYPE ROTAX 582 NANO GEARBOX. FACTORY-SUPPLIED A2-70 SS 304 SOCKET HEAD SCREWS USED FOR ATTACHMENT.

Prototype mods that have been approved since 1/1/2008 Page 9 30/11/20 LAA Technical Leaflet TL 3.17 AVID SPEEDWING 13907 SUPPLEMENTARY FORWARD RADIATOR ADDITIONAL TRANSVERSE RADIATOR FITTED TO BOTTOM LIP OF ENGINE COWL TO HELP IMPROVE ROTAX 582 NANO LIQUID COOLING OF ROTAX 582 ENGINE. RADIATOR FITTED TO LOWER COWLING USING SUITABLE REMOVEABLE BRACKETS. AVID SPEEDWING 15072 PEERY 71" X 37" PROPELLER INSTALLATION OF PEERY 71" X 37" PROPELLER. ROTAX 582 NANO INSTALLATION AVID SPEEDWING (MODIFIED) 13649 ENGINE CHANGE TO FIT ROTAX 582 C 3:1 C BOX FITTED, WITH IVOPROP 3 BLADED 72" DIAMETER PROPELLER ROTAX 582 BVIV BOX AND AND PROP CHANGE AVID SPEEDWING MK4 12750 LASER SINTERED NYLON POWDER LASER SINTERED NYLON AIRBOX SUBSTITUTED FOR ALUMINIUM ORIGINAL, TO SUIT JABIRU 2200A BVYX PROTOTYPING AIR BOX REPLACEMENT ENGINE. AVID SPEEDWING MK4 13416 RAY ALLEN ELECTRIC PITCH TRIM SYSTEM INSTALLATION OF RAY ALLEN 6A SERVO TO CUSTOM MADE ALUMINIUM PLATE ATTACHED TO JABIRU 2200A BVYX INSTALLATION PORT TAILPLANE UNDERSIDE UNDER COVERING FABRIC TO OPERATE A HINGED . SERVO COVERED WITH AERODYNAMIC FAIRING. AVID SPEEDWING MK4 12501 PROPELLER CHANGE GROUND ADJUSTABLE VERSION OF THE IVOPROP THREE BLADED 72" DIAMETER SUBSTITUTED, TO ROTAX 582 OZEE AVOID COMPLICATION OF IN-FLIGHT ADJUSTABLE PITCH VERSION AVRO 504K 13616 REPLACEMENT OF LE RHONE 110HP REPLACEMENT PISTON ASSEMBLIES MANUFACTURED TO PATTERN USING SUBSTITUTE MATERIALS LE RHONE 110 HP ADEV ENGINE PISTON ASSEMBLIES AND PROCESSES AVRO 504K 13617 REPLACEMENT OF LE RHONE 110HP REPLACEMENT LINERS MADE TO PATTERN USING SUBSTITUTE MATERIALS AND LE RHONE 110 HP ADEV ENGINE CYLINDER LINERS PROCESSES AVRO 504K 13618 REPLACEMENT OF LE RHONE 110HP REPLACEMENT CONNECTING RODS MADE TO PATTERN USING SUBSTITUTE MATERIALS AND LE RHONE 110 HP ADEV ENGINE CONNECTING RODS PROCESSES BA SWALLOW 2 13150 UNDERCARRIAGE SUPPORT ORIGINAL UNDERCARRIAGE SUPPORT STRUT FOUND CORRODED INTERNALLY, SO REPLACED WITH POBJOY NIAGRA III ADPS REPLACEMENT PATTERN PART MADE FROM 4130 N MATERIAL. WELDING TO BE BY A SUITABLY CAA APPROVED WELDER BARKER CHARADE 12939 MAIN WHEEL SPATS TO PREVENT MUD CONVENTIONAL MOULDED FIBREGLASS WHEEL SPATS ADDED JABIRU 2200A CBUN ON WING/APPEARANCE/DRAG REDUCTION BEAGLE A.109 15058 PROPELLER CHANGE TO HARTZELL HC- INSTALLATION OF HARTZELL HC-C2YR-1BFP/F7497 CONSTANT SPEED PROPELLER ON LYCOMING O- LYCOMING O-360-A1A ASRK C2YR-1BFP/F7497 360-A1A. BEAGLE A.61 SERIES 2 13296 HERCULES 7856258-ST 78" X 56" INSTALLATION OF HERCULES 7856258-ST 78 INCH DIAMETER X 56 INCH PITCH PROPELLER. DE HAVILLAND GIPSY MAJOR 10 MK ASCH PROPELLER INSTALLATION 1-1 BEAGLE A.61 SERIES 2 12911 HOFFMANN HO21-198B 146LK INSTALLATION OF HOFFMANN HO21-198B 146LK PROPELLER DE HAVILLAND GIPSY MAJOR 10 MK ASAJ PROPELLER 1-1A BEAGLE AUSTER D5 SERIES 180 13506 SENSENICH M76EMMS-0-60 76" X 60" INSTALLATION OF SENSENICH M76EMMS-0-60 76 INCH DIAMETER X 60 INCH PITCH PROPELLER. LYCOMING O-360-A1A ASNC PROPELLER INSTALLATION BEDE BD-4 13711 DUAL ELECTRONIC IGNITION DUAL LIGHTSPEED PLASMA 1 FITTED LYCOMING O-320-A2B BOPD FLIGHT MANUAL SUPPLEMENT REFERS BEDE BD-4 12367 NOSE LEG STRUT NOSE LEG STRUT HOME MANUFACTURED TO DESIGNER'S DRAWINGS AND INCORPORATING BD-4 LYCOMING O-320-E2F BYLS DESIGN IMPROVEMENT '4-56' THAT CALLS FOR INCREASED WALL THICKNESS OF 0.125 INCH INSTEAD OF 0.065 INCH. LGN-3A REINFORCEMENT STRAP, AS CALLED UP IN PREVIOUS MODIFICATION TO 0.065 WALL THICKNESS STRUT, ALSO FITTED. BEDE BD-4 13745 PROPELLER CHANGE TO HERCULES HERCULES 7262408-S 72 INCH DIAMETER X 62 INCH PITCH PROPELLER INSTALLATION. LYCOMING O-320-E2F BYLS 7262408-S BENSEN B8 12481 ENGINE CHANGE SUBSTITUTED ROTAX 532 BCGB BENSEN B8MR 14276 SIMPLE ROTOR A CONVENTIONAL BENSEN-STYLE ROTOR BRAKE FITTED, OPERATED BY PRESSING FORWARD ON ROTAX 532 BUPF THE STICK AFTER SETTING THE BRAKE IN THE 'ON' POSITION AT THE MAST HEAD. CONVENTIONAL BUNGEE AUTO-RELEASE

Prototype mods that have been approved since 1/1/2008 Page 10 30/11/20 LAA Technical Leaflet TL 3.17 BENSEN B8MR 14277 FUEL CONTENT ASSESSMENT SAFETY INSTRUMENT SYSTEM ENHANCED BY THE ADDITION OF FUEL LEVEL AND FUEL FLOW SENSORS ROTAX 532 BUPF ENHANCEMENT DISPLAYING VIA CUSTOM DISPLAY UNIT ALSO SHOWING PITCH TRIM POSITION.

INSTALLATION PARTIALLY APPROVED AT THIS TIME WITH FUEL LEVEL ONLY FUNCTIONAL, FUEL FLOW SENSOR REMOVED DUE TO ERRONEOUS READINGS WHEN ELECTRIC PUMP OPERATED. FUEL FLOW INDICATOR MARKED INOP PENDING RESOLUTION BENSEN B8MR 14278 ADJUSTABLE PITCH TRIM PITCH TRIM CONTROLLED VIA CONVENTIONAL TRIM BIAS SPRINGS BUT OPERATED VIA AN ROTAX 532 BUPF ELECTRIC JACK, POSITION INDICATED ON CUSTOM ELECTRONIC DISPLAY ALONG WITH FUEL QUANTITY, FLOW AND FUEL REMAINING. OPERATING SWITCH FITTED IN VICINITY OF THROTTLE CONTROL ON LEFT HAND SIDE OF COCKPIT. CONVENTIONAL SAFETY BUNGEES INCLUDED THROUGH TRIM SPRINGS TO RETAIN PIECES OF SPRING IF SPRING FAILS, PREVENTING PROP OR ROTOR STRIKE. BOLKOW BO 208C JUNIOR 12515 CONVERT TO SPIN-ON ENGINE OIL FILTER SPIN-ON OIL FILTER FITTED OF STCed TYPE. CONTINENTAL O-200-A ATDO

BOLKOW BO 208C JUNIOR 13658 ZEFTRONICS G1200N GENERATOR INSTALLATION OF ZEFTRONICS G1200N GENERATOR CONTROL UNIT SUBSTITUTING DELCO REMY CONTINENTAL O-200-A ATDO CONTROL UNIT 1118736 REGULATOR. BOLKOW BO-208A2 JUNIOR 14304 CONSPICUITY LIGHTS INSTALLATION OF TWO 28LED LIGHT UNITS IN FRONT ENGINE BAFFLES FOR INCREASED CONTINENTAL O-200-A ASZD CONSPICUITY BOLKOW BO-208A2 JUNIOR 12515 CONVERT TO SPIN-ON ENGINE OIL FILTER SPIN-ON OIL FILTER FITTED OF STCed TYPE. CONTINENTAL O-200-A ASZD

BOWERS FLY BABY 1A 13490 SUSPENDED RUDDER PEDALS WITH TOE SUBSTITUTION OF FLOOR-HINGED RUDDER PEDALS AND HYDRAULIC HEEL BRAKES WITH NEW CONTINENTAL C90-14F UPID OPERATED BRAKE PEDALS SUSPENDED RUDDER PEDALS INCORPORATING VANS RV CYLINDERS AND BRAKE PEDALS. BOWERS FLY BABY 1A 12322 ENGINE CHANGE TO CONTINENTAL O- CHANGE OF ENGINE TO CONTINENTAL O-200-A WITH MCCAULEY 1A105/SCM 71 INCH DIAMETER X CONTINENTAL O-200-A BUYU 200-A WITH MCCAULEY 1A105/SCM 71 X 46 INCH PITCH PROPELLER INSTALLED. 46 BOWERS FLY BABY 1A 12609 PROPELLER CHANGE TO NEWTON TYPE PROPELLER CHANGE TO NEWTON TYPE 07R 69 INCH DIAMETER X 45 INCH PITCH. CONTINENTAL O-200-A BUYU 07R 69" X 45" BOWERS FLY BABY 1A 12957 HERCULES 6945242 69" X 45.5" INSTALLATION OF HERCULES 6945242 69 INCH DIAMETER X 45.5 INCH PITCH PROPELLER. CONTINENTAL O-200-A BUYU BOWERS FLY BABY 1A/1B 12567 MACHINE GUN NOISE SIMULATOR PROPANE/OXYGEN SYSTEM INSTALLED BASED ON WELDING TORCH TECHNOLOGY WITH CONTINENTAL C90-8F BNPV ELECTRONIC IGNITION / IGNITOR AND SAFETY PRESSURE RELIEF VALVE BRANDLI BX2 CHERRY 13159 HERCULES 6359274-S 63" X 59" INSTALLATION OF HERCULES 6359274-S 63 INCH DIAMETER X 59 INCH PITCH PROPELLER. CONTINENTAL C90-12F BXUX PROPELLER BRISTELL NG5 SPEED WING 14950 DYNON AUTOPILOT INSTALLATION INSTALLATION OF DYNON DUAL AUTOPILOT SYSTEM, CONSISTING OF DYNON SV32 PITCH SERVO JABIRU 3300A CILL AND SV42 ROLL SERVO MOUNTED IN STANDARD BRACKETS AND USING HARDWARE SUPPLIED BY THE AIRFRAME MANUFACTURER. SERVOS ARE CONTROLLED BY A DYNON D100 EFIS UNIT AND PANEL MOUNTED AP74 INTERFACE UNIT. PITCH TRIM IS DISABLED UNTIL AN ARMING SWITCH IS DEPRESSED. BRISTELL NG5 SPEED WING 14130 RE-POSITION TRIM SWITCHES INSTALLATION OF TWO RAY ALLEN TRIM SWITCHES IN CENTRE CONSOLE AFT OF THROTTLE LEVER. JABIRU 3300A NTPS HOOP GUARD INSTALLED BETWEEN SWITCHES. BRISTELL NG5 SPEED WING 14422 DYNON AUTOPILOT INSTALLATION DYNON DUAL-AXIS AUTOPILOT SYSTEM INSTALLED, CONSISTING OF SV32 AND SV42 SERVOS JABIRU 3300A RVEA CONTROLLED BY A DYNON D180 EFIS. SERVOS MOUNTED AND CONNECTED TO CONTROL SYSTEM USING BRACKETS AND FIXTURES SUPPLIED BY THE AIRCRAFT KIT MANUFACTURER. SYSTEM INCORPORATES REQUIRED TRIM DISCONNECT SWITCH. BRISTELL NG5 SPEED WING 14181 DYNON SKYVIEW DUAL AXIS AUTO-PILOT INSTALLATION OF DYNON DUAL AXIS AUTO-PILOT CONTROLLED WITH DYNON SKYVIEW EFIS. ROTAX 912-ULS DLAF INSTALLATION BRISTELL NG5 SPEED WING 14181 DYNON SKYVIEW DUAL AXIS AUTO-PILOT INSTALLATION OF DYNON DUAL AXIS AUTO-PILOT CONTROLLED WITH DYNON SKYVIEW EFIS. ROTAX 912-ULS PIPZ INSTALLATION BRISTELL NG5 SPEED WING 15441 WOODCOMP SR3000/3N 1720MM INSTALLATION OF WOODCOMP SR3000/3N 1720MM DIAMETER PROPELLER ROTAX 912-ULS PIPZ DIAMETER PROPELLER INSTALLATION

Prototype mods that have been approved since 1/1/2008 Page 11 30/11/20 LAA Technical Leaflet TL 3.17 BRISTELL NG5 SPEED WING 14505 DYNON SKYVIEW DUAL AXIS AUTO-PILOT INSTALLATION OF A DYNON SKYVIEW DUAL AXIS AUTO-PILOT WITH DYNON BUTTON MODULE ROTAX 912-ULS CIPT INSTALLATION AUTO-PILOT CONTROL INTERFACE. INCLUDES VARIABLE SPEED AUTO-TRIM THAT OPERATES WHEN AUTO-PILOT IS ENGAGED AND REVERTS TO FIXED REDUCED TRIM SPEED WHEN AUTO-PILOT IS DISENGAGED. BRISTELL NG5 SPEED WING 14730 WOODCOMP SR3000/3N 1720MM WOODCOMP SR3000/3N 1720MM DIAMETER PROPELLER INSTALLATION ROTAX 912-ULS CIPT DIAMETER PROPELLER INSTALLATION BRISTELL NG5 SPEED WING 14830 ELECTRONICS INTERNATIONAL EI FT-60 INSTALLATION OF ELECTRONICS INTERNATIONAL EI FT-60 'RED CUBE' FUEL FLOW TRANSDUCER IN ROTAX 912-ULS JANF FUEL FLOW TRANSDUCER INSTALLATION FUEL LINE TO PORT CARBURETTOR ONLY.

BRISTELL NG5 SPEED WING 14231 GARMIN G3X DUAL AXIS AUTO-PILOT INSTALLATION OF GARMIN G3X DUAL AXIS AUTO-PILOT WITH A GMC 307 CONTROLLER AND ROTAX 912-ULS JANF INSTALLATION INCORPORATING PITCH TRIM SPEED CONTROL, AUTO-TRIM AND TRIM RUNAWAY PROTECTION.

BRISTELL NG5 SPEED WING 14751 PITCH TRIM SYSTEM MODIFICATIONS MANUFACTURE AND INSTALLATION OF A LONG PITCH TRIM OPERATING HORN AND LONGER ROTAX 912-ULS JANF TRAVEL RAY ALLEN PITCH TRIM SERVO T3-12A TO MECHANICALLY REDUCE PITCH TRIM OPERATING SPEED WITHOUT THE NEED FOR A SERVO SPEED REDUCER. TAILPLANE LOWER SKIN REINFORCED LOCALLY AROUND LONGER SLOT NECESSARY FOR SERVO PUSH-ROD. BRISTELL NG5 SPEED WING 14582 FIT BRS FOR SAFETY BRS-7 LSA AIRCRAFT PARACHUTE RECOVERY SYSTEM FITTED. ROCKET AND PARACHUTE PACK ROTAX 912-ULS ZGAB LOCATED BETWEEN INSTRUMENT PANEL AND FIREWALL. ACTIVATION HANDLE ATTACHED TO LOWER EDGE OF INSTRUMENT PANEL, INCORPORATING SAFETY PIN. INCLUDES BRIDLES TO ATTACH PARACHUTE TO AIRFRAME AND ASSOCIATED INTERNAL AND EXTERNAL WARNING PLACARDS. BRISTELL NG5 SPEED WING 14950 DYNON AUTOPILOT INSTALLATION INSTALLATION OF DYNON DUAL AUTOPILOT SYSTEM, CONSISTING OF DYNON SV32 PITCH SERVO ROTAX 912-ULS ZGAB AND SV42 ROLL SERVO MOUNTED IN STANDARD BRACKETS AND USING HARDWARE SUPPLIED BY THE AIRFRAME MANUFACTURER. SERVOS ARE CONTROLLED BY A DYNON D100 EFIS UNIT AND PANEL MOUNTED AP74 INTERFACE UNIT. PITCH TRIM IS DISABLED UNTIL AN ARMING SWITCH IS DEPRESSED. BRISTELL NG5 SPEED WING 14735 INSTALLATION OF FT60 FUEL FLOW FT60 FUEL FLOW METER MOUNTED TO FIREWALL, BETWEEN ELECTRIC FUEL PUMP AND ENGINE- ROTAX 912-ULS CJRS METER DRIVEN PUMP, AS PER MANUFACTURER'S INSTRUCTIONS. BRISTELL NG5 SPEED WING 14751 PITCH TRIM SYSTEM MODIFICATIONS MANUFACTURE AND INSTALLATION OF A LONG PITCH TRIM OPERATING HORN AND LONGER ROTAX 912-ULS CJRS TRAVEL RAY ALLEN PITCH TRIM SERVO T3-12A TO MECHANICALLY REDUCE PITCH TRIM OPERATING SPEED WITHOUT THE NEED FOR A SERVO SPEED REDUCER. TAILPLANE LOWER SKIN REINFORCED LOCALLY AROUND LONGER SLOT NECESSARY FOR SERVO PUSH-ROD. BRISTELL NG5 SPEED WING 14387 LITHIUM POWERBLOC 11S INSTALLATION OF LITHIUM POWERBLOC 11S BATTERY IN STANDARD BATTERY CONTAINER IN ROTAX 912-ULS COLF ENGINE BAY. BRISTELL NG5 SPEED WING 14783 AUTOPILOT INSTALLATION DYNON 2-AXIS AUTOPILOT INSTALLED, CONSISTING OF CUSTOM SERVO MOUNTS, 2 OFF DYNON ROTAX 912-ULS COLF SV42 SERVOS, CONTROLLED BY DYNON SKYVIEW UNIT. SYSTEM INCORPORATES A TRIM ISOLATION BUTTON. BRISTELL NG5 SPEED WING 15154 SILENT HEKTIK THERMOSTATICALLY INSTALLATION OF SILENT HEKTIK INTEGRATED OIL VALVE PT.NO. F1210 REPLACING OIL PUMP ROTAX 912-ULS COLF CONTROLLED OIL & COOLANT VALVE HOUSING FRONT PLATE, THERMOSTATICALLY CONTROLLED TO DIRECT OIL THROUGH THE OIL INSTALLATIONS COOLER WHEN THE OIL TEMPERATURE IS ABOVE 85°C AND SILENT HEKTIK INTEGRATED COOLANT VALVE PT.NO. F1208 REPLACING COOLANT PUMP HOUSING, THERMOSTATICALLY CONTROLLED TO DIRECT COOLANT THROUGH THE COOLANT RADIATOR WHEN THE COOLANT TEMPERATURE IS ABOVE 80°C BRISTELL NG5 SPEED WING 14181 DYNON SKYVIEW DUAL AXIS AUTO-PILOT INSTALLATION OF DYNON DUAL AXIS AUTO-PILOT CONTROLLED WITH DYNON SKYVIEW EFIS. ROTAX 912-ULS CKTN INSTALLATION BRISTELL NG5 SPEED WING 14972 SHORAI LITHIUM IRON PHOSPHATE INSTALLATION OF SHORAI LFX18L1-BS12 LITHIUM IRON PHOSPHATE BATTERY IN PLACE OF ROTAX 912-ULS CKTN BATTERY STANDARD LEAD ACID BATTERY.

Prototype mods that have been approved since 1/1/2008 Page 12 30/11/20 LAA Technical Leaflet TL 3.17 BRISTELL NG5 SPEED WING 14973 FUEL FLOW TRANSDUCER EI RED CUBE FT-60 FUEL FLOW SENSOR AND IN-LINE FILTER ADDED TO FUEL SYSTEM BETWEEN ROTAX 912-ULS CKTN FUEL RETURN LINE JUNCTION AND CARBURETTORS, MOUNTED IN ENGINE BAY IN ACCORDANCE WITH THE MANUFACTURER'S INSTRUCTIONS. BRISTELL NG5 SPEED WING 15308 AIRMASTER AP332SCTFH-WWR68W 68 AIRMASTER AP332SCTFH-WWR68W(CW)-RE2.25-10.3SP-200F1.5RME 68 INCH DIAMETER ROTAX 912-ULS CKTN INCH DIAMETER PROPELLER PROPELLER INSTALLATION. INSTALLATION BRISTELL NG5 SPEED WING 14886 INSTALLATION OF FUEL FLOW TWO FT-60 FUEL FLOW TRANSDUCERS INSTALLED, ONE ON THE FLOW LINE AND ONE ON THE ROTAX 912-ULS STUU TRANSDUCERS RETURN LINE. TRANSDUCERS MOUNTED IN ACCORDANCE WITH THE MANUFACTURER'S INSTRUCTIONS IN THE ENGINE BAY. BRISTELL NG5 SPEED WING 15320 MGL iEFIS EXPLORER DUAL AXIS AUTO- INSTALLATION OF MGL DUAL AUTO-PILOT SYSTEM, COMPRISING MGL ROLL AND PITCH SERVOS ROTAX 912-ULS STUU PILOT INSTALLATION MOUNTED IN STANDARD BRACKETS AND USING HARDWARE SUPPLIED BY THE AIRFRAME MANUFACTURER BRM AERO. SERVOS ARE CONTROLLED BY AN MGL iEFIS EXPLORER EFIS UNIT WITH iBOX. PITCH TRIM IS DISABLED UNTIL AN ARMING SWITCH ON LEFT OF THROTTLE HANDLE IS DEPRESSED.

BRISTELL NG5 SPEED WING 14181 DYNON SKYVIEW DUAL AXIS AUTO-PILOT INSTALLATION OF DYNON DUAL AXIS AUTO-PILOT CONTROLLED WITH DYNON SKYVIEW EFIS. ROTAX 912-ULS NGCC INSTALLATION BRISTELL NG5 SPEED WING 14923 SHORAI LITHIUM IRON PHOSPHATE INSTALLATION OF SHORAI LFX18A1-BS12 LITHIUM IRON PHOSPHATE BATTERY IN PLACE OF ROTAX 912-ULS NGCC BATTERY STANDARD LEAD-ACID BATTERY. BRISTELL NG5 SPEED WING 15068 KASPAR KA1/2-PA 1620MM DIAMETER INSTALLATION OF KASPAR KA1/2-PA 1620MM DIAMETER PROPELLER WITH KASPAR K-850M-000 ROTAX 912-ULS NGAA PROPELLER INSTALLATION ELECTRONIC CONTROLLER WHICH ALTERS BLADE PITCH BASED ON AIRSPEED, VIA THE AIRCRAFT'S PITOT/STATIC SYSTEM. DUE TO THE POSSIBILITY OF PROPELLER PITCH CONTROL FAILURE CAUSING ENGINE OVER-SPEED AN ELECTRONIC ENGINE MANAGEMENT SYSTEM (EMS) OR OTHER DEVICE THAT RECORDS RECENT ENGINE RPM HISTORY MUST BE FITTED AND BE OPERATIONAL. BRISTELL NG5 SPEED WING 14631 ADDITION OF STANDARD BRISTELL AUTO- STANDARD BRISTELL AUTO PILOT SERVO INSTALLATION CONNECTED TO DYNON SKYVIEW SYSTEM. ROTAX 912-ULS IOVE PILOT SERVOS PITCH TRIM FITTED WITH MOMENTARY SWITCH TO ENABLE SYSTEM MOVEMENT. BRISTELL NG5 SPEED WING 14631 ADDITION OF STANDARD BRISTELL AUTO- STANDARD BRISTELL AUTO PILOT SERVO INSTALLATION CONNECTED TO DYNON SKYVIEW SYSTEM. ROTAX 912-ULS LNDA PILOT SERVOS PITCH TRIM FITTED WITH MOMENTARY SWITCH TO ENABLE SYSTEM MOVEMENT. BRISTELL NG5 SPEED WING 14505 DYNON SKYVIEW DUAL AXIS AUTO-PILOT INSTALLATION OF A DYNON SKYVIEW DUAL AXIS AUTO-PILOT WITH DYNON BUTTON MODULE ROTAX 912-ULS MLSY INSTALLATION AUTO-PILOT CONTROL INTERFACE. INCLUDES VARIABLE SPEED AUTO-TRIM THAT OPERATES WHEN AUTO-PILOT IS ENGAGED AND REVERTS TO FIXED REDUCED TRIM SPEED WHEN AUTO-PILOT IS DISENGAGED. BRISTELL NG5 SPEED WING 14973 FUEL FLOW TRANSDUCER EI RED CUBE FT-60 FUEL FLOW SENSOR AND IN-LINE FILTER ADDED TO FUEL SYSTEM BETWEEN ROTAX 912-ULS MLSY FUEL RETURN LINE JUNCTION AND CARBURETTORS, MOUNTED IN ENGINE BAY IN ACCORDANCE WITH THE MANUFACTURER'S INSTRUCTIONS. BRISTELL NG5 SPEED WING 14631 ADDITION OF STANDARD BRISTELL AUTO- STANDARD BRISTELL AUTO PILOT SERVO INSTALLATION CONNECTED TO DYNON SKYVIEW SYSTEM. ROTAX 912-ULS ORBT PILOT SERVOS PITCH TRIM FITTED WITH MOMENTARY SWITCH TO ENABLE SYSTEM MOVEMENT. BRISTELL NG5 SPEED WING 14631 ADDITION OF STANDARD BRISTELL AUTO- STANDARD BRISTELL AUTO PILOT SERVO INSTALLATION CONNECTED TO DYNON SKYVIEW SYSTEM. ROTAX 912-ULS MOGN PILOT SERVOS PITCH TRIM FITTED WITH MOMENTARY SWITCH TO ENABLE SYSTEM MOVEMENT. BRISTELL NG5 SPEED WING 14231 GARMIN G3X DUAL AXIS AUTO-PILOT INSTALLATION OF GARMIN G3X DUAL AXIS AUTO-PILOT WITH A GMC 307 CONTROLLER AND ROTAX 912-iS CIPG INSTALLATION INCORPORATING PITCH TRIM SPEED CONTROL, AUTO-TRIM AND TRIM RUNAWAY PROTECTION.

BRISTELL NG5 SPEED WING 14353 FITTING OF EARTHX ETX 900 LITHIUM FITMENT OF EARTHX ETX900 LITHIUM IRON PHOSPHATE BATTERY IN THE STANDARD BATTERY ROTAX 912-iS CIPG BATTERY MOUNT ON THE FORWARD FACE OF THE FIREWALL. BATTERY WARNING OUTPUT CONNECTED TO GARMIN G3X.

IN ADDITION, APPROVAL OF EARTHX BATTERY MODELS ETX680C, ETX680, ETX12A, ETX18C, ETX18F, ETX24C, ETX24D, ETX36C, ETX36D AND ETX36E FOR INCLUSION IN SM14337. BRISTELL NG5 SPEED WING 15180 PARK BRAKE OPERATING LEVER STANDARD PUSH-PULL PARK BRAKE MECHANISM REPLACED WITH LEVER-TYPE PARK BRAKE ROTAX 912-iS CIPG MOUNTED ON THE CENTRE CONSOLE. Prototype mods that have been approved since 1/1/2008 Page 13 30/11/20 LAA Technical Leaflet TL 3.17 BRISTELL NG5 SPEED WING 14541 SUPERCHARGED ROTAX 912 ULS ENGINE FITTED WITH FLYGAS OPERATING AT 8.925 TIMES CRANKSHAFT SPEED ROTAX 912-ULS (MODIFIED) NGII (4.2:1 INTERNAL GEARS AND 2.125 PULLEY RATIO). ENGINE MODIFIED WITH COMPRESSION REDUCING SPACER RINGS, IMPROVED CRANKCASE JOINT DOWELS AND WELDED CRANKSHAFT. G- NGII FLIGHT MANUAL SUPPLEMENT SUPERCHARGED ENGINE REFERS, ALSO AAN LAA-385-1000 Supp 5. BRISTELL NG5 SPEED WING 14631 ADDITION OF STANDARD BRISTELL AUTO- STANDARD BRISTELL AUTO PILOT SERVO INSTALLATION CONNECTED TO DYNON SKYVIEW SYSTEM. ROTAX 912-ULS (MODIFIED) NGII PILOT SERVOS PITCH TRIM FITTED WITH MOMENTARY SWITCH TO ENABLE SYSTEM MOVEMENT. BUCKER BU133C 14550 IGNITION HARNESS REPLACEMENT TO ELIMINATE RADIO INTERFERENCE, REAR SET OF SPARK PLUGS REPLACED WITH NGK BR6ES WARNER SUPER SCARAB 185 BUTX AUTOMOTIVE SPARK PLUGS WITH COMMERCIALLY AVAILABLE 18/14MM ADAPTORS AND SPIRO PRO 8MM IGNITION LEADS BULLDOG MODEL 120/124 15387 INSTALLATION OF SLICK START BOOSTER CHAMPION AEROSPACE SLICK START MAGNETO BOOSTER SYSTEM INSTALLED IAW SLICK SERVICE LYCOMING AEIO-360-A1B6 ASAL LETTER SL2-96 AND FAA STC SA593CH. BULLDOG MODEL 120/124 15388 INSTALLATION OF REPLACEMENT SEAT SCHROTH 4-04-150280 HARNESSES INSTALLED IAW CAA MOD AA009/03. LYCOMING AEIO-360-A1B6 ASAL BELT HARNESS BULLDOG SERIES 120 MODEL 14945 NIGHT/IFR CLEARANCE NIGHT IFR CLEARANCE - FAST TRACK PROCESS LYCOMING AEIO-360-A1B6 CBCB 121 BULLDOG SERIES 120 MODEL 15098 NIGHT & IFR CLEARANCE FORMERLY TCd AIRCRAFT - NIGHT IFR CLEARANCE LYCOMING IO-360-A1B6 BZME 121 BULLDOG SERIES 120 MODEL 14675 MODERNISATION OF EXTERNAL LIGHTS INSTALLATION OF: LYCOMING IO-360-A1B6 CBAN 121 TELEDYNE ALPHABEAM PAR 36 TAXY AND IN PLACE OF ORIGINAL GE LIGHT UNITS AND WHELAN ORION 650 WING TIP MOUNTED LED POSITION AND STROBE LIGHTS IN PLACE OF ORIGINAL GRIMES UNITS AND WHELAN 500 LED RUDDER MOUNTED TAIL POSITION AND STROBE LIGHT IN PLACE OF ORIGINAL GRIMES UNIT. ALL ANTI-COLLISION LIGHTS SYNCHRONISED TO FLASH TOGETHER. BULLDOG SERIES 120 MODEL 14003 HAND OPERATED RUDDER/NOSE WHEEL INSTALLATION OF HAND OPERATED RUDDER/NOSE WHEEL AND WHEEL BRAKE LYCOMING IO-360-A1B6 CBBS 121 STEERING AND BRAKE CONTROLS CONTROLS MOUNTED TO A FORMED ALUMINIUM BASE PLATE THAT IS BOLTED TO THE FLOOR IN FRONT OF THE P1 SEAT AND BRACED TO THE CENTRE CONSOLE WITH AN ADDITIONAL BRACKET.

THE RUDDER LEVER IS MOUNTED BESIDE THE CENTRE CONSOLE TO BE OPERATED BY THE PILOTS RIGHT HAND. A PUSH-ROD CONNECTS THE RUDDER LEVER BELOW ITS PIVOT TO THE RIGHT HAND P1 RUDDER PEDAL VIA A CUSTOM MADE BRACKET. FORWARD MOVEMENT OF THE UPPER PART OF THE RUDDER LEVER RESULTS IN LEFT RUDDER/NOSE WHEEL MOVEMENT AND VICE VERSA.

THE TWO BRAKE LEVERS ARE MOUNTED SIDE BY SIDE ON THE LEFT SIDE OF THE COCKPIT ROTATING ON A COMMON PIVOT. THE BOTTOM OF EACH BRAKE LEVER CONNECTS DIRECTLY TO THE PISTON ROD OF A BRAKE MASTER CYLINDER, WHICH IS MOUNTED UNDER THE P1 SEAT. PUSHING THE TOP OF THE BRAKE LEVERS OPERATES THE BRAKES. THE ADDITIONAL MASTER CYLINDERS ARE PLUMBED IN SERIES BETWEEN THE AIRCRAFT'S ORIGINAL MASTER CYLINDERS AND THE SLAVE CYLINDERS.

BULLDOG SERIES 120 MODEL 14639 BRAKE UPGRADE WITH DISABLED HAND INSTALLATION OF CLEVELAND WHEELS AND BRAKES TO REPLACE THE ORIGINAL DUNLOP WHEELS LYCOMING IO-360-A1B6 CBBS 121 CONTROLS AND BRAKES. WHEELS (ASSEMBLY NUMBER 40-84) ARE THE SAME SIZE AS ORIGINAL; BRAKES (ASSEMBLY NUMBER 30-41) AND BRAKE TORQUE PLATE (75-39) FIT THE ORIGINAL AXLE WITH THE USE OF CUSTOM BUSHES TO MATCH THE HOLE SIZES. BRAKE ACTUATION LEVER/RESERVOIR REMAINS THE SAME.

Prototype mods that have been approved since 1/1/2008 Page 14 30/11/20 LAA Technical Leaflet TL 3.17 BULLDOG SERIES 120 MODEL 14995 HAND BRAKE LEVERS INSTALLATION SUBSTITUTION OF HAND OPERATED BRAKE SYSTEM INSTALLED TO COCKPIT LEFT SIDE AS PART OF LYCOMING IO-360-A1B6 CBBS 121 LAA MODIFICATION 14003 WITH TWO INDEPENDENT HAND OPERATED LEVERS AS USED IN THE IKARUS C42 AIRCRAFT, EACH INCORPORATING A MASTER CYLINDER AND MECHANICAL PARKING BRAKE FEATURE, ONE MOUNTED TO THE P1 CONTROL COLUMN, THE OTHER TO THE HAND OPERATED RUDDER CONTROL LEVER VIA INCORPORATED CLAMP. CADET III MOTOR GLIDER 13698 PROPELLER CHANGE TO HERCULES INSTALLATION OF HERCULES 5827396-S 58 INCH DIAMETER X 27 INCH PITCH PROPELLER. VW 1600 AYAN 5827396-S CAMPBELL CRICKET 15200 FITMENT OF DRAGON WINGS DRAGON WINGS 23' DIAMETER ROTORS SUBSTITUTED VW 1835 AYRC ROTORBLADES CAMPBELL CRICKET 15201 ENGINE CHANGE TO EVERETT 1835CC TWIN CARB CONVERTED VW ENGINE FROM EVERETT G-BMZN SUBSTITUTED VW 1835 AYRC TWIN CARB EVERETT CASA 1-131 SERIES 2000 12317 Manufacture of new piston rings, . E.N.M.A. TIGRE G-IV-B BWHP gudgeon pins CASA 1-131 SERIES 2000 12358 REPLACEMENT OF IGNITION HARNESS . E.N.M.A. TIGRE G-IV-B BWHP CASA 1-131-E SERIES 2000 13057 INSTALLATION OF ELECTRONIC ELECTRONIC REPLACING MECHANICAL TACHOMETER PER APPLICANT'S SUBMISSION. E.N.M.A. TIGRE G-IV-A2 CDLC & BATTERY CASA 1-131-E SERIES 2000 13293 CARBURETTOR TYPE CHANGE ROTEC THROTTLE BODY TGI-40-4 INSTALLED IN PLACE OF EXISTING CARBURETTOR E.N.M.A. TIGRE G-IV-A5 CGTX CASA 1-131E SERIES 1000 11518 FITTING ELLISON EFS4 THROTTLE BODY ELLISON EFS4 THROTTLE BODY INJECTOR FITTED USING ADAPTOR PER APPLICANT'S DRAWING. E.N.M.A. TIGRE G-IV-A2 BZJV INJECTOR CASA 1-131E SERIES 1000 14784 HERCULES 8458425-S, 84" X 58" INSTALLATION OF HERCULES 8458425-S, 84 INCH DIAMETER X 58 INCH PITCH PROPELLER. E.N.M.A. TIGRE G-IV-B BHPL PROPELLER INSTALLATION CASA 1-131E SERIES 2000 14173 E.N.H.A. HC 212-111 PROPELLER INSTALLATION OF E.N.H.A. HC 212-111 PROPELLER E.N.M.A. TIGRE G-IV-A5 BEDA INSTALLATION CASA 1-131E SERIES 2000 10843 TO MODIFY AIR INDUCTION ASSEMBLY INSTALLATION OF AIR INDUCTION PLENUM FABRICATED FROM ALUMINIUM. E.N.M.A. TIGRE G-IV-B BECT NO AIR FILTER FITTED. AIR STRAIGHTENER VANES NOT FITTED. CASA 1-131E SERIES 2000 13851 ENMA TIGRE G-IV-B ENGINE AND INSTALLATION OF ENMA TIGRE G-IV-B ENGINE AND HOFFMANN HO23D-212B155K PROPELLER. E.N.M.A. TIGRE G-IV-B BPTS HOFFMANN HO23D-212B155K PROPELLER INSTALLATIONS CASA 1-131E SERIES 2000 14516 DEEP ROCKERBOX OIL LUBRICATION RETROFIT AFTERMARKET DEEP ROCKERBOX COVERS SUPPLIED BY J.ROSENBURG, OIL FILLED E.N.M.A. TIGRE G-IV-B BPTS SYSTEM RATHER THAN GREASE FILLED, PER GIPSY MAJOR ENGINE CONFIGURATION CASA 1-131E SERIES 2000 10843 TO MODIFY AIR INDUCTION ASSEMBLY INSTALLATION OF AIR INDUCTION PLENUM FABRICATED FROM ALUMINIUM. E.N.M.A. TIGRE G-IV-B BYIJ NO AIR FILTER FITTED. AIR STRAIGHTENER VANES NOT FITTED. CASA 1-131E SERIES 2000 12522 ENGINE CHANGE TO ENMA TIGRE G-IV-B. RE-INSTALLATION OF ENMA TIGRE G-IV-B ENGINE (S/N 6111) WITH LODGE CJL 135 83 INCH E.N.M.A. TIGRE G-IV-B CDRU DIAMETER X 62 INCH PITCH PROPELLER. CASA 1-131E SERIES 2000 12666 PROPELLER CHANGE TO MT211R132-6V INSTALLATION OF MT 211R132-6V PROPELLER ON TIGRE G-IV-B ENGINE. E.N.M.A. TIGRE G-IV-B BUVN

CASSUTT RACER IIIM 12331 PROPELLER CHANGE TO STERBA 60" X CHANGE OF PROPELLER TO STERBA 60" DIAMETER X 72" PITCH CONTINENTAL O-200-A BOMB 72" CASSUTT RACER IIIM 13854 REPLACEMENT WING TIPS NEW MOULDED COMPOSITE WING TIPS FITTED. CONTINENTAL O-200-A BOMB CASSUTT RACER IIIM 13931 PROPELLER CHANGE TO HERCULES INSTALLATION OF HERCULES 6070439-S 60 INCH DIAMETER X 70 INCH PITCH PROPELLER. CONTINENTAL O-200-A BOMB 6070439-S CASSUTT RACER IIIM 12575 PROPELLER CHANGE TO STERBA 60" X PROPELLER CHANGE TO STERBA 60" X 72" CONTINENTAL O-200-A BPVO 72" CASSUTT RACER IIIM 14060 B&C LIGHTWEIGHT STARTER FITMENT TO B&C 320-1 LIGHTWEIGHT STARTER INSTALLED ON CONTINENTAL O-200-A IN ACCORDANCE WITH CONTINENTAL O-200-A BPVO O-200 ENGINE MANUFACTURER'S INSTRUCTIONS, INCLUDING ASSOCIATED WIRING, SWITCHES, CIRCUIT BREAKERS, CONTACTORS, FASTENERS AND WARNING LIGHTS.

EXISTING BATTERY REPLACED WITH RACING BATTERIES RBA-300 LITHIUM IRON PHOSPHATE BATTERY. CASSUTT RACER IIIM 13026 FITMENT OF B & C LIGHTWEIGHT LIGHTWEIGHT B+C STARTER FITTED ALONG WITH ASSOCIATED SWITCH AND WIRING, BATTERY CONTINENTAL O-200-A RUNT STARTER MOUNTED IN SUITABLE MOUNTING FORWARD OF CONTROL COLUMN Prototype mods that have been approved since 1/1/2008 Page 15 30/11/20 LAA Technical Leaflet TL 3.17 CASSUTT RACER IIIM 12630 PROPELLER CHANGE TO STERBA 60" X PROPELLER CHANGE TO STERBA 60 INCH DIAMETER X 70 INCH PITCH. CONTINENTAL O-200-A OLHR 70" CASSUTT RACER IIIM 13240 RACING BATTERY RBA-300 INSTALLATION OF RACING BATTERY RBA-300 LITHIUM IRON PHOSPHATE BATTERY ON FORWARD CONTINENTAL O-200-A LEFT FACE OF FIREWALL. CASSUTT RACER IIIM 12331 PROPELLER CHANGE TO STERBA 60" X CHANGE OF PROPELLER TO STERBA 60" DIAMETER X 72" PITCH CONTINENTAL O-200-A CSUT (MODIFIED) 72" CESSNA 120 15205 HERCULES 7042350-S PROPELLER INSTALLATION OF HERCULES 7042350-S 70 INCH DIAMETER X 42 INCH PITCH PROPELLER. CONTINENTAL C85-12F AJJT INSTALLATION CESSNA 120 15127 PROVISION OF 5.2V DC POWER FOR SUB-PANEL ADDED BELOW MAIN INSTRUMENT PANEL, INCORPORATING ANKER USB OUTLETS, 12V CONTINENTAL C85-12F AKTS PILOTAWARE ROSETTA POWER SOCKET AND ASSOCIATED CIRCUIT BREAKER/SWITCH. CESSNA 120 14235 ORATEX 6000 FABRIC COVERING ON COVERING OF WINGS WITH ORATEX 6000 FABRIC IN ACCORDANCE WITH ORATEX FITTING CONTINENTAL C85-12F AKVM CESSNA 120 INSTRUCTIONS CESSNA 120 13917 SPIN-ON OIL FILTER ADAPTER FOR INSTALLATION OF CUSTOM MADE SPIN-ON OIL FILTER ADAPTER P/N 79001003 WITH CHAMPION CONTINENTAL C85-12F BRJC CONTINENTAL PC60 (O-200) CH48108 OR C138 OR BLUE PRINT ADT32109 OIL FILTER.

AT ISSUE 4: APPLICABILITY EXTENDED TO CONTINENTAL C90-12 ENGINE. AT ISSUE 6: APPLICABILITY EXTENDED TO CONTINENTAL C85-12F ENGINE. AT ISSUE 7: APPLICABILITY EXTENDED TO CONTINENTAL C90-14F ENGINE. CESSNA 120 13555 F & M ENTERPRISES T.A.F.-L SPIN ON OIL F&M ENTERPRISES T.A.F.-L OIL FILTER ADAPTER FITTED PER STC SE7559SW. FILTERS ACCEPTABLE CONTINENTAL C85-12F BRPH FILTER ADAPTOR FITMENT CHAMPION CH48108-1, TEMPEST AA-48108, CHALLENGER AVIATION CP-48108-C.

CESSNA 120 14126 INSTALLATION OF B & C STARTER B+C STARTER INSTALLED USING STC SE00145W1 CONTINENTAL C85-12F BRPH CESSNA 120 12776 PROPELLER CHANGE TO MCCAULEY PROPELLER CHANGE TO MCCAULEY 1B90/CM 70 INCH DIAMETER X 48 INCH PITCH. CONTINENTAL C85-12F BVUZ 1B90/CM 70" X 48" CESSNA 120 13693 ENGINE CHANGE TO CONTINENTAL C90- INSTALLATION OF CONTINENTAL C90-14F ENGINE AND MCCAULEY 1A90/CF 71 INCH DIAMETER X CONTINENTAL C90-14F BRXH 14F 48 INCH PITCH PROPELLER. CESSNA 120 12806 PROPELLER CHANGE TO McCAULEY PROPELLER CHANGED TO McCAULEY 1B90/CM 71" x 46" CONTINENTAL O-200-A BRPF 1B90/CM 7146 CESSNA 120 15086 CONTINENTAL O-200-A ENGINE INSTALLATION OF A CONTINENTAL O-200-A ENGINE INSTALLATION WITH A MCCAULEY CONTINENTAL O-200-A BRPF INSTALLATION WITH MCCAULEY 1B90/CM7146 71" X 46" PROPELLER. 1B90CM7146 PROPELLER CESSNA 120 12719 PROPELLER CHANGE TO MCCAULEY PROPELLER CHANGE TO MCCAULEY 1A100/MCM 69 INCH DIAMETER X 50 INCH PITCH. CONTINENTAL O-200-A BUKO 1A100/MCM 69" X 50" CESSNA 120 13475 SENSENICH 69CK-0-48L 69" X 48" INSTALLATION OF SENSENICH 69CK-0-48L 69 INCH DIAMETER X 48 INCH PITCH PROPELLER CONTINENTAL O-200-A JOLY PROPELLER INSTALLATION CESSNA 120 14136 REPLACEMENT COWL LATCHES - STC REF INSTALLATION OF FOUR DIP DAVIS COWL LATCHES PER STC NO. SA01139CH CONTINENTAL O-200-A BUHZ SA01139CH CHAMPION 7ECA 15347 MCCAULEY 1C90/ALM7243 72'' x 43'' MCCAULEY 1C90/ALM7246 72 INCH DIAMETER PROPELLER (SN 50151) OVERHAULED AND RE- LYCOMING O-235-C1 BPMM PROPELLER INSTALLATION PITCHED FROM 46 TO 43 INCHES. REMARKED AS 1C90/ALM7243. CHAMPION 7ECA 15355 FITTING OF VORTEX GENERATORS STC FITTING OF MICRO AERODYNAMICS VORTEX GENERATORS AS FAA SUPPLEMENTARY TYPE LYCOMING O-235-C1 BPMM CERTIFICATE SA00232SE WITH MICRO AERODYNAMICS INSTALLATION MANUAL MA2056 REV A. 20 PAIRS OF VORTEX GENERATORS MOUNTED TO THE UPPER SURFACE OF EACH WING AND 7 PAIRS MOUNTED TO THE UNDER SURFACE OF EACH HORIZONTAL STABILISER. CHAMPION 7FC (MODIFIED) 12316 PROPELLER CHANGE TO SENSENICH 76AK-CHANGE PROPELLER TO SENSENICH 76AK-2-44, 72" DIAMETER X 44" PITCH CONTINENTAL C90-12F APYT 2-44, 72" X 44" CHILTON DW.1A 13765 OMISSION OF MIDDLE (UNDER CENTRE SECTION OF FLAP OMITTED IN REGION BELOW FUSELAGE. INNER RIBS OF EACH FLAP WALTER MIKRON 3B DWCB FUSELAGE) SECTION OF CENTRE FLAP SECTION INCREASED TO 3/8" WIDTH. RESULTING FUSELAGE APERTURE COVERED IN 1MM PLYWOOD WITH UNDERLYING CROSS PIECE TO PREVENT DISTORTION.

Prototype mods that have been approved since 1/1/2008 Page 16 30/11/20 LAA Technical Leaflet TL 3.17 CHILTON DW1 14695 HERCULES 6253529-S 62" x 53" INSTALLATION OF HERCULES 6253529-S 62 INCH DIAMETER X 53 INCH PITCH PROPELLER. WALTER MIKRON 2 AFGI PROPELLER INSTALLATION CHILTON DW1 13990 FLAP TORQUE-TUBE UNIVERSAL JOINTS SUBSTITUTION OF HIGH QUALITY COMMERCIALLY AVAILABLE UNIVERSAL JOINT ASSEMBLIES IN WALTER MIKRON 3A JUJU FLAP TORQUE TUBES CHRISTAVIA MK1 12309 IMPROVED PILOT SEAT CRASH SEAT MOUNTINGS RECONFIGURED FOR IMPROVED CRASH ENERGY ABSORPTION PER APPLICANT'S CONTINENTAL O-200-A MRED PROTECTION DRAWING CHRISTAVIA MK1 12310 THREE PIECE WINDSCREEN THREE PIECE 1/8" THICK POLYCARBONATE WINDSCREEN SUBSTITUTED FOR PERSPEX CURVED CONTINENTAL O-200-A MRED WINDSCREEN SHOWN ON DRAWINGS. APPLICANT'S DRAWING REFERS CHRISTAVIA MK1 12340 PROPELLER CHANGE TO NEWTON TYPE PROPELLER CHANGE TO NEWTON TYPE 07R 69 INCH DIAMETER X 48 INCH PITCH. CONTINENTAL O-200-A MRED 07R 69" X 48" CHRISTAVIA MK1 13254 HERCULES 6843289-S 68" x 43" INSTALLATION OF HERCULES 6843289-S 68 INCH DIAMETER x 43 INCH PITCH PROPELLER CONTINENTAL O-200-A MRED PROPELLER INSTALLATION CHRISTEN EAGLE II 14410 INCREASE OF AEROBATIC WEIGHT LIMITS INCREASE IN MAXIMUM AEROBATIC WEIGHT TO 1555 Lbs WITH CORRESPONDING REDUCTION IN LYCOMING AEIO-360-A1D NUTA AEROBATIC 'G' LIMITS FROM +7g, -5g TO +6g, -4g CHRISTEN EAGLE II 12768 BATTERY RELOCATION TO ENGINE INSTALLATION OF BATTERY IN STEEL FABRICATED BATTERY BOX ONTO PORT SIDE OF ENGINE LYCOMING AEIO-360-A1D EGIL MOUNT PORT SIDE MOUNTING FRAME ATTACHED USING 4 OFF STAINLESS STEEL P-CLIPS. CHRISTEN EAGLE II 12267 INSTALLATION OF SMOKE SYSTEM 'SMOKING AIRPLANES' UNIT INSTALLED ON FORWARD FLOOR PER MANUFACTURER'S LYCOMING AEIO-360-A1D CFIF INSTRUCTIONS. CLEARANCE TO MOVING PARTS OF FLYING CONTROL SYSTEM TO BE NOT LESS THAN 1/2". CHRISTEN EAGLE II 13227 LIGHTSPEED CDI III ELECTRONIC REPLACEMENT OF ORIGINAL RIGHT HAND MAGNETO WITH LIGHTSPEED PLASMA III ELECTRONIC LYCOMING AEIO-360-A1D KLAW IGNITION TO REPLACE RH MAGNETO. IGNITION SYSTEM. CHRISTEN EAGLE II 11666 SKYDYNAMICS MAXI-SUMP, INTAKE AND NEW OIL SUMP, INTAKE AND EXHAUST SYSTEM INSTALLED ON ENGINE IN ACCORDANCE WITH SKY LYCOMING AEIO-360-A1D KLAW EXHAUST INSTALLATION DYNAMICS CORPORATION INSTALLATION INSTRUCTIONS FOR THE MAXI-SUMP AND PROVISOS IN LAA LETTER DATED 28/07/2011. CHRISTEN EAGLE II 12267 INSTALLATION OF SMOKE SYSTEM 'SMOKING AIRPLANES' UNIT INSTALLED ON FORWARD FLOOR PER MANUFACTURER'S LYCOMING AEIO-360-A1D KLAW INSTRUCTIONS. CLEARANCE TO MOVING PARTS OF FLYING CONTROL SYSTEM TO BE NOT LESS THAN 1/2". CHRISTEN EAGLE II 12267 INSTALLATION OF SMOKE SYSTEM 'SMOKING AIRPLANES' UNIT INSTALLED ON FORWARD FLOOR PER MANUFACTURER'S LYCOMING IO-360-A1A IXII INSTRUCTIONS. CLEARANCE TO MOVING PARTS OF FLYING CONTROL SYSTEM TO BE NOT LESS THAN 1/2". CIVILIAN COUPE 02 14558 REPLACEMENT PROPELLER ATTACHMENT AFTER AN IN-SERVICE FAILURE OF ONE OF THE ORIGINAL STEPPED PROPELLER BOLTS, ORIGINAL ARMSTRONG GENET MAJOR 1A ABNT BOLTS PROPELLER BOLTS REPLACED BY A25-48L BOLTS WITH CUSTOM STAINLESS STEEL TOP HAT BUSHES SIDDELEY AT HEAD AND NUT ENDS TO REPLICATE EFFECT OF STEPPED BOLTS AND NUTS. BOLTS RETAINED BY A27-LS SLOTTED NUTS SP90-E12 SPLIT PINS AND AN900-716 WASHERS.

COLIBRI MB2 14044 ENGINE CHANGE TO VW 1834 CC NEWLY CONVERTED 1834cc VW ENGINE SUBSTITUTED VW 1834 BKRH COLIBRI MB2 14093 PROPELLER CHANGE TO HERCULES PROPELLER CHANGE TO HERCULES 563959-S VW 1834 BKRH 563959-S COLIBRI MB2 13234 ADDITION OF SECOND ELECTRIC FUEL INSTALLATION OF 2ND ELECTRIC FUEL PUMP (FACET 50105) DOWNSTREAM IN SERIES WITH VW 1834 BNDP PUMP ORIGINAL FACET ELECTRIC PUMP MOUNTED ON FIREWALL. COLIBRI MB2 12753 QC-3145 'QUICK-CHANGER' ENGINE OIL INSTALLATION OF QC-3145 'QUICK-CHANGER' ENGINE OIL QUICK DRAIN VALVE WITH SPACER TO VW 1834 BRWV QUICK DRAIN VALVE AVOID EXCESSIVE PENETRATION INTO SUMP. VALVE BODY AND VALVE CAP TO BE WIRE LOCKED WHEN CLOSED. COLIBRI MB2 14297 FITMENT OF LEBURG ELECTRONIC DUAL LEBURG IGNITION FITTED VW 1834 BKCI IGNITIION COLOMBAN MC-30 LUCIOLE 14508 ALTERNATIVE BRAKE HANDLES AUTOMATIC DIFFERENTIAL BRAKE FEATURE OPERATED BY AILERON ACTION DELETED AND WHEEL BRIGGS AND 0114-E1 LVCY BRAKES OPERATED BY TWIN FINGER BRAKES ON FLOOR INFRONT OF CONTROL COLUMN USING STRATTON EXISTING CABLE SYSTEM COLOMBAN MC30 LUCIOLE 14508 ALTERNATIVE BRAKE HANDLES AUTOMATIC DIFFERENTIAL BRAKE FEATURE OPERATED BY AILERON ACTION DELETED AND WHEEL BRIGGS AND 0114-E1 CIBJ BRAKES OPERATED BY TWIN FINGER BRAKES ON FLOOR INFRONT OF CONTROL COLUMN USING STRATTON EXISTING CABLE SYSTEM Prototype mods that have been approved since 1/1/2008 Page 17 30/11/20 LAA Technical Leaflet TL 3.17 CORBEN JUNIOR ACE MODEL E 12624 PROPELLER CHANGE TO ALAN JAMES AJ PROPELLER CHANGE TO ALAN JAMES AJ 7236/AJ/65-75 72 INCH DIAMETER X 36 INCH PITCH. THIS CONTINENTAL A75-8F BSDI 7236/AJ/65-75 72" X 36" PROPELLER IS BASED ON THE EVRA D.11.28.1.B. CORBEN JUNIOR ACE MODEL E 13247 HERCULES 7246290-S 72" X 46" PROPELLER CHANGE TO HERCULES 7246290-S 72 INCH DIAMETER X 46 INCH PITCH. CONTINENTAL A75-8F BSDI PROPELLER CORBY CJ-1 STARLET 13706 REPLACEMENT OF EXISTING ELECTRONIC INSTALLATION OF LEBURG SYSTEM BUT WITH CUSTOM POSITION SENSOR HAPI MAGNUM 75 ILSE IGNITION INSTALLATION CORBY CJ-1 STARLET 13382 HERCULES 5445297-S 54" X 45" INSTALLATION OF HERCULES 5445297-S 54 INCH DIAMETER X 45 INCH PITCH PROPELLER VW 1834 CCXO PROPELLER INSTALLATION INSTALLATION. CORBY CJ-1 STARLET 13941 TRIM SPRING BIAS TYPE ELEVATOR TRIM SYSTEM FITTED VW 1834 CCXO COSMIC WIND 12476 PROPELLER CHANGE TO STERBA 60" X PROPELLER CHANGE TO STERBA 60" X 70" WITH 'RACE PROFILE'. CONTINENTAL C90-14F ARUL 70" COZY MK4 13670 CATTO 3 BLADED 66" X 75" PROPELLER INSTALLATION OF A CATTO 3 BLADED 66 INCH DIAMETER X 75 INCH PITCH PROPELLER. LYCOMING O-360-A4A BYLZ INSTALLATION CP 301S 12959 COWLING FAIRINGS BALSA WOOD FAIRINGS ADDED TO FUSELAGE BOTTOM TO REAR OF COWLING AT SIDES, SIMILAR CONTINENTAL C90-14F DENS TO JODEL 150 TYPE TO IMPROVE AIRFLOW AROUND FUSELAGE AND WING ROOT CP 301S 13505 REAR FUEL TANK REMOVAL REAR FUEL TANK REMOVED AND PIPEWORK BLANKED OFF, PLUMBING AND FUEL SELECTOR CONTINENTAL C90-14F DENS REVISED ACCORDINGLY CP 301S 13722 REBALANCING OF HOFFMANN BALANCING OF HOFFMAN PROPELLER FOLLOWING REFURBISHING BY HERCULES. PROPELLER CONTINENTAL C90-14F DENS PROPELLER AFTER REFURBISHING BALANCED USING METHOD OF INSERTING A SMALL SLUG OF LEAD INTO A SHALLOW HOLE (5mm DEEP x 12mm DIA) DRILLED IN THE FLAT FACE OF THE HUB. HOLE PLUGGED WITH A BEECH PLUG GLUED IN PLACE PER STANDARD HERCULES PROCEDURE CP 301S 13909 CANOPY ATTACHMENT CANOPY HALVES AND WINDSCREEN REPLACED, USING SIKAFLEX 295i UV ADHESIVE IN THE CONTINENTAL C90-14F DENS MANNER ALREADY ACCEPTED BY LAA ON RV AND MCR AIRCRAFT CP 301S 14437 STC CONTINENTAL PUSHROD TUBE INSTALLATION OF FAA STC SE00533SE: REAL GASKET CORP CONTINENTAL ENGINE PUSHROD TUBE CONTINENTAL C90-14F DENS MODIFICATION MODIFICATION. INSTALLED IN ACCORDANCE WITH MANUFACTURER'S INSTRUCTIONS. CP301S 12914 REPLACEMENT EXHAUST SYSTEM - AIRWORLD JODEL D117 EXHAUST ADAPTED TO FIT EMERAUDE CP301S WITH MINOR CONTINENTAL PC60 BSVE AIRWORLD ADJUSTMENTS ONLY CP301S 13076 HERCULES 6650318-S 66" X 50" INSTALLATION OF HERCULES 6650318-S 66 INCH DIAMETER X 50 INCH PITCH PROPELLER. CONTINENTAL PC60 BSVE PROPELLER CP301S 13909 CANOPY ATTACHMENT CANOPY HALVES AND WINDSCREEN REPLACED, USING SIKAFLEX 295i UV ADHESIVE IN THE CONTINENTAL PC60 BSVE MANNER ALREADY ACCEPTED BY LAA ON RV AND MCR AIRCRAFT CRICKET MK4 13712 AIR SCOOPS TO IMPROVE ENGINE AIR SCOOPS ADDED TO COOLANT RADIATOR TO IMPROVE COOLING ROTAX 582 CCPD COOLING CRICKET MK6A 15053 ROTOR BLADE CHANGE ROTORS CHANGED TO DRAGON WINGS 22' DIAMETER ROTAX 582 CBWN CRICKET MK6A 12623 REPAIR OF ROTORDYNE ROTOR BLADES TRAILING EDGES RIVETTED ROTAX 582 CFJD

CURRIE WOT 13976 HERCULES 7043313-S PROPELLER HERCULES 7043313-S 70 INCH DIAMETER X 43 INCH PITCH PROPELLER INSTALLATION. CONTINENTAL C90-14F BXMX INSTALLATION CURRIE WOT 12899 NEWTON 07R 69" X 49" PROPELLER INSTALLATION OF NEWTON 07R 69 INCH DIAMETER X 49 INCH PITCH PROPELLER CONTINENTAL C90-8F ASBA CURRIE WOT 12312 ENGINE CHANGE TO WALTER MICRON III ENGINE CHANGE TO WALTER MICRON III AS OVERHAULED BY AEROTECHNIK WALTER MIKRON 3 CWOT

CZAW SPORTCRUISER 12917 FLOSCAN FUEL FLOW METER INSTALLATION OF FLOSCAN 201B FUEL FLOW TRANSDUCER UPSTREAM OF BOTH FUEL PUMPS FOR JABIRU 3300A XERO DYNON D120 ENGINE MONITORING SYSTEM. CZAW SPORTCRUISER 12918 SKYBRIGHT STROBE LIGHTING INSTALLATION OF WING TIP AND FIN TIP SKYBRIGHT STROBES WITH TWO POWER SUPPLIES JABIRU 3300A XERO WITHIN REAR FUSELAGE. CZAW SPORTCRUISER 13093 TRUTRAK DIGIFLIGHT IIVS DUAL AXIS INSTALLATION OF SERVOS USING CZAW MOUNTING HARDWARE. JABIRU 3300A XERO AUTOPILOT THROTTLE MOUNTED PITCH TRIM ENABLING SWITCH INSTALLED.

Prototype mods that have been approved since 1/1/2008 Page 18 30/11/20 LAA Technical Leaflet TL 3.17 CZAW SPORTCRUISER 15442 CAMIT 40 AMP ALTERNATOR CAMIT 40 AMP BELT DRIVEN ALTERNATOR FITTED ON REAR STARBOARD SIDE OF ENGINE JABIRU 3300A XERO FITTED IN ACCORDANCE WITH CAMIT CAEARFI3.5 "FITTING INSTRUCTION FOR 40AMP ALTERNATOR RH ON 3300 JABIRU ENGINE" 40 AMP CIRCUIT BREAKER FITTED ON OUTPUT OF ALTERNATOR ISOLATION SWITCH AND 10 AMP CIRCUIT BREAKER FITTED ON VOLTAGE SENSE/WARNING LIGHT LINE MASTER CONTACTOR FITTED CZAW SPORTCRUISER 14140 SECOND BATTERY INSTALLATION ORIGINAL 16AH LEAD-ACID BATTERY REPLACED BY TWO ANTIGRAVITY ATX12-24 22AH LITHIUM JABIRU 3300A WOOO IRON PHOSPHATE BATTERIES. ONE BATTERY TAKES THE ORIGINAL BATTERY'S POSITION, THE OTHER IS INSTALLED USING THE SAME HARDWARE AT THE SAME POSITION ON THE PORT SIDE. THE BATTERIES ARE CONNECTED IN PARALLEL AND USE WIRING OF THE SAME SPECIFICATION AS THE ORIGINAL ARRANGEMENT.

EFIS/EMS UNIT MUST BE PROGRAMMED TO PROVIDE A CLEAR OVER-VOLTAGE WARNING WHEN THE ELECTRICAL SYSTEM VOLTAGE EXCEEDS 14.5 V. A PLACARD MUST BE CLEARLY VISIBLE TO THE PILOT STATING "IN THE EVENT OF AN OVER-VOLTAGE WARNING, DISCONNECT ALTERNATOR".

CZAW SPORTCRUISER 14356 ENGINE CHANGE TO CAMIT 3300 ENGINE CHANGED TO CAMIT CAE 3300 JABIRU 3300A WOOO CZAW SPORTCRUISER 14712 FUEL FLOW MONITORING SYSTEM ELECTRONICS INTERNATIONAL FT-60 RED CUBE FUEL FLOW TRANSDUCER INSTALLED IN FUEL JABIRU 3300A CHXG SYSTEM BETWEEN RETURN T AND CARBURETTOR. CZAW SPORTCRUISER 12938 DYNON D100/ AP74 DUAL AXIS AUTO INSTALLATION OF DYNON DUAL AXIS AUTO PILOT CONTROLLED BY D100 EFIS WITH AP74 CONTROL JABIRU 3300A CGMM PILOT HEAD. ALSO INSTALLATION OF PITCH TRIM DISABLEMENT FEATURE THAT IS ACTIVE WHEN AUTO-PILOT POWER SWITCH IS ON WITH ADDITIONAL MOMENTARY OVER-RIDE SWITCH. CZAW SPORTCRUISER 13089 STRENGTHENING OF THE MK1 NOSELEG 2MM THICK 4130 DOUBLER SECTION WELDED TO TOP FACE OF NOSELEG. JABIRU 3300A DGSC

CZAW SPORTCRUISER 13680 STRENGTHENER OF NOSE LEG FORK 3RD LEAF ADDED TO NOSE LEG FORK ASSEMBLY. STRUCTURALLY BONDED TO OTHER LEAVES AND JABIRU 3300A CIAX SECURED BY AN-3 BOLTS. CZAW SPORTCRUISER 12673 SERIES II WING CENTRE SECTION WING SPAR CENTRE SECTION REINFORCED TO REPLICATE ARRANGEMENT OF UPRIGHTS ON ZENAIR ROTAX 912-ULS CZAW UPGRADE CH601 XL. MAXIMUM WEIGHT AUTHORISED IS REDUCED TO 560 KG; ROUGH AIR SPEED VNO IS REDUCED TO 102 KTS. CZAW SPORTCRUISER 12605 REMOVAL OF FLAP HANGER (PORT) CRACK DRESSSED OUT AS PHOTOGRAPH PROVIDED BY APPLICANT. CRACK CAUSED BY ERROR IN ROTAX 912-ULS CRWZ STRESS RAISERS. CONSTRUCTION. CZAW SPORTCRUISER 13086 WOODCOMP SR3000/2W 1740MM INSTALLATION OF WOODCOMP SR3000/2W 1740MM DIAMETER PROPELLER WITH WOODCOMP ROTAX 912-ULS CRWZ DIAMETER PROPELLER. BLADE PITCH CONTROL UNIT. CZAW SPORTCRUISER 12718 INSTALLATION OF FUEL FLOW SENSOR INSTALLATION OF FLOSCAN 201A-6 FUEL FLOW SENSOR. THE SENSOR IS LOCATED ON A BRACKET ROTAX 912-ULS CRWZ ON THE CABIN FLOOR ON THE AIRCRAFT'S CENTRELINE. THE SENSOR IS POSITIONED BETWEEN THE FUEL SELECTOR AND GASCOLATOR WITH A ROTAX COMPLIANT FUEL FILTER IMMEDIATELY UPSTREAM OF THE SENSOR. CZAW SPORTCRUISER 12364 ENGINE CHANGE A ENGINE FITTED ROTAX 912-ULS SASI CZAW SPORTCRUISER 13802 PROPELLER CHANGE TO AIRMASTER AIRMASTER AP420-SNR64ZN 64 INCH DIAMETER 2 BLADED PROPELLER INSTALLATION. ROTAX 912-ULS SASI AP420-SNR64ZN

Prototype mods that have been approved since 1/1/2008 Page 19 30/11/20 LAA Technical Leaflet TL 3.17 CZAW SPORTCRUISER 14208 ROTEC LIQUID COOLED CYLINDER HEADS INSTALLATION OF ROTEC ENGINEERING'S LIQUID COOLED CYLINDER HEADS (LCH) KIT FITTED IN ROTAX 912-ULS SASI TO JABIRU 3300A ENGINE AND BATTERY ACCORDANCE WITH THE MANUFACTURER'S INSTRUCTIONS TO THE PREVIOUSLY INSTALLED JABIRU REPOSITIONING 3300A ENGINE.

SINGLE DAVIS CRAIG EWP80 ELECTRIC COOLANT PUMP INSTALLED WHOSE SPEED IS CONTROLLED BY AN ELECTRONIC CONTROL UNIT. COOLANT EXPANSION TANK WITH 1.1 BAR RATED PRESSURE CAP FITTED. OVERFLOW LINE FITTED TO EXPEL EXCESS COOLANT INTO COWLING AIR OUTLET AREA. CUSTOM MADE STAINLESS STEEL RECTANGULAR SECTION COOLANT DISTRIBUTION MANIFOLD MOUNTED BEHIND ENGINE AND SUPPORTED FROM ENGINE MOUNTING FRAME VIA RUBBER ANTI- VIBRATION MOUNTS. BATTERY INSTALLED IN CUSTOM MADE BATTERY BOX IN REAR PARCEL SHELF. CZAW SPORTCRUISER 15052 ENGINE & PROPELLER CHANGE ROTAX 912-ULS AND FITI ECO COMPETITION PROPELLER FITTED ON CZECH SPORT AIRCRAFT ROTAX 912-ULS SASI ENGINE MOUNT. CZAW SPORTCRUISER 15305 PROPELLER CHANGE TO WOODCOMP SR INSTALLATION OF WOODCOMP SR 3000/3N 1700MM DIAMETER PROPELLER ROTAX 912-ULS SASI 3000/3N CZAW SPORTCRUISER 12524 WOODCOMP KLASSIC EFFIC 170/3/RF PROPELLER CHANGE TO WOODCOMP EFFIC 170/3/RF (MODIFIED). MODIFICATION IS THE ROTAX 912-ULS CESZ (MODIFIED). REMOVAL OF THE STAINLESS STEEL LEADING EDGE ANTI-ERROSION STRIP FROM EACH BLADE AND APPLICATION OF PLASTIC LEADING EDGE TAPE TO FIT THE RECESS MOULDED INTO THE LEADING EDGE. CZAW SPORTCRUISER 13438 LANDING LIGHT PARTS FOR AIRCRAFT 55W ROUND LANDING LIGHT UNIT MOUNTED TO BOTTOM ENGINE COWL, ROTAX 912-ULS CGNG INCLUDING LOCAL REINFORCEMENT OF COWL, SWITCH, 5A CIRCUIT BREAKER AND WIRING.

CZAW SPORTCRUISER 14524 WOODCOMP SR3000/3N 1720MM INSTALLATION OF WOODCOMP SR3000/3N 1720MM DIAMETER PROPELLER WITH WOODCOMP ROTAX 912-ULS CGNG DIAMETER PROPELLER INSTALLATION ELECTRONIC CONSTANT SPEED CONTROLLER.

CZAW SPORTCRUISER 13093 TRUTRAK DIGIFLIGHT IIVS DUAL AXIS INSTALLATION OF SERVOS USING CZAW MOUNTING HARDWARE. ROTAX 912-ULS EDDS AUTOPILOT THROTTLE MOUNTED PITCH TRIM ENABLING SWITCH INSTALLED. CZAW SPORTCRUISER 13006 DYNON D100 / AP74 DUAL AXIS AUTO- INSTALLATION OF DYNON DUAL AXIS AUTO PILOT CONTROLLED BY D100 EFIS WITH AP74 CONTROL ROTAX 912-ULS FELX PILOT HEAD INCLUDING PITCH TRIM DISENABLE FEATURE AND ENABLE SWITCH. CZAW SPORTCRUISER 14323 WOODCOMP SR3000/2WN 1730MM INSTALLATION OF WOODCOMP SR3000/2WN 1730MM DIAMETER PROPELLER. ROTAX 912-ULS FELX DIAMETER PROPELLER INSTALLATION CZAW SPORTCRUISER 12808 INSTALLATION OF THERMOSTATIS P6-H- INSTALLATION OF THERMOSTATIS P6-H-190 THERMOSTATIC OIL BYPASS VALVE BETWEEN OIL ROTAX 912-ULS MOOV 190 THERMOSTATIC OIL BYPASS VALVE. COOLER AND OIL PUMP ON ROTAX 91X SERIES ENGINES.

CZAW SPORTCRUISER 12487 SKYFLASH STROBE SYSTEM SKYFLASH STROBE SYSTEM INSTALLED PER MANUFACTURER'S INSTRUCTIONS, LAMP ON TOP OF ROTAX 912-ULS MUTT FIN CZAW SPORTCRUISER 15024 WOODCOMP SR3000/3N, 1720MM INSTALLATION OF WOODCOMP SR3000/3N, 1720MM DIAMETER PROPELLER ROTAX 912-ULS MUTT DIAMETER PROPELLER INSTALLATION CZAW SPORTCRUISER 13020 FUEL FLOW TRANSDUCER FLOSCAN 201B TRANSDUCER ADDED TO FUEL SYSTEM DOWNSTREAM OF RETURN LINE BLEED OFF ROTAX 912-ULS JAYZ AND FUEL PRESSURE SENSOR. CZAW SPORTCRUISER 12938 DYNON D100/ AP74 DUAL AXIS AUTO INSTALLATION OF DYNON DUAL AXIS AUTO PILOT CONTROLLED BY D100 EFIS WITH AP74 CONTROL ROTAX 912-ULS JAYZ PILOT HEAD. ALSO INSTALLATION OF PITCH TRIM DISABLEMENT FEATURE THAT IS ACTIVE WHEN AUTO-PILOT POWER SWITCH IS ON WITH ADDITIONAL MOMENTARY OVER-RIDE SWITCH. CZAW SPORTCRUISER 12305 SOFT START MODULE INSTALLATION OF CON-AIR SPORTS SOFT START MODULE TO ROTAX 912-ULS ENGINE IN ROTAX 912-ULS VIIZ ACCORDANCE WITH CON-AIR SPORTS INSTRUCTIONS AND SM12305 LEAFLET. CZAW SPORTCRUISER 12938 DYNON D100/ AP74 DUAL AXIS AUTO INSTALLATION OF DYNON DUAL AXIS AUTO PILOT CONTROLLED BY D100 EFIS WITH AP74 CONTROL ROTAX 912-ULS SCRZ PILOT HEAD. ALSO INSTALLATION OF PITCH TRIM DISABLEMENT FEATURE THAT IS ACTIVE WHEN AUTO-PILOT POWER SWITCH IS ON WITH ADDITIONAL MOMENTARY OVER-RIDE SWITCH. Prototype mods that have been approved since 1/1/2008 Page 20 30/11/20 LAA Technical Leaflet TL 3.17 CZAW SPORTCRUISER 13671 SENSENICH 3B0R5R68C-0 68 68" INSTALLATION OF A SENSENICH 3B0R5R68C-0 68, 68 INCH DIAMETER GROUND ADJUSTABLE ROTAX 912-ULS SCRZ DIAMETER PROPELLER INSTALLATION PROPELLER. CZAW SPORTCRUISER 13086 WOODCOMP SR3000/2W 1740MM INSTALLATION OF WOODCOMP SR3000/2W 1740MM DIAMETER PROPELLER WITH WOODCOMP ROTAX 912-ULS EZZE DIAMETER PROPELLER. BLADE PITCH CONTROL UNIT. CZAW SPORTCRUISER 12784 TRIO EZ PILOT (ROLL) AND TRIO EZ-2 TRIO EZ PILOT (ROLL) AND TRIO EZ-2 (PITCH) AUTO-PILOT SERVOS INSTALLED IN SIMILAR ROTAX 912-ULS CRUI (PITCH) AUTO-PILOT INSTALLATIONS. LOCATIONS TO FACTORY INSTALLED TRUTRAK AUTO-PILOT SERVOS. ATTACHMENT OF PUSH-RODS IDENTICAL TO FACTORY INSTALLATION BUT DIFFERENT SERVO DESIGN REQUIRED ADDITIONAL MOUNTING BRACKETRY. TRIM 'ARM' MOMENTORY SWITCH INSTALLED TO AVOID POSSIBILITY OF TRIM RUN-AWAY. CZAW SPORTCRUISER 12933 AVTEK IDROVARIO AVY 2HS 1760MM DIA INSTALLATION OF ELECTRO/HYDRAULIC AVTEK IDROVARIO AVY 2HS 1760MM DIA PROPELLER ROTAX 912-ULS CRUI PROPELLER WITH FLYBOX CONTROLLER. CZAW SPORTCRUISER 14933 WOODCOMP SR3000/3N 1720MM WOODCOMP SR3000/3N 1720MM DIAMETER PROPELLER INSTALLATION WITH FLYBOX PR1-P ROTAX 912-ULS MOGS DIAMETER PROPELLER INSTALLATION ELECTRONIC CONSTANT SPEED CONTROLLER. CZAW SPORTCRUISER 12783 FLEXITEC AUTOMATIC FIRE FLEXITEC FIRE EXTINGUISHER BOTTLE ATTACHED TO AFT FACE OF FIREWALL WITH TUBING ROUTED ROTAX 912-ULS KRUZ EXTINGUISHER AROUND ENGINE COMPARTMENT. EXTINGUISHANT IS HFC 227EA. CZAW SPORTCRUISER 12852 FUEL FLOW TRANSDUCER INSTALLATION OF FLOSCAN 201A-6 FUEL FLOW TRANSDUCER IN ENGINE COMPARTMENT. ROTAX 912-ULS KRUZ CZAW SPORTCRUISER 15472 REINFORCEMENT OF FIREWALL AT NOSE CUSTOM BRACKETS AND SHIMS FABRICATED IN ORDER TO REINFORCE NOSE LEG ATTACHMENT ROTAX 912-ULS CFKB LEG ATTACHMENT STRUCTURE ON FIREWALL I.A.W CZECH SPORT AIRCRAFT (CSA) SB-CR-32 (& SB-SC-048)

EXISTING FIREWALL VERTICAL WEBS SF0157L/P DIFFER IN DETAIL FROM LATER PRODUCTION ITEMS: FORWARD FLANGE TURN OUTWARD; LATER PRODUCTION ITEMS TURN INWARD

ITEMS SF0602L/P, SF0604N & SF0601L/P CUSTOM FABRICATED FROM 0.050" 2024T3 SHEET TO FIT SHIMS FABRICATED FROM 0.050" 2024T3 SHEET AS REQUIRED

LONGER GRIP LENGTH RIVETS USED WHERE REQUIRED

OTHERWISE REINFORCEMENT I.A.W CSA INSTRUCTIONS

CZAW SPORTCRUISER 13696 WOODCOMP SR3000/3N 1720MM INSTALLATION OF WOODCOMP SR3000/3N 1720MM DIAMETER PROPELLER INSTALLATION ROTAX 912-ULS ENST DIAMETER PROPELLER INSTALLATION CZAW SPORTCRUISER 14460 WOODCOMP SR3000/3N 1720MM INSTALLATION OF WOODCOMP SR3000/3N 1720MM DIAMETER PROPELLER ROTAX 912-ULS CFLG DIAMETER PROPELLER INSTALLATION CZAW SPORTCRUISER 14770 MGL DUAL AXIS AUTO-PILOT INSTALLATION OF MGL AVIONICS DUAL AXIS AUTO-PILOT DRIVEN BY MGL iEFIS. ROTAX 912-ULS CFLG INSTALLATION CZAW SPORTCRUISER 12938 DYNON D100/ AP74 DUAL AXIS AUTO INSTALLATION OF DYNON DUAL AXIS AUTO PILOT CONTROLLED BY D100 EFIS WITH AP74 CONTROL ROTAX 912-ULS TUGI PILOT HEAD. ALSO INSTALLATION OF PITCH TRIM DISABLEMENT FEATURE THAT IS ACTIVE WHEN AUTO-PILOT POWER SWITCH IS ON WITH ADDITIONAL MOMENTARY OVER-RIDE SWITCH. CZAW SPORTCRUISER 13680 STRENGTHENER OF NOSE LEG FORK 3RD LEAF ADDED TO NOSE LEG FORK ASSEMBLY. STRUCTURALLY BONDED TO OTHER LEAVES AND ROTAX 912-ULS DADZ SECURED BY AN-3 BOLTS. CZAW SPORTCRUISER 12938 DYNON D100/ AP74 DUAL AXIS AUTO INSTALLATION OF DYNON DUAL AXIS AUTO PILOT CONTROLLED BY D100 EFIS WITH AP74 CONTROL ROTAX 912-ULS CZSC PILOT HEAD. ALSO INSTALLATION OF PITCH TRIM DISABLEMENT FEATURE THAT IS ACTIVE WHEN AUTO-PILOT POWER SWITCH IS ON WITH ADDITIONAL MOMENTARY OVER-RIDE SWITCH. CZAW SPORTCRUISER 13696 WOODCOMP SR3000/3N 1720MM INSTALLATION OF WOODCOMP SR3000/3N 1720MM DIAMETER PROPELLER INSTALLATION ROTAX 912-ULS CFIU DIAMETER PROPELLER INSTALLATION CZAW SPORTCRUISER 13355 WOODCOMP VARIA 170-2-R INSTALLATION OF WOODCOMP VARIA 170-2-R 1700MM DIAMETER WITH MANUALLY OPERATED ROTAX 912-ULS IBUZ PITCH CHANGE SYSTEM VIA WINDER MOUNTED TO INSTRUMENT PANEL.

Prototype mods that have been approved since 1/1/2008 Page 21 30/11/20 LAA Technical Leaflet TL 3.17 CZAW SPORTCRUISER 12938 DYNON D100/ AP74 DUAL AXIS AUTO INSTALLATION OF DYNON DUAL AXIS AUTO PILOT CONTROLLED BY D100 EFIS WITH AP74 CONTROL ROTAX 912-ULS IBUZ PILOT HEAD. ALSO INSTALLATION OF PITCH TRIM DISABLEMENT FEATURE THAT IS ACTIVE WHEN AUTO-PILOT POWER SWITCH IS ON WITH ADDITIONAL MOMENTARY OVER-RIDE SWITCH. CZAW SPORTCRUISER 13576 FUEL FLOW TRANSDUCER INSTALLATION FUEL FLOW MONITORING SYSTEM INCORPORATING THE ELECTRONICS INTERNATIONAL FT-60 'RED ROTAX 912-ULS IBUZ CUBE' TRANSDUCER INSTALLED IN THE FUEL LINE AFTER THE FUEL VAPOUR RETURN LINE AND BEFORE THE TEE FOR THE TWO CARBURETTORS. CZAW SPORTCRUISER 14866 WOODCOMP SR 3000/3 1700MM INSTALLATION OF WOODCOMP SR 3000/3 1700MM DIAMETER PROPELLER ROTAX 912-ULS IBUZ DIAMETER PROPELLER INSTALLATION CZAW SPORTCRUISER 12718 INSTALLATION OF FUEL FLOW SENSOR INSTALLATION OF FLOSCAN 201A-6 FUEL FLOW SENSOR. THE SENSOR IS LOCATED ON A BRACKET ROTAX 912-ULS SPCZ ON THE CABIN FLOOR ON THE AIRCRAFT'S CENTRELINE. THE SENSOR IS POSITIONED BETWEEN THE FUEL SELECTOR AND GASCOLATOR WITH A ROTAX COMPLIANT FUEL FILTER IMMEDIATELY UPSTREAM OF THE SENSOR. CZAW SPORTCRUISER 12938 DYNON D100/ AP74 DUAL AXIS AUTO INSTALLATION OF DYNON DUAL AXIS AUTO PILOT CONTROLLED BY D100 EFIS WITH AP74 CONTROL ROTAX 912-ULS SCCZ PILOT HEAD. ALSO INSTALLATION OF PITCH TRIM DISABLEMENT FEATURE THAT IS ACTIVE WHEN AUTO-PILOT POWER SWITCH IS ON WITH ADDITIONAL MOMENTARY OVER-RIDE SWITCH. CZAW SPORTCRUISER 13723 DYNON D100/AP74 DUAL AXIS AUTO- INSTALLATION OF DYNON DUAL AXIS AUTO-PILOT IN FUSELAGE IN ACCORDANCE WITH CZAW ROTAX 912-ULS CGLP PILOT INSTALLATION DRAWING SI0020N, OPERATED BY A DYNON D100 VIA A DYNON AP74 AUTO-PILOT CONTROL MODULE. SV32 SERVOS USED FOR PITCH AND ROLL FUNCTIONS. MOMENTARY TOGGLE PITCH TRIM ENABLE SWITCH INSTALLED ON INSTRUMENT PANEL CENTRE CONSOLE JUST FORWARD OF THROTTLE LEVER. CZAW SPORTCRUISER 14772 WOODCOMP SR3000/2W 1740MM INSTALLATION OF WOODCOMP SR3000/2W 1740MM DIAMETER PROPELLER WITH ELECTRONIC ROTAX 912-ULS CGLP DIAMETER PROPELLER INSTALLATION MANUAL VARIABLE PITCH CONTROLLER. CZAW SPORTCRUISER 12987 INSTALLATION OF FUEL FLOW METER INSTALLATION OF FUEL FLOW METER INCORPORATING A FLOSCAN 201 TRANSDUCER AND MGL ROTAX 912-ULS SCSC ODYSSEY DISPLAY. TRANSDUCER INSTALLED AFTER FUEL VAPOUR RETURN IN LINE TO PORT CARBURETTOR. CZAW SPORTCRUISER 13841 MGL ODYSSEY DUAL AXIS AUTO-PILOT INSTALLATION OF MGL DUAL AXIS AUTO-PILOT CONTROLLED BY MGL ODYSSEY EFIS. ROLL AND ROTAX 912-ULS SCSC INSTALLATION PITCH SERVOS MOUNTED TO BRACKETS ATTACHED TO FUSELAGE FLOOR. PITCH TRIM ISOLATED WHEN AUTO-PILOT POWER SWITCH SELECTED ON. NO TRIM ENABLING SWITCH INSTALLED. CZAW SPORTCRUISER 14206 TRUTRAK VIZION 385 AUTOPILOT INSTALLATION OF TRUTRAK VIZION 385 DUAL AXIS AUTO-PILOT WITH SERVOS' INSTALLED IN ROTAX 912-ULS MISJ INSTALLATION ACCORDANCE WITH MANUFACTURER'S INSTRUCTIONS (ILLUSTRATED PARTS CATALOGUE REV 0, FIG 22-10-01 REFERS). PITCH TRIM ELECTRICALLY ISOLATED WHEN AUTO-PILOT POWER IS ON. PITCH TRIM MOMENTARY ENABLING SWITCH INSTALLED. PITCH SERVO SPEED REDUCER FITTED IN ACCORDANCE WITH LAA MOD-338-014. CZAW SPORTCRUISER 12758 AOA DUPLICATE PITOT USING STANDARD INSTALLATION OF A DYNON ANGLE OF ATTACK PITOT ON A STANDARD CZAW PITOT MOUNT ON ROTAX 912-ULS HMPS CZAW MOUNT THE STARBOARD WING TO PROVIDE PRESSURE DATA FOR AN EFIS. STANDARD CZAW PITOT PORT RETAINED ON PORT WING TO PROVIDE PRESSURE FOR NORMAL ANALOGUE GAUGES.

CZAW SPORTCRUISER 14524 WOODCOMP SR3000/3N 1720MM INSTALLATION OF WOODCOMP SR3000/3N 1720MM DIAMETER PROPELLER WITH WOODCOMP ROTAX 912-ULS HMPS DIAMETER PROPELLER INSTALLATION ELECTRONIC CONSTANT SPEED CONTROLLER.

CZAW SPORTCRUISER 12653 STROBE/NAV LIGHT INSTALLATION FITMENT OF AVEO 'E' SERIES PORT, STARTBOARD AND REAR STROBE AND NAVIGATION LIGHTS ROTAX 912-ULS WWZZ AND ASSOCIATED CIRCUIT BREAKERS, SWITCHES AND WIRING. CZAW SPORTCRUISER 13571 2-AXIS AUTOPILOT INSTALLATION DYNON D100 AND AP74 DUAL AXIS AUTO-PILOT USING TWO DYNON SV32 SERVOS INSTALLED AS ROTAX 912-ULS WWZZ PER FACTORY STANDARD. CZAW SPORTCRUISER 13370 AVTEK IDROVARIO AVY 2HS 1760MM DIA INSTALLATION OF ELECTRO/HYDRAULIC AVTEK IDROVARIO AVY 2HS 1760MM DIA PROPELLER ROTAX 912-ULS JONL PROPELLER INSTALLATION. WITH FLYBOX CONTROLLER AND REMOTE SLIDER POTENTIOMETER RPM CONTROL.

Prototype mods that have been approved since 1/1/2008 Page 22 30/11/20 LAA Technical Leaflet TL 3.17 CZAW SPORTCRUISER 12938 DYNON D100/ AP74 DUAL AXIS AUTO INSTALLATION OF DYNON DUAL AXIS AUTO PILOT CONTROLLED BY D100 EFIS WITH AP74 CONTROL ROTAX 912-ULS CGJT PILOT HEAD. ALSO INSTALLATION OF PITCH TRIM DISABLEMENT FEATURE THAT IS ACTIVE WHEN AUTO-PILOT POWER SWITCH IS ON WITH ADDITIONAL MOMENTARY OVER-RIDE SWITCH. CZAW SPORTCRUISER 13550 IMPROVED NOSE WHEEL PIVOT ALTERNATIVE DESIGN OF NOSE WHEEL PIVOT OF INCREASED STRENGTH AND IMPROVED ROTAX 912-ULS CGJT ASSEMBLY MAINTAINABILITY DUE TO PROBLEMS WITH CORROSION AND CRACKING ON ORIGINAL UNIT CZAW SPORTCRUISER 13579 IMPROVED NOSE WHEEL FORK REPLACEMENT FORK COMPONENT MANUFACTURED FROM TITANIUM ALLOY RATHER THAN ROTAX 912-ULS CGJT ASSEMBLY ALUMINIUM ALLOY TO AVOID PROBLEM OF FATIGUE CRACKING AT BOLT HOLES ATTACHING FORK TO BLOCK CZAW SPORTCRUISER 12938 DYNON D100/ AP74 DUAL AXIS AUTO INSTALLATION OF DYNON DUAL AXIS AUTO PILOT CONTROLLED BY D100 EFIS WITH AP74 CONTROL ROTAX 912-ULS CGIP PILOT HEAD. ALSO INSTALLATION OF PITCH TRIM DISABLEMENT FEATURE THAT IS ACTIVE WHEN AUTO-PILOT POWER SWITCH IS ON WITH ADDITIONAL MOMENTARY OVER-RIDE SWITCH. CZAW SPORTCRUISER 13576 FUEL FLOW TRANSDUCER INSTALLATION FUEL FLOW MONITORING SYSTEM INCORPORATING THE ELECTRONICS INTERNATIONAL FT-60 'RED ROTAX 912-ULS CGIP CUBE' TRANSDUCER INSTALLED IN THE FUEL LINE AFTER THE FUEL VAPOUR RETURN LINE AND BEFORE THE TEE FOR THE TWO CARBURETTORS. CZAW SPORTCRUISER 12938 DYNON D100/ AP74 DUAL AXIS AUTO INSTALLATION OF DYNON DUAL AXIS AUTO PILOT CONTROLLED BY D100 EFIS WITH AP74 CONTROL ROTAX 912-ULS KUIP PILOT HEAD. ALSO INSTALLATION OF PITCH TRIM DISABLEMENT FEATURE THAT IS ACTIVE WHEN AUTO-PILOT POWER SWITCH IS ON WITH ADDITIONAL MOMENTARY OVER-RIDE SWITCH. CZAW SPORTCRUISER 12938 DYNON D100/ AP74 DUAL AXIS AUTO INSTALLATION OF DYNON DUAL AXIS AUTO PILOT CONTROLLED BY D100 EFIS WITH AP74 CONTROL ROTAX 912-ULS CGJS PILOT HEAD. ALSO INSTALLATION OF PITCH TRIM DISABLEMENT FEATURE THAT IS ACTIVE WHEN AUTO-PILOT POWER SWITCH IS ON WITH ADDITIONAL MOMENTARY OVER-RIDE SWITCH. CZAW SPORTCRUISER 15345 ENGINE & PROP CHANGE TO ROTAX 912 ENGINE CHANGED TO ROTAX 912-ULS WITH KASPAR THREE BLADED PROPELLER ROTAX 912-ULS CGJS ULS & KASPAR KA-4/3-PA DAVIS DA-2A 12486 PROPELLER CHANGE TO NEWTON TYPE PROPELLER CHANGE TO NEWTON TYPE 07, 67" DIA X 52" PITCH PROPELLER CONTINENTAL O-200-A BPFL 07, 67" DIA X 52" PITCH PROPELLER DAVIS DA-2A 14150 HERCULES 6656471-S 66" x 56" INSTALLATION OF HERCULES 6656471-S 66 INCH DIAMETER X 56 INCH PITCH PROPELLER CONTINENTAL O-200-A BPFL PROPELLER INSTALLATION 12478 PROPELLER CHANGE TO WARP DRIVE 2 CHANGE OF PROPELLER TO WARP DRIVE 2 BLADED 64" DIAMETER ROTAX 532 BNYX BLADED 64" DIAMETER DENNEY KITFOX 12635 ENGINE CHANGE TO ROTAX 582 ENGINE CHANGE TO ROTAX 582 WITH 'C' TYPE GEARBOX / 3.0:1 INSTALLED WITH BED MOUNT ROTAX 582 BONY AND GSC TECH-III 66 INCH DIAMETER X 13.25 DEGREES PITCH. DENNEY KITFOX 11721 DUAL THROTTLE CONTROL SECOND PUSH-PULL THROTTLE ADDED FOR DUAL CONTROL OPERATION ROTAX 582 BONY DENNEY KITFOX 12990 ENGINE CHANGE TO ROTAX 582 ENGINE CHANGE TO ROTAX 582 WITH B TYPE GEARBOX AND REDUCTION RATIO OF 2.58:1 FITTED ROTAX 582 BPKK WITH AN IVOPROP 'ULTRALIGHT' 3 BLADED 66 INCH DIAMETER PROPELLER SET TO PRODUCE 6400 RPM STATIC. DENNEY KITFOX 14201 CATEGORY CHANGE TO MICROLIGHT CATEGORY CHANGE TO MICROLIGHT INVOLVING RE-COMMISSIONING FLAP CONTROL SYSTEM ROTAX 582 BPKK AND CHECKING FULL SPAN WINGS, NOISE CERTIFICATE ISSUED DENNEY KITFOX 14184 REPLACEMENT OF WINGS & WING UNDAMAGED WINGS, WING LIFT STRUTS AND FLAPPERONS FROM DENNEY KITFOX Mk 3 G-BUNM ROTAX 582 KFOX STRUTS SUBSTITUTED IN THEIR ENTIRETY, INCLUDING LARGER FUEL TANKS TOTALLING 17.6 IMP GALLONS CAPACITY. SIGNIFICANT DIFFERENCE IS STRONGER CONFIGURATION OF WING SPAR TUBES AND UPRATED STRUT TUBES. DENNEY KITFOX 13084 KITFOX DUAL THROTTLE CONTROL DUAL FITTED USING SEPARATE PUSH-PULL CABLES ROTAX 912-UL FOXC DENNEY KITFOX 4-1200 12285 GROVE SPRING UNDERCARRIAGE GROVE SPRING MAIN GEAR SUBSTITUTED IN ACCORDANCE WITH GROVE INSTALLATION ROTAX 912-UL BXWH SPEEDSTER INSTRUCTIONS DENNEY KITFOX 4-1200 15090 KIEV 273/1700 PROPELLER INSTALLATION INSTALLATION OF KIEV 273/1700 1700 MM DIAMETER PROPELLER ROTAX 912-UL BXWH SPEEDSTER DENNEY KITFOX MK2 13470 HERCULES 5932334-S 59 X 32 PROPELLER INSTALLATION OF HERCULES 5932334-S 59 INCH DIAMETER X 32 INCH PITCH PROPELLER. JABIRU 2200A BTDC INSTALLATION Prototype mods that have been approved since 1/1/2008 Page 23 30/11/20 LAA Technical Leaflet TL 3.17 DENNEY KITFOX MK2 15079 ADD TOE BRAKES TO THE P2 SIDE INSTALLATION OF TOE BRAKES TO P2 RUDDER PEDALS INCORPORATING P1 TYPE BRAKE PEDALS JABIRU 2200A BTDC MODIFIED TO BE MIRROR IMAGE AND NEW MASTER CYLINDER LUGS WELDED TO P2 RUDDER PEDALS. MATCO MASTER CYLINDERS FITTED TO BOTH P1 AND P2 SIDES AND REMOTE BRAKE FLUID RESERVOIR FITTED TO FRONT OF FIREWALL. DENNEY KITFOX MK2 14896 ENGINE CHANGE TO KFM 112M ENGINE INSTALLATION SUBSTITUTED COMPLETE FROM G-CTOY KFM 112M RWSS DENNEY KITFOX MK2 13982 CATEGORY CHANGE TO MICROLIGHT CATEGORY CHANGE TO MICROLIGHT PER ALREADY ACCEPTED CONFIGURATION AAN PFA 172-0174 ROTAX 582 BSDD Sup. 17 NOISE CERTIFICATE ISSUED DENNEY KITFOX MK2 13155 PROPELLER CHANGE TO IVOPROP 3 C TYPE GEARBOX OF 3:1 RATIO WITH SIDERAIL ENGINE MOUNT AND IVOPROP 3 BLADED 68" ROTAX 582 BSFX BLADED 68" DIAMETER DIAMETER PROPELLER FITTED. DENNEY KITFOX MK2 13521 CATEGORY CHANGE GROUP A TO FULL FUNCTION OF FLAPPERONS RESTORED. MICROLIGHT NOISE CERTIFICATE OBTAINED ROTAX 582 BSUZ MICROLIGHT DENNEY KITFOX MK2 14918 CATEGORY CHANGE TO MICROLIGHT MICROLIGHT CONVERSION WITH OPERABLE FLAPS AND NOISE CERTIFICATE ROTAX 582 BSVK DENNEY KITFOX MK2 15047 PROPELLER CHANGE TO POWERFIN FL ROTAX C TYPE GEARBOX FITTED WITH 3:1 REDUCTION RATIO, TO SUIT POWERFIN FL368T3 ROTAX 582 BUIP 368T3 PROPELLER. DENNEY KITFOX MK2 14502 Category change from Group A to CATEGORY CHANGE TO MICROLIGHT AFTER CHECKING THAT AIRCRAFT HAS STANDARD LENGTH ROTAX 582 FOXS Microlight WINGS, AND FULLY FUNCTIONING FLAPPERONS AND A NOISE CERTIFICATE. DENNEY KITFOX MK2 13940 PROPELLER CHANGE TO WOODCOMP PROPELLER REPLACED BY WOODCOMP KLASSIC 175/3/L . REDUCTION DRIVE REMAINS A 'C TYPE' ROTAX 582 LEED KLASSIC 175/3/L ROTAX UNIT WITH 3:1 REDUCTION RATIO DENNEY KITFOX MK2 15272 CARGO POD KITFOX-SUPPLIED BAGGAGE POD OPTIONALLY INSTALLED BENEATH FUSELAGE. BAGGAGE ROTAX 582 LEED RETENTION STRAPS ADDED. MAXIMUM LOAD TO BE CARRIED IN POD IS 15 KG. DENNEY KITFOX MK2 15324 REMOVE MK2 EMPENAGE & REPLACE AS PART OF ACCIDENT REPAIRS, LATER IMPROVED KITFOX MK 3 TAILPLANE, ELEVATORS, FIN AND ROTAX 582 BRCT WITH MK3 EMPENAGE RUDDER SUBSTITUTED, AND ALSO KITFOX Mk 3 UPRATED TAILPLANE STRUTS DENNEY KITFOX MK2 15340 CATEGORY CHANGE TO SEP - DISABLE FLAP SYSTEM DISABLED BY REMOVING NOTCHES FROM FALP GATE SO FLAPS CANNOT BE LATHED ROTAX 582 BRCT FLAP GATE MECHANISM DOWN IN FLIGHT, BUT CAN BE LOWERED DURING WING FOLD PROCEDURE. AIRCRAFT NOW SEP CATEGORY DENNEY KITFOX MK2 13038 CATEGORY CHANGE TO MICROLIGHT AIRCRAFT RECLASSIFIED AS A MICROLIGHT. ROTAX 582 BTTY DENNEY KITFOX MK2 13135 HEADER FUEL TANK LOW LEVEL LOW LEVEL WARNING SITCH ADDED TO HEADER TANK, OPERATING LIGHT ON PANEL. ROTAX 582 BTTY INDICATOR DENNEY KITFOX MK2 13225 KITFOX MKII OPTIMA WING FILLET MOD FOAM WING FILLER PIECE INTRODUCED BY OPTIMA MOD HAS DISSOLVED IN PETROL, FUMES, ROTAX 582 BTDN REPLACED BY WOOD INSERT TO FULFILL SAME FUNCTION DENNEY KITFOX MK2 13798 ENGINE CHANGE TO ROTAX 582 UL INSTALLATION OF ROTAX 582-UL ENGINE WITH GSC TECH III 68 INCH DIAMETER X 10 DEGREES ROTAX 582 FOXX PITCH AT 25.5 INCHES RADIUS PROPELLER. DENNEY KITFOX MK2 13426 ENGINE CHANGE TO ROTAX 582/48 INSTALLATION OF ROTAX 582/48 ENGINE WITH C TYPE GEARBOX RATIO 3.47:1 USING EXISTING ROTAX 582/48 BTVC ENGINE WITH C TYPE GEARBOX. BASE MOUNTING. KIEV 183 3 BLADED 183CM DIAMETER X 34 DEGREES PITCH AT 35CM RADIUS PROPELLER INSTALLED. DENNEY KITFOX MK3 13347 KFM 112 ENGINE FIT KFM 112 ENGINE AND DENNEY STANDARD KFM ENGINE INSTALLATION KIT RETRO-FITTED KFM 112 CTOY DENNEY KITFOX MK3 12640 OPTIMA WING MODIFICATION THE 'OPTIMA' MODIFICATION PACKAGE IS INSTALLED, INCORPORATING SHORTENING OF EACH KFM 112 CTOY WING BY ONE RIB BAY, ADDITION OF HOERNER-TYPE WING TIPS AND FLATTENING THE BOTTOM OF THE WING SECTION. DENNEY KITFOX MK3 15170 WOODCOMP KLASSIC 170/3/L INSTALLATION OF WOODCOMP KLASSIC 170/3/L, 1740MM DIAMETER PROPELLER. ROTAX 582 BTNR PROPELLER INSTALLATION DENNEY KITFOX MK3 12438 GROVE UNDERCARRIAGE SUBSTITUTED GROVE ALUMINIUM SPRING UNDERCARRIAGE SUBSTITUTED FOLLOWING INSTRUCTIONS SUPPLIED ROTAX 582 BUOL BY GROVE. PREVIOUSLY APPROVED ON G-BZAR/G-BVGO/G-RAYA DENNEY KITFOX MK3 12692 FITTING AEROCET 1100 AMPHIBIOUS AEROCET 1100 AMPHIBIOUS FLOATS FITTED ROTAX 582 BWSN FLOATS APPROVED FOR WATER-BORNE OPERATION ONLY PENDING FINALISING OF WHEELED UNDERCARRIAGE DENNEY KITFOX MK3 12259 GROVE AIRCRAFT MAIN GEAR GROVE AIRCRAFT MAIN GEAR ROTAX 912 BUPW DENNEY KITFOX MK3 12341 GROVE MAIN UNDERCARRIAGE GROVE TYPE MAIN UNDERCARRIAGE SUBSTITUTED ROTAX 912 BUPW

Prototype mods that have been approved since 1/1/2008 Page 24 30/11/20 LAA Technical Leaflet TL 3.17 DENNEY KITFOX MK3 12640 OPTIMA WING MODIFICATION THE 'OPTIMA' MODIFICATION PACKAGE IS INSTALLED, INCORPORATING SHORTENING OF EACH ROTAX 912 BWYI WING BY ONE RIB BAY, ADDITION OF HOERNER-TYPE WING TIPS AND FLATTENING THE BOTTOM OF THE WING SECTION. DENNEY KITFOX MK3 12641 SMOOTH COWLING A SMOOTH AVID-STYLE ENGINE COWL IS INTRODUCED, MANUFACTURED USING GLASS FIBRE ROTAX 912 BWYI REINFORCED PLASTIC INCORPORATING FIRE RETARDANT POLYESTER RESIN. COWL IS ATTACHED TO AIRFRAME AS PER THE ORIGINAL COWL. DENNEY KITFOX MK3 13330 ENGINE & PROPELLER CHANGE ROTAX 912-UL ENGINE AND IVOPROP 3 BLADED 72" DIA PROPELLER FITTED ROTAX 912-UL BUDR DENNEY KITFOX MK3 12438 GROVE UNDERCARRIAGE SUBSTITUTED GROVE ALUMINIUM SPRING UNDERCARRIAGE SUBSTITUTED FOLLOWING INSTRUCTIONS SUPPLIED ROTAX 912-UL BWSJ BY GROVE. PREVIOUSLY APPROVED ON G-BZAR/G-BVGO/G-RAYA DENNEY KITFOX MK3 14409 ENGINE TYPE/MODEL CHANGE ENGINE CHANGE TO ROTAX 912-UL WITH KIEV 273/1700 3 BLADED PROPELLER, USING STANDARD ROTAX 912-UL BWSJ KITFOX INSTALLATION KIT FOR ROTAX 912-UL ENGINE. DENNEY KITFOX MK3 14978 WOODCOMP PROPULS AE 174 3 BLADED INSTALLATION OF A WOODCOMP PROPULS AE 174, 3 BLADED 1740MM DIAMETER PROPELLER. ROTAX 912-UL RFOX 1740MM DIAMETER PROPELLER INSTALLATION DENNEY KITFOX MK3 12576 PROPELLER CHANGE TO ARPLAST INSTALLATION OF ARPLAST ECOPROP 170R 110/3 PROPELLER OF NEWLY INSTALLED ROTAX 912-UL ROTAX 912-UL BXCW ECOPROP 170R 110/3 ENGINE. DENNEY KITFOX MK3 12577 ENGINE CHANGE TO ROTAX 912-UL ENGINE CHANGE TO ROTAX 912-UL WITH ECOPROP 170R 110/3 PROPELLER FITTED. ROTAX 912-UL BXCW DENNEY KITFOX MK4 12993 ROTAX 912-A2 ENGINE AND ARPLAST INSTALLATION OF ROTAX 912-A2 ENGINE WITH ARPLAST ECOPROP 170R/130/3 3 BLADED 1700MM ROTAX 912-A2 PHYL ECOPROP 170R/130/3 PROPELLER INST. DIAMETER PROPELLER.

DENNEY KITFOX MK4 12285 GROVE SPRING UNDERCARRIAGE GROVE SPRING MAIN GEAR SUBSTITUTED IN ACCORDANCE WITH GROVE INSTALLATION ROTAX 912-A2 PHYL INSTRUCTIONS DENNEY KITFOX MK4 14910 ENGINE CHANGE TO ROTAX 912 UL ENGINE CHANGED TO ROTAX 912-UL WITH WOODCOMP KLASSIC 170/3/R PROPELLER, USING ROTAX 912-UL HOBO (MODIFIED) STANDARD ROTAX 912 INSTALLATION KIT FOR KITFOX 4. FACET ELECTRIC FUEL PUMP AND FUEL PRESSURE GAUGE INCLUDED AT ISSUE 2 AFTER SUBSEQUENT ADDITION AS STAGE 2. DENNEY KITFOX MK4 14562 CLIPPED WING AND ALUMINIUM ALLOY WING SPAN CLIPPED TO THAT OF SPEEDSTER VARIANT. 0.015" L163 SHEET BONDED TO RIBS AND ROTAX 912-UL CJLM (MODIFIED) WING LEADING EDGE SKIN FRONT SPAR ON TOP OF FALSE RIBS EXTENDING FROM TOP OF FRONT SPAR TO STRINGER, ON TOP SURFACE OF BOTH WINGS FROM OUTBOARD EDGE OF WING FUEL TANK TO WING TIP. ADHESIVE IS 3M STRUCTURAL ADHESIVE. WING FABRIC IS GLUED TO ALLOY SHEETS AT RIB POSITIONS.

DENNEY KITFOX MK4-1200 12285 GROVE SPRING UNDERCARRIAGE GROVE SPRING MAIN GEAR SUBSTITUTED IN ACCORDANCE WITH GROVE INSTALLATION ROTAX 912-UL BVEY INSTRUCTIONS DENNEY KITFOX MK4-1200 10565 HINGED DOOR CONTROLLING AIR INSTALLATION OF HINGED DOOR INSTALLED WITHIN INLET DUCT IN FRONT OF RADIATOR AND ROTAX 912-UL BVEY THROUGH RADIATOR OPERATED FROM COCKPIT VIA CABLE TO ADJUST VOLUME OF AIR THROUGH RADIATOR. DENNEY KITFOX MK4-1200 12974 ELECTRIC CARBURETTOR HEATERS INSTALLATION OF AN 'ICE ELIMINATOR' CARBURETTOR HEATER SUPPLIED BY ST AVIATION ROTAX 912-UL BVGO SERVICES TO BOTH CARBURETTORS. SEPARATE 30W AND 60W ELEMENT SWITCHES FITTED FOR EACH CARBURETTOR. DENNEY KITFOX MK4-1200 10565 HINGED DOOR CONTROLLING AIR INSTALLATION OF HINGED DOOR INSTALLED WITHIN INLET DUCT IN FRONT OF RADIATOR AND ROTAX 912-UL BVGO THROUGH RADIATOR OPERATED FROM COCKPIT VIA CABLE TO ADJUST VOLUME OF AIR THROUGH RADIATOR. DH60 G GIPSY MOTH 13992 HERCULES DH 5180/5 PROPELLER INSTALLATION OF HERCULES REPLICA DH5180/5 PROPELLER. DE HAVILLAND GIPSY 1 ABDA INSTALLATION DH60G III MOTH MAJOR 14029 ALTERNATIVE PUMP MECHANISM FOR n DH GIPSY MAJOR 1C ACGZ AUXILLIARY FUEL TANK DH60G III MOTH MAJOR 14030 ALTERNATIVE ENGINE RPM INDICATION TWIN ELECTRICAL TACHOS FOTTED, DRIVEN BY TACHO GENERATOR IN FRONT FUSELAGE, OF TYPE DH GIPSY MAJOR 1C ACGZ SYSTEM NORMALLY FITTED TO CHIPMUNK. DH60G III MOTH MAJOR 14032 IMPROVED FRONT LOWER HARNESS m DH GIPSY MAJOR 1C ACGZ ATTACHMENT DH60G III MOTH MAJOR 14892 INSTALLATION OF 'COMFORT' STANDARD REAR WINDSCREEN REPLACED BY ALTERNATIVE MOULDED COMFORT WINDSCREEN OF DH GIPSY MAJOR 1C ACGZ WINDSCREEN GREATER SIZE FOR BETTER IN-FLIGHT COMFORT

Prototype mods that have been approved since 1/1/2008 Page 25 30/11/20 LAA Technical Leaflet TL 3.17 DH60M GIPSY MOTH 13718 ENGINE CHANGE TO DH GIPSY 2 S2 DH GIPSy 2 S2 ENGINE NOW FITTED, BUT WITH MARVEL SCHEBLER CARBURETTOR AND SLICK DE HAVILLAND GIPSY 2 S2 AAMY (MODIFIED) & PROP CHANGE MAGNETOS SUBSTITUTED. EXHAUST, FUEL SYSTEM AND ENGINE CONTROLS MODIFIED TO SUIT (MODIFIED) NEW ENGINE INSTALLATION DH80A PUSS MOTH 14157 PROPELLER CHANGE TO HOFFMANN PROPELLER CHANGED TO HOFFMANN HO21 198B-157 LK DE HAVILLAND GIPSY MAJOR 1C ABLS HO21-198B-157LK DH80A PUSS MOTH 14687 HERCULES 7862707-S 78" x 62" INSTALLATION OF HERCULES 7862707-S 78 INCH DIAMETER X 62 INCH PITCH PROPELLER DH GIPSY MAJOR 1C AAZP PROPELLER INSTALLATION DH82A TIGER MOTH 13413 HOOKER HARNESS INSTALLATION HOOKER HARNESSES FITTED TO FRONT AND REAR COCKPITS. SHOULDER HARNESSES CONNECTED DE HAVILLAND GIPSY MAJOR 1 CGYN TO TRANSVERSE CABLE VIA TWIN LINKS CONNECTING TO SINGLE PULLEY PER E-MAIL 17.9.12.

DH82A TIGER MOTH 13502 HERCULES 7856339-S 78" X 56" INSTALLATION OF HERCULES 7856339-S 78 INCH DIAMETER X 56 INCH PITCH PROPELLER DE HAVILLAND GIPSY MAJOR 1 AHUV PROPELLER INSTALLATION DH82A TIGER MOTH 13413 HOOKER HARNESS INSTALLATION HOOKER HARNESSES FITTED TO FRONT AND REAR COCKPITS. SHOULDER HARNESSES CONNECTED DE HAVILLAND GIPSY MAJOR 1 ARTL TO TRANSVERSE CABLE VIA TWIN LINKS CONNECTING TO SINGLE PULLEY PER E-MAIL 17.9.12.

DH82A TIGER MOTH 13810 ANGLIA SAILPLANES PILOT'S RESTRAINT 'Z' HARNESS MADE BY RE-STRAPPING EXISTING TANGS ADJUSTERS AND RELEASE UNIT, FITTING DE HAVILLAND GIPSY MAJOR 1 ANHK 'Z' HARNESS INDIVIDUAL SHOULDER HARNESS TANGS USING EITHER SCHROTH SEPARATOR LINKS OR SUTTON SHORT FLEXIBLE CABLES RATHER THAN CHIPMUNK TYPE TRIANGULAR PLATE OF MOD 152. MOD ONLY APPLICABLE TO HARNESSES RE-STRAPPED BY ANGLIA SAILPLANES.

DH82A TIGER MOTH 13606 PROPELLER CHANGE TO HERCULES HERCULES 7856339-ST 78 INCH DIAMETER X 56 INCH PITCH PROPELLER INSTALLATION. DE HAVILLAND GIPSY MAJOR 1C AJVE 7856339-ST DH82A TIGER MOTH 14210 HERCULES LA604-HP PROPELLER INSTALLATION OF HERCULES REPLICA OF A LANG LA604 PROPELLER DESIGNATED LA604-HP. DE HAVILLAND GIPSY MAJOR 1C BEWN INSTALLATION DH82A TIGER MOTH 13607 HERCULES 7856339-ST PROPELLER HERCULES 7856339-ST 78 INCH DIAMETER X 56 INCH PITCH PROPELLER INSTALLATION. DE HAVILLAND GIPSY MAJOR 1F ECDS INSTALLATION DH82A TIGER MOTH 15124 FITMENT OF MAIN WHEEL BRAKES AND MATCO HYDRAULIC MAIN WHEEL BRAKES AND CASTORING TAILWHEEL FITTED. UNDERCARRIAGE DE HAVILLAND GIPSY MAJOR 1H ANEH TAIL WHEEL RAKE LEFT UNALTERED. WARNING PLACARD FITTED TO COCKPIT. DH82A TIGER MOTH 15106 HOFFMANN HO21-198B-157LK INSTALLATION OF HOFFMANN HO21-198B-157LK PROPELLER DE HAVILLAND GIPSY MAJOR 1H ANRN PROPELLER INSTALLATION DH82A TIGER MOTH 14239 HERCULES LA604-HP PROPELLER INSTALLATION OF HERCULES LA604-HP PROPELLER, REPLICA OF LA604 PROPELLER MADE USING DE HAVILLAND GIPSY MAJOR 1H ANEN INSTALLATION BEECH WOOD RATHER THAN HONDURAS MAHOGANY. DH82A TIGER MOTH 14880 INSTALL BRAKE SYSTEM WHEEL BRAKES INTRODUCED AS APPROVED BY CAA AAN 29159 DH GIPSY MAJOR 1C AXXV DH82A TIGER MOTH 14386 CUSTOM JOINT 'H' DOWEL BOLTS AND CUSTOM DOWEL BOLTS MANUFACTURED FROM EN24T MATERIAL SHANK DIAMETER INCREASED DH GIPSY MAJOR 1F ANFI SPACER BUSHES TO SUIT OF HOLES AND SHANK LENGTHENED TO PROVIDE FULL ENGAGEMENT OF SHANK ON FITTING AND INCORPORATE SPACER BUSHES TO ALLOW EASIER TIGHTENING OF NUTS

DH82B QUEEN BEE 13836 PROPELLER CHANGE TO HERCULES HERCULES 7856339-ST 78 INCH DIAMETER X 56 INCH PITCH PROPELLER INSTALLATION. DE HAVILLAND GIPSY MAJOR 1 BLUZ 7856339-ST DH82C TIGER MOTH (MODIFIED) 14626 ADDITION OF A WIND DRIVEN ADDITION OF ELECTRICAL SYSTEM CONSISTING OF A BATTERY AND WIND DRIVEN GENERATOR DH GIPSY MAJOR 1C FCTK ALTERNATOR AND BATTERY UNDER BELLY OF AIRCRAFT AND ASSOCIATED COMPONENTS INSTALLATION DH83C FOX MOTH 14139 PILOT SHOULDER HARNESS PILOTS HARNESS INSTALLATION DE HAVILLAND GIPSY MAJOR 1C CIPJ DH85 LEOPARD MOTH 14405 METALLIC MATERIALS SUBSTITUTIONS ALTERNATIVE MATERIAL FOR WHEEL AXLES, ENGINE MOUNT TUBING AND UNDERCARRIAGE DE HAVILLAND GIPSY MAJOR 10 MK ACMA PISTON TUBES, DUE TO LACK OF AVAILABILITY OF ORIGINAL SPEC MATERIALS 1 DH85 LEOPARD MOTH 14406 INTRODUCTION OF TAIL WHEEL LOCK TAILWHEEL LOCK ADDED TO CASTORING TAILWHEEL, CONTROLLABLE FROM COCKPIT USING DE HAVILLAND GIPSY MAJOR 10 MK ACMA BOWDEN CABLE AND CONTROL LEVER AND IDENTIFIED AS TO FUNCTION BY AN ASSOCIATED 1 PLACARD DH87B HORNET MOTH 14148 HERCULES LA596/3-H PROPELLER INSTALLATION OF HERCULES REPLICA OF A LANG LA596/3, 6.5 FT DIAMETER X 5.36 FT PITCH DE HAVILLAND GIPSY MAJOR 10 MK ADND INSTALLATION PROPELLER WHICH WAS DESIGNED FOR USE ON THE GIPSY MAJOR 1 ENGINE WHOSE MAXIMUM 2 RPM IS 2400. Prototype mods that have been approved since 1/1/2008 Page 26 30/11/20 LAA Technical Leaflet TL 3.17 DHC-1 CHIPMUNK 22 14272 TANK TO COLLECT OIL EXHAUSTED FROM INSTALLATION OF A TANK TO COLLECT OIL EXHAUSTED FROM VACUUM PUMP SIMILAR TO THE DE HAVILLAND GIPSY MAJOR 10 MK ATHD VACUUM PUMP TYPE FITTED TO 105 CANADIAN CHIPMUNKS. 2 DHC-1 CHIPMUNK 22 14939 ENGINE OIL AND FUEL FLEXIBLE HOSES Engine fuel and oil hoses replaced with convoluted PTFE stainless steel braided hose (p/n AR##S) DE HAVILLAND GIPSY MAJOR 10 MK BFAX with Progold fittings. Previous mod 14657 cleared this type of hose and end fitting for oil hoses on 2 Chipmunk, this modification extends this to include the two engine flexible fuel hoses.

DHC-1 CHIPMUNK 22 14531 SOLID STATE VOLTAGE REGULATOR CUSTOM SOLID STATE VOLTAGE REGULATOR MODULE SUBSTITUTED INCLUDING MOSFET DEVICES DE HAVILLAND GIPSY MAJOR 10 MK PVET FOR REVERSE FUNCTION BLOCKING AND THE ADDITION OF AN ALTERNATOR ON/OFF SWITCH 2

DHC-1 CHIPMUNK 22 14531 SOLID STATE VOLTAGE REGULATOR CUSTOM SOLID STATE VOLTAGE REGULATOR MODULE SUBSTITUTED INCLUDING MOSFET DEVICES DE HAVILLAND GIPSY MAJOR 10 MK BWMX FOR REVERSE FUNCTION BLOCKING AND THE ADDITION OF AN ALTERNATOR ON/OFF SWITCH 2

DHC-1 CHIPMUNK 22 14657 ENGINE OIL FLEXIBLE HOSES ENGINE OIL PIPES REPLACED USING PRO-GOLD CONVOLUTED PTFE HOSE WITH MATCHING PRO- DE HAVILLAND GIPSY MAJOR 10 MK BWMX GOLD LARGE RADIUS END FITTINGS 2 DHC-1 CHIPMUNK 22 14295 SOLID STATE VOLTAGE REGULATOR INSTALLATION OF A TRANSPRO IB308-3280-24V SOLID STATE VOLTAGE REGULATOR TO REPLACE DH GIPSY MAJOR 10 MK 2 BBMZ INSTALLATION THE ORIGINAL CARBON PILE REGULATOR WHICH IS UNRELIABLE AND DIFFICULT TO OBTAIN. INCLUDES A DIODE TO REPLACE THE REVERSE CURRENT RELAY. COCKPIT SWITCH INSTALLED BETWEEN THE FIELD OUTPUT AND THE GENERATOR. COCKPIT MOUNTED VOLTMETER INSTALLED TO MONITOR VOLTAGE AT LEAST UNTIL RELIABILITY HAS BEEN ESTABLISHED. DHC-1 CHIPMUNK 22 13753 SUBSTITUTION OF RIVET TYPES IN SUBSTITUTE CHERRYMAX 3213 AND 3243 RIVETS USED TO REPLACE 'SMOKING' CHOBERT RIVETS IN DH GIPSY MAJOR 10 MK 2 BCYM TAILPLANE TAILPLANE, IN APPROXIMATELY 20 LOCATIONS FOR RIVETS ATTACHING TAILPLANE SKIN AND REPLACING SOLID CSK AS2230 RIVETS IN APPROXIMATELY EIGHT LOCATIONS ATTACHING STIFFENERS TO SKIN DHC-1 CHIPMUNK 22 14914 COMPOSITE MANUFACTURE INSTALLATION OF SPINNER DOME MANUFACTURED FROM CARBON FIBRE REINFORCED PLASTIC DH GIPSY MAJOR 10 MK 2 BBMO AND INSTALLATION THAT MATES WITH THE EXISTING CAST ALUMINIUM BACK PLATE FOR FAIREY REED PROPELLERS IN THE SAME WAY AS THE ORIGINAL ALUMINIUM SPINNER DOME. SPINNER DOME SECURED WITH 2BA T25 TORX BOLTS INTO EXISTING ANCHOR NUTS IN BACK PLATE. DHC-1 CHIPMUNK 22 13846 FITMENT OF SPATS INSTALLATION OF GRP MAIN WHEEL SPATS DH GIPSY MAJOR 10 MK 2 AOUP DHC-1 CHIPMUNK 22 15296 ALTERNATIVE FUEL CELLS REPLACEMENT 'BLADDER' FUEL CELLS MANUFACTURED BY PREMIER FUEL SYSTEMS LTD USING DH GIPSY MAJOR 10 MK 2 CGAO ORIGINALS AS PATTERNS. REPLACEMENTS CONSTRUCTED FROM A SIMILAR BALLISTIC NYLON FABRIC WITH A PVC-NITRILE- BLEND RUBBER COATING TO THE ORIGINALS. ORIGINAL FITTINGS REUSED. DHC-1 CHIPMUNK 22 14916 ENGINE CHANGE TO LYCOMING O-360- ENGINE CHANGE FROM LYCOMING 0-360-A4A to -A3A LYCOMING O-360-A4A BCSA (LYCOMING) A3A DHC-1 CHIPMUNK 22A 14939 ENGINE OIL AND FUEL FLEXIBLE HOSES Engine fuel and oil hoses replaced with convoluted PTFE stainless steel braided hose (p/n AR##S) DE HAVILLAND GIPSY MAJOR 10 MK BVTX with Progold fittings. Previous mod 14657 cleared this type of hose and end fitting for oil hoses on 2 Chipmunk, this modification extends this to include the two engine flexible fuel hoses.

DHC-1 CHIPMUNK 22A 14404 SOLID-STATE REGULATOR AND INSTALLATION OF A TRANSPRO IB308 SOLID STATE VOLTAGE REGULATOR IN PLACE OF THE DH GIPSY MAJOR 10 MK 2 BXDG GENERATOR FIELD SWITCH ORIGINAL CARBON PILE REGULATOR - ORIGINAL REVERSE CURRENT RELAY RETAINED - AND A INSTALLATIONS 28VDC/10A GUARDED GENERATOR FIELD SWITCH LOCATED ON FRONT COCKPIT LH SWITCH PANEL REPLACING THE ORIGINAL GENERATOR TEST SWITCH. DHC-1 CHIPMUNK 22A 14657 ENGINE OIL FLEXIBLE HOSES ENGINE OIL PIPES REPLACED USING PRO-GOLD CONVOLUTED PTFE HOSE WITH MATCHING PRO- DH GIPSY MAJOR 10 MK 2 BXDG GOLD LARGE RADIUS END FITTINGS DHC-1 CHIPMUNK 22A 15087 INSTALL USB CHARGING PORT ALFATRONIX DUAL USB POWER SUPPLY MOUNTED ON CUSTOM BRACKET ADJACENT TO DH GIPSY MAJOR 10 MK 2 ARWB INSTRUMENT PANEL, INCLUDING IN-LINE FUSE. DR 107 ONE DESIGN 12346 ENGINE CHANGE TO ECI TITAN O-320- CHANGE OF ENGINE TO ECI TITAN O-320-A1B1N WITH MTV-11-C-C/C183-59b PROPELLER. ECI TITAN EXP O-320- RIHN A1B1N. A1B1N DR 107 ONE DESIGN 13199 SIDE HINGE CANOPY SIDE HINGED RATHER THAN SLIDING CANOPY LYCOMING AEIO-320-D1B TAZZ Prototype mods that have been approved since 1/1/2008 Page 27 30/11/20 LAA Technical Leaflet TL 3.17 DR 107 ONE DESIGN 12839 ONE DESIGN ENGINE MODIFICATIONS P-MAG IGNITION INSTALLED IN PLACE OF STANDARD MAGNETOS LYCOMING IO-360-B1B CEPZ DR 107 ONE DESIGN 12400 PROPELLER CHANGE SENSENICH W76EM-66G PROPEELER FITTED LYCOMING IO-360-B1E LOAD DR 107 ONE DESIGN 14024 MID-WING MODIFICATION WING RAISED TO MID-WING POSITION LYCOMING O-320-D2A PBII DR 107 ONE DESIGN 15130 SIDE HINGE CANOPY SIDE HINGED CANOPY SIMILAR IN ALL BUT MINOR DETAIL TO THAT ON ONE DESIGN G-IIPB. LYCOMING O-320-D2A PBII DR 107 ONE DESIGN 12829 ENGINE CHANGE TO LYCOMING O-360 ENGINE CHANGE TO LYCOMING O-360 A1A WITH MT 180R170-4G PROPELLER. LYCOMING O-360-A1A IIID A1A (MODIFIED) DR 107 ONE DESIGN 11355 ALUMINIUM AILERONS SHEET ALUMINIUM AILERON SURFACES DESIGNED, CONSTRUCTED AND INSTALLED ON THIS LYCOMING O-360-A1A IIID AIRCRAFT. (MODIFIED)

MASS BALANCE WEIGHT ALTERED TO SUIT LIGHTER AILERONS. DR 107 ONE DESIGN 13944 STRAP HINGES - RUDDER RUDDER REPLACED WITH AN IDENTICAL RUDDER BUT USING IMPROVED STRAP HINGES WITH LYCOMING O-360-A1A IIID REPLACEABLE BEARING SHELLS OF THE TYPE AND IN THE SAME CONFIGURATION AS USED ON (MODIFIED) CHRISTEN EAGLE DR 107 ONE DESIGN 14113 AIRFLOW PERFORMANCE FUEL INSTALLATION OF AIRFLOW PERFORMANCE INC. FM-150 SYSTEM. LYCOMING O-360-A1A IIID INJECTION SYSTEM (MODIFIED) DR 107 ONE DESIGN 14225 VANS TYPE TAILWHEEL SPRING ROD AND INSTALLATION OF A VANS RV-8 TAILWHEEL SPRING ROD AND TAILWHEEL ASSEMBLY INSTALLED IN LYCOMING O-360-A1A IIID TAILWHEEL ASSEMBLY INSTALLATION CUSTOM MADE WELDED 4130 STEEL BRACKET MOUNTED TO REAR FUSELAGE USING ORIGINAL (MODIFIED) MOUNTING POINTS. DR 107 ONE DESIGN 14813 WHIRLWIND 200C 77 INCH DIAMETER INSTALLATION OF WHIRLWIND 200C 77 INCH DIAMETER PROPELLER LYCOMING O-360-A1A IIID PROPELLER INSTALLATION (MODIFIED) DR 107 ONE DESIGN 13199 SIDE HINGE CANOPY SIDE HINGED RATHER THAN SLIDING CANOPY SUPERIOR XP-IO-360-B1AA3 CVII DR 107 ONE DESIGN 13237 P-MAG P-114 DUAL ELECTRONIC INSTALL DUAL E-MAG P-114 P-MAG IGNITION UNITS, IN ACCORDANCE WITH THE SUPERIOR XP-IO-360-B1AA3 CVII IGNITION MANUFACTURER'S INSTRUCTIONS. DR 107 ONE DESIGN 12047 AILERON PUSHROD REPLACEMENT ALTERNATIVE DESIGN OF AILERON PUSHROD SUPERIOR XP-IO-360-B1AA3 CVII DR 107 ONE DESIGN 11355 ALUMINIUM AILERONS SHEET ALUMINIUM AILERON SURFACES DESIGNED, CONSTRUCTED AND INSTALLED ON THIS SUPERIOR XP-IO-360-B1AA3 CVII AIRCRAFT.

MASS BALANCE WEIGHT ALTERED TO SUIT LIGHTER AILERONS. DR 107 ONE DESIGN 13778 SIDE-HINGED ONE-PIECE CANOPY SIDE-HINGED ONE-PIECE CANOPY. SUPERIOR XP-IO-320-B1AC2 RWOD (MODIFIED) DR 107 ONE DESIGN 12047 AILERON PUSHROD REPLACEMENT ALTERNATIVE DESIGN OF AILERON PUSHROD SUPERIOR XP-IO-320-B1AC2 RWOD (MODIFIED) DR 107 ONE DESIGN 14119 USE ORATEX 6000 TO COVER PARTS OF ORATEX 6000 USED TO COVER REAR FUSELAGE, AND AILERONS. SUPERIOR XP-IO-320-B1AC2 RWOD AIRCRAFT (MODIFIED) DR 107 ONE DESIGN 14226 SUPERIOR XP-IO-320-B1AC2 (MODIFIED) INSTALLATION OF A SUPERIOR XP-IO-320-B1AC2 MODIFIED WITH THE INCLUSION OF: SUPERIOR XP-IO-320-B1AC2 RWOD ENGINE INSTALLATION 1. ECI 340 4.125 INCH CRANKSHAFT PT NO. AEL34104-3 (MODIFIED) 2. ACE PERFORMANCE AX40 LIGHTWEIGHT CYLINDER ASSEMBLIES, VALVES AND SPRINGS 3. ACE PERFORMANCE LIGHTWEIGHT PISTONS AND CON-RODS - (CAPACITY = 357 CU IN, CR 8.7:1, ESTIMATED POWER = 190 - 195 HP) 4. SKY DYNAMICS COLD SUMP WITH SWINGING ARM OIL PICK-UP 5. SKY DYNAMICS LIGHTWEIGHT FLYWHEEL - NO ALTERNATOR DRIVE 6. DUAL P-MAG P114-L4 MODEL ELECTRONIC IGNITION

MTV-12-B-C/C183-17e 183CM (72 INCH) DIAMETER PROPELLER FITTED DR 107 ONE DESIGN 14314 VANS RV-8 TAILWHEEL ASSEMBLY AND VANS RV-8 TAILWHEEL ASSEMBLY, INCORPORATING A 6" TAILWHEEL. SUPERIOR XP-IO-320-B1AC2 RWOD SPRING ROD INSTALLATION (MODIFIED) DR 107 ONE DESIGN 14363 EARTHX LITHIUM BATTERY EARTHX ETX900 LITHIUM IRON PHOSPHATE BATTERY MOUNTED IN CUSTOM-BUILT STRUCTURE IN SUPERIOR XP-IO-320-B1AC2 RWOD REAR FUSELAGE. (MODIFIED) DRUINE D.31 TURBULENT 13090 COIL IGNITION FOR ENGINE STARTING SINGLE COIL IGNITION SYSTEM FOR STARTING, IN ADDITION TO EXISTING DUAL MAGNETO BVLU IGNITION SYSTEM. DRUINE D.31 TURBULENT 13353 CHANGE OF MAIN WHEELS Ikarus C42 main wheels substituted VW 1500 APUY Prototype mods that have been approved since 1/1/2008 Page 28 30/11/20 LAA Technical Leaflet TL 3.17 DRUINE D.31 TURBULENT 12332 PROPELLER CHANGE TO TENNESSEE PROPELLER CHANGE TO TENNESSEE PROPELLERS 58" DIAMETER X 31" PITCH. VW 1500 ATBS PROPELLERS 58" X 31" DRUINE D.31 TURBULENT 13056 PROPS INC. 54" X 38" PROPELLER INSTALLATION OF PROPS INC. 54 INCH DIAMETER X 38 INCH PITCH PROPELLER CROPPED FROM 58 VW 1500 ATBS INCHES DIAMETER. DRUINE D.31 TURBULENT 13169 PROPELLER CHANGE TO EVRA L38/81/17 EVRA-BUILT COPY OF LODGE CJL 129 54" x 32" PROPELLER FITTED VW 1600 APIZ

DRUINE D.31 TURBULENT 13367 RWG 101C 59" X 31" PROPELLER INSTALLATION OF RWG 101C 59 INCH DIAMETER X 31 INCH PITCH PROPELLER. VW 1600 APVZ INSTALLATION DRUINE D.31 TURBULENT 14436 HOT AIR BOX SCREEN INSTALLATION SCREEN FITTED TO COLD AIR INLET TO HOT AIR SELECTOR BOX TO PREVENT INGRESS OF FOREIGN VW 1600 ARGZ BODIES, INTRODUCED AS A RESULT OF A PARTIAL ENGINE FAILURE CAUSED BY INGESTING THE REMAINS OF A BALLOON DURING A TIGER CLUB BALLOON BURSTING DEMONSTRATION. APPLICABLE ONLY TO AIRCRAFT FITTED WITH A SEPARATE PILOT-SELECTABLE CARBURETTOR HOT AIR SUPPLY DRUINE D.31 TURBULENT 12840 INSTALLATION OF LEBURG EI10A LEBURG ELECTRONIC IGNITION FITTED EXCEPT SENSORS MOUNTED ON FRONT COWLING VW 1600 ASFX ELECTRONIC IGNITION SYSTEM NOSEBOWL. BMW BELT DRIVEN ALTERNATOR FITTED. ELECTRONIC IGNITION UNITS MOUNTED IN CCOKPIT DRUINE D.31 TURBULENT 12821 PROPELLER CHANGE TO NEWTON TYPE PROPELLER CHANGE TO NEWTON TYPE 15L 58 INCH DIAMETER X 38 INCH PITCH. VW 1600 AWMR 15L 58" X 38" DRUINE D.31 TURBULENT 12802 PROPELLER CHANGE TO EVRA Z3405 PROPELLER CHANGE TO EVRA Z3405, 4.75' DIAMETER X 2.45' PITCH. VW 1600 BUKH DRUINE D.31 TURBULENT 13769 ALTERNATIVE PAINT SYSTEM ALTERNATIVE LOW-COST FABRIC TREATMENT USING DOMESTIC EXTERIOR GRADE PAINT SYSTEM VW 1700 ARIM RATHER THAN DOPE BASED SYSTEM TO FILL WEAVE AND PROVIDE WEATHERPROOFING AND UV PROTECTION DRUINE D.31 TURBULENT 13914 SHOULDER HARNESS ATTACHMENT SHOULDER HARNESS ATTACHED TO TAILWHEEL SPRING MOUNTING AREA VIA STRANDED STEEL VW 1700 ARIM CABLE, WITH APPROPRIATE MOUNTING POINT ON AND REINFORCEMENT OF BAGGAGE LOCKER FLOOR DRUINE D.31 TURBULENT 13235 HERCULES 5635292-S 56" x 35" INSTALLATION OF HERCULES 5635292-S 56 INCH DIAMETER X 35 INCH PITCH PROPELLER. VW 1600 ARBZ (MODIFIED) DRUINE D.31 TURBULENT 13800 UPRATE WING SPAR TO ROLLASON D31A WING SPAR UPRATED TO D31A TYPE WITH ASSOCIATED CHANGED TO FUSELAGE FRAME 323 VW 1834 AREZ (MODIFIED) TURBULENT TYPE POSITION TO ACCOMMODATE DRUINE D.31A TURBULENT 13481 HERCULES 5635338-S 56 X 35 PROPELLER INSTALLATION OF HERCULES 5635338-S 56 INCH DIAMETER X 35 INCH PITCH PROPELLER. VW 1700 BKXR INSTALLATION. DRUINE D.31A TURBULENT 10521 LEBURG IGNITION SYSTEM Leburg ignition fitted VW 1700 BKXR DRUINE D.5 TURBI 13414 HERCULES 6740322-S 67" X 40" INSTALLATION OF HERCULES 6740322-S 67 INCH DIAMETER X 40 PITCH PROPELLER. WALTER MIKRON 3 AOTK PROPELLER INSTALLATION DRUINE D.62B CONDOR 14553 NAV/STROBE LIGHTING AEROLED NS180 WING TIP NAV/STROBE LIGHTS INSTALLED ON EXISTING WING-TIP POSITIONS. CONTINENTAL O-200-A AWSN INCLUDING ASSOCIATED SWITCHES, CIRCUIT BREAKERS AND WIRING. DRUINE D.62B CONDOR 13682 MATCO TAILWHEEL ASSEMBLY INSTALLATION OF MATCO WHLT-6 TAILWHEEL INSTALLATION. HOLE IN MOUNTING BASE CONTINENTAL O-200-A AXGS INSTALLATION INCREASED IN DIAMETER FROM 5/16" TO 7/16" TO MATCH ORIGINAL LEAF SPRING. DRUINE D.62B CONDOR 13242 HERCULES 6753282-S 67" x 53" PROPELLER CHANGE TO HERCULES 6753282-S 67 INCH DIAMETER X 53 INCH PITCH. CONTINENTAL O-200-A AYFC PROPELLER DRUINE D.62B CONDOR 12772 PROP CHANGE TO MCCAULEY INSTALLATION OF MCCAULEY 1A105/SCM 71" DIAMETER X 47" PITCH PROPELLER. CONTINENTAL O-200-A ATAU 1A105/SCM 71" X 47" DRUINE D.62B CONDOR 13774 PROPELLER CHANGE TO HERCULES HERCULES 6848420-S 68 INCH DIAMETER X 48 INCH PITCH PROPELLER INSTALLATION. CONTINENTAL O-200-A ATAU 6848420-S DRUINE D.62B CONDOR 13881 PROPELLER CHANGE TO HERCULES INSTALLATION OF HERCULES 6846430-S 68 INCH DIAMETER X 46 INCH PITCH PROPELLER. CONTINENTAL O-200-A ATVW 6846430-S DRUINE D.62B CONDOR 12385 BATTERY RELOCATED TO FIREWALL BATTERY BOX FITTED TO FIREWALL TO IMPROVE CG POSITION CONTINENTAL O-200-A AVOH DRUINE D.62B CONDOR 13793 RELOCATION OF BATTERY BATTERY RELOCATED TO FORWARD FACE OF FIREWALL FOR CG REASONS, FIREWALL REINFORCED CONTINENTAL O-200-A AWEI INTERNALLY AND CUSTOM BATTERY BOX FABRICATED DRUINE D.62B CONDOR 13794 INSTALLATION OF NACA VENTS NACA DUCT INLETS ADDED TO EACH SIDE OF FORWARD FUSELAGE IN COCKPIT SIDES, FEEDING CONTINENTAL O-200-A AWEI PUNKAH-LOUVRES FOR COCKPIT VENTILATION Prototype mods that have been approved since 1/1/2008 Page 29 30/11/20 LAA Technical Leaflet TL 3.17 DRUINE D.62B CONDOR 13881 PROPELLER CHANGE TO HERCULES INSTALLATION OF HERCULES 6846430-S 68 INCH DIAMETER X 46 INCH PITCH PROPELLER. CONTINENTAL O-200-A AWEI 6846430-S DRUINE D.62C CONDOR 13820 REPLACEMENT EXHAUST PIPES REPLACEMENT EXHAUST STACKS MANUFACTURED BY CKT TO DRAWING 'EXHAUST FOR CONDOR CONTINENTAL O-240-A ATAV D62C' DATED 15.2.14 DUKERIES BULLDOG 200 13645 IMPROVED NOSE LEG SEAL ALTERNATIVE NOSE LEG HYDRAULIC SEAL PER APPLICANT DETAILS LYCOMING AEIO-360-A1B6 BDOG DUKERIES BULLDOG 200 13843 COSMETIC IMPROVEMENT TO SIDE TWO ADDITIONAL SIDE WINDOWS INCORPORATED INTO NON-STRUCTURAL PART OF COCKPIT IN LYCOMING AEIO-360-A1B6 BDOG WINDOWS PART OF STRUCTURE REPLACING CANOPY IN STANDARD BULLDOG. DYNAERO MCR 01 (VLA) 12780 BERINGER HYDRAULIC BRAKE KIT FOR BERINGER BRAKES INSTALLED IN ACCORDANCE WITH BERINGER INSTRUCTIONS ROTAX 912 CCWH DYNAERO MCR01 DYNAERO MCR 01 (VLA) 13097 TREAT FUEL TANK WITH PHENOL FUEL TANK TREATED WITH PHENOL NOVOLAC SEALANT IN ACCORDANCE WITH MANUFACTURER'S ROTAX 912 CCWH NOVOLAC INSTRUCTIONS, AND IMMERSION TESTS CARRIED OUT ON THE FIRST INSTALLATION USING BOTH AND UNLEADED MOGAS CONTAIING ETHANOL. DYNAERO MCR 01 (VLA) 13392 FLAPPERON DRIVE SCREW AND REPLACEMENT FLAPPERON DRIVE SCREW AND SHEAVE NUTS MADE LOCALLY MANUFACTURED ROTAX 912 CCWH CARRIAGE FOLOWING WEAR PROBLEMS WIH ORIGINAL PARTS. PULLEY RETAINED BY WOODRUFF KEY FOR IMPROVED SECURITY. EAA BIPLANE 13331 REDUCTION OF PROPELLER DIAMETER PROPELLER CLIPPED TO 70" DIAMETER AND REBALANCED AND RE-FINISHED LYCOMING O-235 BPUA TO 70" EAA BIPLANE 15043 REPLACE MAGNETOS INSTALLATION OF 2X E-MAP P MODEL 114 ELECTRONIC IGNITION MODULES. LYCOMING O-320-E3D BBMH EAA BIPLANE MODEL P 13176 PROPELLER CHANGE TO JAMES 73" x 52" REPLICA PROPELLER OF FLOTTORP 73" x 52" AS PREVIOUSLY FITTED LYCOMING O-290-G AVZW

EDGE 360 12365 LIGHTSPEED PLASMA III IGNITION LIGHTSPEED PLASMA III SYSTEM INSTALALED IN ACCORDANCE WITH MANUFACTURER'S LYCOMING IO-360-C1E6 ZVKO REPLACING ONE MAGNETO RECOMMENDATIONS

MODIFICATION ACEPTED FOR USE WITH WOODEN PROPELLERS ONLY ESCAPADE 13789 PROPELLER CHANGE TO HERCULES INSTALLATION OF HERCULES 6034393-S 60 INCH DIAMETER X 34 INCH PITCH PROPELLER. JABIRU 2200A CFBO 6034393-S ESCAPADE 12261 UL POWER UL260I UL POWER UL260I INSTALLED DURING AIRCRAFT BUILD. ELECTRICAL INSTALLATION AS PER UL POWER 260i MCUB APPLICATION. ESCAPADE 12924 PROPELLER CHANGE TO NEWTON 11R PROPELLER CHANGE TO NEWTON 11R 60" X 41" UL POWER 260i MCUB 60" X 41" ESCAPADE 13388 RAISED BAGGAGE SPACE FLOOR BAGGAGE BAY FLOOR REPLACED WITH PLYWOOD AND FOAM ALTERNATIVE TWO-LEVEL STEPPED UL POWER 260i MCUB DESIGN WITH CLOTH COVER, ENCLOSING ELEVATOR PUSHROD. ESCAPADE 12775 FUEL LEVEL GAUGES INSTALLATION OF FLOAT OPERATED FUEL LEVEL GAUGE IN EACH WING FUEL TANKS BY UL POWER 260i DRPK PENETRATION OF WING ROOT RIB. APPROVAL BASED ON SIMILARITY WITH MOD 12155. ESCAPADE 13625 VORTEX GENERATORS STOLSPEED VORTEX GENERATORS FITTED TO WING UPPER SURFACES ONLY AT 10% WING UL POWER 260i DRPK

ESCAPADE 13959 HERCULES 6138447-S PROPELLER INSTALLATION OF HERCULES 6138447-S 61 INCH DIAMETER X 38 UL POWER 260i DRPK INSTALLATION INCH PITCH PROPELLER. ESCAPADE 12513 STARBOARD WING FLAP PULLEY BLOCK DRILLING OF FOUR 1/8" HOLES FOR FLAP PULLEY BLOCK ATTACHMENT ON OUTBOARD SIDE UL POWER 260i LEEK ATTACHMENT MIS-DRILLING INSTEAD OF INBOARD OF RIB 4. ESCAPADE 14220 PROPELLER CHANGE TO NEWTON 11R PROPELLER CHANGE TO NEWTON 11R 60" X 41.5" UL POWER 260i LEEK 60" X 41.5" ESCAPADE 14369 IMPROVEMENT TO DOORS DOORS MODIFIED TO INCORPORATE ALLOY COVERING OF LOWER HALVES AND IMPROVED LATCH UL POWER 260i LEEK ARRANGEMENTS. ALSO INCORPORATES IMPROVED DRAUGHT SEALING. EUROFOX 912(S) 14196 FT-60 RED CUBE FUEL FLOW INSTALLATION OF ELECTRONICS INTERNATIONAL INC. FT-60 'RED CUBE' FUEL FLOW TRANSDUCER ROTAX 912-ULS CGYC TRANSDUCER INSTALLATION AFT OF THE FIREWALL BETWEEN ELECTRIC AND MECHANICAL FUEL PUMPS. EUROFOX 912(S) 14429 MATCO PARKING BRAKE VALVE ORIGINAL PARKING BRAKE VALVES REPLACED WITH MATCO PVPV-D PARKING BRAKE VALVE ROTAX 912-ULS CHIH MOUNTED IN SAME POSITION AND USING SAME HYDRAULIC FITTINGS. EUROFOX 912(S) 13493 DUC SWIRL 3 BLADED 1730 MM X 24.5° INSTALLATION OF DUC SWIRL 3 BLADED 1730 MM DIAMETER X 24.5 DEGREES PITCH AT 75% ROTAX 912-ULS ETUG AT 75% RADIUS PROPELLER. RADIUS PROPELLER

Prototype mods that have been approved since 1/1/2008 Page 30 30/11/20 LAA Technical Leaflet TL 3.17 EUROFOX 912(S) 13573 DYNON WING LEVELLER FITMENT OF EUROFOX FACTORY-PRODUCED SERVO MOUNTING BRACKET, DYNON SV32 ROLL ROTAX 912-ULS COLY SERVO, DYNON AP74 CONTROLLER, DYNON D10A EFIS AND ASSOCIATED FITTINGS AND ELECTRICAL CONNECTIONS.

CONTROL UNIT PARAMETERS SET AS NOTED IN FLIGHT TEST REPORT DATED 3/10/14. EUROFOX 912(S) 15509 KIEV 263/1700 PROPELLER INSTALLATION INSTALLATION OF KIEV 263/1700 3 BLADED 1700mm DIAMETER GROUND ADJUSTABLE COMPOSITE ROTAX 912-ULS FOXO PROPELLER. EUROFOX 912(S) 14577 UNDERCARRIAGE SAFETY STROP The main undercarriage legs are fitted with swaged stranded steel cable safety strops at the ROTAX 912-ULS OSGU fuselage side attachment to hold the undercarriage legs in position in the event of an undercarriage attachment bolt failure. EUROFOX 912(S) 15501 BATTERY ISOLATION SWITCH INSTALLATION OF BATTERY ISOLATOR SWITCH BETWEEN BATTERY NEGATIVE TERMINAL AND ROTAX 912-ULS OSGU AIRFRAME GROUND. LOCATED ON FRONT OF SEAT PAN. EUROFOX 912(S) 14196 FT-60 RED CUBE FUEL FLOW INSTALLATION OF ELECTRONICS INTERNATIONAL INC. FT-60 'RED CUBE' FUEL FLOW TRANSDUCER ROTAX 912-ULS CIML TRANSDUCER INSTALLATION AFT OF THE FIREWALL BETWEEN ELECTRIC AND MECHANICAL FUEL PUMPS. EUROFOX 912(S) 15330 DUC SWIRL-3-L 1730MM DIAMETER 3 INSTALLATION OF DUC SWIRL-3-L 1730MM DIAMETER 3 BLADE PROPELLER. ROTAX 912-ULS SMKR BLADE PROPELLER INSTALLATION EUROFOX 912(S) 14594 INSTALLATION OF ROTAX 912-ULS (EP ROTAX 912-ULS ENGINE MODIFIED TO GIVE 120 HP MAXIMUM POWER OUTPUT. ROTAX 912-ULS (EP CHUP MODIFIED) MODIFIED) EUROFOX 912(S) 14594 INSTALLATION OF ROTAX 912-ULS (EP ROTAX 912-ULS ENGINE MODIFIED TO GIVE 120 HP MAXIMUM POWER OUTPUT. ROTAX 912-ULS (EP CIOF MODIFIED) MODIFIED) EUROFOX 912(S) 14594 INSTALLATION OF ROTAX 912-ULS (EP ROTAX 912-ULS ENGINE MODIFIED TO GIVE 120 HP MAXIMUM POWER OUTPUT. ROTAX 912-ULS (EP CIWG MODIFIED) MODIFIED) EUROFOX 912(S) 14594 INSTALLATION OF ROTAX 912-ULS (EP ROTAX 912-ULS ENGINE MODIFIED TO GIVE 120 HP MAXIMUM POWER OUTPUT. ROTAX 912-ULS (EP CKAB MODIFIED) MODIFIED) EUROFOX 912(S) 14577 UNDERCARRIAGE SAFETY STROP The main undercarriage legs are fitted with swaged stranded steel cable safety strops at the ROTAX 912-ULS (EP OSGC fuselage side attachment to hold the undercarriage legs in position in the event of an MODIFIED) undercarriage attachment bolt failure. EUROFOX 912(S) 15501 BATTERY ISOLATION SWITCH INSTALLATION OF BATTERY ISOLATOR SWITCH BETWEEN BATTERY NEGATIVE TERMINAL AND ROTAX 912-ULS (EP OSGC AIRFRAME GROUND. LOCATED ON FRONT OF SEAT PAN. MODIFIED) EUROFOX 912iS 13975 WOODCOMP PROPULS AE 174 INSTALLATION OF WOODCOMP PROPULS AE 174 3 BLADED 1740MM DIAMETER GROUND ROTAX 912-iS TTUG INSTALLATION ADJUSTABLE PROPELLER. EUROFOX 912iS 14870 UPDATE FUEL SYSTEM FUEL SYSTEM REVISED TO STANDARD GIVEN IN ROTAX INSTALLATION MANUAL USING AN6 PIPE ROTAX 912-iS ODGC FITTINGS, ALLOY FUEL PIPES AND ANDAIR CHECK VALVES, FILTERS AND SHUT OFF VALVE. EUROFOX 912iS 15143 START POWER TIMED RELAY START POWER SWITCH REPLACED WITH LUKESFIELD AVIATION TIMED RELAY MODULE. ROTAX 912-iS ODGC EUROFOX 912iS 14447 DYNON SKYVIEW DUAL AXIS AUTO-PILOT INSTALLATION OF DYNON SKYVIEW DUAL AXIS AUTO-PILOT WITH BOTH SERVOS MOUNTED TO A ROTAX 912-iS EFSD INSTALLATION EUROFOX MADE WELDED FRAME THAT IS BOLTED TO PRE-EXISTING LUGS WELDED TO THE FUSELAGE STRUCTURE UNDERNEATH THE PILOT'S SEAT. THE ROLL SERVO IS CONNECTED VIA PUSH-ROD TO THE PORT SIDE FORWARD AILERON BELLCRANK. THE PITCH SERVO IS CONNECTED VIA PUSH-ROD TO THE CENTRAL BELLCRANK BELOW THE PITCH PUSH-ROD ON THE PITCH TORQUE TUBE. EUROFOX 912iS 15294 KANARDIA HORIS BACKUP INSTALLATION OF KANARDIA HORIS AS BACKUP TO PFD IN CONJUNCTION WITH KANARDIA UPSL ROTAX 912-iS GTWL UNINTERRUPTIBLE POWER SUPPLY UNIT. HORIS CONFIGURED SO THAT ONLY THE MAIN 'AD-AHRS' SCREEN CAN BE ACCESSED IN FLIGHT. EUROFOX 914 14917 INSTALLATION OF AIR INTAKE NACA ENGINE INTAKE AIR ROUTED VIA NEW NACA DUCT IN ENGINE COWLING VIA SCAT HOSE AND AIR ROTAX 914-UL CIKH DUCT FILTER, TO PROVIDE A COOLER SOURCE OF AIR. EUROFOX 914 14594 INSTALLATION OF ROTAX 912-ULS (EP ROTAX 912-ULS ENGINE MODIFIED TO GIVE 120 HP MAXIMUM POWER OUTPUT. ROTAX 914-F2 CIBF MODIFIED) EUROFOX 914 15263 ENGINE CHANGE TO ROTAX 914 TURBO INSTALLATION OF ROTAX 914-F2 ENGINE IN ACCORDANCE WITH EUROFOX UK 914 BUILD MANUAL ROTAX 914-F2 CIBF SUPPLEMENT ISSUE 2 AND WIRING DIAGRAM 404-13-1 REV D.

Prototype mods that have been approved since 1/1/2008 Page 31 30/11/20 LAA Technical Leaflet TL 3.17 EUROPA 12366 PROPELLER CHANGE TO WARP DRIVE 3 PROPELLER CHANGE TO WARP DRIVE 3 BLADED 62 INCH MID-WEST GIAE.100R BWIJ BLADED 62 INCH EUROPA 12771 COOLANT TEMPERATURE CONTROL CONAIR COOLANT THERMOSTAT INSTALLED BETWEEN ENGINE AND 1ST RADIATOR WITH BYPASS MID-WEST GIAE.100R BWIJ INSTALLED BETWEEN 2ND RADIATOR AND HEADER TANK. EUROPA 13321 NSI CAP 140 3 BLADED 64" DIAMETER INSTALLATION OF AN NSI CAP 140 3 BLADED 64 INCH DIAMETER VARIABLE PITCH PROPELLER MID-WEST GIAE.100R BWIJ PROPELLER INSTALLATION FITTED WITH WARP DRIVE BLADE. EUROPA 14192 WOODCOMP SR3000/3N 1625MM INSTALLATION OF WOODCOMP SR3000/3N 1625MM DIAMETER VARIABLE PITCH PROPELLER MID-WEST GIAE.100R BWIJ DIAMETER PROPELLER INSTALLATION MANUALLY CONTROLLED BY COCKPIT SWITCH. EUROPA 14796 DYNON HEATED PITOT/AOA HEAD INSTALLATION OF DYNON HEATED PITOT/ANGLE OF ATTACK HEAD IN PLACE OF STANDARD ROTAX 912-UL BVIZ INSTALLATION EUROPA PITOT/STATIC HEAD ON PORT WING UNDERSIDE. HEATER CONTROLLER MOUNTED IN CENTRAL TUNNEL ATTACHED TO PORT SIDE WALL. TWO STATIC PORTS, ONE IN EACH FUSELAGE SIDE, INSTALLED IN ACCORDANCE WITH EUROPA CLASSIC INSTRUCTIONS, WITH THE ADDITION OF A 2 X 2MM SQUARE SECTION X 45MM LONG DAM ATTACHED VERTICALLY 7.5MM FORWARD OF EACH STATIC PORT TO REDUCE THE LOCAL STATIC PRESSURE OVER THE PORT. EUROPA 14797 WING TIP MOUNTED POSITION AND INSTALLATION OF 'AVIOLIGHTS NAVIGATOR ULTRA 360' POSITION AND STROBE LIGHTS TO WING ROTAX 912-UL BVIZ STROBE LIGHTS INSTALLATION TIPS. EUROPA 15411 WOODCOMP SR3000/3N 1625MM 3 WOODCOMP SR3000/3N 1625MM 3 BLADE PROPELLER INSTALLATION WITH WOODCOMP 5A ROTAX 912-UL BVLV BLADE PROPELLER INSTALLATION MANUALLY OPERATED BLADE PITCH CONTROLLER. EUROPA 13342 FUEL SELECTOR REPLACEMENT ANDAIR F-S20 FUEL SELECTOR SUBSTITUTED, WITH APPRORIATE MOUNTING BRACKET AND ROTAX 912-UL BVOW REMOTE CONTROL ARRANGEMENT EUROPA 13842 PROPELLER CHANGE TO AIRMASTER INSTALLATION OF AIRMASTER AP332 62 INCH DIAMETER PROPELLER. ROTAX 912-UL BVOW AP332 EUROPA 14593 AIRMASTER AP332CTFH-WDR62N 62 INSTALLATION OF AN AIRMASTER AP332CTFH-WDR62N 62 INCH DIAMETER PROPELLER. ROTAX 912-UL OPJK INCH DIAMETER PROPELLER INSTALLATION EUROPA 13070 REPLACEMENT OF RUBBER FILLER HOSE RUBBER FUEL FILLER HOSE AS SUPPLIED IN EUROPA KIT HAS NOW BEEN REPLACED BY SUITABLE ROTAX 912-UL BWYD WITH ALLOY PIPE ALUMINIUM ALLOY PIPE, BENT TO CONFORM WITH REQUIRED SHAPE AND RETAINED BY SHORT RUBBER CONNECTOR HOSE AND TWO JUBILEE CLIPS AT EACH END. RUBBER CONNECTOR HOSES MUST BE FUEL-PROOF - SUITABLE FOR PERMANENT CONTACT WITH FUEL CONTAINING ETHANOL. EUROPA 14450 REPOSITION EUROPA CLASSIC OIL REPOSITIONING OF OIL COOLER FROM AFT OF PORT SIDE COOLANT RADIATOR TO CENTRALLY ROTAX 912-UL BWFH COOLER WITHIN LOWER COWLING, WITH CUSTOM MOULDED HOUSING. EXPELLED COOLING AIR DIVIDED BETWEEN STANDARD EXIT IN LOWER COWLING AND THROUGH EXIT DUCT IN NEW HOUSING BELOW LOWER COWLING. EUROPA 12705 INSTALLATION OF FINGER BRAKES SUBSTITUTION OF FOOT OPERATED BRAKE SYSTEM BY INSTALLATION OF FINGER BRAKES USING ROTAX 912-UL BWDX EUROPA XS TYPE MATCO MASTER CYLINDERS MOUNTED ON GRP/PLYWOOD SHELF IN CENTRE TUNNEL. EUROPA 11969 TAILPLANE TORQUE TUBE DRIVE PIN REPLACEMENT OF TP14 PINS WITH CLOSE TOLERANCE BOLTS AND NUTS WITH SHAPED SPACERS ROTAX 912-UL BXLK MODIFICATION TO ENABLE CLAMPING OF TAILPLANE TORQUE TUBE, TAILPLANE DRIVE BELLCRANK TP09 AND TAILPLANE DRIVE PLATES TP12. EUROPA 10111 MUDGUARD INSTALATION TO STOP MUD ETC BEING THROWN UP INTO U/C TUNNEL ROTAX 912-UL BXLK EUROPA 12338 PROPELLER CHANGE TO AIRMASTER CHANGE OF PROPELLER TO AIRMASTER AP332 X 64 INCH DIAMETER, USING AC200 CONSTANT ROTAX 912-UL DURO AP332, 64 INCH DIAMETER. SPEED CONTROLLER. EUROPA 11639 AIRMASTER AP332 3 BLADED 62" INSTALLATION OF AIRMASTER AP332 3 BLADED 62" DIAMETER ELECTRIC CONSTANT SPEED ROTAX 912-UL OEZY DIAMETER PROPELLER PROPELLER USING THE AIRMASTER AC200 CONTROLLER. EUROPA 12470 PROPELLER CHANGE TO WOODCOMP SR PROPELLER CHANGE TO WOODCOMP SR 3000-3/B 1625MM DIAMETER WITH FACTORY FITTED ROTAX 912-UL LABS 3000-3/B 1625MM DIAMETER STOP TO PREVENT REVERSE OPERATION AND NO FEATHERING CAPABILITY.

Prototype mods that have been approved since 1/1/2008 Page 32 30/11/20 LAA Technical Leaflet TL 3.17 EUROPA 15504 EUROPA IGNITECH IGNITION TWIN IGNITECH IGNITION MODULES INSTALLED TO REPLACE ROTAX MODULES ROTAX 912-UL CLAV IGNITECH LOOM MADE FROM FRNC (FLAME RESISTANT NON CORROSIVE) WIRING

MODULES INSTALLED ON COCKPIT SIDE OF FIREWALL (STARBOARD SIDE BELOW WINDSCREEN) LOOMS PASSED THROUGH FIRE-RESISTANT SHEATH PROTUDING INTO ENGINE BAY

MODULES ALSO 12V DC POWERED WHEN STARTER MOTOR ENGAGED

EUROPA 12607 FUEL SIGHT GAUGE RE-POSITIONING RE-POSITIONING OF FUEL SIGHT GAUGE TO RUN UP CORNER OF SEAT BACK AND PORT FUSELAGE ROTAX 912-UL BYIK SIDE. EUROPA 12016 TRI GEAR MASTER CYLINDERS RE- INSTALLATION OF TWO EUROPA MONO-WHEEL TYPE MASTER CYLINDERS IN CENTRE TUNNEL ROTAX 912-UL FLOR POSITIONED TO CENTRE TUNNEL INSTEAD OF STANDARD TWIN MASTER CYLINDERS FOR TRI GEAR FINGER BRAKES. EUROPA 14714 WOODCOMP SR3000/3N 1625MM INSTALLATION OF WOODCOMP SR3000/3N 1625MM DIAMETER PROPELLER. ROTAX 912-UL MFHI DIAMETER PROPELLER INSTALLATION EUROPA 13201 FUEL FLOW MONITORING SYSTEM FUEL FLOW MONITORING SYSTEM INSTALLATION INCORPORATING TWO EI FT-60 'RED CUBE' ROTAX 912-UL PATS TRANSDUCERS; ONE IN THE FUEL SUPPLY LINE, THE OTHER IN THE FUEL RETURN LINE. EUROPA 10410 PHENOLIC MOULDED FIREWALL GRAHAM SINGLETON MOULDED PHENOLIC FIREWALL OPTION ROTAX 912-UL PATS EUROPA 12607 FUEL SIGHT GAUGE RE-POSITIONING RE-POSITIONING OF FUEL SIGHT GAUGE TO RUN UP CORNER OF SEAT BACK AND PORT FUSELAGE ROTAX 912-UL PATS SIDE. EUROPA 14053 COCKPIT HEATER INSTALLATION OF COCKPIT HEATER USING HEAT EXCHANGER AROUND SILENCER AND ROTAX 912-UL OJHL INDEPENDENT CABLE CONTROLLED VALVES FEEDING HOT AIR THROUGH A HOLE THROUGH BOTH FOOTWELLS BETWEEN THE RUDDER PEDALS. EUROPA 14485 GA PROP 160 160CM DIAMETER BLADES INSTALLATION OF GA PROPS 160, 160CM DIAMETER BLADES INTO ARPLAST PV50 PROPELLER HUB. ROTAX 912-UL OJHL FITTED TO ARPLAST PV50 HUB DESIGNATION: ARPLAST PV50/GA PROP 160

EUROPA 10247 ROTAX 912-ULS INSTALLATION ROTAX 912-ULS SUBSTITUTED FOR 912-UL ROTAX 912-ULS DAMY EUROPA 14765 ROTAX 912 ULS ENGINE AND WARP INSTALLATIONS OF ROTAX 912-ULS ENGINE AND WARP DRIVE RPM 3 BLADED 62" DIAMETER ROTAX 912-ULS SNOP DRIVE RPM 3 BLADED 62" DIAMETER PROPELLER. PROPELLER INSTALLATIONS EUROPA 11969 TAILPLANE TORQUE TUBE DRIVE PIN REPLACEMENT OF TP14 PINS WITH CLOSE TOLERANCE BOLTS AND NUTS WITH SHAPED SPACERS ROTAX 912-ULS SNOP MODIFICATION TO ENABLE CLAMPING OF TAILPLANE TORQUE TUBE, TAILPLANE DRIVE BELLCRANK TP09 AND TAILPLANE DRIVE PLATES TP12. EUROPA 13070 REPLACEMENT OF RUBBER FILLER HOSE RUBBER FUEL FILLER HOSE AS SUPPLIED IN EUROPA KIT HAS NOW BEEN REPLACED BY SUITABLE ROTAX 912-ULS SNOP WITH ALLOY PIPE ALUMINIUM ALLOY PIPE, BENT TO CONFORM WITH REQUIRED SHAPE AND RETAINED BY SHORT RUBBER CONNECTOR HOSE AND TWO JUBILEE CLIPS AT EACH END. RUBBER CONNECTOR HOSES MUST BE FUEL-PROOF - SUITABLE FOR PERMANENT CONTACT WITH FUEL CONTAINING ETHANOL. EUROPA 12339 TP6 PIP PIN HOLE REPAIR DURING INST ADDITION OF NAS1149 WASHER WITHIN LAYUP AT BASE OF MOD 73 CAVITY TO REPAIR DOUBLE ROTAX 912-ULS OURO OF MOD 73. DRILLED HOLE FOR PIP PIN IN TP06 SLEEVE. EUROPA 13112 ROTAX 912-ULS ON NEW DESIGN INSTALLATION OF ROTAX 912-ULS ENGINE WITH AIRMASTER AP332 64 INCH DIAMETER ELECTRIC ROTAX 912-ULS OURO MOUNT WITH AIRMASTER AP332 64" DIA CONSTANT SPEEDING PROPELLER USING NEW DESIGN ENGINE MOUNTING FRAME PT. NO. PAM- PROP. EUROPA-MT912, DERIVED FROM EUROPA CLASSIC 912 MOUNT BUT PLACES ENGINE IN IDENTICAL POSITION AS XS MOUNT/ROTAX RING MOUNT COMBINATION AND NEW ENGINE COWLINGS, PT.NOS. PAM-EUROPA-9CU (UPPER) AND PAM-EUROPA-9CL (LOWER).

EUROPA 14106 WOODCOMP SR200/3, 3 BLADED INSTALLATION OF WOODCOMP SR200/3, 3 BLADED 1625MM DIAMETER GROUND ADJUSTABLE ROTAX 912-ULS NDOL 1625MM DIAMETER PROPELLER PROPELLER. INSTALLATION

Prototype mods that have been approved since 1/1/2008 Page 33 30/11/20 LAA Technical Leaflet TL 3.17 EUROPA 14900 ROTAX 912-ULS ENGINE AND AIRMASTER INSTALLATION OF ROTAX 912-ULS ENGINE AND AIRMASTER AP332 63" DIAMETER PROPELLER. ROTAX 912-ULS EMIN AP332 63" DIAMETER PROPELLER FOR INCREASED OIL COOLING CAPACITY, 13 ROW OIL COOLER FITTED BEHIND PORT SIDE COOLANT INSTALLATION RADIATOR IN PLACE OF ORIGINAL 10 ROW OIL COOLER WHICH WAS MOUNTED TO LOWER COWLING CENTRALLY UNDER PROPELLER SPINNER, UTILISING EXISTING AIR INLET. OIL COOLERS PLUMBED IN SERIES.

EUROPA 14121 WOODCOMP SR200/3 1625MM INSTALLATION OF WOODCOMP SR200/3, 1625 MM DIAMETER PROPELLER. ROTAX 912-ULS DAYS DIAMETER PROPELLER INSTALLATION EUROPA 13452 ENGINE CHANGE TO ROTAX 912 ULS & STANDARD ROTAX ENGINE INSTALLATION BUT WITH COWLING OF NEVILLE EYRE DESIGN AS ROTAX 912-ULS RICS PROP CHANGE TO AIRMASTER AP332 PREVIOUSLY APPROVED BY LAA. EUROPA 13118 RETROFIT ROTAX 912-ULS ENGINE WITH FEPLACE SUBARU ENGINE WITH ROTAX 912-ULS USING STANDARD EUROPA XS INSTALLATION. ROTAX 912-ULS TERN STANDARD FIT OPERATING LIMITATIONS REVERT TO STANDARD EUROPA OPERATING LIMITATIONS FOR ROTAX 912-ULS VERSION.

EUROPA 11489 ROTAX 912-ULS ENGINE RETROFIT 912-ULS ENGINE FITTED WITH INSTALLATION PER G-BXII ROTAX 912-ULS TERN EUROPA 10823 TO IMPROVE FUEL SYSTEM ALUMINIUM FUEL PIPES INTRODUCED AND ALTERNATIVE FUEL VENT ARRANGEMENT. ISSUE 2 OF ROTAX 912-ULS BXGG THIS MOD RAISED FOR EUROPA G-DEBR (LATTERLY G-URMS) WHICH HAS SIMILAR INSTALLATION BUT DIFFERING BY INSTALLATION OF ANDAIR FUEL SELECTOR VALVE, EUROPA MOD 60 FUEL GAUGE AND STANDARD SIGHT GAUGE. EUROPA 14240 AIRMASTER AP332SCTF-WWR64W 64 INSTALLATION OF AIRMASTER AP332SCTF-WWR64W 64 INCH DIAMETER ELECTRIC CONSTANT ROTAX 912-ULS BXGG INCH DIAMETER PROPELLER SPEED PROPELLER. AIRMASTER AP332 HUB USED WITH WHIRLWIND PROPELLER BLADES SECURED INSTALLATION WITH STEEL BLADE FERRULES. EUROPA 12352 FRESH AIR VENTILATION INSTALLATION OF CLOSABLE FRESH AIR INLET DOOR IN ROOF BETWEEN DOOR HINGES WITH ROTAX 912-ULS VPSJ DUCTING TO FEED TWO INDEPENDENT CLOSABLE EYE-BALL OUTLET VENTS IN CEILING PANEL. EUROPA 12353 HYDROSTATIC FUEL QUANTITY GAUGES INSTALLATION OF THREE OFF SKYDRIVE FLG1 HYDROSTATIC FUEL QUANTITY GAUGES IN INSIDE ROTAX 912-ULS VPSJ FACES OF HEADRESTS; ONE EACH FOR MAIN AND RESERVE SIDES OF FUEL TANK IN STARBOARD HEADREST, VISIBLE TO PILOT AND ONE FOR THE RESERVE IN THE PORT SIDE HEADREST, VISIBLE TO THE REFUELLER. EUROPA 12354 FUEL FEED SYSTEM FUEL FEED SYSTEM CONTROLLED BY FUEL PRESSURE SWITCHES THAT COMMAND THE ROTAX 912-ULS VPSJ APPROPRIATE 'MAIN' OR 'RESERVE' FUEL PUMP TO OPERATE AUTOMATICALLY. EUROPA 12408 MOVE POSITION OF BRAKE LEVER TO P1 INSTALLATION OF BRAKE LEVER TO LEFT HAND CONTROL COLUMN AND INCLUDE PARKING BRAKE ROTAX 912-ULS VPSJ CONTROL COLUMN VALVE WITH OPERATING CONTROL ON CENTRE TUNNEL. EUROPA 14378 AIRMASTER AP332SCTF-WWR64W 64 INSTALLATION OF AIRMASTER AP332SCTF-WWR64W 64 INCH DIAMETER ELECTRIC CONSTANT ROTAX 912-ULS VPSJ INCH DIAMETER PROPELLER SPEED PROPELLER. AIRMASTER AP332 HUB USED WITH WHIRLWIND PROPELLER BLADES SECURED INSTALLATION WITH STEEL BLADE FERRULES. EUROPA 14826 ADDITION OF WING TIP NAV LIGHTS MIDLAND MODEL E NAV LIGHTS MOUNTED ON WING TIPS. INCLUDING ASSOCIATED WIRING, ROTAX 912-ULS SNOZ SWITCH AND CIRCUIT BREAKER. EUROPA 12323 FINGER OPERATED BRAKES INSTALLATION OF TWO 'MONO-WHEEL' TYPE BRAKE MASTER CYLINDERS IN CENTRE TUNNEL ROTAX 912-ULS TSUE INSTALLATION. SUPPORTED BETWEEN TUNNEL SIDE-WALL AND COMPOSITE BRACKET, ONE FOR EACH WHEEL BRAKE. EUROPA 10507 WING LEVELLING AUTO-PILOT STANDARD EUROPA CLUB MOD TO FIT NAVAID, TRIO OR TRUTRAK WING LEVELLER. ROTAX 912-ULS OBJT EUROPA 14906 AIRMASTER AP332 64 INCH DIAMETER INSTALLATION OF AIRMASTER AP332 64 INCH DIAMETER PROPELLER ROTAX 912-ULS OBJT PROPELLER INSTALLATION EUROPA 13072 CONSPICUITY LIGHT INSTALLATION INSTALLATION OF 55W HALOGEN LAMP TO FRONT OF OIL COOLER/RADIATOR DUCT TO SHINE ROTAX 912-ULS MAUS FORWARDS THROUGH DUCT INLET FOR INCREASED CONSPICUITY AND SIGNALLING.

ISSUE 2 RAISED TO INCLUDE CREE 10W LED LAMP. EUROPA 13587 FINGER BRAKES 2 OFF KART COMPONENTS MANUFACTURING LTD MASTER BRAKE CYLINDERS FITTED TO TOP OF ROTAX 912-ULS CGVX CENTRAL TUNNEL NEXT TO THROTTLE.

Prototype mods that have been approved since 1/1/2008 Page 34 30/11/20 LAA Technical Leaflet TL 3.17 EUROPA 14179 REPOSITIONING OF BRAKE MASTER MASTER CYLINDER REPOSITIONED BETWEEN THE FLAP/GEAR AND THROTTLE LEVERS. ROTAX 912-ULS YETI CYLINDER INCORPORATES AN ADDITIONAL ANGLE BRACKET SUPPORT AND CUT AWAY PART OF THE THROTTLE BOX FLANGE TO ACCOMMODATE MASTER CYLINDER FLUID TOP-UP. EUROPA 14467 FUEL SELECTOR VALVE HANDLE POSITIONING OF FUEL SELECTOR VALVE LEVER IN RECESS ON CENTRE TUNNEL TOP, VIA ROTAX 912-ULS YETI POSITIONED IN RECESS ON CENTRE ALUMINIUM TUBE EXTENSION SHAFT, FOR EASE OF ACCESS. TUNNEL TOP. EUROPA 13987 CUSTOM MADE BAGGAGE BAY WITH CUSTOM MADE BAGGAGE BAY AS PER EUROPA XS BUT MADE USING 4MM PLYWOOD WITH 1 PLY ROTAX 912-ULS YETI LARGE ACCESS HOLE OF 600 GSM BIAXIAL GLASSCLOTH EACH SIDE INSTEAD OF 3MM R63.80 FOAM CORE WITH 3 PLIES OF 300 GSM BI-DIRECTIONAL GLASSCLOTH FOR THE FLOOR. ONE SINGLE LARGE ACCESS HOLE, SPANNING FROM OUTBOARD EDGE OF BOTH OF THE TWO ORIGINAL ACCESS HOLES. ACCESS HOLE COVER MADE IN SAME WAY AS FLOOR, SECURED WITH 16 X AN525-10R BOLTS INTO MS21047-3 ANCHOR NUTS. ALUMINIUM ANGLE PIECES INSTALLED AT INBOARD RIB POSITIONS FOR ADDITIONAL SUPPORT FOR COVER. EUROPA 14588 MUDGUARD FOR MAIN WHEEL MUDGUARD FOR MAIN WHEEL (MONOWHEEL) - SUITS MCCREARY AIRTRAC 7.00 X 6 TYRE ROTAX 912-ULS YETI EUROPA 14873 WOODCOMP SR3000/3A 1625MM INSTALLATION OF WOODCOMP SR3000/3A 1625MM DIAMETER PROPELLER OPERATED WITH ROTAX 912-ULS YETI DIAMETER PROPELLER INSTALLATION WOODCOMP MANUALLY OPERATED ELECTRIC CONTROLLER. EUROPA 11354 PROVISION OF CONTROL LOCK An aluminuim fabricated device is attached to the seat bulkhead to secure the control column ROTAX 912-ULS YETI when the aircraft is parked. This hinges up and stows under the seat cushion in flight. EUROPA 13223 WING TIP STROBES WING TIP STROBES FITTED SIMILAR TO SM 10713 BUT FOR CLASSIC WING RATHER THAN XS. ROTAX 912-ULS UMPY EUROPA 13411 WOODCOMP SR3000/3W 1625 MM INSTALLATION OF WOODCOMP SR3000/3W 1625 MM DIAMETER PROPELLER ROTAX 912-ULS UMPY DIAMETER PROPELLER INSTALLATION EUROPA 14559 CONSPICUITY LIGHT INSTALLATION INSTALLATION OF LED CONSPICUITY LIGHT INTO ENGINE COOLING AIR INTAKE. ROTAX 912-ULS UMPY EUROPA 15190 PITOT-STATIC HEAD INSTALLATION INSTALLATION OF NON-STANDARD PITOT-STATIC HEAD TO PORT WING UNDERSIDE IN POSITION ROTAX 912-ULS ITST THAT DIFFERS FROM THAT DESCRIBED IN EUROPA INSTRUCTIONS. EUROPA 15359 DUAL MGL FUEL FLOW TRANSDUCERS INSTALLATION OF TWO MGL PLASTIC FUEL FLOW TRANSDUCER IN FUEL SYSTEM, BOTH BEHIND ROTAX 912-ULS ITST INSTALLATION THE FIREWALL, WITH ONE BETWEEN ELECTRIC AND MECHANICAL FUEL PUMPS (PT No. 172671) AND ONE IN THE RETURN LINE (PT NO. 172672). FUEL FLOW RESTRICTOR JET INSTALLED IN BOTH TRANSDUCERS PER MGL INSTRUCTIONS. EUROPA 13345 STROBE FITTED TO RUDDER TRAILING AFT FACING LED STROBE LIGHT UNIT INSTALLED ON RUDDER AT LOWER CORNER ROTAX 912-ULS IVES EDGE ON PLATFORM BEHIND AERODYNAMIC FAIRING. EUROPA 13801 ROTAX 912-ULS ENGINE AND INSTALLATION OF ROTAX 912-ULS ENGINE WITH WOODCOMP SR3000/3 1625MM DIAMETER ROTAX 912-ULS IVES WOODCOMP SR3000/3 1625MM DIA PROPELLER. PROPELLER EUROPA 10986 PROVISION OF CABIN HEAT A FLAPPER VALVE IS INSTALLED ON THE COOLING DUCT DOWNSTREAM OF THE COOLANT ROTAX 912-ULS URMS RADIATOR WHICH ROUTES A FLOW OF HOT AIR INTO EACH FOOTWELL. THE SELECTION OF CABIN HEAT IS CONTROLLED VIA A SINGLE BOWDEN CABLE ROUTED THROUGH TO THE CABIN. THE FOOTWELL VENTS ARE CONTROLLED THROUGH A STAINLESS "DAISY" VALVE WHICH IS CONTROLLABLE EACH SIDE THROUGH TWO PUSH-PULL CABLES. EUROPA 14394 LED LANDING LIGHT INSTALLATION INSTALLATION OF LED LANDING LIGHT IN ENGINE LOWER COWLING. ROTAX 912-ULS URMS EUROPA 14396 WING TIP NAVIGATION LIGHTS & INSTALLATION OF OE195 LED COMBINED NAVIGATION AND STROBE LIGHTS ON WING TIPS. ROTAX 912-ULS URMS STROBES INSTALLATION EUROPA 14656 DYNON HEATED PITOT/AoA PROBE INSTALLATION OF A DYNON HEATED PITOT/AOA PROBE AT SIMILAR POSITION TO ORIGINAL ROTAX 912-ULS URMS INSTALLATION STANDARD EUROPA XS PITOT HEAD, PORT WING UNDERSIDE. HEATER CONTROLLER MOUNTED TO PORT WING LEADING EDGE ROOT RIB. STATIC SOURCE WITHIN CENTRAL TUNNEL OF FUSELAGE. EUROPA 14807 AUXILIARY BATTERY SECOND BATTERY FITTED IN SUPPORT OF NIGHT/IFR APPLICATION ROTAX 912-ULS URMS EUROPA 15013 NIGHT/IFR CLEARANCE NIGHT IFR CLEARANCE ROTAX 912-ULS URMS

Prototype mods that have been approved since 1/1/2008 Page 35 30/11/20 LAA Technical Leaflet TL 3.17 EUROPA 12672 LIFT RESERVE INDICATOR FITMENT OF AN INAIR INSTRUMENTS LLC LIFT RESERVE INDICATOR AND ASSOCIATED WING- ROTAX 912-ULS LEBE MOUNTED PROBE.

NOTE THAT THIS UNIT IS NOT A REPLACEMENT FOR THE AIRCRAFT'S NORMAL STALL WARNING UNIT. EUROPA 13831 INSTALLATION OF ROTAX 912-ULS INSTALLATION OF ROTAX 912-ULS ENGINE WITH WOODCOMP SR3000/3A 1625 MM DIAMETER ROTAX 912-ULS WUFF ENGINE AND WOODCOMP SR3000/3A PROPELLER WITH SMART AVIONICS CSC-1/G CONTROLLER. 1625MM DIA PROPELLER EUROPA 13070 REPLACEMENT OF RUBBER FILLER HOSE RUBBER FUEL FILLER HOSE AS SUPPLIED IN EUROPA KIT HAS NOW BEEN REPLACED BY SUITABLE ROTAX 912-ULS WUFF WITH ALLOY PIPE ALUMINIUM ALLOY PIPE, BENT TO CONFORM WITH REQUIRED SHAPE AND RETAINED BY SHORT RUBBER CONNECTOR HOSE AND TWO JUBILEE CLIPS AT EACH END. RUBBER CONNECTOR HOSES MUST BE FUEL-PROOF - SUITABLE FOR PERMANENT CONTACT WITH FUEL CONTAINING ETHANOL. EUROPA 10986 PROVISION OF CABIN HEAT A FLAPPER VALVE IS INSTALLED ON THE COOLING DUCT DOWNSTREAM OF THE COOLANT ROTAX 912-ULS WUFF RADIATOR WHICH ROUTES A FLOW OF HOT AIR INTO EACH FOOTWELL. THE SELECTION OF CABIN HEAT IS CONTROLLED VIA A SINGLE BOWDEN CABLE ROUTED THROUGH TO THE CABIN. THE FOOTWELL VENTS ARE CONTROLLED THROUGH A STAINLESS "DAISY" VALVE WHICH IS CONTROLLABLE EACH SIDE THROUGH TWO PUSH-PULL CABLES. EUROPA 11347 STICK MOUNTED BRAKE MASTER BRAKE MASTER CYLINDER MOUNTED ON STICK TOP WITH HANDBRAKE LEVER PER APPLICANT'S ROTAX 912-ULS WUFF CYLINDER SUBMISSION EUROPA 13987 CUSTOM MADE BAGGAGE BAY WITH CUSTOM MADE BAGGAGE BAY AS PER EUROPA XS BUT MADE USING 4MM PLYWOOD WITH 1 PLY ROTAX 912-ULS WUFF LARGE ACCESS HOLE OF 600 GSM BIAXIAL GLASSCLOTH EACH SIDE INSTEAD OF 3MM R63.80 FOAM CORE WITH 3 PLIES OF 300 GSM BI-DIRECTIONAL GLASSCLOTH FOR THE FLOOR. ONE SINGLE LARGE ACCESS HOLE, SPANNING FROM OUTBOARD EDGE OF BOTH OF THE TWO ORIGINAL ACCESS HOLES. ACCESS HOLE COVER MADE IN SAME WAY AS FLOOR, SECURED WITH 16 X AN525-10R BOLTS INTO MS21047-3 ANCHOR NUTS. ALUMINIUM ANGLE PIECES INSTALLED AT INBOARD RIB POSITIONS FOR ADDITIONAL SUPPORT FOR COVER. EUROPA 14963 LED LIGHT BAR INSTALLATION TO INCREASE AIRCRAFT CONSPICUITY WITH LED LIGHT BAR INSTALLED BELOW LOWER LIP OF AIR ROTAX 912-ULS WUFF COWLING FOR CONSPICUITY INTAKE. EUROPA 13544 FINGER BRAKES FINGER OPERATED BRAKE LEVERS (2 OFF) MOUNTED ON CENTRAL TUNNEL. SYSTEM USES EUROPA ROTAX 912-ULS MLXP MASTER CYLINDERS WHICH ARE MOUNTED TO THE TUNNEL USING FOOT BRAKE BRACKETS. CUSTOM 'DASH POTS' ARE INSTALLED TO FILL THE FLUID RESERVOIRS. EUROPA 15167 ROTAX 912-ULS ENGINE & WOODCOMP ROTAX 912-ULS ENGINE & WOODCOMP SR3000/3N, 1625MM DIAMETER PROPELLER ROTAX 912-ULS SELF SR3000/3N, 1625MM DIAMETER INSTALLATION PROPELLER INSTALLATION EUROPA 13282 TRUTRAK DIGITRAK AUTO PILOT (ROLL) INSTALLATION OF TRUTRAK DIGITRAK AUTO-PILOT (ROLL) SYSTEM IN ACCORDANCE WITH EUROPA ROTAX 912-ULS CFLI INSTALLATION MOD 75 WITH THE EXCEPTION OF USING A MACHINED 6082-T6 ROLL CONTROL DRIVE ARM THAT IS CLAMPED AND BONDED TO THE AILERON TORQUE TUBE THAT RUNS UNDERNEATH THE STARBOARD SEAT THIGH SUPPORT. EUROPA 11906 TAILPLANE TORQUE TUBE CLAMPS INSTALLATION OF MACHINED DURAL CLAMPS TO PREVENT RELATIVE MOVEMENT, BY FRICTION, ROTAX 912-ULS CFLI BETWEEN THE COMPONENTS OF THE TAILPLANE TORQUE TUBE ASSEMBLY TP4, TP9 AND TP12.

EUROPA 13264 TO RETAIN NOSE WHEEL BEARINGS INSTALLATION OF SPACERS AND SHIMS BETWEEN WHEEL BEARING INNER RACES TO ENABLE ROTAX 912-ULS CGDH WITHOUT LOCTITE BEARING PRE-LOADING TO WHEEL MATCO'S SPECIFICATIONS AND AVOID THE USE OF LOCTITE TO PREVENT THE RACES FROM SPINNING WITH THE WHEEL. EUROPA 13265 SPOOL PIECE FOR USING ORIGINAL SUBSTITUTION OF EUROPA PART MG 02 BRAKE CALLIPER TORQUE PLATE WITH MATCO STANDARD ROTAX 912-ULS CGDH MATCO BRAKE SLIDES TORQUE PLATE ATTACHED TO CUSTOM MACHINED S316 'SPOOL PIECE'. EUROPA 13266 DUAL MASTER CYLINDERS / FOOT INSTALLATION OF A PAIR OF EUROPA SUPPLIED 'KART COMPONENTS' FOOT BRAKES IN P2 ROTAX 912-ULS CGDH BRAKES FOOTWELL INCORPORATING BRAKE PEDAL SUPPORTS FOR P1 AND P2 BRAKE PEDAL LEVERS AGAINST PRESSURE EXERTED THROUGH OPERATION OF OPPOSITE BRAKE MASTER CYLINDER.

Prototype mods that have been approved since 1/1/2008 Page 36 30/11/20 LAA Technical Leaflet TL 3.17 EUROPA 13267 UPRATED BRAKE LINES INSTALLATION OF STEEL BRAID REINFORCED HYDRAULIC HOSE IN PLACE OF EUROPA KIT SUPPLIED ROTAX 912-ULS CGDH PLAIN NYLON HOSE. EUROPA 13612 INSTALLATION OF MODIFIED STD MOD INSTALLATION OF STANDARD MOD 11906 TORQUE TUBE CLAMPS WITH TORQUE TRANSFER PINS ROTAX 914-UL PEGY 11906 TORQUE TUBE CLAMPS MODIFIED WITH CIRCLIP GROOVES AND TP10 NYLON BUSHES MODIFIED WITH GROOVES FOR MASS BALANCE ARM CABLE SUPPORTS. EUROPA 14482 CONSPICUITY LIGHTS INSTALLATION INSTALLATION OF TWO QUAD LAMP LED CONSPICUITY LIGHTS (SQUADRON PRO LED SPOT), ONE ROTAX 914-UL STUE IN EACH MODIFIED OUTRIGGER FAIRING. EUROPA 10823 TO IMPROVE FUEL SYSTEM ALUMINIUM FUEL PIPES INTRODUCED AND ALTERNATIVE FUEL VENT ARRANGEMENT. ISSUE 2 OF ROTAX 914-UL STUE THIS MOD RAISED FOR EUROPA G-DEBR (LATTERLY G-URMS) WHICH HAS SIMILAR INSTALLATION BUT DIFFERING BY INSTALLATION OF ANDAIR FUEL SELECTOR VALVE, EUROPA MOD 60 FUEL GAUGE AND STANDARD SIGHT GAUGE. EUROPA 10051 TAILPLANE PIP-PIN COVER REMOVABLE THREADED WATER FITTING SCREWED INTO MOULDED THREADS IN PIP PIN RECESSES ROTAX 914-UL STUE

EUROPA 10297 ADDITION OF DOOR LOCK DOOR LOCKS ADDED ROTAX 914-UL STUE EUROPA 11354 PROVISION OF CONTROL LOCK An aluminuim fabricated device is attached to the seat bulkhead to secure the control column ROTAX 914-UL STUE when the aircraft is parked. This hinges up and stows under the seat cushion in flight. EUROPA 10623 ENHANCEMENT OF TAILPLANE DRIVE clamp added around tailplane torque tube in attempt to avoid wear developing in dowel pin holes ROTAX 914-UL STUE in service and slop between TP12, TP4, and TP9. Applicable to any Europa subject to acceptable centre of gravity position and inspection on completion. EUROPA 14840 ELECTRICAL SYSTEM (SECONDARY) A SECONDARY ELECTRICAL SYSTEM IS INSTALLED, INCORPORATING AN ADDITIONAL BATTERY ROTAX 914-UL STUE (VARLEY LI-5), AN ADDITIONAL ALTERNATOR AND REGULATOR (B&C) AND AN AUXILIARY BUS.

NOTE THAT THE SECONDARY SYSTEM IS NOT INDEPENDENT OF THE PRIMARY ELECTRICAL SYSTEM AND THE PRIMARY SYSTEM MUST BE POWERED FOR THE SECONDARY SYSTEM TO SUPPLY CURRENT.

ISSUE 2: SYSTEM AMENDED SO THAT MAIN FUEL PUMP RUNS DIRECT FROM MAIN REGULATOR.

EUROPA 14841 FUEL SYSTEM IMPROVEMENTS - ANDAIR GAS375 GASCOLATOR ADDED BETWEEN FUEL PUMPS AND PRESSURE REGULATOR, ROTAX 914-UL STUE MOUNTED IN THE LOWER FUSELAGE AND INCORPORATING A HINGED ACCESS PANEL.

- WELDED ALLOY ELBOW JOINING INLET 'COBRA' FITTING TO FUEL TANK. EUROPA 14588 MUDGUARD FOR MAIN WHEEL MUDGUARD FOR MAIN WHEEL (MONOWHEEL) - SUITS MCCREARY AIRTRAC 7.00 X 6 TYRE ROTAX 914-UL STUE EUROPA 14322 WOODCOMP SR3000/3NW 1626MM INSTALLATION OF WOODCOMP SR3000/3NW 1625MM DIAMETER PROPELLER WITH WOODCOMP ROTAX 914-UL OMIK DIAMETER PROPELLER INSTALLATION CS5 CONSTANT SPEED CONTROLLER. EUROPA 12016 TRI GEAR MASTER CYLINDERS RE- INSTALLATION OF TWO EUROPA MONO-WHEEL TYPE MASTER CYLINDERS IN CENTRE TUNNEL ROTAX 914-UL PUDS POSITIONED TO CENTRE TUNNEL INSTEAD OF STANDARD TWIN MASTER CYLINDERS FOR TRI GEAR FINGER BRAKES. EUROPA 10507 WING LEVELLING AUTO-PILOT STANDARD EUROPA CLUB MOD TO FIT NAVAID, TRIO OR TRUTRAK WING LEVELLER. ROTAX 914-UL PTAG EUROPA 12403 WOODCOMP SR3000/3W 1625MM PROPELLER CHANGE TO WOODCOMP SR3000/3W 1625MM DIAMETER ROTAX 914-UL PTAG DIAMETER EUROPA 14358 FINGER BRAKES INSTALLATION INSTALLATION OF EUROPA SUPPLIED 'KART COMPONENTS' WHEEL BRAKE MASTER CYLINDERS TO ROTAX 914-UL JHYS CENTRE TUNNEL POSITION MOUNTED TO ORIGINAL FOOT BRAKE MOUNTING BRACKETS.

EUROPA 14362 WOODCOMP SR3000/3NW 1625MM INSTALLATION OF A WOODCOMP SR3000/3NW 1625MM DIAMETER ELECTRIC CONSTANT SPEED ROTAX 914-UL JHYS DIAMETER PROPELLER INSTALLATION PROPELLER CONTROLLED USING A WOODCOMP CS5 ELECTRONIC CONTROLLER. EUROPA 13070 REPLACEMENT OF RUBBER FILLER HOSE RUBBER FUEL FILLER HOSE AS SUPPLIED IN EUROPA KIT HAS NOW BEEN REPLACED BY SUITABLE ROTAX 912-ULS FR EIKY WITH ALLOY PIPE ALUMINIUM ALLOY PIPE, BENT TO CONFORM WITH REQUIRED SHAPE AND RETAINED BY SHORT RUBBER CONNECTOR HOSE AND TWO JUBILEE CLIPS AT EACH END. RUBBER CONNECTOR HOSES MUST BE FUEL-PROOF - SUITABLE FOR PERMANENT CONTACT WITH FUEL CONTAINING ETHANOL.

Prototype mods that have been approved since 1/1/2008 Page 37 30/11/20 LAA Technical Leaflet TL 3.17 EUROPA 13609 BRAKE MASTER CYLINDER SYSTEM INSTALLATION OF STANDARD TRIGEAR FOOT BRAKE MASTER CYLINDERS TO REINFORCED CENTRE ROTAX 912-ULS FR EIKY TUNNEL UNDERSIDE TO PROVIDE FINGER BRAKES. EUROPA 13849 ROTAX 912 ULS FR & AIRMASTER AP308 INSTALLATIONS OF ROTAX 912-ULS FR ENGINE AND AIRMASTER AP308 64 INCH DIAMETER ROTAX 912-ULS FR EIKY INSTALLATIONS PROPELLER EUROPA 13349 UL POWER 260iS ENGINE AND INSTALLATION OF A UL POWER UL260iS ENGINE WITH A WOODCOMP SR3000/3J 1630MM UL POWER 260iS BWUP WOODCOMP SR3000/3J PROPELLER DIAMETER PROPELLER. INSTALLATION EUROPA NG 14554 DYNON/AOA/PITOT HEAD INSTALLATION OF DYNON UNHEATED PITOT HEAD P/N 100141-000 ON GRETZ MOUNT. MOUNT IS ROTAX 912-ULS OVPM ATTACHED TO THE PORT WING SKIN OUTBOARD OF AILERON BELLCRANK ACCESS PANEL. SKIN IS LOCALLY STIFFENED USING 1/8" PLYWOOD BONDED TO SKIN WITH 2 PLIES OF GFRP OVER. INSTALLATION INCLUDES ADDITION OF STATIC PORTS TO REAR FUSELAGE AS PER 'EUROPA CLASSIC'. ANGLE OF ATTACK IS DISPLAYED USING DYNON D100 EFIS.

EUROPA NG 14555 WINGTIP LIGHTS WHELEN MICROBURST III WING TIP LED NAV/STROBE LIGHT UNIT MOUNTED ON EACH WING TIP. ROTAX 912-ULS OVPM UNITS ARE MOUNTED TO 1/4" PLY WOOD BONDED TO INSIDE OF WINGTIP SKIN, WITH 2 PLIES OF GFRP OVER. ATTACHMENT IS BY M3 BOLTS INTO 'NUTSERTS' EPOXIED INTO PLY. INCLUDES ASSOCIATED WIRING AND CIRCUIT PROTECTION.

EUROPA NG 14659 ROTAX 912-iS SPORT ENGINE AND INSTALLATION OF ROTAX 912-iS SPORT ENGINE AND AIRMASTER AP332 64 INCH DIAMETER ROTAX 912-iS XSRF AIRMASTER AP332 PROPELLER PROPELLER. INSTALLATION FUEL SYSTEM INCORPORATES CUSTOM MADE FUEL TANK OUTLET FITTINGS WITH WATER DRAIN FACILITY. EUROPA XS 12708 TRIO EZ-3 ALTITUDE HOLD AUTO-PILOT INSTALLATION OF TRIO EZ-3 ALTITUDE HOLD AUTO-PILOT WITH SERVO MOUNTED ON INSIDE FACE JABIRU 3300A CHAH OF STARBOARD INNER BAGGAGE BAY SUPPORT RIB AND SHORT PUSH-ROD DRIVING STEEL FABRICATED LUG BONDED AND RIVETTED TO UNDERSIDE OF PITCH PUSH-ROD. EUROPA XS 13258 ROTEC LIQUID COOLED CYLINDER HEADS ROTEC ENGINEERING'S LIQUID COOLED CYLINDER HEADS (LCH) KIT FITTED IN ACCORDANCE WITH JABIRU 3300A CHAH TO JABIRU 3300A ENGINE THE MANUFACTURER'S INSTRUCTIONS TO THE PREVIOUSLY INSTALLED JABIRU 3300A ENGINE. TWO COOLANT PUMPS FITTED AND CONFIGURED IN SERIES, ONE OF WHICH WHOSE SPEED IS CONTROLLED BY AN ELECTRONIC CONTROL UNIT, THE OTHER AS A BACK-UP WHICH IS OPERATED BY A MANUALLY OPERATED SWITCH AND WHICH RUNS AT FULL SPEED ONLY. COOLANT EXPANSION TANK (EX-MAZDA RX-8) WITH 1.1 BAR RATED PRESSURE CAP FITTED. OVERFLOW LINE FITTED TO EXPEL EXCESS COOLANT INTO COWLING AIR OUTLET AREA.

EUROPA XS 15416 WATER COOLED JABIRU 3300 ROTEC WATER COOLED ENGINE CYLINDER HEADS SUBSTITUTED, WITH ASSOCIATED LIQUID JABIRU 3300A CCFK COOLANT SYSTEM, RADIATOR, ELECTRIC FAN, THERMOSTAT AND ELECTRIC COOLANT PUMP. EUROPA XS 14308 HERCULES 6054510-S 60" X 54" INSTALLATION OF HERCULES 6054510-S 60 INCH DIAMETER X 54 INCH PITCH PROPELLER JABIRU 3300A CGNZ PROPELLER INSTALLATION EUROPA XS 15369 REPLACEMENT CONTROL COLUMNS INSTALLATION OF CUSTOM MADE STAINLESS STEEL CRANKED CONTROL COLUMNS. ROTAX 912-UL FIZY EUROPA XS 14038 FINGER BRAKES INSTALLATION INSTALLATION OF TWO KART COMPONENTS BRAKE MASTER CYLINDERS UNDER CENTRE TUNNEL ROTAX 912-UL IOWE FOR TO PROVIDE FINGER BRAKES. BRAKE LEVERS FROM MONO-WHEEL MODEL USED.

EUROPA XS 13304 FUEL SYSTEM CHANGES RUBBER FUEL HOSES BETWEEN SELECTOR VALVE AND FIREWALL REPLACED WITH ALUMINIUM ROTAX 912-UL CGZV ALLOY PIPES AND ASSOCIATED FITTINGS. FUEL TANK SELECTOR VALVE REPOSITIONED, WITH REMOTE VALVE SELECTOR VIA AN EXTENSION SHAFT. 'AN' FITTINGS USED IN CONNECTING COMPONENTS. FUEL LOW PRESSURE SWITCH INCORPORATED, WITH ASSOCIATED WARNING LAMP. EUROPA XS 13072 CONSPICUITY LIGHT INSTALLATION INSTALLATION OF 55W HALOGEN LAMP TO FRONT OF OIL COOLER/RADIATOR DUCT TO SHINE ROTAX 912-ULS TAGR FORWARDS THROUGH DUCT INLET FOR INCREASED CONSPICUITY AND SIGNALLING.

ISSUE 2 RAISED TO INCLUDE CREE 10W LED LAMP. Prototype mods that have been approved since 1/1/2008 Page 38 30/11/20 LAA Technical Leaflet TL 3.17 EUROPA XS 14727 AOA PROBE AN ANGLE OF ATTACK PROBE IS MOUNTED ON ALLOY PLATE COVERING BELLCRANK ACCESS PANEL ROTAX 912-ULS NHRJ ON THE STARBOARD WING. ANGLE OF ATTACK MONITORING AND WARNING IS PROVIDED BY A DYNON SKYVIEW UNIT. EUROPA XS 14728 FUEL SYSTEM CHANGES PROVISION OF LTS3A FUEL GAUGE HOUSED IN AN EXTERNAL CHAMBER ATTACHED TO THE MAIN ROTAX 912-ULS NHRJ FUEL TANK, WITH INTEGRAL SIGHT GAUGE. ALSO INCLUDES USE OF ALLOY FUEL LINES, MAINTENANCE FUEL VALVES, SEPARATE GASCOLATORS FOR MAIN AND RESERVE TANKS, PROTECTION OF FUEL SYSTEM FROM BAGGAGE BAY ITEMS USING PLYWOOD BOXING. EUROPA XS 13808 WING TIP STROBE/NAV LIGHT INSTALLATION OF AVEO ENGINEERING POWERBURST PLUS LED NAVIGATION/STROBE LIGHTS ON ROTAX 912-ULS NHRJ INSTALLATION WING TIPS EUROPA XS 14415 AIRMASTER AP332SCTF-WWR64W 64 INSTALLATION OF AIRMASTER AP332SCTF-WWR64W 64 INCH DIAMETER ELECTRIC CONSTANT ROTAX 912-ULS CCUL INCH DIAMETER PROPELLER SPEED PROPELLER. AIRMASTER AP332 HUB USED WITH WHIRLWIND PROPELLER BLADES SECURED INSTALLATION WITH STEEL BLADE FERRULES. EUROPA XS 14504 WOODCOMP SR3000/3N 1625 MM INSTALLATION OF WOODCOMP SR3000/3N 1625 MM DIAMETER PROPELLER WITH WOODCOMP ROTAX 912-ULS MEGG DIAMETER PROPELLER INSTALLATION MANUAL PITCH CHANGE CONTROLLER EUROPA XS 13808 WING TIP STROBE/NAV LIGHT INSTALLATION OF AVEO ENGINEERING POWERBURST PLUS LED NAVIGATION/STROBE LIGHTS ON ROTAX 912-ULS CDVS INSTALLATION WING TIPS EUROPA XS 14760 WOODCOMP SR3000/3N 1625MM INSTALLATION OF WOODCOMP SR3000/3N 1625MM DIAMETER PROPELLER. ROTAX 912-ULS CDVS DIAMETER PROPELLER INSTALLATION EUROPA XS 12581 PROPELLER CHANGE TO AIRMASTER PROPELLER CHANGE TO AIRMASTER AP332, 64 INCH DIAMETER USING BLADES FROM PRE-USED ROTAX 912-ULS CBHI AP332, 64 INCH DIAMETER WARP DRIVE 62 INCH DIAMETER PROPELLER. EUROPA XS 13586 BERINGER WHEEL AND BRAKE INSTALLATION OF BERINGER WHEEL AND BRAKE KIT FEATURING P1 STICK MOUNTED BRAKE LEVER ROTAX 912-ULS CBHI INSTALLATION. AND INCLUDING PRESSURE LIMITING VALVE. EUROPA XS 13012 TWIN ANDAIR GASCOLATORS FITTED INSTALLATION OF AN ANDAIR GA375 GASCOLATOR BETWEEN EACH FUEL TANK OUTLET AND AN ROTAX 912-ULS LDVO ANDAIR 3 POSITION FUEL SELECTOR VALVE. FUEL RETURN LINE INTO FUEL TANK'S VENT BOSS VIA GRAHAM SINGLETON FITTING. EUROPA XS 13022 CABIN HEATER A FABRICATED ALUMINIUM ALLOY BOX INCORPORATING A COCKPIT-CONTROLLABLE FLAP IS ROTAX 912-ULS LDVO ATTACHED TO THE COOLANT RADIATOR. SCAT HOSES DUCT THIS WARM AIR TO VALVES IN THE FIREWALL THAT DIRECT THE AIR INTO THE COCKPIT. EUROPA XS 13201 FUEL FLOW MONITORING SYSTEM FUEL FLOW MONITORING SYSTEM INSTALLATION INCORPORATING TWO EI FT-60 'RED CUBE' ROTAX 912-ULS LDVO TRANSDUCERS; ONE IN THE FUEL SUPPLY LINE, THE OTHER IN THE FUEL RETURN LINE. EUROPA XS 13203 FUEL STOP TAPS FOR MAINTENANCE INSTALLATION OF A STOP TAP IN THE FUEL LINE BETWEEN EACH FUEL TANK OUTLET AND THE ROTAX 912-ULS LDVO RESPECTIVE GASCOLATOR, LOCATED IN CENTRE TUNNEL, TO ENABLE GASCOLATOR MAINTENANCE WITH MINIMUM FUEL SPILLAGE. THESE STOP TAPS ARE WIRE LOCKED OPEN WHEN NOT IN USE.

EUROPA XS 10371 ALTERATION TO TAILWHEEL STEERING & INSTALLATION OF TAILWHEEL STEERING BELLCRANK AND BRACKETS ON FORWARD FACE OF REAR ROTAX 912-ULS LDVO INST. OF 'CLASSIC' RUDDER DRIVE BULKHEAD AND THE INCORPORATION OF THE EUROPA CLASSIC METHOD OF RUDDER DRIVE VIA PUSHROD INTO CS29 BUILT INTO RUDDER LEADING EDGE. EUROPA XS 12338 PROPELLER CHANGE TO AIRMASTER CHANGE OF PROPELLER TO AIRMASTER AP332 X 64 INCH DIAMETER, USING AC200 CONSTANT ROTAX 912-ULS LDVO AP332, 64 INCH DIAMETER. SPEED CONTROLLER. EUROPA XS 13676 FINGER BRAKES USING TWO MONO TYPE INSTALLATION OF FINGER BRAKE MASTER CYLINDERS USING TWO KART COMPONENTS MASTER ROTAX 912-ULS LDVO BRAKE CYLINDERS CYLINDERS AS PROVIDED IN THE KIT FOR THE MONOWHEEL VERSION, MOUNTED IN THE CENTRAL TUNNEL. EUROPA XS 14587 WING AND FLAP ROOT FILLET FAIRINGS FILLET FAIRING ADDED TO ROOT UPPER SURFACE OF WINGS AND FLAPS ROTAX 912-ULS PLPM

EUROPA XS 15273 DYNON PITOT/ANGLE OF ATTACK PROBE INSTALLATION OF DYNON PITOT/ANGLE OF ATTACK PROBE INSTALLATION ON GRETZ MAST ROTAX 912-ULS PLPM INSTALLATION ON GRETZ MAST MOUNTED TO STARBOARD WING UNDERSIDE OUTBOARD OF AILERON BELLCRANK INSPECTION HATCH. PROBE SUPPLIES AIR DATA TO ANGLE OF ATTACK INDICATION SYSTEM ONLY AND NOT TO THE AIRCRAFT'S MAIN PITOT-STATIC SYSTEM. EUROPA XS 13808 WING TIP STROBE/NAV LIGHT INSTALLATION OF AVEO ENGINEERING POWERBURST PLUS LED NAVIGATION/STROBE LIGHTS ON ROTAX 912-ULS PLPM INSTALLATION WING TIPS Prototype mods that have been approved since 1/1/2008 Page 39 30/11/20 LAA Technical Leaflet TL 3.17 EUROPA XS 12347 FLOSCAN FUEL FLOW GAUGE FLOSCAN FUEL FLOWMETER INTRODUCED PER APPLICANT'S SUBMISSION ROTAX 912-ULS BZNY INTRODUCED EUROPA XS 12350 FUEL PRESSURE SENSOR DYNON FUEL PRESSURE SENSOR INTRODUCED AS DESCRIBED IN APPLICANT'S SUBMISSION ROTAX 912-ULS BZNY EUROPA XS 12581 PROPELLER CHANGE TO AIRMASTER PROPELLER CHANGE TO AIRMASTER AP332, 64 INCH DIAMETER USING BLADES FROM PRE-USED ROTAX 912-ULS BZNY AP332, 64 INCH DIAMETER WARP DRIVE 62 INCH DIAMETER PROPELLER. EUROPA XS 12970 SCHICKE GR6 REGULATOR SUBSTITUTION OF DUCATI REGULATOR WITH SCHICKE GR6 REGULATOR ON ROTAX 912-ULS ROTAX 912-ULS SMDH ENGINE. SUITABLE ON ALL ROTAX 91X SERIES ENGINES EUROPA XS 10507 WING LEVELLING AUTO-PILOT STANDARD EUROPA CLUB MOD TO FIT NAVAID, TRIO OR TRUTRAK WING LEVELLER. ROTAX 912-ULS SMDH EUROPA XS 12338 PROPELLER CHANGE TO AIRMASTER CHANGE OF PROPELLER TO AIRMASTER AP332 X 64 INCH DIAMETER, USING AC200 CONSTANT ROTAX 912-ULS SMDH AP332, 64 INCH DIAMETER. SPEED CONTROLLER. EUROPA XS 12581 PROPELLER CHANGE TO AIRMASTER PROPELLER CHANGE TO AIRMASTER AP332, 64 INCH DIAMETER USING BLADES FROM PRE-USED ROTAX 912-ULS KIMM AP332, 64 INCH DIAMETER WARP DRIVE 62 INCH DIAMETER PROPELLER. EUROPA XS 12637 FINGER BRAKES (KART COMPONENTS STANDARD BRAKE MASTER CYLINDERS REPLACED WITH KART COMPONENTS MASTER CYLINDERS ROTAX 912-ULS SAMY MASTER CYLINDERS) MOUNTED ON AN ALLOY ANGLE. IN ALL OTHER RESPECTS THE ARRANGEMENT IS AS PER EUROPA MOD 65. EUROPA XS 10427 INSTALL SKYDRIVE 912 CARB HEAT SKYDRIVE COOLANT-TYPE CARB HEAT SYSTEM FITTED ROTAX 912-ULS CBOF EUROPA XS 10507 WING LEVELLING AUTO-PILOT STANDARD EUROPA CLUB MOD TO FIT NAVAID, TRIO OR TRUTRAK WING LEVELLER. ROTAX 912-ULS CBOF EUROPA XS 12411 EASE OF MAINTENANCE MODIFICATIONS EASE OF MAINTENANCE MODS INCLUDE: ROTAX 912-ULS NESA 1. SUBSTITUTION OF 3/8" DIAMETER PARALELL PINS WITH AN386-3-19A TAPER PINS WITH AN975- 4 NUTS AND AN364-4 WASHERS TO SECURE THEM. NOTE: INCORPORATION OF EUROPA SERVICE BULLETIN STILL REQUIRED. 2. SUBSTITUTION OF STANDARD MASS BALANCE ARM GUIDE WITH ALUMINIUM UPRIGHTS AND PLASTIC GUIDE WHEEL ON MASS BALANCE ARM. 3. FUEL PUMP MOUNTED TO INNER RIB OF PORT THIGH SUPPORT. EUROPA XS 14809 ALUMINIUM ELBOW FUEL FILLER TUBE INSTALLATION OF FORMED ALUMINIUM ALLOY ELBOW FUEL FILLER TUBE WITH FUEL PROOF ROTAX 912-ULS DDBD INSTALLATION RUBBER CONNECTOR TUBES (OR RUBBER CONNECTOR TUBES MADE FROM THE ORIGINAL EUROPA SUPPLIED FUEL FILLER ELBOW, SUBJECT TO ANNUAL INSPECTION) TO REPLACE ORIGINALLY SUPPLIED NITRILE RUBBER FUEL FILLER ELBOW.

EUROPA XS 12871 CABIN FRESH AIR VENTS ULTIMATE VENT STYLE OF CABIN AIR VENTS, ONE EACH INSTALLED IN FUSELAGE SIDE BELOW ROTAX 912-ULS KIRB WINDSCREEN. EUROPA XS 15494 COWL FLAP INSTALLATION INSTALLATION OF CUSTOM MADE PILOT OPERATED COWL FLAP IN ENGINE LOWER COWLING. ROTAX 912-ULS CICA

EUROPA XS 10823 TO IMPROVE FUEL SYSTEM ALUMINIUM FUEL PIPES INTRODUCED AND ALTERNATIVE FUEL VENT ARRANGEMENT. ISSUE 2 OF ROTAX 912-ULS CBXW THIS MOD RAISED FOR EUROPA G-DEBR (LATTERLY G-URMS) WHICH HAS SIMILAR INSTALLATION BUT DIFFERING BY INSTALLATION OF ANDAIR FUEL SELECTOR VALVE, EUROPA MOD 60 FUEL GAUGE AND STANDARD SIGHT GAUGE. EUROPA XS 11969 TAILPLANE TORQUE TUBE DRIVE PIN REPLACEMENT OF TP14 PINS WITH CLOSE TOLERANCE BOLTS AND NUTS WITH SHAPED SPACERS ROTAX 912-ULS PUPY MODIFICATION TO ENABLE CLAMPING OF TAILPLANE TORQUE TUBE, TAILPLANE DRIVE BELLCRANK TP09 AND TAILPLANE DRIVE PLATES TP12. EUROPA XS 10986 PROVISION OF CABIN HEAT A FLAPPER VALVE IS INSTALLED ON THE COOLING DUCT DOWNSTREAM OF THE COOLANT ROTAX 912-ULS PUPY RADIATOR WHICH ROUTES A FLOW OF HOT AIR INTO EACH FOOTWELL. THE SELECTION OF CABIN HEAT IS CONTROLLED VIA A SINGLE BOWDEN CABLE ROUTED THROUGH TO THE CABIN. THE FOOTWELL VENTS ARE CONTROLLED THROUGH A STAINLESS "DAISY" VALVE WHICH IS CONTROLLABLE EACH SIDE THROUGH TWO PUSH-PULL CABLES. EUROPA XS 13905 STROBE UNIT INSTALLATION BAILEYS SINGLE HEAD CONTROL UNIT INSTALLED ON PORT BAGGAGE BAY SUPPORT RIB. SINGLE ROTAX 912-ULS CGVJ STROBE HEAD MOUNTED ON TOP OF FIN VIA AN ALLOY MOUNTING PLATE. EUROPA XS 12257 REPLACEMENT OF FUEL FILTER WITH ANDAIR MINI-GASCOLATOR SUBSTITUTED FOR EUROPA STANDARD FUEL FILTER ROTAX 912-ULS JHKP GASCOLATOR EUROPA XS 13285 MAIN WHEEL FAIRINGS INSTALLATION OF MAIN WHEEL FAIRINGS; THE FRONT FAIRING MOUNTED TO THE SWINGING ARM ROTAX 912-ULS JHKP AND THE AFT FAIRING MOUNTED TO THE FUSELAGE UNDERSIDE. Prototype mods that have been approved since 1/1/2008 Page 40 30/11/20 LAA Technical Leaflet TL 3.17 EUROPA XS 10371 ALTERATION TO TAILWHEEL STEERING & INSTALLATION OF TAILWHEEL STEERING BELLCRANK AND BRACKETS ON FORWARD FACE OF REAR ROTAX 912-ULS JHKP INST. OF 'CLASSIC' RUDDER DRIVE BULKHEAD AND THE INCORPORATION OF THE EUROPA CLASSIC METHOD OF RUDDER DRIVE VIA PUSHROD INTO CS29 BUILT INTO RUDDER LEADING EDGE. EUROPA XS 10410 PHENOLIC MOULDED FIREWALL GRAHAM SINGLETON MOULDED PHENOLIC FIREWALL OPTION ROTAX 912-ULS JHKP EUROPA XS 11969 TAILPLANE TORQUE TUBE DRIVE PIN REPLACEMENT OF TP14 PINS WITH CLOSE TOLERANCE BOLTS AND NUTS WITH SHAPED SPACERS ROTAX 912-ULS GCAC MODIFICATION TO ENABLE CLAMPING OF TAILPLANE TORQUE TUBE, TAILPLANE DRIVE BELLCRANK TP09 AND TAILPLANE DRIVE PLATES TP12. EUROPA XS 14555 WINGTIP LIGHTS WHELEN MICROBURST III WING TIP LED NAV/STROBE LIGHT UNIT MOUNTED ON EACH WING TIP. ROTAX 912-ULS GCAC UNITS ARE MOUNTED TO 1/4" PLY WOOD BONDED TO INSIDE OF WINGTIP SKIN, WITH 2 PLIES OF GFRP OVER. ATTACHMENT IS BY M3 BOLTS INTO 'NUTSERTS' EPOXIED INTO PLY. INCLUDES ASSOCIATED WIRING AND CIRCUIT PROTECTION.

EUROPA XS 12441 FUEL FLOW COMPUTER FLOWSCAN 201 INSTALLED IN ACCORDANCE WITH FLOWSCAN INSTRUCTIONS ROTAX 912-ULS CERI EUROPA XS 14400 AIRMASTER AP332, 64 INCH DIAMETER INSTALLATION OF AIRMASTER AP332 64 INCH DIAMETER PROPELLER. ROTAX 912-ULS CDBX PROPELLER INSTALLATION EUROPA XS 15241 ELECTRICAL MODIFICATIONS MODIFICATIONS TO ELECTRICAL SYSTEM INCLUDING: ROTAX 912-ULS CDBX 1. BATTERY REPOSITIONING TO UNDER BAGGAGE BAY. 2. AVEO POWERBURST DAYLIGHT NAV/STROBE LIGHTS INSTALLED ON WINGTIPS. 3. CONSPICUITY LIGHT HOUSED IN GRP POD BOTH INDEPENDENTLY BOLTED TO UNDERSIDE OF LOWER COWLING AIR INTAKE DUCT. EUROPA XS 12564 FITTING STROBE LIGHTS TO FUSELAGE STROBE LIGHTS FITTED ABOVE AND BELOW FUSELAGE ROTAX 912-ULS CEMI EUROPA XS 12338 PROPELLER CHANGE TO AIRMASTER CHANGE OF PROPELLER TO AIRMASTER AP332 X 64 INCH DIAMETER, USING AC200 CONSTANT ROTAX 912-ULS IPOD AP332, 64 INCH DIAMETER. SPEED CONTROLLER. EUROPA XS 10513 WHELEN STROBE LIGHTS ADDED TO WHELEN A600-PR14 COMBINED NAV/STROBE UNITS INSTALLED TO WING TIPS 2 X 3 CORE CABLES ROTAX 912-ULS WIKI WINGTIPS ROUTED THROUGH WING ROOT DISCONNECTS TO SKYFLASH SF D2 STROBE UNIT MOUNTED BEHIND COCKPIT MODULE BULKHEAD. EUROPA XS 14108 MODIFICATIONS TO FUEL DELIVERY AND INSTALLATION OF TWO ANDAIR GA375 GASCOLATORS, MOUNTED TO CUSTOM MADE METAL ROTAX 912-ULS CFKZ DRAINAGE SYSTEMS BRACKET IN CENTRE TUNNEL BETWEEN THIGH SUPPORTS, IN PLACE OF PUROLATOR PRO 805 IN- LINE FILTERS, ANDAIR FS20-7 FUEL SELECTOR VALVE IN PLACE OF 210-CL VALVE. ELECTRIC FUEL PUMP REPOSITIONED FROM UNDER BAGGAGE BAY FLOOR TO SIDEWALL OF CENTRE TUNNEL. INSTALLATION OF CAV110 FUEL DRAIN VALVES IN SEAT PANS INSTEAD OF REAR FUSELAGE.

EUROPA XS 15468 CONSPICUITY LIGHT INSTALLATION OF LED LAMP UNIT INTO REDUNDANT NACA INLET IN STARBOARD SIDE OF LOWER ROTAX 912-ULS CFKZ COWLING FOR USE AS A CONSPICUITY LIGHT. EUROPA XS 14027 SMARTASS-3 SPEAKING AIRSPEED INSTALLATION OF SMART AVIONICS SMARTASS-3 SPEAKING AIRSPEED INDICATOR. ROTAX 912-ULS CEYK INDICATOR INSTALLATION EUROPA XS 12488 FINGER BRAKES USING EUROPA INSTALLATION OF FINGER BRAKES SYSTEM IN TOP OF CENTRE TUNNEL TO THE RIGHT OF THE ROTAX 912-ULS IRPW SUPPLIED TOE BRAKE CYLINDERS THROTTLE LEVER USING TWO INDIVIDUAL KART COMPONENTS MASTER CYLINDERS UTILISING ONE STANDARD FOOT BRAKE MOUNTING BRACKET AND SIDE-WALL MOUNTING AS PER MONOWHEEL AIRCRAFT. EUROPA XS 12489 FUEL SYSTEM MODIFICATIONS MODIFICATIONS TO FUEL SYSTEM INCLUDING INSTALLATION OF ANDAIR FS20X2 FUEL SELECTOR ROTAX 912-ULS IRPW VALVE WITH EXTENSION TO SELECTOR HANDLE MOUNTED INTO CENTRE TUNNEL TOP, AN ANDAIR GAS375 GASCOLATOR ADJACENT TO THE SELECTOR VALVE, REPOSITIONING OF THE FUEL SIGHT GAUGE TO THE SEAT BACK JUST TO THE LEFT OF THE CENTRE TUNNEL, FUEL TANK AND SIGHT GAUGE VENTS MOUNTED TO THE FUSELAGE UNDERSIDE WITH SYPHON-BREAK PLUMBING INTO THE FUEL FILLER MOULDING AND FUEL TANK DRAINS MOUNTED INTO REMOVABLE ACCESS PANEL BENEATH GASCOLATOR. EUROPA XS 13590 WING TIP NANO STROBE LIGHTS (LED) INSTALLATION OF WING TIP MOUNTED LED STROBE LIGHT UNITS. POWER SUPPLY MOUNTED ROTAX 912-ULS IRPW UNDER CENTRAL TUNNEL AREA AND SECURED WITH A GRP COVER. EUROPA XS 14589 ROTAX 912iS ENGINE INSTALLATION INSTALLATION OF ROTAX 912iS ENGINE WITH AIRMASTER AP332SCTF-WWR64-W 64 INCH ROTAX 912-iS NICX DIAMETER PROPELLER INSTALLATION. Prototype mods that have been approved since 1/1/2008 Page 41 30/11/20 LAA Technical Leaflet TL 3.17 EUROPA XS 14590 WHELEN MICROBURST II WINGTIP WHELEN MICROBURST II WINGTIP MOUNTED NAVIGATION AND STROBE LIGHTS INSTALLATION. ROTAX 912-iS NICX MOUNTED NAVIGATION AND STROBE LIGHTS EUROPA XS 14591 CENTRE TUNNEL TOP REPLACEMENT REPLACEMENT OF PREVIOUSLY CUT AWAY CENTRE TUNNEL'S TOP SURFACE AND THE ROTAX 912-iS NICX AND FINGER BRAKES INSTALLATION INSTALLATION OF FINGER BRAKES USING THE ORIGINAL KIT SUPPLIED COMPONENTS BRAKE MASTER CYLINDERS. EUROPA XS 10986 PROVISION OF CABIN HEAT A FLAPPER VALVE IS INSTALLED ON THE COOLING DUCT DOWNSTREAM OF THE COOLANT ROTAX 912-iS NICX RADIATOR WHICH ROUTES A FLOW OF HOT AIR INTO EACH FOOTWELL. THE SELECTION OF CABIN HEAT IS CONTROLLED VIA A SINGLE BOWDEN CABLE ROUTED THROUGH TO THE CABIN. THE FOOTWELL VENTS ARE CONTROLLED THROUGH A STAINLESS "DAISY" VALVE WHICH IS CONTROLLABLE EACH SIDE THROUGH TWO PUSH-PULL CABLES. EUROPA XS 14708 DYNON PITOT/AOA HEAD AND INSTALLATION OF DYNON PITOT/AOA HEAD (NOT HEATED) INSTALLATION IN SAME POSITION AS ROTAX 912-iS NICX REPOSITIONED STATIC SOURCE STANDARD EUROPA PITOT/STATIC HEAD. INSTALLATION STATIC PORTS IN FUSELAGE SIDES, PER EUROPA CLASSIC. EUROPA XS 12546 TRIO AVIONICS EZ-1 ALTITUDE HOLD TRIO AVIONICS EZ-1 ALTITUDE HOLD AUTO-PILOT WITH AUTO TRIM FACILITY. SERVO MOUNTED ROTAX 914-UL JULZ AUTO-PILOT WITH AUTO TRIM UNDER PORT SEAT THIGH SUPPORT WITH PUSH-ROD DRIVING THE CS-10 PITCH TORQUE TUBE, APPROPRIATELY MODIFIED WITH ADDITIONAL DRIVE LUGS, DIRECTLY. EUROPA XS 12589 AUTOMATIC SERVO CONTROLLED INSTALLATION OF A CENTRALLY PIVOTED COWLING FLAP IN THE RADIATOR/OIL COOLER AIR ROTAX 914-UL JULZ COWLING FLAP OUTLET DUCT THAT IS AUTOMATICALLY CONTROLLED BY A MAC SERVO DRIVEN BY ELECTRONIC DATA FROM A THERMOCOUPLE READING COOLANT TEMPERATURE. EUROPA XS 12548 PROPELLER CHANGE TO AIRMASTER INSTALLATION OF WARP DRIVE 62 INCH DIAMETER BLADES INTO AN AIRMASTER AP332 HUB ROTAX 914-UL BZTI AP332 63" DIAMETER RESULTING IN A 63 INCH DIAMETER PROPELLER. EUROPA XS 12403 WOODCOMP SR3000/3W 1625MM PROPELLER CHANGE TO WOODCOMP SR3000/3W 1625MM DIAMETER ROTAX 914-UL XSDJ DIAMETER EUROPA XS 13399 LONG RANGE FUEL TANK INSTALLATION OF A TEMPORARY 92 USABLE LITRE CAPACITY LONG RANGE FUEL TANK WHICH IS ROTAX 914-UL XSDJ DESIGNED TO FIT ON PASSENGER SEAT. PASSENGER SEAT BELTS USED, ALONG WITH ADDITIONAL CUSTOM MADE STRAPPING, TO SECURE TANK. BULB PUMP PRIMED SYPHON SYSTEM INTO MAIN FUEL TANK IDENTICAL IN FUNCTION TO EUROPA FACTORY LONG RANGE FUEL TANK INSTALLATION. INCLUDES CUSTOM MADE FUNNEL WHICH FITS AND LOCKS INTO LONG RANGE TANK FILLER RECEPTACLE TO ENABLE FILLING WITH REFUELLING NOZZLE OUTSIDE OF COCKPIT.

EUROPA XS 14570 WOODCOMP SR3000/3NW 1625MM INSTALLATION OF WOODCOMP SR3000/3NW 1625MM DIAMETER PROPELLER ROTAX 914-UL XSDJ DIAMETER PROPELLER INSTALLATION EUROPA XS 14571 BERINGER MAIN WHEEL AND BRAKE INSTALLATION OF BERINGER WHEEL AND BRAKE WITH BRAKE LEVER MOUNTED IN CENTRE ROTAX 914-UL XSDJ INSTALLATION CONSOLE. EUROPA XS 14572 GARMIN G3X TOUCH DUAL AXIS AUTO- INSTALLATION OF GARMIN G3X TOUCH DUAL AXIS AUTO-PILOT USING GSA 28 SERVOS INSTALLED ROTAX 914-UL XSDJ PILOT INSTALLATION USING GARMIN MOUNTING HARDWARE FOLLOWING THE EUROPA MOD 75 AND 76 INSTRUCTIONS. EUROPA XS 12403 WOODCOMP SR3000/3W 1625MM PROPELLER CHANGE TO WOODCOMP SR3000/3W 1625MM DIAMETER ROTAX 914-UL IVER DIAMETER EUROPA XS 13429 WOODCOMP SR3000/3W 1625MM INSTALLATION OF WOODCOMP SR3000/3W 1625MM DIAMETER PROPELLER WITH SMART ROTAX 914-UL BZTN DIAMETER PROPELLER INSTALLATION AVIONICS CSC/1G CONTROLLER. EUROPA XS 10371 ALTERATION TO TAILWHEEL STEERING & INSTALLATION OF TAILWHEEL STEERING BELLCRANK AND BRACKETS ON FORWARD FACE OF REAR ROTAX 914-UL FITY INST. OF 'CLASSIC' RUDDER DRIVE BULKHEAD AND THE INCORPORATION OF THE EUROPA CLASSIC METHOD OF RUDDER DRIVE VIA PUSHROD INTO CS29 BUILT INTO RUDDER LEADING EDGE. EUROPA XS 10410 PHENOLIC MOULDED FIREWALL GRAHAM SINGLETON MOULDED PHENOLIC FIREWALL OPTION ROTAX 914-UL FITY EVANS VP-1 12301 PROPELLER CHANGE TO NEWTON TYPE CHANGE OF PROPELLER TO NEWTON TYPE 21 LE 57" X 33" VW 1834 GVPI 21 LE 57" X 33"

Prototype mods that have been approved since 1/1/2008 Page 42 30/11/20 LAA Technical Leaflet TL 3.17 EVANS VP-1 SERIES 2 14149 LEBURG IGNITIONS MAGNETOS REPLACED WITH DUAL LEBURG ELECTRONIC IGNITION. INSTALLATION OF ASSOCIATED VW 1834 AYUJ HONDA ALTERNATOR, BATTERIES, SENSORS, CONTROL UNIT AND WIRING. SENSORS ARE MOUNTED AT THE REAR OF THE ENGINE ON BESPOKE BRACKETS. BATTERIES ARE MOUNTED BELOW THE ENGINE ON A BESPOKE FRAME. EVANS VP-1 SERIES 2 12454 FIT LEBURG IGNITION TO VW 1835 CC STANDARD LEBURG INSTALLATION PER LEBURG INSTALLATION INSTRUCTIONS VW 1834 BAPP ENGINE EVANS VP-1 SERIES 2 12477 MAUW INCREASE TO 800 LBS MAUW INCREASE TO 800 LBS VW 1834 BAPP EVANS VP-1 SERIES 2 13138 NEWTON 15L 57" X 33" PROPELLER INSTALLATION OF NEWTON 15L 57 INCH DIAMETER X 33 INCH PITCH PROPELLER. VW 1834 BAPP EVANS VP-1 SERIES 2 15123 PROP CHANGE TO HERCULES 5835737-5 PROPELLER CHANGED TO HERCULES 5835737-5 VW 1834 BDTB

EVANS VP-1 SERIES 2 12913 LEBURG IGNITION TO VW 1835 CC INSTALLATION OF LEBURGH ELECTRONIC IGNITION SYSTEM, INCORPORATING D MICKLEBURGH VW 1834 BDUL ENGINE RECOMMENDED HONDA CBR 600 COILS AND ALTERNATOR AND ELECTREX REGULATOR, TO REPLACE THE ORIGINALLY FITTED LUCAS SR4 MAGNETOS. EVANS VP-2 13288 SENSENICH W72CK44 72" X 44" PROPELLER CHANGE TO SENSENICH W72CK44 72 INCH DIAMETER X 44 INCH PITCH. CONTINENTAL A65-8 BUGI PROPELLER EVANS VP-2 12600 PROVISION FOR ENGINE CHANGE FROM PROVISION FOR FITTING VW 2100CC USING INSTALLATION AS ON G-BXOC APPROVED VW 1834 BJZB VW 1834 TO REVMASTER 2100D. PREVSIOUSLY, EXCEPT ENGINE MOUNTING BOLTS ARE 10mm OD x 6.5" EN8.8 SPEC WITH SUITABLE M10 CASTLE NUTS AND SPLIT PINS. PROPELLER IS NEWTON TYPE 15L 59 INCH DIAMETER X 37 INCH PITCH. EVERETT GYROPLANE SERIES 1 11127 INSTALLATION OF HORIZONTAL HORIZONTAL STABILISER INSTALLED IN ACCORDANCE WITH P.LOVEGROVE DRAWING BGL-0241. ROTAX 582 BMZN STABILISER APPLICABLE TO EVERETT, CRICKET AND REPLICA CRICKET GYROPLANES EVERETT GYROPLANE SERIES 1 14890 ENGINE & PROPELLER CHANGE ROTAX 582 ENGINE AND GSC TECH-III PROPELLER SUBSTITUTED IN ACCORDANCE WITH EVERETT ROTAX 582 BMZN SERIES 2 MODEL EXCEPT DUAL IGNITION ROTAX 582 REPLACES SINGLE IGNITION 532 EVERETT GYROPLANE SERIES 1 14214 THROTTLE AND BRAKE QUADRANT RECONFIGURED THROTTLE/BRAKE PEDESTAL VW 1834 BMZS EVERETT GYROPLANE SERIES 1 15001 PRINCE P-TIP 52" X 28" PROPELLER INSTALLATION OF PRINCE P-TIP 52" X 28" PROPELLER, EX G-BMZP. VW 1834 BMZS INSTALLATION EVERETT GYROPLANE SERIES 2 12428 WARP DRIVE RPM 3 BLADED 52" WARP DRIVE RPM 3 BLADED PROPELLER FITTED IN ACCORDANCE WITH MANUFACTURER'S ROTAX 582 BWCK DIAMETER PROPELLER INSTALLATION INSTRUCTIONS. PROPELLER IS 52" DIAMETER AND PITCHED TO SUIT APPLICATION.

EXTRA EA 230 12530 DUAL P-MAG IGNITION FOR LYCOMING DUAL: P-MAGS INSTALLED PER MANUFACTURER'S INSTRUCTIONS. LYCOMING AEIO-360-A1E VOCA AEIO-360-A1E. EXTRA EA 230 12604 PROPELLER CHANGE MTV-9 PROPELER TYPE MTV-9-B-C/C190-18b LYCOMING AEIO-360-A1E VOCA FAIRCHILD 24R-46A 14250 OMNIBUS MOD OMNIBUS MOD RAISED FOR REFERENCE PURPOSES ONLY AT REBUILD - SEE WORKSHEETS RANGER 6-440-C5 BCBL FALCO F8L 13546 DUAL P-MAGS INSTALLATION SUBSTITUTION OF BOTH SLICK MAGNETOS WITH P-MAGS ELECTRONIC IGNITION UNITS WITH LYCOMING IO-320-B1A OCAD IGNITION ADVANCE SET TO 25 DEGREES BTDC.

PLACARD TO BE FITTED NEXT TO MAGNETO SWITCHES STATING 'BEFORE EACH FLIGHT, CHECK PROPER FUNCTION OF SELF POWERING ALTERNATOR WITHIN EACH P-MAG AT 900 RPM'.

FALCO F8L 13776 MGL AUTOPILOT MGL DUAL AXIS AUTO-PILOT INSTALLATION. CAPSTAN ROLL SERVO DIRECT REPLACEMENT OF LYCOMING IO-320-B1A OCAD PREVIOUSLY INSTALLED CENTURY 1 SERVO AND PITCH SERVO MOUNTED BETWEEN FRAMES 6 AND 7 OPERATING PITCH BELLCRANK P/N 760 VIA PUSH-ROD.

SYSTEM CONTROLLED BY AN MGL iEFIS UNIT. FALCO F8L 14163 MT-V-12C/180-57 PROPELLER INSTALLATION OF MT-V-12C/180-57, 180CM DIAMETER 3 BLADED HYDRAULIC CONSTANT SPEED LYCOMING IO-320-B1A RJAM INSTALLATION PROPELLER. FALCO F8L 12334 TRUTRAK WING LEVELLER TRUTRAK WING LEVELLER SYSTEM FITTED IN ACCORDANCE WITH LAA PROCEDURES LYCOMING IO-320-B1A CCOR

Prototype mods that have been approved since 1/1/2008 Page 43 30/11/20 LAA Technical Leaflet TL 3.17 FALCO F8L 14820 GARMIN G3X DUAL AXIS AUTO-PILOT INSTALLATION OF GARMIN G3X DUAL AXIS AUTO-PILOT COMMANDED VIA GARMIN GMC 307 LYCOMING IO-320-B1A CCOR INSTALLATION CONTROLLER. ORIGINALLY FITTED TRUTRAK CAPSTAN ROLL SERVO (UNDER MOD 12334) SUBSTITUTED WITH GARMIN GSA 28 CAPSTAN SERVO. GARMIN GSA 28 PITCH SERVO INSTALLED USING GARMIN SERVO MOUNTING BRACKET ON TWO LATERAL 20MM X 30MM SPRUCE BEARERS BONDED, USING AERODUX GLUE, AND BOLTED THROUGH A PRE-EXISTING 1.5MM THICK PLYWOOD PLATFORM ON 15MM X 20MM SPRUCE BEARERS BONDED TO THE FLOOR, OR FOR THE FORWARD LEFT BOLT, AN ALUMINIUM SPACER.

FALCO F8L 14549 MTV-12-B/180-59b PROPELLER INSTALLATION OF MTV-12-B/180-59b PROPELLER LYCOMING IO-360-B1B FATE INSTALLATION FALCO F8L 14608 DUAL P-MAGS INSTALLATION INSTALLATION OF DUAL P-114 MODEL P-MAGS TO LYCOMING IO-360-B1B ENGINE. LYCOMING IO-360-B1B FATE FALCO F8L 13635 ENGINE CHANGE TO LYCOMING 0-320- INSTALLATION OF LYCOMING O-320-B3B ENGINE WITH HARTZELL HC-C2YL-1BF/F7663A-4 LYCOMING O-320-B3B BYLL B3B PROPELLER. FALCO F8L 12616 PROPELLER CHANGE TO HARTZELL HC- INSTALLATION OF HARTZELL HC-C2YL-1BF/F7663-4 63 INCH HYDRAULIC CONSTANT SPEED LYCOMING O-320-E2A BWYO C2YL-1BF/F7663-4 PROPELLER FALCO F8L 14678 PROPELLER CHANGE TO HERTZELL HC- PROPELLER CHANGED TO HERTZELL HC-C2YL-1BF/7663A-4 LYCOMING IO-320-B1A CYLL C2YL-1BF/7663A-4 (MODIFIED) FALCO F8L 14523 ENGINE & PROPELLER CHANGE POWERPLANT CHANGED TO SUPERIOR XP-IO-320-B1HC3 WITH A MTV-12-C/180-57 PROPELLER. SUPERIOR XP-IO-320-B1HC3 DAMB ENGINE INCORPORATED DUAL P114 P-MAG IGNITION UNITS. FALCON XP 13318 TWO-PART COCKPIT CANOPY CANOPY RE-CONFIGURED IN TWO PARTS WITH IMPROVED LATCHING MECHANISM UL BUYF FOURNIER RF-3 13390 ENGINE CAPACITY INCREASE FROM INCREASE IN ENGINE CAPACITY FROM 1200CC TO 1384CC BY SUBSTITUTING 83mm BORE VW (RECTIMO) 4AR-1200 BIPN 1200CC TO 1384CC CYLINDERS AND PISTONS FOR STANDARD 78MM UNITS. CORRESPONDING INCREASE IN TO 7.5:1. FOURNIER RF3 12260 ENGINE CAPACITY INCREASED TO 1400CC AS PER PREVIOUS MOD 12253 ENGINE CAPACITY INCREASED TO 1400CC BY SUBSTITUTING 83mm VW (RECTIMO) 4AR-1200 AYJD BORE CYLINDERS AND PISTONS FOR STANDARD 78MM UNITS. SPACERS FITTED UNDER CYLINDER BASES TO MAINTAIN ORIGINAL COMPRESSION RATIO. FOURNIER RF3 12613 PROPELLER CHANGE TO NEWTON TYPE PROPELLER CHANGE TO NEWTON TYPE 10L, 52 INCH DIAMETER X 36 INCH PITCH. VW (RECTIMO) 4AR-1200 AYJD 10L, 52 INCH X 36 INCH FOURNIER RF3 13767 ENGINE AND PROPELLER CHANGE AS PER PREVIOUS MOD 12253 ENGINE CAPACITY INCREASED TO 1400CC BY SUBSTITUTING 83mm VW (RECTIMO) 4AR-1200 BIIA BORE CYLINDERS AND PISTONS FOR STANDARD 78MM UNITS. SPACERS FITTED UNDER CYLINDER BASES TO MAINTAIN ORIGINAL COMPRESSION RATIO. PROPELLER CHANGED TO HERCULES 5138286-S 51 INCH DIAMETER X 38 INCH PITCH. FOURNIER RF3 13860 PROPELLER CHANGE TO EVRA D9.28 INSTALLATION OF EVRA D9.28 136CM DIAMETER X 69CM PITCH PROPELLER VW (RECTIMO) 4AR-1200 BNHT FOURNIER RF3 13390 ENGINE CAPACITY INCREASE FROM INCREASE IN ENGINE CAPACITY FROM 1200CC TO 1384CC BY SUBSTITUTING 83mm BORE VW (RECTIMO) 4AR-1200 BNHT 1200CC TO 1384CC CYLINDERS AND PISTONS FOR STANDARD 78MM UNITS. CORRESPONDING INCREASE IN COMPRESSION RATIO TO 7.5:1. FOURNIER RF4D 13511 ENGINE AND PROPELLER CHANGE ENGINE SUBSTITUTED WITH ROLLASON 1600CC ARDEM 4CO2 Mk XI CORE, BUT WITH LEBURG ARDEM 4CO2 MK XI AWBJ DUAL IGNITION FITTED INSTEAD OF CHAIN DRIVEN MAGNETOS. REPLICA OF RECTIMO AR1200 (MODIFIED) INTAKE MANIFOLD USED TO MOUNT THE ARDEM'S ORIGINAL ZENITH CARBURETTOR BENEATH THE CRANKCASE RATHER THAN ABOVE, USING GRAVITY FEED TO CARBURETTOR. FUEL PUMP REMOVED AND BLANKED OFF . EXISTING TWIN BATTERY INSTALLATION ARRANGEMENT USED. COWLINGS WIDENED TO SUIT. FOURNIER RF4D 13686 LIFT HANDLE TO AVOID LIFTING BY OPTIONAL WOODEN DOWEL TAIL LIFTING BAR REPLACED BY SPRUNG LOADED RETRACTABLE VW 1400 AVKD TAILPLANE TELESCOPIC TUBULAR LIFTING BAR, WITH SUITABLE GUSSET REINFORCEMENT OF FUSELAGE IF NOT ALREADY PRESENT. FOURNIER RF4D 12721 PROPELLER CHANGE TO NEWTON TYPE PROPELLER CHANGE TO NEWTON TYPE 09L 54" X 36" VW 1600 AVWY 09L 54" X 36" FOURNIER RF4D 14000 STICK MOUNTED HAND LEVER OPERATED INSTALLATION OF CLEVELAND BRAKE DISC AND CALLIPER AND MATCO HAND BRAKE LEVER VW 1835 AWLZ DISC BRAKE SYSTEM INSTALLATION MOUNTED TO CONTROL COLUMN.

Prototype mods that have been approved since 1/1/2008 Page 44 30/11/20 LAA Technical Leaflet TL 3.17 FOURNIER RF4D 14137 ENGINE CHANGE TO VW 1835 1835cc ENGINE FITTED IN ACCORDANCE WITH AAN PFA-834-544 sup 4. VW 1835 AWLZ FOURNIER RF4D 14395 HERCULES 5447526-S 54" X 47" INSTALLATION OF HERCULES 5447526-S 54 INCH DIAMETER X 47 INCH PITCH PROPELLER VW 1835 AWLZ PROPELLER INSTALLATION FOURNIER RF4D 12253 ENGINE CAPACITY INCREASED TO 1400CC ENGINE CAPACITY INCREASED TO 1400CC BY SUBSTITUTING 83mm BORE CYLINDERS AND PISTONS VW (RECTIMO) 4AR-1200 AWGN FOR STANDARD 78MM UNITS. SPACERS FITTED UNDER CYLINDER BASES TO MAINTAIN ORIGINAL COMPRESSION RATIO. FOURNIER RF4D 12384 AILERON GAP SEALS AILERON GAP SEALS FITTED PER APLICANT'S SUBMISSION VW (RECTIMO) 4AR-1200 AWGN FOURNIER RF4D 12876 ADDITION OF OIL COOLER OIL COOLER ADDED PER EXISTING CONCESSION 0317 RAISED FOR G-BNHT, ALSO CLEARED VW (RECTIMO) 4AR-1200 AWGN PREVIOUSLY ON G-AWLZ. M.WOOLLARD LETTER DATED 18.7.96 AND 'FOURNIER RF3/RF4OIL COOLER INSTALLATION INSTRUCTIONS ' PROVIDES NECESSARY DETAILS FOURNIER RF4D 13214 ENGINE CHANGE TO RECTIMO/JMR 4AR ENGINE CHANGED FOR REPLACEMENT VW/RECTIMO AR1200 TYPE CONVERSION OF 1776CC VW (RECTIMO) 4AR-1200 AWGN 1200/1776 CAPACITY FOURNIER RF4D 13248 PROPELLER CHANGE TO HERCULES HERCULES PROPELLR FITTED AS ABOVE VW (RECTIMO) 4AR-1200 AWGN 5237279 FOURNIER RF4D 13724 RUDDER PEDALS MOVED TWO INCHES RUDDER PEDALS BOLTED IN PLACE 2" FORWARD OF STANDARD POSITION AND LINKS ADDED TO VW (RECTIMO) 4AR-1200 AWGN FORWARD RUDDER CABLES TO SUIT. RETROSPECTIVE MOD RAISED TO APPROVE MOD DONE SOME TIME PREVIOUSLY FOURNIER RF4D 13725 AILERON OPERATING ARM FASTENER DUE TO EXFOLIATION CORROSION IN ORIGINAL PARTS, AILERON OPERATING ARM ANGLES PART VW (RECTIMO) 4AR-1200 AWGN SUBSTITUTION NUMBERS 4.12.04/H WERE REMADE IN IN 2024-T3 EXTRUDED ANGLE AND BEARING INSERT ATTACHED TO ANGLES USING M5 STEEL CAPSCREWS AND ASSOCIATED WASHERS AND SELF- LOCKING NUTS RATHER THAN 5mm SOLID ALUMINIUM RIVETS, TO AVOID DIFFICULTY IN FORMING RIVET SHOP HEADS WITHOUT APPROPRIATE TOOLING. FOURNIER RF4D 13726 REMOVAL OF HAND-STARTER HAND STARTER SYSTEM REMOVED AS HERCULES PROPELLER BACKPLATE MAKES NO PROVISION VW (RECTIMO) 4AR-1200 AWGN FOR RING GEAR. STARTER SYSTEM REDUNDANT AS AIR STARTS POSSIBLE BY WINDMILLING AND GROUND STARTS NORMALLY CARRIED OUT BY HAND SWINGING. FOURNIER RF4D 13727 GOPRO FIN-CAM MOUNT GO-PRO CAMERA MOUNTED AT TIP OF FIN VW (RECTIMO) 4AR-1200 AWGN FOURNIER RF4D 13780 VARIATION OF AEROBATIC LIMITATIONS . VW (RECTIMO) 4AR-1200 AWGN

FOURNIER RF4D 13782 EXTENDED ENGINE BREATHER AND PEE ENGINE OIL BREATHER PIPE EXTENDED TO VICINITY OF TAILWHEEL TO PREVENT OIL STAINING. VW (RECTIMO) 4AR-1200 AWGN TUBE PEE TUBE FITTED EXITING IN SAME VICINITY

FOURNIER RF4D 13783 FLYING CONTROL IMPROVEMENT ELEVATOR STOPS ALTERED TO INCREASE RANGE OF CONTROL MOVEMENT TO UP 25 DEGREES, VW (RECTIMO) 4AR-1200 AWGN MEASURES DOWN 20 DEGREES. RUDDER STOPS INTRODUCED TO LIMIT TRAVEL TO DESIGNER'S SPECIFIED RANGE AND RUDDER GAP SEAL INTRODUCED. FOURNIER RF4D 13784 SEVERAL DRAG-REDUCTION MEASURES VHF AERIAL RELOCATED INTERNAL TO FUSELAGE VW (RECTIMO) 4AR-1200 AWGN FAIRING OF WING OUTRIGGERS AND WHEEL CUFFS FOURNIER RF4D 15225 PYROTECHNICS EQUIPMENT PYROTECHNIC INSTALLATION ON WING TIPS AND FIN TIP AND ASSOCIATED ELECTRICAL FIRING VW (RECTIMO) 4AR-1200 AWGN SYSTEM FOURNIER RF4D 13865 HERCULES 5138286-S PROPELLER HERCULES 5138286-S 51 INCH DIAMETER X 38 INCH PITCH PROPELLER INSTALLATION. VW (RECTIMO) 4AR-1200 BHJN INSTALLATION FOURNIER RF4D 13348 HERCULES 5237279-S 52" X 37" INSTALLATION OF HERCULES 5237279-S 52 INCH DIAMETER X 37 INCH PITCH PROPELLER VW (RECTIMO) 4AR-1200 AWEK PROPELLER FOURNIER RF5 12361 CASTERING TAILWHEEL MODIFICATION OF TAILWHEEL ASSEMBLY TO INCORPORATE FRIDOLIN WEZEL VERSION 1 DESIGN LIMBACH 1834 (MOD) AZRK TO ENABLE DISCONNECTION OF TAILWHEEL FORK FROM CONTROL SYSTEM ALLOWING FULL 360 DEGREE CASTERING FOR GROUND HANDLING ONLY. PLUNGER LOCK DEVICE VARIES FROM ORIGINAL DESIGN BEING A SIMPLE FLAT STEEL PLATE SUBSTITUTING MACHINED KNOB.

FOURNIER RF5 12907 HERCULES 5736237 57" X 36" PROPELLER INSTALLATION OF HERCULES 5736237 57" X 36" PROPELLER. LIMBACH SL1700-E AZJC

FOURNIER RF5 12991 METAL SPLIT HUB TAILWHEEL CUSTOM TAILWHEEL HUB MANUFACTURED TO ACCEPT TOST 200 x 50 6 PLY TYRE LIMBACH SL1700-E AZJC

Prototype mods that have been approved since 1/1/2008 Page 45 30/11/20 LAA Technical Leaflet TL 3.17 FOURNIER RF5 12824 LOCKABLE CASTORING TAILWHEEL 360 DEGREE CASTORING TAILWHEEL FOR EASE OF GROUND HANDLING WITH LOCKING FEATURE LIMBACH SL1700-E AZJC TO ENABLE TAILWHEEL STEERING ON THE GROUND. DESIGN IN ACCORDANCE WITH CLUB FOURNIER INTERNATIONAL DOCUMENT CFI-FAU 07/2003 WEZEL VERSION 1. REF LBA STC NO. PS 0010 695/2. FOURNIER RF5 13945 ENGINE CHANGE & PROPELLER CHANGE ENGINE CHANGED TO HIGHER POWER VARIANT AS DESCRIBED IN AAN AND PROPELLER REPLACED LIMBACH SL1700-E AZJC TO HERCULES 5736237-S BY HERCULES 5736237 FOURNIER RF5 13762 ENGINE CHANGE TO LIMBACH L2400 D01 MODIFIED LIMBACH L2400 DOI FITTED, INCLUDING OPTIONALLY USE OF HERCULES PROPELLER LIMBACH L2400-D01 AYME (MODIFIED) (MODIFIED) FOURNIER RF5 13988 ENGINE CHANGE TO VW 2180 LIMBACH ENGINE REPLACED WITH VW 2180cc SUPPLIED BY GREAT PLAINS IN COMPONENT FORM, VW 2180 BEVO FITTED WITH LIMBACH BACKPLATE AND ADDITINAL ELECTRONIC IGNITION. HERCULES PROPELLER FITTED FOURNIER RF5B 12824 LOCKABLE CASTORING TAILWHEEL 360 DEGREE CASTORING TAILWHEEL FOR EASE OF GROUND HANDLING WITH LOCKING FEATURE LIMBACH L2000 E0 SSWV TO ENABLE TAILWHEEL STEERING ON THE GROUND. DESIGN IN ACCORDANCE WITH CLUB FOURNIER INTERNATIONAL DOCUMENT CFI-FAU 07/2003 WEZEL VERSION 1. REF LBA STC NO. PS 0010 695/2. FRED SERIES 3 12888 PROPELLER CHANGE PROPELLER NOW LODGE CJL 124 57 x 31 or Szep 59 x 33 or Szep 56 x 36. ENGINE VW 1776 VW 1776 USTY FRED SERIES 3 13844 INSTALLATION OF ELEVATOR TRIM TAB INSTALLATION OF AN ELEVATOR TRIM TAB, MOUNTED TO THE PORT ELEVATOR'S TRAILING EDGE VW 1834 BWAP AND PILOT OPERATED BY A COCKPIT MOUNTED LEVER VIA A PUSH-PULL CABLE. GLASAIR II-S FT 12643 INSTALLATION OF GROVE ALUMINIUM INSTALLATION OF GROVE ALUMINIUM UNDERCARRIAGE LEGS IN PLACE OF ORIGINAL GLASSFIBRE LYCOMING IO-360-B1E LAIR UNDERCARRIAGE LEGS. LEGS. GLASAIR II-S FT 12644 PROPELLER CHANGE TO HARTZELL HC- CHANGE TO HARTZELL HC-C2YR-1BFP/F7497, 74 INCH DIAMETER HYDRAULIC CONSTANT SPEED LYCOMING IO-360-B1E LAIR C2YR-1BFP/F7497 PROPELLER. GLASAIR II-S FT 12742 INSTALLATION OF AUTO PILOT WING NAVAID DEVICES AP-1 AND S2 WING LEVELLER FITTED PER APPLICANT'S DRAWINGS SUPPLIED LYCOMING IO-360-B1E LAIR LEVELLER GLASAIR IIS RG 14824 HARTZELL HC-F2YC-1F/F7663D-4 72" INSTALLATION OF HARTZELL HC-F2YC-1F/F7663D-4 72" DIAMETER PROPELLER. LYCOMING IO-320-D1A BUBT DIAMETER PROPELLER INSTALLATION GLASAIR RG 13993 RUDDER/AILERON INTERLINK SPRING INTERLINK SYSTEM INTRODUCED AS PART OF NIGHT IFR ACCEPTANCE PACKAGE, TO LYCOMING O-320-D1A TRUK IMPROVE APPARENT LATERAL STABILITY GLASAIR RG 14265 UNDERWING HEATED PITOT HEAD AND INSTALLATION OF PH502-12 WING MOUNTED HEATED PITOT HEAD AND STANDARD FUSELAGE LYCOMING O-320-D1A TRUK FUSELAGE MOUNTED STATIC AND MOUNTED STATIC SOURCE. ALTERNATE SOURCE INSTALLATIONS GLASAIR SUPER IIS RG 12925 FUEL SELECTOR VALVE SUBSTITUTION OF KIT SUPPLIED FUEL SELECTOR VALVE WITH ANDAIR FS20X2-FMF FUEL SELECTOR LYCOMING IO-360-B1E CDAB VALVE. GLASAIR SUPER IIS RG 12926 ELEVATOR TRIM CABLE SUBSTITUTION OF KIT SUPPLIED 3/32" DIAMETER 7X7 ELEVATOR TRIM CABLE WITH 1/16" 7X7 LYCOMING IO-360-B1E CDAB CABLE GLASAIR SUPER IIS RG 12927 LANDING GEAR WARNING HORN SYSTEM INSTALLATION OF THROTTLE OPERATED MICRO SWITCH INTO UNDERCARRIAGE-UP WARNING LYCOMING IO-360-B1E CDAB SYSTEM TO PREVENT HORN SOUNDING AFTER UNDERCARRIAGE IS SELECTED UP WHEN FLAPS ARE STILL DEPLOYED WITH WIDE OPEN THROTTLE, TYPICALLY DURING INITIAL CLIMB AFTER TAKE-OFF.

GLASAIR SUPER IIS RG 13818 S-TEC DUAL AXIS AUTO-PILOT S-TEC DUAL AXIS AUTO-PILOT INSTALLED IN ACCORDANCE WITH STODDARD HAMILTON LYCOMING IO-360-B1E CDAB INSTALLATION INSTRUCTIONS. ROLL SERVO MOUNTED IN PORT WING TO OPERATE AILERON CONTROL VIA PUSH- ROD. PITCH CAPSTAN SERVO MOUNTED IN REAR FUSELAGE TO DRIVE PITCH IDLER VIA CABLES. PITCH TRIM SERVO SPEED SLOWED TO 10 SECONDS FOR FULL TRIM RANGE USING A MAPLIN WC76H PULSE WIDTH MODULATOR.

Prototype mods that have been approved since 1/1/2008 Page 46 30/11/20 LAA Technical Leaflet TL 3.17 GLASAIR SUPER IIS RG 13974 FITMENT OF GARMIN G3X TOUCH AUTO- GARMIN G3X TOUCH DUAL AXIS AUTO-PILOT INSTALLATION. SUPERIOR XP-IO-360-B1A2 LASR PILOT PITCH SERVO ATTACHED TO GARMIN MOUNTING BRACKET RIVETED TO 2MM THICK ALUMINIUM PLATED EMBEDDED IN GRP REINFORCED PAD ON FUSELAGE FLOOR PREVIOUSLY OCCUPIED BY S- TEC 60-2 AUTO-PILOT COMPUTER UNITS. PUSH-ROD ATTACHED TO PITCH CONTROL SYSTEM IDLER IN REAR FUSELAGE. ROLL SERVO IN PORT WING MOUNTED TO PLATE SUPPORTED BETWEEN BRACKETS PREVIOUSLY INSTALLED FOR THE REMOVED S-TEC SERVO MOULDED INTO THE UPPER AND LOWER WING SKINS. PUSH-ROD ATTACHED TO AILERON BELLCRANK. GLASAIR SUPER IIS RG 14936 ELECTRONIC IGNITION IN PLACE OF ONE SUREFLY ELECTRONIC IGNITION FITTED IN PLACE OF ONE OF THE MAGNETOS. THIS IS A DIRECT SUPERIOR XP-IO-360-B1A2 LASR MAGNETO BOLT-IN REPLACEMENT UNIT FOR ONE OF THE MAGNETOS BUT REQUIRES ELECTRICAL POWER FROM THE 12 VOLT BUS. GLASSAIR SUPER II-SRG 12885 PROPELLER CHANGE TO MT MTV-12-B/183-59B INSTALLED ON LYCOMING IO-360-B1E. LYCOMING IO-360-B1E OPNH GLASTAR 13404 MTV-7-D/170-112 PROPELLER INSTALLATION OF MTV-7-D/170-112 ELECTRICALLY IN-FLIGHT ADJUSTABLE PROPELLER USING MT P- CONTINENTAL IO-240-B BYEK INSTALLATION. 120-U AUTOMATIC CONTOLLER. GLASTAR 13515 RELOCATE/REPLACE BATTERY BATTERY RELOCATED TO FIREWALL USING CONVENTIONAL BATTERY BOX INSTALLATION, TO CONTINENTAL IO-240-B BYEK IMPROVE EMPTY CG POSITION GLASTAR 14124 HERCULES 6953461-S 69" X 53" INSTALLATION OF HERCULES 6953461-S 69" X 53" PROPELLER CONTINENTAL IO-240-B BYEK PROPELLER INSTALLATION GLASTAR 12592 INSTALLATION OF NAVAID DEVICES AP-1 WING LEVELLER DEVICE FITTED. SERVO MOUNTED ON ALUMINIUM ALLOY BRACKETS ATTACHED LYCOMING O-320-D2A SACH AUTOPILOT AND S-2 SERVO TO THE CONTROL . ACTUATOR ARM CONNECTS SERVO TO STARBOARD AILERON HORN VIA A SPINDLE AND CRANK. GLASTAR 13804 JPI FS-450 FUEL FLOW MONITORING INSTALLATION OF A JPI FS-450 FUEL FLOW MONITORING SYSTEM USING A FLOSCAN 231 LYCOMING O-320-D2G SKUA SYSTEM TRANSDUCER. GLASTAR 12794 PROPELLER REPITCHED TO 56" PROPELLER NOW SENSENICH 74DM7S16-0-56 LYCOMING O-320-D2J MHGS GLASTAR 14004 DYNON D10A DUAL AXIS AUTOPILOT INSTALLATION OF DYNON D10A DUAL AXIS AUTO-PILOT USING CAPSTAN SERVOS IN ACCORDANCE LYCOMING O-320-D3G CBAR INSTALLATION WITH GLASAIR SPORTSMAN AUTOPILOT INSTALLATION MANUAL AND DYNON AUTOPILOT SERVO INSTALLATION GUIDE (CAPSTAN) DOCUMENT 101385-000, REVISION D, MOUNTED ON CUSTOM MADE MOUNTING PLATE AND BRACKETS. GLASTAR 15166 BOOST PUMP ADDED FACET 40108 FUEL BOOST PUMP ADDED TO FUEL SYSTEM, INCLUDING ASSOCIATED WIRING, LYCOMING O-320-E2D CKZX CIRCUIT BREAKER, SWITCH AND INDICATOR LAMP. FUEL PRESSURE SENSOR CONNECTED TO EFIS.

GLASTAR 14981 FITMENT OF LIESE SILENCER LIESE 60X300-L EXHAUST SILENCER INSTALLED. LYCOMING YO-320-D2A LSTA (MODIFIED) GLASTAR 14357 ENGINE CHANGE TO LYCOMING O-360 . LYCOMING O-360-B1B LSTR B1B GLOBE GC-1B SWIFT 12845 PROPELLER CHANGE TO MCCAULEY PROPELLER CHANGE TO MCCAULEY 1C172/MDM 76 INCH DIAMETER X 59 INCH PITCH ACHIEVED CONTINENTAL O-300-A BFNM 1C172/MDM 76" X 59" BY RE-PITCHING 53 INCH PITCH PROPELLER. GOMHOURIA 181 MK6 13334 SMOKING AIRPLANES SA-100H SMOKE EASILY REMOVABLE INSTALLATION OF SMOKING AIRPLANES SA-100H SMOKE SYSTEM, INCLUDING CONTINENTAL O-300-A TPWX SYSTEM OIL TANK AND ATTACHED PUMP, ON P2 SEAT. TANK ASSEMBLY IS SECURED WITH FABRIC WEBBING STRAP WITH SPRUNG LATCH ROUTED UNDER SEAT PAN AND OVER TANK AND PREVENTED FROM MIGRATING FORWARD OR AFT BY INTEGRALLY MOULDED BOSSES ON TANK TOP SURFACE. P2 SEAT BELTS FASTENED AROUND TANK ASSEMBLY TO ADD SECURITY AND ENSURE NO LOOSE STRAPS. 14959 KIEV 283/1800 PROPELLER INSTALLATION INSTALLATION OF KIEV 283/1800 1800MM DIAMETER 3 BLADED PROPELLER ROTAX 912-ULS RPPO

GROPPO TRAIL 14081 ADDING DOWNWARD POINTING REMOVABLE OBSERVATION PLATFORM FITTED IN REAR OF COCKPIT WITH ASSOCIATED CHANGES ROTAX 912-ULS SMLI CAMERA AND LIDAR, AND SIDEWAYS TO FUSELAGE STRUCTURE TO ALLOW APERTURES IN THE FLOOR AND PORT SIDE FOR TRACKING POINTING CAMERA GIMBAL PURPOSES. RE-ROUTE PORT RUDDER CABLE AND RE-LOCATE FLAP MOTOR TO MAKE SPACE FOR EQUIPMENT. GROPPO TRAIL 14372 ATTACHMENT OF WILDLIFE TRACKING & ANTENNAS FITTED TO WING STRUT AND WING TIP. WING STRUT ANTENNA IS A DIRECTIONAL 148 ROTAX 912-ULS SMLI DOWNLOAD ANTENNAS MHz DIPOLE WHILE ANTENNA IN WING TIP IS A 2.4 GHz PANEL ANTENNA. Prototype mods that have been approved since 1/1/2008 Page 47 30/11/20 LAA Technical Leaflet TL 3.17 GROPPO TRAIL 14373 FITTING OF 2 AXIS AUTOPILOT AS PER INSTALLATION OF MGL SERVOS AND ASSOCIATED LINKAGES TO AILERON AND ELEVATOR ROTAX 912-ULS SMLI MANUFACTURERS DESIGN CONTROLS TO PROVIDE DUAL AXIS AUTOPILOT WHEN CONNECTED TO MGL iEFIS AS ALREADY INSTALLED. GROPPO TRAIL 14204 AVEO POWERBURST NAV/STROBE AVEO POWERBURST NAV/STROBE LIGHTS FITTED TO WINGTIPS USING M3 RIVNETS AND SCREWS. ROTAX 912-ULS ROPO LIGHTS AVEO POSISTROBE XP POSITION/STROBE LIGHT FITTED TO TOP OF RUDDER FAIRING USING M3 RIVNUTS AND STROBES. INSTALLED AS PER MANUFACTURER'S INSTRUCTIONS, INCLUDING ASSOCIATED SWITCHING, FUSES AND WIRING.

GROPPO TRAIL 13648 LEADING EDGE WINDSCREEN COSMETIC IMPROVEMENT TO ATTACHMENT OF WINDSCREEN LIP SAUER S 2400 UL ROFS ATTACHMENT GROPPO TRAIL 13899 PROPELLER CHANGE TO HERCULES ALTERNATIVE HERCULES 6238333-S PROPELLER INSTALLED SAUER S 2400 UL ROFS 6238333-S GROPPO TRAIL 14302 CURVED AILERON CONNECTING BAR INSTALLATION OF A GROPPO DESIGNED AND MANUFACTURED CURVED SQUARE SECTION BAR TO SAUER S 2400 UL ROFS CONNECT THE AILERON CONTROLS WITHIN THE COCKPIT TO INCREASE HEAD CLEARANCE.

GROPPO TRAIL 14090 HERCULES 6238333-S 62" X 38" INSTALLATION OF HERCULES 6238333-S 62 INCH DIAMETER X 38 INCH PITCH PROPELLER SAUER S 2400 UL ROPP PROPELLER INSTALLATION GROPPO TRAIL MK2 14081 ADDING DOWNWARD POINTING REMOVABLE OBSERVATION PLATFORM FITTED IN REAR OF COCKPIT WITH ASSOCIATED CHANGES ROTAX 912-ULS SMLZ CAMERA AND LIDAR, AND SIDEWAYS TO FUSELAGE STRUCTURE TO ALLOW APERTURES IN THE FLOOR AND PORT SIDE FOR TRACKING POINTING CAMERA GIMBAL PURPOSES. RE-ROUTE PORT RUDDER CABLE AND RE-LOCATE FLAP MOTOR TO MAKE SPACE FOR EQUIPMENT. GROPPO TRAIL MK2 15182 INSTALLATION OF FUEL FLOWMETER JP INSTRUMENTS FS-450 FUEL FLOW TRANSDUCER INSTALLED IN FUEL SYSTEM BETWEEN ROTAX 912-ULS CLCO MECHANICAL FUEL PUMP AND CARBURETTORS. HAL-26 PUSH PAK 14878 HERCULES 7045261-S 70" X 45" INSTALLATION OF HERCULES 7045261-S 70 INCH DIAMETER X 45 INCH PITCH PROPELLER. CONTINENTAL C90-8F AVPO PROPELLER INSTALLATION HAPI CYGNET SF-2A 12584 ENGINE CHANGE TO ROTAX 912-UL. CHANGE OF ENGINE TO ROTAX 912-UL WITH EUROPA CLASSIC ENGINE MOUNTING FRAME, ROTAX 912-UL BYYC EUROPA XS EXHAUST SYSTEM AND WARP DRIVE 2 BLADED 68 INCH DIAMETER PROPELLER. HATZ CB-1 12965 PROPELLER CHANGE TO LODGE CJL 104 INSTALLATION OF LODGE CJL 104 74 INCH DIAMETER X 54 INCH PITCH PROPELLER. LYCOMING O-320-A2B BXXH 74" X 54" IKARUS C42 FB UK 13656 ROTAX 912-UL AND KIEV 263/1700 INSTALLATION OF ROTAX 912-UL ENGINE AND KIEV 263/1700 X 24 DEGREES PITCH AT 35CM ROTAX 912-UL CBJW PROPELLER INSTALLATIONS RADIUS PROPELLER IKARUS C42 FB UK 13656 ROTAX 912-UL AND KIEV 263/1700 INSTALLATION OF ROTAX 912-UL ENGINE AND KIEV 263/1700 X 24 DEGREES PITCH AT 35CM ROTAX 912-UL GSCV PROPELLER INSTALLATIONS RADIUS PROPELLER IKARUS C42 FB UK 13450 FIT JUNKERS BRS TO ICARUS & INCREASE BALLISTIC CHUTE INSTALLATION AND MAX GROSS WEIGHT INCREASE TO 473 Kg, UNDERCARRIAGE ROTAX 912-UL GSCV MAUW TO 473KG BOLTS UPRATED PER BMAA AAN 1044 IKARUS C42 FB UK 14679 ENGINE CHANGE TO ROTAX 912-F3 ENGINE CHANGED TO ROTAX 912-F3; ORIGINAL WARPDRIVE 3 BLADED 68" X 25° PROPELLER ROTAX 912-UL NDPA INSTALLED. IKARUS C42 FB UK 15476 IGNITECH SMD MODULES TWIN IGNITECH IGNITION MODULES INSTALLED TO REPLACE ROTAX MODULES ROTAX 912-UL CDCO IGNITECH LOOM MADE FROM FRNC (FLAME RESISTANT NON CORROSIVE) WIRING

MODULES INSTALLED ON TOP OF FUSELAGE TUBE IN FRONT OF INSTRUMENT PANEL

MODULES ALSO 12V DC POWERED WHEN STARTER MOTOR ENGAGED IKARUS C42 FB UK 12826 PROPELLER CHANGE TO NEUFORM CR3-V-PROPELLER CHANGE TO NEUFORM CR3-V-R2H 170CM DIAMETER, 3 BLADED, HYDRAULIC IN-FLIGHT ROTAX 912-UL CEFA R2H 170CM DIAMETER. ADJUSTABLE PROPELLER. IKARUS C42 FB UK 12830 CATEGORY CHANGE TO GROUP A GROUP A CONFIGURATION ROTAX 912-UL CEFA IKARUS C42 FB UK 13551 CATEGORY CHANGE TO MICROLIGHT RE WEIGH, OBTAIN NOISE CERTIFICATE AND RE PLACARD WITH MIOCROLIGHT PLACARDS PER AAN ROTAX 912-UL CEFA PFA 322-430 issue 9.. MAX EMPTY WEIGHT 268 KG AS MICROLIGHT

Prototype mods that have been approved since 1/1/2008 Page 48 30/11/20 LAA Technical Leaflet TL 3.17 IKARUS C42 FB UK 15449 IGNITECH REPLACEMENT IGNITION TWIN IGNITECH IGNITION MODULES INSTALLED TO REPLACE ROTAX MODULES ROTAX 912-ULS OFBU MODULES MODULES INSTALLED ON CUSTOM TRAY BEHIND INSTRUMENT PANEL ABOVE BATTERY MODULES ALSO 12V DC POWERED WHEN STARTER MOTOR ENGAGED IKARUS C42 FB UK 12308 CATEGORY CHANGE FROM MICROLIGHT CATEGORY CHANGE FROM MICROLIGHT TO GROUP 'A' INCLUDING GROSS WEIGHT INCREASE TO ROTAX 912-ULS GBET TO GROUP 'A' 473KG FOLLOWING INCORPORATION OF FIBERFRAX FIREWALL MATERIAL, PITOT DRAIN AND ASI CORRECTION PLACARD. IKARUS C42 FB UK 12313 CHANGE OF PROPELLER TO ARPLAST PROPELLER CHANGE TO ARPLAST ECOPROP 170R130/3 ROTAX 912-ULS GBET ECOPROP 170R130/3 IKARUS C42 FB UK 13358 CATEGORY CHANGE TO MICROLIGHT CATEGORY CHANGE TO C42 FB UK ROTAX 912-ULS GBET IKARUS C42 FB UK 13450 FIT JUNKERS BRS TO ICARUS & INCREASE BALLISTIC CHUTE INSTALLATION AND MAX GROSS WEIGHT INCREASE TO 473 Kg, UNDERCARRIAGE ROTAX 912-ULS ICRS MAUW TO 473KG BOLTS UPRATED PER BMAA AAN 1044 IKARUS C42 FB UK 14622 REFURBISH FUSELAGE WITH VINYL WRAP WRAPPING OF NON-STRUCTURAL AIRFRAME PARTS (ENGINE COWLING, COCKPIT ROOF, HATCHES, ROTAX 912-ULS OVLA FINISH UPPER AND LOWER FUSELAGE SHELLS, COCKPIT BASE, WHEEL SPATS) WITH HEXIS HX20000 VINYL FILM. IKARUS C42 FB UK 12667 CATEGORY CHANGE TO MICROLIGHT CATEGORY CHANGE AS C42 FB UK ROTAX 912-ULS INJA IKARUS C42 FB UK 14749 KIEV 283/1800 X 24 DEGREES PITCH AT INSTALLATION OF KIEV 283/1800 X 24 DEGREES PITCH AT 48.5 CM RADIUS PROPELLER. ROTAX 912-ULS IKUS 48.5 CM RADIUS PROPELLER INSTALLATION IKARUS C42 FB UK 13360 CATEGORY CHANGE TO MICROLIGHT CATEGORY CHANGE TO C42 FB UK ROTAX 912-ULS NSBB IKARUS C42 FB UK 12460 PROPELLER CHANGE TO NEUFORM 3 CHANGE OF PROPELLER TO NEUFORM 3 BLADED 175CM DIAMETER X 27 DEGREES PITCH AT ROTAX 912-ULS CLIF BLADED 175CM DIAMETER 36.5CM RADIUS. ISAACS FURY II 14759 OIL COOLER OIL COOLER MOUNTED TO UNDERSIDE OF FUSELAGE WITH ASSOCIATED HOSES, MOUNTING CONTINENTAL C90-12F AYJY BRACKETS AND CONNECTIONS TO ENGINE. ISAACS FURY II 13917 SPIN-ON OIL FILTER ADAPTER FOR INSTALLATION OF CUSTOM MADE SPIN-ON OIL FILTER ADAPTER P/N 79001003 WITH CHAMPION CONTINENTAL C90-14F BIYK CONTINENTAL PC60 (O-200) CH48108 OR C138 OR BLUE PRINT ADT32109 OIL FILTER.

AT ISSUE 4: APPLICABILITY EXTENDED TO CONTINENTAL C90-12 ENGINE. AT ISSUE 6: APPLICABILITY EXTENDED TO CONTINENTAL C85-12F ENGINE. AT ISSUE 7: APPLICABILITY EXTENDED TO CONTINENTAL C90-14F ENGINE. ISAACS FURY II 14699 INSTALLATION OF HYDRAULIC DISC INDEPENDENT HYDRAULIC DISC BRAKES FITTED. OPERATED BY LEVERS FITTED TO THE RUDDER CONTINENTAL C90-14F EHMF BRAKES PEDALS. INCORPORATES ANTI-ROTATION FEATURE TO PREVENT CALIPERS ROTATING ON AXLE.

ISAACS FURY II 15121 HERCULES 7143788-S 71" x 43" INSTALLATION OF HERCULES 7143788-S 71 INCH DIAMETER X 43 INCH PITCH PROPELLER CONTINENTAL C90-14F EHMF PROPELLER INSTALLATION ISAACS FURY II 13180 SPIN ON OIL FILTER FITTED EXTERNAL SPIN ON OIL FILTER PER STC SE00825W1 LYCOMING O-235-H2C BWWN ISAACS FURY II 12945 MTWA INCREASE & FORWARD CG LIMIT INCREASE IN MAXIMUM TOTAL WEIGHT AUTHORISED FROM 1000LBS TO 1050LBS AND REVISION LYCOMING O-290-3 ASCM REVISION OF CG FORWARD LIMIT FROM 44.0 INCHES FORWARD OF DATUM TO 45.0 INCHES FORWARD OF DATUM. ISAACS FURY II 12946 GT-2/182/VTT-FW5-1/4SRTC PROPELLER INSTALLATION OF GT-2/182/VTT-FW5-1/4SRTC 182CM DIAMETER X 133CM PITCH WOODEN LYCOMING O-290-3 ASCM INSTALLATION PROPELLER. ISAACS FURY II 15261 P-MAG P114-L4 ELECTRONIC IGNITION E-MAG P-MAG P114-L4 ELECTRONIC IGNITION MODULE INSTALLED IN PLACE OF PORT SIDE LYCOMING O-290-3 ASCM UNIT INSTALLATION MAGNETO TO LYCOMING O-290-C ENGINE.

IGNITION ADVANCE SET TO 'A CURVE' ISAACS FURY II 13663 HERCULES 7646385-S 76" x 46" INSTALLATION OF HERCULES 7646385-S 76 INCH DIAMETER x 46 INCH PITCH PROPELLER LYCOMING O-290-D BKFK PROPELLER INSTALLATION ISAACS FURY II 13705 PROPELLER CHANGE TO CHRIS LODGE PROPELLER REPLACED BY LODGE CJL 111 76" x 54" LYCOMING O-320-E2A BBVO DRG 111 ISAACS SPITFIRE 13453 REVISED MAIN UNDERCARRIAGE AND GROVE LEAF SPRING MAIN UNDERCARRIAGE SUBSTITUTED. TWO PIECE MAIN GEAR, EACH BOLTED CONTINENTAL O-200-A ISAC MOUNTING TO SUBSTANTIAL WOOD BLOCKS IN WOOD BOX SPAR OF MAINPLANE Prototype mods that have been approved since 1/1/2008 Page 49 30/11/20 LAA Technical Leaflet TL 3.17 ISAACS SPITFIRE 14170 TAILWHEEL SPRING ARRANGEMENT ORIGINAL TAILWHEEL ARRANGEMENT REPLACED WITH A PAIR OF NESTED EN45 STEEL LEAF CONTINENTAL O-200-A ISAC SPRINGS ATTACHED TO AN ALUMINIUM TAILWHEEL BLOCK. SPRINGS ARE MOUNTED TO THE LOWER VIA A PAIR OF ASH TRANSVERSE MEMBERS, SPRUCE FILLER BLOCKS AND PLY PLATES USING 3/8" BOLTS. ISAACS SPITFIRE 14171 CANOPY FRONT FRAME AND FAIRING PANELS OF SLIDING CANOPY REPLACED WITH STEEL TUBE HOOP CONTINENTAL O-200-A ISAC WHICH PROVIDES WIDER GLAZED CROSS-SECTION AT THE FORWARD PORTION OF THE CANOPY (OVERALL CANOPY WIDTH REMAINS THE SAME). GLAZING ALTERED TO SUIT NEW PROFILE. FRONT WINDSCREEN HOOP ALTERED TO MATCH CANOPY PROFILE. 2 OFF 0.25" DIAMETER LOCATION PINS AND 0.049" 4130 STEEL GUSSETS ADDED TO REAR OF CANOPY TO MATE WITH 4130 STEEL LOCATOR PLATES MOUNTED ON FORWARD FACE OF FUSELAGE FRAME, INCLUDING 3/16" PLY DOUBLER ON AFT FACE OF FRAME AND SECURED WITH 3/16" BOLTS. ISAACS SPITFIRE 14172 CANOPY LATCH CANOPY LATCH RE-DESIGNED TO ALLOW AUTOMATIC LATCHING AND EXTERNAL RELEASE. LATCH CONTINENTAL O-200-A ISAC TAKES THE FORM OF A SPRING-LOADED MECHANISM HINGED TO THE UNDERSIDE OF THE UPPER CANOPY HOOP. IT ENGAGES ON A STRIKER PLATE ON THE FIXED PART (WINDSCREEN HOOP). CANOPY IS RELEASED BY PULLING DOWN ON AN INTERNAL HANDLE OR BY PUSHING DOWN ON AN EXTERNAL BUTTON. PLACARDS INDICATE HOW THE MECHANISM OPERATES. CANOPY HOOP REINFORCED BY WELDING A STEEL PLATE TO THE AFT SIDE IN THE AREA OF THE LATCH MECHANISM. ISAACS SPITFIRE 14190 LITHIUM IRON BATTERY INSTALLATION VARLEY LI-5 LITHIUM IRON PHOSPHATE BATTERY MOUNTED IN 16 SWG ALLOY BATTERY BOX CONTINENTAL O-200-A ISAC MOUNTED ON THE FORWARD FACE OF THE FIREWALL. 14443 PROPELLER CHANGE TO GT-2/151/VZR- GT-2/151/VZR-FW101SRTC FITTED TO JABIRU 2200A ENGINE. JABIRU 2200A CFGH FW101SRTC JABIRU J160 12850 TRUTRAK ADI PILOT 1 AUTO-PILOT (ROLL) INSTALLATION OF TRUTRAK ADI PILOT 1 AUTO-PILOT (ROLL) WITH SERVO MOUNTED TO JABIRU 2200A CFSJ INSTALLATION STRUCTURE BETWEEN SEATS, DRIVING AILERON CABLES VIA ADDITIONAL BELLCRANK BRACKET PT. NO. 1450-066 AND PROTECTED WITH COVER BOLTED IN PLACE. JABIRU J160 12850 TRUTRAK ADI PILOT 1 AUTO-PILOT (ROLL) INSTALLATION OF TRUTRAK ADI PILOT 1 AUTO-PILOT (ROLL) WITH SERVO MOUNTED TO JABIRU 2200A CIBU INSTALLATION STRUCTURE BETWEEN SEATS, DRIVING AILERON CABLES VIA ADDITIONAL BELLCRANK BRACKET PT. NO. 1450-066 AND PROTECTED WITH COVER BOLTED IN PLACE. JABIRU J400 12725 INSTALLATION OF VORTEX GENERATORS STOLSPEED VORTEX GENERATORS INSTALLED ON WING UPPER SURFACE AND TAILPLANE LOWER CAMIT CAE 3300 KEVI SURFACE IN ACCORDANCE WITH 'INSTRUCTIONS FOR INSTALLING STOLSPEED VGs ON YOUR AIRCRAFT' AND MOD 12725 FIGS 1 AND 2 TO IMPROVE PERFORMANCE AND HANDLING.

JABIRU J400 14365 ENGINE CHANGE TO CAMIT CAE3300 CAMIT CAE 3300 ENGINE SUBSTIUTED CAMIT CAE 3300 KEVI JABIRU J400 12296 ANALOGUE OIL PRESSURE GAUGE UMA OIL PRESSURE GAUGE INSTALLED ON INSTRUMENT PANEL. FEED FOR PRESSURE LINE TEED JABIRU 3300A SAZY INTO POSITION AT OIL PRESSURE SWITCH ADJACENT TO OIL FILTER POSITION USING AN FITTINGS.

JABIRU J400 12297 COWL COOLNG AIR INTAKES FITMENT OF 'EYEBROWS' TO UPPER EDGE OF COWLING INTAKE EACH SIDE TO PROMOTE BETTER JABIRU 3300A SAZY FLOW OF AIR OVER CYLINDER HEADS AT HIGH ANGLES OF ATTACK. COWL RE-MADE TO INCORPORATE THESE FEATURES. JABIRU J400 12725 INSTALLATION OF VORTEX GENERATORS STOLSPEED VORTEX GENERATORS INSTALLED ON WING UPPER SURFACE AND TAILPLANE LOWER JABIRU 3300A SAZY SURFACE IN ACCORDANCE WITH 'INSTRUCTIONS FOR INSTALLING STOLSPEED VGs ON YOUR AIRCRAFT' AND MOD 12725 FIGS 1 AND 2 TO IMPROVE PERFORMANCE AND HANDLING.

JABIRU J400 13009 BERINGER MAIN WHEELS AND BRAKES BERINGER MAIN WHEELS, AXLES AND BRAKES SUBSTITUTED WITH 5.00 x 5 10 PLY TYRES AND JABIRU 3300A SAZY SUBSTITUTED BRAKE PRESSURE LIMITER VALVE PER BERINGER INSTALLATION INSTRUCTIONS AND WHEEL AXLE CALCULATION

Prototype mods that have been approved since 1/1/2008 Page 50 30/11/20 LAA Technical Leaflet TL 3.17 JABIRU J400 14367 REPLACEMENT OIL COOLER ORIGINAL OIL COOLER REPLACED WITH MOCAL 7 ROW X 235 MM WIDE X 51 MM DEEP. COOLER IS JABIRU 3300A JABJ MOUNTED BELOW THE ENGINE SUMP, AS PER THE ORIGINAL, USING ALLOY BRACKETS. THE NEW COOLER IS PERPENDICULAR TO THE AXIS OF THE ENGINE, RATHER THAN RACKED BACK AT AN ANGLE. HOSES ARE UPGRADED TO 1/2" DIAMETER FROM 3/8" DIAMETER AS PER THE ENGINE MANUFACTURER'S RECOMMENDATION. JABIRU J400 13010 DYNON D10A/AP74 AUTO-PILOT (ROLL) INSTALLATION OF DYNON ROLL CONTROL AUTO-PILOT SERVO TO CENTRAL TUNNEL ACTUATING A JABIRU 3300A OZIE SYSTEM DRIVE PLATE TO OPERATE THE AILERON CONTROL CABLES. DYNON AP74 CONTROLLER USED WITH D10A EFIS. JABIRU J400 12725 INSTALLATION OF VORTEX GENERATORS STOLSPEED VORTEX GENERATORS INSTALLED ON WING UPPER SURFACE AND TAILPLANE LOWER JABIRU 3300A CDLS SURFACE IN ACCORDANCE WITH 'INSTRUCTIONS FOR INSTALLING STOLSPEED VGs ON YOUR AIRCRAFT' AND MOD 12725 FIGS 1 AND 2 TO IMPROVE PERFORMANCE AND HANDLING.

JABIRU J400 13997 ENGINE CHANGE TO CAMit CAE 3300 JABIRU 3300A ENGINE REPLACED BY CAMIT CAE 3300 JABIRU 3300A CDLS JABIRU J400 13009 BERINGER MAIN WHEELS AND BRAKES BERINGER MAIN WHEELS, AXLES AND BRAKES SUBSTITUTED WITH 5.00 x 5 10 PLY TYRES AND JABIRU 3300A JJAB SUBSTITUTED BRAKE PRESSURE LIMITER VALVE PER BERINGER INSTALLATION INSTRUCTIONS AND WHEEL AXLE CALCULATION JABIRU J400 12725 INSTALLATION OF VORTEX GENERATORS STOLSPEED VORTEX GENERATORS INSTALLED ON WING UPPER SURFACE AND TAILPLANE LOWER JABIRU 3300A CDUT SURFACE IN ACCORDANCE WITH 'INSTRUCTIONS FOR INSTALLING STOLSPEED VGs ON YOUR AIRCRAFT' AND MOD 12725 FIGS 1 AND 2 TO IMPROVE PERFORMANCE AND HANDLING.

JABIRU J400 13685 AUTO PILOT PITCH AND ROLL (WITH TRIAL FIT OF PITCH AND ROLL AUTOPILOT. AFTER UNSUCCESSFUL TRIALS, PITCH AND ROLL SERVOS JABIRU 3300A GRLW SERVOS REMOVED) AND ASSOCIATED PUSHRODS REMOVED, LEAVING ONLY REDUNDANT AUTO PILOT HEAD AND SWITCH ON INSTRUMENT PANEL, REDUNDANT SERVO MOUNTING PADS AND REDUNDANT DRIVE ARM ON AILERON BELLCRANK IN PLACE. AUTOPILOT CONTROL UNIT AND SWITCH ON PANEL MARKED AS UNSERVICABLE JABIRU J400 12725 INSTALLATION OF VORTEX GENERATORS STOLSPEED VORTEX GENERATORS INSTALLED ON WING UPPER SURFACE AND TAILPLANE LOWER JABIRU 3300A GRLW SURFACE IN ACCORDANCE WITH 'INSTRUCTIONS FOR INSTALLING STOLSPEED VGs ON YOUR AIRCRAFT' AND MOD 12725 FIGS 1 AND 2 TO IMPROVE PERFORMANCE AND HANDLING.

JABIRU J400 12396 TRUTRAK ADI PILOT 1 WING LEVELLER INSTALLATION OF TRUTRAK ADI PILOT 1 WING LEVELLER DEVICE. SERVO CONNECTED TO THE JABIRU 3300A RTFM COMMON DRIVE PLATE ON THE CONTROL COLUMN LINK VIA A PUSH ROD. JABIRU J400 12404 RETRO FIT AUTOPILOT (TRUTRAK) TRUTRAK ADI PILOT 1 WING-LEVELLER FITTED. SERVO CONNECTED TO BELLCRANK AT AFT END OF JABIRU 3300A SIZZ CONTROL COLUMN. JABIRU J400 12725 INSTALLATION OF VORTEX GENERATORS STOLSPEED VORTEX GENERATORS INSTALLED ON WING UPPER SURFACE AND TAILPLANE LOWER JABIRU 3300A SIZZ SURFACE IN ACCORDANCE WITH 'INSTRUCTIONS FOR INSTALLING STOLSPEED VGs ON YOUR AIRCRAFT' AND MOD 12725 FIGS 1 AND 2 TO IMPROVE PERFORMANCE AND HANDLING.

JABIRU J400 13009 BERINGER MAIN WHEELS AND BRAKES BERINGER MAIN WHEELS, AXLES AND BRAKES SUBSTITUTED WITH 5.00 x 5 10 PLY TYRES AND JABIRU 3300A SIZZ SUBSTITUTED BRAKE PRESSURE LIMITER VALVE PER BERINGER INSTALLATION INSTRUCTIONS AND WHEEL AXLE CALCULATION JABIRU J400 12725 INSTALLATION OF VORTEX GENERATORS STOLSPEED VORTEX GENERATORS INSTALLED ON WING UPPER SURFACE AND TAILPLANE LOWER JABIRU 3300A REAF SURFACE IN ACCORDANCE WITH 'INSTRUCTIONS FOR INSTALLING STOLSPEED VGs ON YOUR AIRCRAFT' AND MOD 12725 FIGS 1 AND 2 TO IMPROVE PERFORMANCE AND HANDLING.

JABIRU J430 13574 FUEL FLOW MONITORING SYSTEM INSTALLATION OF FUEL FLOW MONITORING SYSTEM USING FLOSCAN 201A-6 TRANSDUCER AND JABIRU 3300A CCID INSTALLATION MGL ENIGMA EMS. 13010 DYNON D10A/AP74 AUTO-PILOT (ROLL) INSTALLATION OF DYNON ROLL CONTROL AUTO-PILOT SERVO TO CENTRAL TUNNEL ACTUATING A JABIRU 3300A MUTZ SYSTEM DRIVE PLATE TO OPERATE THE AILERON CONTROL CABLES. DYNON AP74 CONTROLLER USED WITH D10A EFIS.

Prototype mods that have been approved since 1/1/2008 Page 51 30/11/20 LAA Technical Leaflet TL 3.17 JABIRU J430 13009 BERINGER MAIN WHEELS AND BRAKES BERINGER MAIN WHEELS, AXLES AND BRAKES SUBSTITUTED WITH 5.00 x 5 10 PLY TYRES AND JABIRU 3300A MUTZ SUBSTITUTED BRAKE PRESSURE LIMITER VALVE PER BERINGER INSTALLATION INSTRUCTIONS AND WHEEL AXLE CALCULATION JABIRU J430 12393 FLAP SPEED WARNER WARNING DEVICE INSTALLED SUCH THAT WHEN FLAPS ARE DEPLOYED (AS SENSED BY A JABIRU 3300A CEKW MICROSWITCH) AND WHEN AIRSPEED IS TOO HIGH (AS SENSED BY AN AIR PRESSURE SWITCH) A BUZZER SOUNDS. THE SYSTEM IS POWERED BY A SEPARATE 9V BATTERY. JABIRU J430 14633 MAGNECOR HT LEADS Standard Jabiru ignition leads replaced by equivalent Magnecore 7mm Electrosport HT leads for JABIRU 3300A CEKW reduced electrical interference with radios. JABIRU J430 15307 AUTOPILOT INSTALLATION OF TRUTRAK ADI PILOT 1 WING LEVELLING AUTO-PILOT WITH SERVO MOUNTED TO JABIRU 3300A CEFP CENTRAL TUNNEL DIRECTLY UNDER AILERON CONTROL BELLCRANK JABIRU J430 13009 BERINGER MAIN WHEELS AND BRAKES BERINGER MAIN WHEELS, AXLES AND BRAKES SUBSTITUTED WITH 5.00 x 5 10 PLY TYRES AND JABIRU 3300A RCST SUBSTITUTED BRAKE PRESSURE LIMITER VALVE PER BERINGER INSTALLATION INSTRUCTIONS AND WHEEL AXLE CALCULATION JABIRU J430 13010 DYNON D10A/AP74 AUTO-PILOT (ROLL) INSTALLATION OF DYNON ROLL CONTROL AUTO-PILOT SERVO TO CENTRAL TUNNEL ACTUATING A JABIRU 3300A JABU SYSTEM DRIVE PLATE TO OPERATE THE AILERON CONTROL CABLES. DYNON AP74 CONTROLLER USED WITH D10A EFIS. JABIRU J430 12399 PROPELLER CHANGE TO SENSENICH PROPELLER CHANGE TO SENSENICH 'EZ-PITCH' 2A0J5R64ZN 60" DIAMETER SET AT 21 DEGREES AT JABIRU 3300A CEPM 2A0J5R64ZN 60" DIA 70% RADIUS. JABIRU J430 14932 CAMIT FLYWHEEL CLAMP REVISED CLAMP ARRANGEMENT TO BETTER RETAIN FLYWHEEL JABIRU 3300A KIDD

NOTE: APPLICABLE TO 1/4" AND 5/16", BUT NOT 3/8", BOLT JABIRU J430 11943 TRUTRAK ADI PILOT 1 / DIGITRAK WING INSTALLATION OF TRUTRAK ADI PILOT 1 OR DIGITRAK WING LEVELLING AUTO-PILOT WITH SERVO JABIRU 3300A LUBY LEVELLING AUTO-PILOT MOUNTED TO CENTRAL TUNNEL DIRECTLY UNDER AILERON CONTROL BELLCRANK JABIRU J430 13009 BERINGER MAIN WHEELS AND BRAKES BERINGER MAIN WHEELS, AXLES AND BRAKES SUBSTITUTED WITH 5.00 x 5 10 PLY TYRES AND JABIRU 3300A CFZD SUBSTITUTED BRAKE PRESSURE LIMITER VALVE PER BERINGER INSTALLATION INSTRUCTIONS AND WHEEL AXLE CALCULATION JABIRU J430 12995 FUEL PUMP AND FILTER REPOSITION STANDARD KIT ELECTRIC FUEL PUMP AND FILTER RELOCATED TO UNDER PILOT'S SEAT. JABIRU 3300A OHRA JABIRU J430 15112 WINDSCREEN DEMISTER INSTALLATION DUCTING WITH PILOT OPERATED VALVE TO PROVIDE WARM AIR ALONG LOWER EDGE OF JABIRU 3300A OHRA WINDSCREEN. JABIRU J430 15113 PROPELLER FLANGE ATTACHMENT WITH LONG PROPELLER FLANGE SECURED TO CRANKSHAFT WITH 6 OFF MS21250-06006 3/8 INCH UNF JABIRU 3300A OHRA MS21250 BOLTS AND NORD-LOCK NL11 12 POINT BOLTS WITH NORD-LOCK NL11 WASHERS UNDER THE HEADS INSTEAD OF NAS1351 3/8 WASHERS INCH UNF SOCKET HEAD CAP SCREWS SECURED WITH LOCTITE 620. JABIRU J430 13182 WING LEVELLER WING LEVELLER TYPE DYNON AP74 FITTED JABIRU 3300A ROOO JABIRU SK 14454 ENGINE CHANGE TO CAMIT CAE2200 ENGINE REPLACED WITH CAMIT CAE 2200 CAMIT CAE 2200 EWBC JABIRU SK 14513 PANEL MOUNTED THROTTLE CONTROL RELOCATION OF THROTTLE CONTROL TO SIDE OF INSTRUMENT PANEL, USING COMMERCIALLY CAMIT CAE 2200 EWBC INSTALLATION AVAILABLE MULTI-CORE PUSH-PULL CABLE AND CUSTOM MADE ALUMINIUM ALLOY BRACKET.

JABIRU SK 12787 NEWTON TYPE 11R 60" X 43" PROPELLER PROPELLER CHANGE TO NEWTON TYPE 11R 60 INCH DIAMETER X 43 INCH PITCH. JABIRU 2200A THOT

JABIRU SK 14932 CAMIT FLYWHEEL CLAMP REVISED CLAMP ARRANGEMENT TO BETTER RETAIN FLYWHEEL JABIRU 2200A THOT

NOTE: APPLICABLE TO 1/4" AND 5/16", BUT NOT 3/8", BOLT CRANKSHAFTS JABIRU SK 13418 NEWTON 11R 60" X 42" PROPELLER INSTALLATION OF NEWTON TYPE 11R 60 INCH DIAMETER X 42 INCH PITCH PROPELLER. JABIRU 2200A BYNS INSTALLATION. JABIRU SK 10479 TWIN THROTTLE TWIN PLUNGER TYPE THROTTLE CONTROLS, ONE EACH INSTALLED TO EACH OUTBOARD SIDE OF JABIRU 2200A BYBZ INSTRUMENT PANEL. JABIRU SK 13660 BELT DRIVEN EXTERNAL 40 AMP INSTALLATION OF BELT DRIVEN BRIGGS AND STRATTON 825524 ALTERNATOR MOUNTED TO REAR JABIRU 2200A BYBZ ALTERNATOR OF ENGINE WITH MOUNTING KIT DESIGNED AND SUPPLIED BY CAMIT - MANUFACTURER OF JABIRU ENGINES.

Prototype mods that have been approved since 1/1/2008 Page 52 30/11/20 LAA Technical Leaflet TL 3.17 JABIRU SK 14033 FLYWHEEL CRUSH PLATE AND SPACER (IN CIRCULAR STEEL FLYWHEEL CRUSH PLATE AND SPACER ADDED AS LOAD SPREADER. ATTACHMENT JABIRU 2200A BYBZ COMMERCIAL CONFIDENCE) SCREWS LOCKED USING NORDLOCK X SERIES WASHERS RATHER THAN LOCTITE. TORQUE SCREWS TO 24 FT LBS. JABIRU SK 14932 CAMIT FLYWHEEL CLAMP REVISED CLAMP ARRANGEMENT TO BETTER RETAIN FLYWHEEL JABIRU 2200A UKOZ

NOTE: APPLICABLE TO 1/4" AND 5/16", BUT NOT 3/8", BOLT CRANKSHAFTS JABIRU SK 13371 SENSENICH W60HJ-46G INSTALLATION OF SENSENICH W60HJ-46G 60 INCH DIAMETER X 46 INCH PITCH PROPELLER. JABIRU 2200A BYIA JABIRU SP-430 12386 CONVERSION OF UL TO SP-430 UL WINGS REPLACED WITH SK WINGS TO CONVERT JABIRU UL TO SP430. JABIRU 2200A DMAC JABIRU SP-470 13393 INSTALLATION OF MGL AVIONICS FUEL INSTALLATION OF FUEL FLOW MONITORING SYSTEM INCORPORATING MGL DUAL FLOW PLASTIC JABIRU 2200A CCVN FLOW MONITORING SYSTEM BODY FLOW TRANSDUCER WITH LOW FLOW RATE JET FACTORY INSTALLED AND MGL FF-1 FUEL MANAGEMENT COMPUTER JABIRU SP-470 14144 NEWTON 11R 60" x 40" PROPELLER INSTALLATION OF NEWTON 11R 60 INCH DIAMETER X 40 INCH PITCH PROPELLER JABIRU 2200A IPAT INSTALLATION JABIRU SPL-450 13885 CATEGORY CHANGE TO GROUP A CATEGORY CHANGE INVOLVING REDUCTION IN FLAP DEFLECTION TO 33 DEGREES BY ADJUSTMENT JABIRU 2200A BYTV OF PUSHROD IN FLAP SYSTEM JABIRU SPL-450 14221 ENGINE CHANGE TO CAMiT CAE 2200 ENGINE CHANGED TO CAMIT CAE 2200SLRE JABIRU 2200A BYTV SLRE JABIRU SPL-450 13280 STOLSPEED VORTEX GENERATORS STOLSPEED VORTEX GENERATORS INSTALLED ON WING UPPER SURFACE AND TAILPLANE LOWER JABIRU 2200A BYTV SURFACE IN ACCORDANCE WITH 'INSTRUCTIONS FOR INSTALLING STOLSPEED VGs ON YOUR AIRCRAFT' TO IMPROVE PERFORMANCE AND HANDLING. JABIRU SPL-450 13647 CATEGORY CHANGE TO GROUP A FLAP TRAVEL RESTRICTED TO 33 DEGREES JABIRU 2200A BYYL JABIRU SPL-450 13660 BELT DRIVEN EXTERNAL 40 AMP INSTALLATION OF BELT DRIVEN BRIGGS AND STRATTON 825524 ALTERNATOR MOUNTED TO REAR JABIRU 2200A BYYL ALTERNATOR OF ENGINE WITH MOUNTING KIT DESIGNED AND SUPPLIED BY CAMIT - MANUFACTURER OF JABIRU ENGINES. JABIRU SPL-450 10479 TWIN THROTTLE TWIN PLUNGER TYPE THROTTLE CONTROLS, ONE EACH INSTALLED TO EACH OUTBOARD SIDE OF JABIRU 2200A BYYL INSTRUMENT PANEL. JABIRU SPL-450 14801 FUEL SYSTEM MONITORING INSTALLATION OF COMPONENTS TO MONITOR FUEL SYSTEM: JABIRU 2200A BYYL - UL FLIGHT LINE FUEL PRESSURE SENDER & GAUGE - FLOSCAN 201A-6 FUEL FLOW SENDER - FLIGHT DATA SYSTEMS FC-10 FUEL FLOW COMPUTER - VERTICAL FLOAT TANK LEVEL SENDER AND GAUGE JABIRU SPL-450 12900 PROPELLER CHANGE TO NEWTON 11R PROPELLER CHANGE TO NEWTON TYPE 11R 60 INCH DIAMETER X 42 INCH PITCH. JABIRU 2200A BZGT 60" X 42" JABIRU SPL-450 13626 CATEGORY CHANGE TO GROUP A CATEGORY CHANGE TO GROUP A BY REVERTING TO SPL-450 CONFIGURATION WITH REDUCED JABIRU 2200A BZGT FLAP TRAVEL. JABIRU SPL-450 12689 CATEGORY CHANGE TO GROUP A FLAP DEFLECTION ANGLE REDUCED TO STANDARD SHOWN IN JABIRU BUILD MANUAL, NEUTRAL JABIRU 2200A OGSA FLAP POSITION NOW LEVEL JABIRU SPL-450 12919 FIT MGL STRATOMASTER EXTREME STRATOMASTER TRANSDUCER FITTED BETWEEN TANK AND FIREWALL, JABIRU 2200A OGSA JABIRU UL 13541 HERCULES 5840355-S 58" x 40" INSTALLATION OF HERCULES 5840355-S 58 INCH DIAMETER X 40 INCH PITCH PROPELLER. JABIRU 2200A BYJD PROPELLER INSTALLATION JABIRU UL 12429 PROPELLER CHANGE TO GT-2/151/VZR PROPELLER CHANGE TO GT-2/151/VZR. JABIRU 2200A RODG CAA NOISE CERTIFICATE REQUIRED. JABIRU UL-450 10598 TO FIT FULL LENGTH RUDDER ALTERNATIVE FULL HEIGHT RUDDER 2068002 FITTED USING JABIRU OPTION KIT AND JABIRU JABIRU 2200A BYYT OPTION FITTING INSTRUCTIONS REF SP-3. JABIRU UL-450 14188 HERCULES 5840355-S PROPELLER INSTALLATION OF HERCULES 5840355-S 58 INCH DIAMETER X 40 INCH PITCH PROPELLER JABIRU 2200A ODGS INSTALLATION JABIRU UL-450 13177 CATEGORY CHANGE TO SPL-450 FLAP TRAVEL REDUCED To 33 DEGREES JABIRU 2200A KKER JABIRU UL-450 14088 CATEGORY CHANGE TO MICROLIGHT UL- CATEGORY CHANGE TO MICROLIGHT AS UL-450 BY INCREASING FLAP DEFLECTION AND OBTAINING JABIRU 2200A KKER 450 NOISE CERTIFICATE AND AMENDING PLACARDS FOLLOWING RE-WEIGH. NEW PERMIT TOF LY AND OPERATING LIMITATIONS ISSUED

Prototype mods that have been approved since 1/1/2008 Page 53 30/11/20 LAA Technical Leaflet TL 3.17 JABIRU UL-450 13564 CATEGORY CHANGE TO GROUP A CATEGORY CHANGE TO SEP AEROPLANE WITH REDUCED MAX FLAP DEFLECTION OF 33 DEGREES JABIRU 2200A LEEE AND DESIGNATED SPL-450 JABIRU UL-450 14014 CATEGORY CHANGE TO MICROLIGHT CATEGORY CHANGE TO MICROLIGHT AND DESIGNATION TO UL-450 BY INCREASING FLAP JABIRU 2200A LEEE DEFLECTION AND FITTING MICROLIGHT WEIGHT PLACARD. NOISE CERTIFICATE ISSUED. JABIRU UL-450 13280 STOLSPEED VORTEX GENERATORS STOLSPEED VORTEX GENERATORS INSTALLED ON WING UPPER SURFACE AND TAILPLANE LOWER JABIRU 2200A LEEE SURFACE IN ACCORDANCE WITH 'INSTRUCTIONS FOR INSTALLING STOLSPEED VGs ON YOUR AIRCRAFT' TO IMPROVE PERFORMANCE AND HANDLING. JABIRU UL-450 10659 TO INSTALL CABIN ROOF WINDOW CABIN ROOF WINDOW BONDED INTO STRUCTURE. JABIRU 2200A JAXS

MODIFICATION NOW SERIES APPROVED TO BE FITTED TO ALL UL, SP, SP-450 AND SK VARIANTS.

MODIFICATION KIT MANUFACTURED BY D&J ENGINEERING.

JABIRU UL-450 13731 CATEGORY CHANGE TO MICROLIGHT FLAP SETTING CHANGED TO GIVE 37-38 DEGREES DEFLECTION TO ALLOW AIRCRAFT TO QUALIFY AS JABIRU 2200A BZIV MICROLIGHT CATEGORY WITH . NOISE CERTIFICATE OBTAINED AND PLACARDS UPDATED. AIRCRAFT RE-WEIGHED. JABIRU UL-450 14012 CATEGORY CHANGE TO MICROLIGHT CATEGORY CHANGE TO MICROLIGHT BY INCREASING FLAP DEFLECTION TO REDUCE STALL SPEED JABIRU 2200A JSPL AND DESIGNATION UL-450 AND FITTING MICROLIGHT PLACARDS, NOISE CERTIFICATE ISSUED JABIRU UL-450 13280 STOLSPEED VORTEX GENERATORS STOLSPEED VORTEX GENERATORS INSTALLED ON WING UPPER SURFACE AND TAILPLANE LOWER JABIRU 2200A CBOP SURFACE IN ACCORDANCE WITH 'INSTRUCTIONS FOR INSTALLING STOLSPEED VGs ON YOUR AIRCRAFT' TO IMPROVE PERFORMANCE AND HANDLING. JABIRU UL-450 12580 CATEGORY CHANGE TO GROUP A ALTER FLAP TRAVEL PER AAN PFA 274-378 SUPPLEMENT 6 TO REMOVE AIRCRAFT FROM JABIRU 2200A BZST MICROLIGHT DEFINITION STALL SPEED RANGE. JABIRU UL-450 14663 CATEGORY CHANGE FROM GROUP A TO CATEGORY CHANGE TO MICROLIGHT BY ADJUSTING FLAP TRAVEL. NOISE CERTIFICATE ISSUED. JABIRU 2200A BZST MICROLIGHT DESIGNATION CHANGED TO UL-450. JABIRU UL-450 13280 STOLSPEED VORTEX GENERATORS STOLSPEED VORTEX GENERATORS INSTALLED ON WING UPPER SURFACE AND TAILPLANE LOWER JABIRU 2200A CNAB SURFACE IN ACCORDANCE WITH 'INSTRUCTIONS FOR INSTALLING STOLSPEED VGs ON YOUR AIRCRAFT' TO IMPROVE PERFORMANCE AND HANDLING. JABIRU UL-450 13956 QUICK DE-RIG OF WINGS, WING STRUTS BOLTED ATTACHMENTS TO WING, STRUT, AILERON AND FLAP CONTROLS RECONFIGURED TO USE JABIRU 2200A CNAB AND CONTROLS CASTLE NUTS AND SAFETY PINS RATHER THAN STIFF NUTS, TO ALLOW FOR RIGGING AND DE- RIGGING OF WINGS BY THE PILOT BEFORE AND AFTER EACH FLIGHT (WHEN DESIRED) AS A PILOT MAINTENANCE ACTIVITY. FAIRINGS REVISED TO PROVIDE ACCESS (AND INSPECTION ACCESS) AS REQUIRED JABIRU UL-450 11125 INSTALL A CAPACITANCE FUEL GAUGE The Skysports capacitance fuel gauging system available from Airworld is installed in accordance JABIRU 2200A CNAB with manufactureres instructions. This provides a useful improvement to the standard sight tube arrangement. JABIRU UL-450 15285 CATEGORY CHANGE FROM GROUP A TO FLAP ANGLE OF DEFLECTION INCREASED TO 37 DEGREES TO ALLOW AIRCRAFT TO BE CATEGORISED JABIRU 2200A CBZM MICROLIGHT AS MICROLIGHT JABIRU UL-450 13230 ELECTRICALLY OPERATED FLAPS EXISTING FLAP SYSTEM CONTROLLED VIA ELECTRIC SERVO PER OPTION ON FOUR SEAT JABIRU JABIRU 2200A ROYC MODELS JABIRU UL-450 10921 ADDITIONAL NOSELEG SUPPORT ADDITIONAL UPPER BEARING ADDED TO NOSELEG MOUNTING TO INCREASE STRENGTH OF JABIRU 2200A OCDW NOSELEG ATTACHMENT. OPTIONAL FIT APPLICABLE TO ALL SP, SK, UL AND SPL MODELS. JABIRU UL-450 12975 CATEGORY CHANGE TO MICROLIGHT FLAP TRAVEL INCREASED JABIRU 2200A CDFK NOISE CERTIFICATE OBTAINED WEIGHED AND WEIGHT SCHEDULE CREATED MICROLIGHT PLACARD ADDED JABIRU UL-450 12467 PROPELLER CHANGE TO SENSENICH PROPELLER CHANGE TO SENSENICH 2A0J5RZ64ZN 60" DIAMETER WITH THE PITCH DIAL SET TO JABIRU 2200A JABZ 2A0J5RZ64ZN 60" DIA, PITCH POSITION 3 POSITION 3.

JODEL DR1051-M1 12471 SLICK OR BENDIX MAGNETO IGNITION SLICK OR BENDIX MAGNETOS FITTED INSTEAD OF COIL SYSTEM USING MODIFICATION 2004-10079 CONTINENTAL O-200-A BHTC APPROVED BY EASA Prototype mods that have been approved since 1/1/2008 Page 54 30/11/20 LAA Technical Leaflet TL 3.17 JODEL DR1051-M1 12710 PROPELLER CHANGE TO HOFFMANN HO PROPELLER CHANGE TO HOFFMANN HO 14-175 128. CONTINENTAL O-200-A BHTC 14-175 128 JODEL DR1051-M1 14382 ENGINE CHANGE TO CONTINENTAL O- . CONTINENTAL O-200-A BHTC 200A JODEL DR1051-M1 14512 PROPELLER CHANGE TO EVRA D11.28.8C . CONTINENTAL O-200-A BHTC

JODEL D112 14743 FIT A STARTER AND ALTERNATOR TO STARTER AND ALTERNATOR FITTED TO A65 ENGINE CONTINENTAL A65-8 BOOH ENGINE JODEL D112 12496 PROPELLER CHANGE TO NEWTON 07R PROPELLER CHANGED TO NEWTON 07R 69" x 47" CONTINENTAL A65-8 BPFD 69" x 47" JODEL D112 13455 NEWTON 07R 69" X 48" PROPELLER NEWTON 07R 69 INCH DIAMETER X 48 INCH PITCH PROPELLER, S/N A02 MANUFACTURED BY ALLEN CONTINENTAL A65-8 INNI HASELDINE, INSTALLED ON CONTINENTAL A65-8 ENGINE. JODEL D112 14183 MDL ALTERNATOR INSTALLATION INSTALLATION OF MDL ALTERNATOR, IN ACCORDANCE WITH AIRWORLD UK INSTRUCTIONS, TO CONTINENTAL A65-8 INNI ENABLE CHARGING OF EXISTING BATTERY. JODEL D112 13053 HERCULES 6952247 69" x 52" INSTALLATION OF HERCULES 6952247 69 INCH DIAMETER X 52 INCH PITCH PROPELLER. CONTINENTAL A65-8F AWVZ JODEL D112 13777 FIT A STARTER MOTOR AND CUSTOM ELECTRIC STARTER AND ALTERNATOR FITTED. CONTINENTAL A65-8F AWVZ ALTERNATOR TO ENGINE JODEL D112 13320 PROPELLER CHANGE TO SENSENICH SENSENICH PROPELLER FITTED AS ABOVE CONTINENTAL A65-8F AYCP W72CK-44 JODEL D112 14602 SPIN-ON OIL FILTER ADAPTER INSTALLATION OF A JPM AVIATION 79001002 SPIN-ON OIL FILTER ADAPTER ONTO CONTINENTAL CONTINENTAL A65-8F AYCP INSTALLATION C85-8F ENGINE AND FITTED WITH A BLUEPRINT ADT32109 OIL FILTER.

ISSUE 2 RAISED TO INCLUDE CONTINENTAL A65-8F ENGINE. ISSUE 3 RAISED TO INCLUDE CONTINENTAL C90-8F ENGINE. JODEL D112 11236 MDL STARTER/ALTERNATOR KIT INSTALLATION OF MDL STARTER AND ALTERNATOR KIT AND BATTERY IN ACCORDANCE WITH CONTINENTAL A65-8F AZHC AIRWORLD UK INSTRUCTIONS. JODEL D112 14094 RWG 105/3 64" X 51" PROPELLER INSTALLATION OF RWG 105/3 64 INCH DIAMETER X 51 INCH PITCH PROPELLER. CONTINENTAL A65-8F BARF INSTALLATION JODEL D112 14602 SPIN-ON OIL FILTER ADAPTER INSTALLATION OF A JPM AVIATION 79001002 SPIN-ON OIL FILTER ADAPTER ONTO CONTINENTAL CONTINENTAL A65-8F BFNG INSTALLATION C85-8F ENGINE AND FITTED WITH A BLUEPRINT ADT32109 OIL FILTER.

ISSUE 2 RAISED TO INCLUDE CONTINENTAL A65-8F ENGINE. ISSUE 3 RAISED TO INCLUDE CONTINENTAL C90-8F ENGINE. JODEL D112 11236 MDL STARTER/ALTERNATOR KIT INSTALLATION OF MDL STARTER AND ALTERNATOR KIT AND BATTERY IN ACCORDANCE WITH CONTINENTAL A65-8F BIVB AIRWORLD UK INSTRUCTIONS. JODEL D112 13484 FIT ALTERNATOR AND STARTER STARTER MOTOR, ALTERNATOR, AND BASIC ELECTRICAL SYSTEM ADDED CONTINENTAL A65-8F BKAO JODEL D112 13557 TURBO ALTERNATOR AND BATTERY TURBO ALTERNATOR FITTED TO BELLY OF AIRCRAFT AND ASSOCIATED BASIC ELECTRICAL CONTINENTAL A65-8F BMIP INSTALLED JODEL D112 14792 HERCULES 6947442-S, 69" X 47" INSTALLATION OF HERCULES 6947442-S 69 INCH DIAMETER X 47 INCH PITCH PROPELLER. CONTINENTAL C90-14F BIEO PROPELLER INSTALLATION JODEL D112 14808 ENGINE & PROPELLER CHANGE TO ENGINE REPLACED WITH CONTINENTAL C90-14F CONTINENTAL C90-14F BIZY CONTINENTAL C90-14F AND EVRA PROPELLER REPLACED WITH EVRA D11.28.1B D11.28.1.B JODEL D112 11236 MDL STARTER/ALTERNATOR KIT INSTALLATION OF MDL STARTER AND ALTERNATOR KIT AND BATTERY IN ACCORDANCE WITH CONTINENTAL C90-8F AYBR AIRWORLD UK INSTRUCTIONS. JODEL D112 (MODIFIED) 12704 ENGINE CHANGE TO CONTINENTAL C90- CONTINENTAL C90-14F ENGINE SUBSTITUTED USING EXISTING ENGINE MOUNT. EVRA D11.28.4C CONTINENTAL C90-14F BHKT 14F PROPELLER FITTED JODEL D112 (MODIFIED) 13879 PROPELLER CHANGE TO MCCAULEY INSTALLATION OF MCCAULEY 1A105/SCM7051 70 INCH DIAMETER X 51 INCH PITCH PROPELLER. CONTINENTAL C90-14F BHKT 1A105/SCM 50/51

Prototype mods that have been approved since 1/1/2008 Page 55 30/11/20 LAA Technical Leaflet TL 3.17 JODEL D112 (MODIFIED) 14771 REAR TANK FITMENT AND PIPING AS PER STANDARD JODEL D117 REAR FUEL TANK FITTED BEHIND SEATS USING STANDARD INSTALLATION CONTINENTAL C90-14F BHKT D117 AS FOR JODEL D117, EXCEPT TANK ARRANGED TO FEED INTO MAIN TANK VIA ELECTRIC PUMP RATHER THAN SELECTED INDEPENDENTLY OF MAIN TANK. JODEL D112 (MODIFIED) 14994 REPLACEMENT EXHAUST SYSTEM EXHAUST SYSTEM MODIFIED WITH CUSTOM SILENCER CONNECTED TO ORIGINAL DOWN PIPES. CONTINENTAL C90-14F BHKT

JODEL D117 13981 ENGINE AND PROPELLER CHANGE INSTALLATION OF CONTINENTAL C90-12F ENGINE USING 20MM LONG LIGHT ALLOY SPACERS CONTINENTAL C90-12F BJOT BETWEEN ENGINE MOUNTING FRAME AND CONICAL RUBBER ENGINE MOUNTINGS TO MAINTAIN ORIGINAL ENGINE POSITION. HERCULES 6856445-S 68 INCH DIAMETER X 56 INCH PITCH PROPELLER FITTED. JODEL D117 13593 NEWTON 07R 69" X 46" PROPELLER INSTALLATION OF NEWTON 07R 69 INCH DIAMETER X 46 INCH PITCH PROPELLER. CONTINENTAL C90-14F ATIZ INSTALLATION JODEL D117 14224 B & C STARTER AND ALTERNATOR B&C BC320-H STARTER UNIT, BC200G ALTERNATOR, PMR1C-14 VOLTAGE REGULATOR AND OMV- CONTINENTAL C90-14F AXCG 14 OVER-VOLTAGE MODULE INSTALLED IN ACCORDANCE WITH MANUFACTURER'S INSTRUCTIONS. INCLUDES ASSOCIATED WIRING, CIRCUIT PROTECTION, RELAYS AND SWITCHES.

JODEL D117 13948 ENGINE CHANGE TO CONTINENTAL C90 CHANGE FROM C90-14F TO C90-16F USING CONICAL INSERTS TO ADAPT MOUNT CONTINENTAL C90-14F AYKT 16F JODEL D117 12694 SMALL ITEMS LOCKER SMALL LOCKER ADDED TO REAR OF MAIN COCKPIT BULKHEAD, AS SHOWN IN APPLICANT'S CONTINENTAL C90-14F BDIH AMENDED DRAWING. JODEL D117 13451 HOFFMANN HO14-178 120 PROPELLER INSTALLATION OF HOFFMANN HO14-178/120 PROPELLER CONTINENTAL C90-14F BHEL INSTALLATION JODEL D117 12662 ENGINE CHANGE TO CONTINENTAL O- ENGINE CHANGE TO CONTINENTAL O-200A WITH EVRA D.11.28.7.C PROPELLER. CONTINENTAL O-200-A AYGA 200A WITH EVRA D.11.28.7.C PROPELLER. JODEL D117 13143 ELECTRIC FUEL PUMP ADDED ELECTRIC FUEL PUMP ADDED IN SERIES AS BACK UP ,WITH EDP, FUEL PRESSURE GAUGE FITTED CONTINENTAL O-200-A AYGA

JODEL D117A 12744 PROPELLER CHANGE TO KEN FERN KF 7047ULS2RR FITTED CONTINENTAL C90-14F AYHX JODEL D117A 13224 FITTING AUXILIARY ELECTRIC FUEL PUMP INSTALLATION OF FACET 40288 SOLID STATE FUEL PUMP, WITH INTEGRAL NON-RETURN VALVE, CONTINENTAL C90-14F BFEH ON FRONT OF FIREWALL STARBOARD SIDE, PLUMBED IN PARALLEL WITH MECHANICAL FUEL PUMP. FUEL PRESSURE GAUGE FITTED. JODEL D117A 14259 SMALL ITEMS LOCKER WOODEN LOCKER MOUNTED TO BULKHEAD AT REAR OF COCKPIT WITH ACCESS THROUGH CONTINENTAL C90-14F BFEH BULKHEAD AND LOCKABLE DOOR FITTED. FOR STORAGE OF ITEMS ON THE GROUND ONLY. NOT FOR USE IN FLIGHT. JODEL D117A 12733 REPLACE BLADDER TYPE DRUM BRAKES REPLACE BLADDER TYPE DRUM BRAKES WITH CLEVELAND DISC BRAKES IN ACCORDANCE WITH R CONTINENTAL C90-14F BIOU WITH CLEVELAND DISC BRAKES HORRELL'S DESIGN AND D HARDAKER'S DRAWINGS.

JODEL D11A 12712 PROPELLER CHANGE TO HOFFMANN HO PROPELLER CHANGE TO HOFFMANN HO 14-170 123, 170CM DIAMETER X 123CM PITCH. CONTINENTAL O-200-A BDBV 14-170 123 JODEL D11A 13640 ENGINE CHANGE TO CONTINENTAL O- O-200A ENGINE INSTALLED IN PLACE OF C90 FITTED PREVIOUSLY, WITH HOFFMANN HO14-170 123 CONTINENTAL O-200-A BDBV 200A PROPELLER. JODEL D120 13917 SPIN-ON OIL FILTER ADAPTER FOR INSTALLATION OF CUSTOM MADE SPIN-ON OIL FILTER ADAPTER P/N 79001003 WITH CHAMPION CONTINENTAL C90-14F AZEF CONTINENTAL PC60 (O-200) CH48108 OR C138 OR BLUE PRINT ADT32109 OIL FILTER.

AT ISSUE 4: APPLICABILITY EXTENDED TO CONTINENTAL C90-12 ENGINE. AT ISSUE 6: APPLICABILITY EXTENDED TO CONTINENTAL C85-12F ENGINE. AT ISSUE 7: APPLICABILITY EXTENDED TO CONTINENTAL C90-14F ENGINE. JODEL D120 13922 PROPELLER CHANGE TO HERCULES INSTALLATION OF HERCULES 694742-S 69 INCH DIAMETER X 47 INCH PITCH PROPELLER. CONTINENTAL C90-14F BHXD 6947442-S

Prototype mods that have been approved since 1/1/2008 Page 56 30/11/20 LAA Technical Leaflet TL 3.17 JODEL D120 13845 PROPELLER CHANGE TO HERCULES INSTALLATION OF HERCULES 6848432-S 68 INCH DIAMETER X 48 INCH PITCH PROPELLER. CONTINENTAL C90-14F BKCW 6848432-S JODEL D120 13942 EVRA D11.28.1.B PROPELLER INSTALLATION OF EVRA D11.28.1.B PROPELLER. CONTINENTAL O-200-A AXNJ INSTALLATION JODEL D120 13912 PROPELLER CHANGE TO HERCULES PROPELLER REPLACED BY HERCULES WOODEN PROPELLER TYPE 6853419-S CONTINENTAL O-200-A AYRS 6853419-S JODEL D120 14161 CONTINENTAL C90-14F REBUILD USING O-REBUILD OF CONTINENTAL C90-14F ENGINE USING CONTINENTAL O-200 CRANKCASE IN CONTINENTAL C90-14F (MODIFIED) BCGM 200 CRANKCASE ACCORDANCE WITH STC NO. SE02172AT. JODEL D120A 13134 HERCULES 7048271-S 70" X 48" INSTALLATION OF HERCULES 7048271-S 70 INCH DIAMETER X 48 INCH PITCH PROPELLER. CONTINENTAL C90-14F BHZV PROPELLER JODEL D120A 12953 PROPELLER CHANGE TO HERCULES INSTALLATION OF HERCULES 6852240 68.5 INCH DIAMETER X 52 INCH PITCH PROPELLER. CONTINENTAL C90-14F BJOE 6852240 68.5" X 52" JODEL D120A 13091 BACK-UP FUEL PUMP FACET BOOST PUMP ADDED TO FUEL SYSTEM ALONG WITH ASSOCIATED FUEL PRESSURE GAUGE CONTINENTAL C90-14F BYBE AND NRT VALVE JODEL D120A 12947 EVRA PROPELLER EVRA D 11 28 7 C PROPELLER FITTED TO CONTINENTAL O-200-A ENGINE. CONTINENTAL O-200-A BJYK JODEL D120A 13826 ENGINE AND PROPELLER CHANGE INSTALLATION OF CONTINENTAL O-200-A ENGINE AND EVRA D11.28.4.C PROPELLER. CONTINENTAL O-200-A BKPX JODEL D14 13683 PROPELLER CHANGE TO HOFFMAN HO27 PROPELLER CHANGED TO HOFFMANN HO27-AHM 187B 150 LYCOMING O-360-A4M BWAB

JODEL D14 13684 UPGRADE FROM 2 TO 4 SEAT/ 1200 KGS REAR SEAT BELTS FITTED TO ALLOW AIRCRAFT TO BE CLEARED AS FOUR SEATER LYCOMING O-360-A4M BWAB GROSS WEIGHT JODEL D14 14017 SMALLER THAN DESIGNED REAR BAGGAGE BAY DOOR REMADE APPROXIMATELY HALF THE NORMAL LENGTH AND TURTLEDECK LYCOMING O-360-A4M BWAB BAGGAGE BAY EXTERNAL ACCESS MODIFIED TO ACCEPT SMALLER DOOR USING CONVENTIONAL SPRUCE AND PLY STRUCTURE

JODEL D140A 14847 DISC BRAKE CONVERSION LOWER LANDING GEAR LEGS REPLACED WITH REDESIGNED LEG AND AXLE TO SUIT CLEVELAND LYCOMING O-360-A3A ARDZ WHEELS AND DISC BRAKES PER G-JRME. JODEL D140A 14848 QUADRANT THROTTLE AND MIXTURE PUSH-PULL CONTROLS REPLACED BY CONVENTIONAL QUADRANT SYSTEM LYCOMING O-360-A3A ARDZ JODEL D140A 14849 CARB HEAT AND COLD AIR INLET SYSTEM CONVENTIONAL PILOT-SELECTABLE CARB HEAT SYSTEM FITTED USING VETTERMAN EXHAUST AND LYCOMING O-360-A3A ARDZ MUFF SIMILAR TO RV TYPE AIRCRAFT. JODEL D140A 14850 SHOULDER HARNESS FOR FRONT SHOULDER HARNESS MOUNTINGS INSTALLED SIMILAR TO THOSE ALREADY ACCEPTED ON G-JRME, LYCOMING O-360-A3A ARDZ OCCUPANTS ADAPTED TO SUIT D140A GEOMETRY JODEL D140C 13742 TRIMMER DRIVE FIX TRIM CABLE ATTACHMENT REPAIRED BY CUTTING OFF BENT PORTION OF THREAD AND FITTING SUPERIOR XP-O-360-A1AC2 REES CUSTOM MADE THREADED ADAPTER TO REPLACE REMOVED PORTION JODEL D140C 15050 ENGINE CHANGE TO SUPERIOR XP-O-360- ENGINE CHANGED SUPERIOR XP-O-360-A1AC2. SUPERIOR XP-O-360-A1AC2 REES A1AC2 JODEL D140E 13007 TRIO EZ PILOT, SINGLE AXIS AUTOPILOT INSTALLATION OF TRIO EZ PILOT, SINGLE AXIS AUTOPILOTIN CUSTOM MADE STEEL MOUNTING LYCOMING O-360-A4A JRME BOX ATTACHED TO WING CENTRE SECTION. SERVO DRIVES CONTROL COLUMN TUBE VIA CLAMPED AND BOLTED BELLCRANK. JODEL D150 13991 ELECTRIC FUEL SYSTEM MODIFICATION MODIFICATION TO FUEL SYSTEM INCLUDING INSTALLATION OF FACET 480532E GOLD-FLO FUEL CONTINENTAL O-200-A BFEB PUMP, SYTEC NON-RETURN VALVE, SYTEC FUEL PRESSURE REGULATOR HOUSED WITHIN ALUMINIUM ENCLOSURE WITH DRAIN TO COWLING AIR OUTLET AREA AT BASE OF FIREWALL, SUCO FUEL PRESSURE SWITCH FOR LOW PRESSURE WARNING LAMP SET TO 3.8 PSI, IN PARALLEL WITH THE ENGINE DRIVEN MECHANICAL FUEL PUMP. JODEL D150 14291 HERCULES 6753467-S PROPELLER INSTALLATION OF HERCULES 6753467-S 67 INCH DIAMETER X 53 INCH PITCH PROPELLER. CONTINENTAL O-200-A BVST INSTALLATION JODEL D150 12777 INSTALLATION OF ANDAIR OIL/AIR AIR/OIL SEPERATOR FITTED PER APPLICANT'S DETAILS CONTINENTAL O-200-A IEJH SEPARATOR JODEL D150 12778 REPLACE ONE BENDIX MAGNETO WITH P- P-MAG INSTALLED IN ACCORDANCE WITH MANUFACTURER'S INSTRUCTIONS CONTINENTAL O-200-A IEJH MAG ELECTRONIC IGNITION JODEL D150 14329 ENGINE PISTON CHANGE C85 PISTONS SUBSTITUTED TO INCREASE COMPRESSION RATIO, AS PREVIOUSLY ACCEPTED BY LAA CONTINENTAL O-200-A IEJH ON VARI-EZE G_VEZE. SLIGHT RELIEF OF CYLINDER HEADS ADJACENT TO SPARK PLUG FOR CLEARANCE. Prototype mods that have been approved since 1/1/2008 Page 57 30/11/20 LAA Technical Leaflet TL 3.17 JODEL D150 13058 HERCULES 6954257 69" X 54" INSTALLATION OF HERCULES 6954257 69 INCH DIAMETER X 54 INCH PITCH PROPELLER. LYCOMING O-235-H2C CECH JODEL D150A 12864 JODEL D150A SHOULDER HARNESS PROVISION OF SHOULDER HARNESS ANCHOR POINT ABOVE SHOULDER LINE. ASH BLOCKS WITH 4E20A CGMH REINFORCEMENT ALUMINIUM ALLOY INSERTS GLUED IN PLACE WITH SPRUCE LONGERONS ONTO GL1 PLY REINFORCEMENTS USING RESORCINOL AND VARNISHED. SHOULDER HARNESS SECURED TO BUSHES USING A113 BOLT AND ASSOCIATED HARDWARE. JODEL D18 14313 ENGINE CHANGE TO CAMIT CAE2200 ENGINE CHANGED - JABIRU 2200A SUBSTITUTED BY CAMIT CAE 2200 CAMIT CAE 2200 OLEM JODEL D18 13336 ENGINE CHANGE TO REVMASTER REVMASTER 2100D ENGINE SUBSTITUTED REVMASTER R2100D BTRZ JODEL D18 14446 REPLACE SECOND IGNITION SYSTEM SECOND IGNITION REPLACED WITH LEBURG IGNITION SYSTEM SO THAT ENGINE SUPPLIED WITH SUBARU EA81 WIBB WITH LEBERG IGNITION TWO LEBURG IGNITION SYSTEMS. SYSTEM USES A 14 Ah AND A 4 Ah BATTERY AND INCORPORATES A 2A FUSE PROTECTING EACH IGNITION MODULE. JODEL D18 12960 PROPELLER CHANGE TO NEWTON TYPE INSTALLATION OF NEWTON TYPE 15L 58 INCH DIAMETER X 38 INCH PITCH PROPELLER. VW (AEROPOWER) 2074 JRKD 15L 58" X 38" JODEL D9 12690 HEEL OPERATED BRAKING SYSTEM HEEL BRAKES FITTED USING MECHANICAL CABLE OPERATED DRUM BRAKE AND HEEL PEDALS VW 1600 BGFJ MOUNTED TO COCKPIT FLOOR JODEL D9 14219 PROPELLER CHANGE TO STERBA 52" x INSTALLATION OF A STERBA 52 INCH DIAMETER X 44 INCH PITCH PROPELLER. VW 1600 BGFJ 44" JODEL DR100A 14425 MATCO WHLT-6 TAIL WHEEL ASSEMBLY INSTALLATION OF MATCO WHLT-6 TAILWHEEL INSTALLATION. HOLE IN MOUNTING BASE CONTINENTAL C90-14F BDMW INSTALLATION INCREASED IN DIAMETER FROM 3/8" TO 7/16" TO MATCH ORIGINAL LEAF SPRING. JODEL DR100A 13238 B&C 200G ALTERNATOR TO REPLACE INSTALLATION OF A B&C 200G PERMANENT MAGNET ALTERNATOR IN PLACE OF DELCO 12V CONTINENTAL C90-14F BFBA DELCO 12V GENERATOR GENERATOR TO CONTINENTAL C90-14F ENGINE. SOLID STATE REGULATOR/RECTIFIER INSTALLED ON DIECAST BOX THAT CONTAINS ASSOCIATED SMOOTHING CAPACITOR, ISOLATION RELAY AND OVER-VOLTAGE TRIP DEVICE WHICH IS MOUNTED TO THE FIREWALL IN PLACE OF THE ORIGINAL MECHANICAL REGULATOR AND HOUSING.

JODEL DR1050 15125 MATCO MC-4GH BRAKE MASTER ISSUE 1. INSTALLATION OF TWO MATCO MC-4GH BRAKE MASTER CYLINDERS REPLACING CONTINENTAL O-200-A JEMM CYLINDERS INSTALLATION AIRWORLD BRAKE MASTER CYLINDERS.

ISSUE 2. INSTALLATION REVISED INCLUDING: - NEW SUPPORT BLOCK MADE AND INSTALLED TO SUPPORT CYLINDER END LUGS AND ALLOW ORIGINAL FRAME MOUNTING BOLT TO BE USED. - EXCHANGE OF TWO PART INTERLINK BETWEEN EACH PISTON ROD AND LEVER WITH SINGLE RIGID END FITTING. - REMOVAL OF CYLINDER RESTRAINING PLATE 'PIECE A' TO ALLOW CYLINDER MOVEMENT DURING BRAKING APPLICATION. - FLEXIBLE HOSES FITTED TO ACCOMMODATE CYLINDER MOVEMENT. JODEL DR1050 13528 DISC BRAKE SYSTEM CUSTOM WHEELS INCORPORATING CUSTOM DISC BRAKE SYSTEM SUBSTITUTED CONTINENTAL O-200-A AYUT JODEL DR1050 14414 ANGUS AVIATION GA-1000 HEATED INSTALLATION OF ANGUS AVIATION GA-1000 HEATED PITOT HEAD CONTINENTAL O-200-A AYUT PITOT JODEL DR1050 12952 PROPELLER CHANGE TO HOFFMANN INSTALLATION OF HOFFMANN HO14-170 S 123, 170CM DIAMETER X 123CM PITCH. CONTINENTAL O-200-A LAKI HO14-170 S 123 JODEL DR1050 13917 SPIN-ON OIL FILTER ADAPTER FOR INSTALLATION OF CUSTOM MADE SPIN-ON OIL FILTER ADAPTER P/N 79001003 WITH CHAMPION CONTINENTAL O-200-A LAKI CONTINENTAL PC60 (O-200) CH48108 OR C138 OR BLUE PRINT ADT32109 OIL FILTER.

AT ISSUE 4: APPLICABILITY EXTENDED TO CONTINENTAL C90-12 ENGINE. AT ISSUE 6: APPLICABILITY EXTENDED TO CONTINENTAL C85-12F ENGINE. AT ISSUE 7: APPLICABILITY EXTENDED TO CONTINENTAL C90-14F ENGINE. JODEL DR1050 14066 EXCHANGE GENERATOR TO ALTERNATOR B&C 200G ALTERNATOR INSTALLED ON ENGINE IN PLACE OF ORIGINAL GENERATOR. INCLUDES CONTINENTAL O-200-A ATWA FITMENT OF B&C PMR1C VOLTAGE REGULATOR AND OVM-14 OVER-VOLTAGE PROTECTION MODULE. INSTALLED IN ACCORDANCE WITH MANUFACTURER'S INSTRUCTIONS REF '200G_INSTALL.WPD, REV B, 1/05' AND 'PMR1C INSTALL INSTR.WPD'. Prototype mods that have been approved since 1/1/2008 Page 58 30/11/20 LAA Technical Leaflet TL 3.17 JODEL DR1050 13822 PROPELLER CHANGE TO HERCULES INSTALLATION OF HERCULES 6853419-S 68 INCH DIAMETER X 53 INCH PITCH PROPELLER. CONTINENTAL O-200-A ARXT 6853419-S JODEL DR1050 14066 EXCHANGE GENERATOR TO ALTERNATOR B&C 200G ALTERNATOR INSTALLED ON ENGINE IN PLACE OF ORIGINAL GENERATOR. INCLUDES CONTINENTAL O-200-A ARXT FITMENT OF B&C PMR1C VOLTAGE REGULATOR AND OVM-14 OVER-VOLTAGE PROTECTION MODULE. INSTALLED IN ACCORDANCE WITH MANUFACTURER'S INSTRUCTIONS REF '200G_INSTALL.WPD, REV B, 1/05' AND 'PMR1C INSTALL INSTR.WPD'. JODEL DR1050 13328 FIT AIRWORLD/F&M SPIN-ON OIL FILTER AIRWORLD / F+M REMOTE OIL FILTER KIT INSTALLED. MINOR CHANGE TO BATTERY INSTALLATION CONTINENTAL O-200-A JEJH CONVERSION TO ACCOMMODATE OIL FILTER INSTALLATION JODEL DR1050 12534 FUEL SELECTOR VALVE CHANGE AND INSTALLATION OF ANDAIR FUEL SELECTOR VALVE FS20X3F ONTO PILOT'S SIDE SPAR MOUNTED CONTINENTAL O-200-A SPOG RELOCATION BRACKET. JODEL DR1050 13713 ENGINE CHANGE TO ROTAX 912ULS ROTAX 912-ULS ENGINE AND WARP DRIVE THREE BLADED PROPELLER SUBSTITUTED ROTAX 912-ULS AWWO JODEL DR1050 14465 ADJUSTMENTS TO WEIGHT AND INCREASE MAXIMUM REAR SEAT LOADING BY MOVING EMPTY CG FORWARDS: ROTAX 912-ULS AWWO BALANCE 1. INSTALLATION OF MATCO WHLT-8L TAILWHEEL ASSEMBLY 2. RELOCATE BATTERY TO FIREWALL USING MODIFIED TQB-17390 BATTERY BOX AND USE OF LARGER BATTERY 3. KEVLAR/CARBON/EPOXY MAINWHEEL SPATS INSTALLED 4. ADDITION OF 4 KG STEEL PROPELLER SPACER

PLACARDS TO NOTE THAT: - MAXIMUM COMBINED WEIGHT ON REAR SEATS IS 85 KG - FOR REAR SEAT LOADS OVER 80 KG, ENSURE AT LEAST 10 LITRES MORE FUEL IN FRONT TANK THANK REAR TANK.

MAXIMUM TAKE-OFF AND LANDING WEIGHTS INCREASED TO 730 KG. JODEL DR1050 14782 DYNON HEATED PITOT/ANGLE OF INSTALLATION OF DYNON HEATED PITOT/ANGLE OF ATTACK PROBE UNDER PORT WING TO ROTAX 912-ULS AWWO ATTACK PROBE INSTALLATION REPLACE ORIGINAL PITOT HEAD. HEATER REGULATOR MOUNTED ON TOP OF PITOT HEAD MOUNTING FLANGE. JODEL DR1050 (MODIFIED) 12588 RESTORE 2 SEAT TO 4 SEAT REMOVAL OF BAGGAGE BAY FLOOR PANEL AND INSTALLATION OF ORIGINAL REAR SEATS AND POTEZ 4E20 ARRD CONFIGURATION STANDARD JODEL REAR SEAT BELTS TO ORIGINAL SEAT BELT ATTACHMENTS. JODEL DR1050-M1 12994 BATTERY MOUNTING BRACKET FOR BATTERY MOUNTING BRACKET FOR ODYSSEY P680 BATTERY CONTINENTAL O-200-A BAEE ODYSSEY P680 BATTERY JODEL DR1050-M1 14780 OVERHAUL OF FUEL SYSTEM FUEL SYSTEM MODERNISED USING ANDAIR FUEL VALVE, FACET FUEL PUMP AND ANDAIR CONTINENTAL O-200-A AYYT GASCOLATOR, WITH APPROPRIATE AN HOSE FITTINGS AND PIPEWORK. JODEL DR1050-M1 15407 EXHAUST WITH SILENCER ATELIER CHABORD TUNED EXHAUST AND SILENCER CONTINENTAL O-200-A AYZK DGAC STC NO. F-C6-SF-0060 JODEL DR1050-M1 14688 HERCULES 7046537-S 70" X 46" INSTALLATION OF HERCULES 7046537-S 70 INCH DIAMETER X 46 INCH PITCH PROPELLER CONTINENTAL O-200-A CIYB PROPELLER INSTALLATION JODEL DR1051 12843 ENGINE CHANGE TO CONTINENTAL C90- ENGINE CHANGE TO CONTINENTAL C90-14F WITH EVRA D.11.28.1.B PROPELLER CONTINENTAL C90-14F BYCS 14F JODEL DR1051 13888 PROPELLER CHANGE TO HERCULES HERCULES 6858395-S 68 INCH DIAMETER X 58 INCH PITCH PROPELLER INSTALLATION. POTEZ 4E20 JWIV 6858395-S JODEL DR1051 (MODIFIED) 13962 FUEL SELECTOR AND MONITORING FUEL SELECTOR REPLACED WITH ANDAIR SELECTOR VALVE. CONTINENTAL O-200-A IOSI SYSTEM FUEL QUANTITY GAUGES REPLACES WITH AIRWORLD UK CAPACITATIVE FUEL MONITOR SYSTEM

JODEL DR1051-M1 13386 LEBURG IGNITION INSTALLATION ON B BANK OF THE POTEZ IGNITION SYSTEM (COIL IGNITION) REPLACED BY SINGLE LEBURG SYSTEM. POTEZ 4E20 BHHE POTEZ ENGINE (B BANK ONLY) EXISTING A BANK IGNITION SYSTEM UNCHANGED.

ACCEPTED FOR A MAXIMUM OF 100 FLYING HOURS ONLY, PENDING LAA ACCEPTANCE OF RESULTS DURING FIRST 100 HOURS AND PROVISION OF AGREED MAINTENANCE INSTRUCTIONS

Prototype mods that have been approved since 1/1/2008 Page 59 30/11/20 LAA Technical Leaflet TL 3.17 JODEL DR1051-M1 13807 PROPELLER CHANGE TO HERCULES INSTALLATION OF HERCULES 6858395-S 68 INCH DIAMETER X 58 INCH PITCH PROPELLER. POTEZ 4E20 BHHE 6858395-S JURCA SIROCCO 12447 IRREVERSABLE ELEVATOR TRIM TAB 60:1 RATIO WORM GEARBOX FITTED TO LEFT COCKPIT SIDEWALL OPERATING EXISTING TAB FRANKLIN 6A-350-C1 CEAO CONTROL CABLE. JUST SUPERSTOL 14431 GARMIN DUAL AXIS AUTO-PILOT AND GARMIN GSA28 AUTOPILOT SERVOS (ROLL AND PITCH) INSTALLED ON CUSTOM BRACKETS AND ROTAX 912-iS MHAN BATTERY TRAY INSTALLATIONS LINKING TO CONTROL SYSTEMS VIA PUSH-RODS. AUTOPILOT FUNCTIONALITY CONTROLLED BY A GARMIN G3X UNIT. PITCH SERVO BRACKET INCORPORATES PROVISION FOR AIRCRAFT BATTERY MOUNTING. JUST SUPERSTOL 15134 STANDBY INSTRUMENTS MGL ASX-2 ELECTRONIC STANDBY AND ASI FITTED. INCORPORATES A BACKUP BATTERY ROTAX 912-iS RHOD POWER SUPPLY. KOLB TWINSTAR MK3 14517 CATEGORY CHANGE FROM MICROLIGHT SECOND SEAT AND ASSOCIATED SEAT HARNESS REMOVED ROTAX 582 MYIK TO SSDR MAX GROSS WEIGHT LIMITED TO 300 Kg KOLB TWINSTAR MK3 12685 DUAL THROTTLE MODIFICATION INSTALLATION OF 2ND THROTTLE CONTROL MOUNTED TO LEFT SIDE OF P1 SEAT. CENTRE ROTAX 582/48 MZGJ (MODIFIED) THROTTLE FITTED WITH 'THROTTLE-CLOSED' LATCH TO PREVENT INADVERTANT OPERATION. THROTTLE CABLE SPLITTER ALLOWS LEFT HAND THROTTLE TO OPERATE UNHINDERED WITH CENTRE THROTTLE LATCHED CLOSED. CENTRE THROTTLE ALSO OPERATES LEFT HAND THROTTLE LEVER. KOLB TWINSTAR MK3 12687 ENGINE CHANGE TO ROTAX 582/48 ENGINE CHANGE TO ROTAX 582/48 WITH GSC TECH III, 3 BLADED 66 INCH DIAMETER X 11.3 ROTAX 582/48 MZGJ (MODIFIED) DEGREES PITCH PROPELLER INSTALLED. KOLB TWINSTAR MK3 12731 REDUCTION OF MAXIMUM FLAP ATTACHMENT OF FLAP LINK PLATE TO NEW HOLE POSITIONED CLOSER TO FLAP LEVER PIVOT (AT ROTAX 582/48 MZGJ (MODIFIED) DEFLECTION. 1.4 INCHES RADIUS FROM 2.1 INCHES) TO REDUCE FLAP MAXIMUM DEFLECTION FROM 55 DEGREES DOWN TO 35 DEGREES DOWN. KOLB TWINSTAR MK3 EXTRA 14381 REPLACE CHARGING SYSTEM WITH A REMOVAL OF EXISTING CHARGING SYSTEM AND INSTALLATION OF BELT-DRIVEN CAMIT 40 AMP JABIRU 2200A IANN BELT DRIVEN ALTERNATOR ALTERNATOR. INCLUDES ASSOCIATED ELECTRICAL SYSTEM CHANGES. NYLOC NUTS REPLACED WITH NUTS AND LOCK-TAB WASHERS. KOLB TWINSTAR MKIII XTRA 13221 CARB PROTECTION HEATER PILOT CONTROLLABLE CARBURETTOR HEAT FITTED FED FROM EXHAUST HEAT MUFF JABIRU 2200A MGPX KOLB TWINSTAR MKIII XTRA 15348 ENGINE & PROP CHANGE TO ROTAX ROTAX 582/47 ENGINE AND GSC TECH III 66" DIAMETER PROPELLER INSTALLED. STANDARD KOLB ROTAX 582/47 CDZS 582/47 & GSC SYSTEMS TECH III 66" X ENGINE MOUNT FOR THIS ENGINE USED. 13.3 LANCAIR 235 14243 ELECTRONIC BACKUP ALTIMETER AND AN MGL ASX-1 ELECTRONIC ASI AND ALTIMETER IS FITTED AS A BACKUP TO THE ASI AND LYCOMING O-235-L2A BSRI ASI ALTIMETER FUNCTIONS WITHIN THE ELECTRONIC PRIMARY FLIGHT DISPLAY. A DEDICATED BACKUP BATTERY AND FLYBOX CONTROL UNIT SUPPLY THE INSTRUMENT WITH POWER IN THE EVENT THAT PRIMARY ELECTRICAL POWER IS LOST. THE BACKUP UNIT USES A SEPARATE (ALREADY INSTALLED) PITOT SOURCE FROM THE PRIMARY INSTRUMENTS. LANCAIR 320 12606 REPLACE MAIN GEAR WHEELS AND EXISTING MATCO WHEELS AND BRAKES ARE REPLACED WITH GROVE WHEELS AND BRAKES. LYCOMING IO-320-B1A FOPP BRAKES LANCAIR 320 13459 MTV-12-C/170-57 PROPELLER INSTALLATION OF MTV-12-C/170-57 PROPELLER LYCOMING IO-320-D1B PJMT INSTALLATION. LARK 95 14261 HERCULES 6950505-S 69" x 50" INSTALLATION OF HERCULES 6950505-S, 69 INCH DIAMETER X 50 INCH PITCH PROPELLER. CONTINENTAL C90-16F LARK PROPELLER INSTALLATION LASER Z200 12435 CARBON FIBRE SPINNER SUBSTITUTED CARBON FIBRE PROPELLER SPINNER MANUFACTURED USING ORIGINAL ALUMINIMUM SPINNER AS LYCOMING AEIO-360-A1E LAZA PLUG FOR SPINNER MOULD. ATTACHMENTS SIMILAR TO ORIGINAL ALUMINIUM SPINNER.

LASER Z200 (MODIFIED) 13262 MTV-15-B-C/C193-34 PROPELLER PROPELLER CHANGE TO MTV-15-B-C/C193-34 193CM DIAMETER CONSTANT SPEED. LYCOMING AEIO-360-A1E VILL LASER Z200 (MODIFIED) 14930 CHRISTEN INVERTED OIL SYSTEM CHRISTEN 801 INVERTED OIL SYSTEM FITTED. LYCOMING O-360-A4A BWKT EMBODIMENT (MODIFIED) LASER Z200 (MODIFIED) 14931 ENGINE CHANGE TO LYCOMING O-360- LYCOMING O-360-A4A (MODIFIED) ENGINE INSTALLED. ENGINE IS MODIFIED WITH A BENDIX FUEL LYCOMING O-360-A4A BWKT A4A (MODIFIED) INJECTION SYSTEM. THE PROPELLER REMAINS A SENSENICH 76EM8S5-0-60. (MODIFIED)

Prototype mods that have been approved since 1/1/2008 Page 60 30/11/20 LAA Technical Leaflet TL 3.17 LASER Z230 15038 RELOCATION OF MAIN BATTERY REDESIGN AND RELOCATION OF BATTERY BOX FROM AFT OF SEAT POSITION TO AFT OF FIREWALL. LYCOMING AEIO-360-A1E CDDP BATTERY BOX CONSTRUCTED FROM 2024-T3 SHEET AND ANGLE, RIVETED TOGETHER AND BOLTED TO FIREWALL. AN665 FORKS SECURED WITH AN3 BOLTS AND A 6061 BAR SECURE THE BATTERY IN POSITION. LETOV LK-2M SLUKA 12537 BOOM STIFFENER AS PER MOD 11672 DRAWINGS SHOW STIFFENER DESIGN AS INCORPORATED 1-V MZBF LETOV LK-2M SLUKA 13034 PROPELLER CHANGE TO WOODCOMP INSTALLATION OF WOODCOMP KLASSIC 160/3/L 1600MM DIAMETER 3 BLADED PROPELLER SET TO ROTAX 447 1-V MZBF KLASSIC 160/3/L 9 DEGREES PITCH. GEARBOX RATIO 2.58:1 LETOV LK-2M SLUKA 12518 ENGINE CHANGE FROM ROTAX 447 TO ENGINE CHANGED TO ROTAX 508 IN THE INTEREST OF GREATER FUEL ECONOMY, USING CUSTOM ROTAX 508 MZOX ROTAX 508 ENGINE MOUNTING CRADLE OF WELDED STEEL CONSTRUCTION PREVIOUSLY DESIGNEFD FOR MW6 APPLICATION LETOV LK-2M SLUKA 12523 BOOM SLEEVE REINFORCEMENT SLEEVE REINFORCEMENT ADDED TO FORWARD BOOM TO PREVENT CRACKING ROTAX 508 MZOX LINNET 2 14371 WHEEL & BRAKE CHANGE ORIGINAL GOODYEAR WHEELS AND BRAKES REPLACED WITH CLEVELAND 40-78B WHEEL AND DISC CONTINENTAL O-200-A ASZR UNITS, CLEEVELAND 30-9 BRAKE UNIT AND WILWOOD RD3619 MASTER CYLINDERS. MOD INCLUDES ASSOCIATED HOSES, FITTINGS AND FASTENERS. LUSCOMBE 8A 12336 4 POINT HARNESS FOUR POINT HARNESS FITTED INSTEAD OF LAP AND DIAGONAL STRAP & INSTALLATION OF CONTINENTAL A65-1 BSUD ADDITIONAL BRACKETS LUSCOMBE 8A 12337 TAIL PULL HANDLE B.A.S. TPH1 LIFT HANDLE FITTTED AT TAIL CONTINENTAL A65-1 BSUD LUSCOMBE 8A 13168 SKYLIGHT SKYLIGHT ADDED TO CABIN ROOF, GENERALLY IN ACCORDANCE WITH ORIGINAL OPTION PER CONTINENTAL A65-8 BPPO LUSCOMBE PARTS MANUAL FIGURE 5 EXCEPT MOULDED RUBBER SEAL USED TO RETAIN PERSPEX RATHER THAN MECHANICAL FASTENERS LUSCOMBE 8A 12336 4 POINT HARNESS FOUR POINT HARNESS FITTED INSTEAD OF LAP AND DIAGONAL STRAP & INSTALLATION OF CONTINENTAL A65-8 BSNT ADDITIONAL BRACKETS LUSCOMBE 8A 12337 TAIL PULL HANDLE B.A.S. TPH1 LIFT HANDLE FITTTED AT TAIL CONTINENTAL A65-8 BSNT LUSCOMBE 8A 14010 HERCULES 7051449-S PROPELLER INSTALLATION OF HERCULES 7051449-S 70 INCH DIAMETER X 51 INCH PITCH PROPELLER. CONTINENTAL A65-8 CCRK INSTALLATION LUSCOMBE 8A 14036 TO FIT OIL FILTER ADAPTER INSTALLATION OF OIL FILTER ADAPTER MANUFACTURED TO DRAWING M12465-A AND FITTED CONTINENTAL A65-8 CCRK WITH CHAMPION C138 FILTER. LUSCOMBE 8A 12474 PROPELLER CHANGE TO SENSENICH CHANGE OF PROPELLER TO SENSENICH W76CK-42 76" DIAMETER X 42" INCH PITCH. CONTINENTAL A65-8F BPOU W76CK-42 76" X 42" LUSCOMBE 8E 14613 ENGINE CHANGE TO CONTINENTAL C85- ENGINE REPLACED WITH C85-12 CONTINENTAL C85-12 BUAO 12 LUSCOMBE 8E 13313 ENGINE PRE-STARTER OILER MANUAL PRE-OILER SYSTEM INTRODUCED INTO MODIFIED MOUNTING FOR REMOTE OIL FILTER CONTINENTAL C85-12F BRHY

LUSCOMBE 8E 13195 INERTIA REEL UPPER TORSO RESTRAINT MOUNTING BEAM FITTED TO INSTALL INERTIA REEL UNITS TO ALLOW A MORE EFFECTIVE CONTINENTAL C85-12F LUSC INSTALLATION SHOULDER HARNESSES INSTALLATION. LUSCOMBE 8E 12886 ENGINE & PROPELLER CHANGE INSTALLATION OF CONTINENTAL C85-12F ENGINE WITH O-200-A COMPONENTS INSTALLED IN CONTINENTAL C85-12F (MODIFIED) BVGY ACCORDANCE WITH STC No. SE00979AT. INCLUDES O-200-A CRANKSHAFT, WHICH HAS 1/4" LONGER STROKE AND O-200-A PISTONS, WHICH ARE 0.11" SHORTER WHICH RESULTS IN A HIGHER COMPRESSION RATIO THAN THE C85 ENGINE OF 6.8:1. THE USE OF 95 RON UNLEADED FUEL TO BS EN 228 (AAN PFA-999-413 SUPPLEMENT 3 REFERS) AND TOTAL UL 91 FUEL (AAN LAA-999-413 SUPPLEMENT 5 REFERS) IS ACCEPTABLE FOR USE WITH THIS ENGINE SUBJECT TO COMPLIANCE WITH THE SPECIAL CONDITIONS DETAILED WITHIN THE AFOREMENTIONED AANs. WITH ABSENCE OF PROPELLER VIBRATION ANALYSIS DATA, METAL PROPELLERS ARE NOT AUTHORISED FOR USE WITH THIS ENGINE. EVRA D.11.28.4.C PROPELLER INSTALLED. LUSCOMBE 8E 13167 HERCULES 7050273-S 70" X 50" INSTALLATION OF HERCULES 7050273-S 70 INCH DIAMETER X 50 INCH PITCH PROPELLER. CONTINENTAL C85-12F (MODIFIED) BVGY PROPELLER. LUSCOMBE 8E 12657 ENGINE CHANGE TO C90-14F. ENGINE CHANGE TO C90-14F WITH MCCAULEY 1B90CM7151 PROPELLER FITTED. CONTINENTAL C90-14F BSSA

Prototype mods that have been approved since 1/1/2008 Page 61 30/11/20 LAA Technical Leaflet TL 3.17 LUSCOMBE 8E 13464 MCCAULEY 1A105/SCM7146 71" X 46" INSTALLATION OF MCCAULEY 1A105/SCM7146 71 INCH DIAMETER X 46 INCH PITCH PROPELLER. CONTINENTAL C90-16F AKUJ PROPELLER INSTALLATION LUSCOMBE 8E 13536 CONTINENTAL C90-16F ENGINE WITH INSTALLATION OF CONTINENTAL C90-16F ENGINE WITH MCCAULEY 1B90/CM 70" X 51" CONTINENTAL C90-16F AKUJ MCCAULEY 1B90/CM 70" X 51" PROPELLER. PROPELLER LUSCOMBE 8E 14398 HERCULES 6852531-S 68" X 52" INSTALLATION OF HERCULES 6852531-S 68 INCH DIAMETER X 52 INCH PITCH PROPELLER. CONTINENTAL C90-16F AKUJ PROPELLER INSTALLATION LUSCOMBE 8E 13011 ENGINE CHANGE TO CONTINENTAL O- ENGINE CHANGE TO CONTINENTAL O-200A WITH MCCAULEY 1B90/CM 71 INCH DIAMETER X 51 CONTINENTAL O-200-A AJKB 200A WITH MCCAULEY 1B90/CM 71" X INCH PITCH. 51" LUSCOMBE 8E 12684 ENGINE CHANGE TO CONTINENTAL O- ENGINE CHANGED TO 0-200A WITH MCCAULEY 1A90 71 x 51 PROPELLER CONTINENTAL O-200-A BPVZ 200A LUSCOMBE 8E 14868 INSTALLATION OF BAS TAIL PULL HANDLE BAS TAIL PULL HANDLE INSTALLED AS PER FAA STC SA3816NM. CONTINENTAL O-200-A BPVZ

LUSCOMBE 8E 12867 PROPELLER CHANGE TO MCCAULEY PROPELLER CHANGE TO MCCAULEY 1B90/CM 71" X 48" CONTINENTAL O-200-A BRGF 1B90/CM 71" X 48" LUSCOMBE 8E 13113 ROLLS ROYCE CONTINENTAL O-200-A ENGINE CHANGE TO ROLLS ROYCE CONTINENTAL O-200-A WITH MCCAULEY 1B90/CM 71 INCH CONTINENTAL O-200-A BRGF WITH MCCAULEY 1B90/CM7150 DIAMETER X 50 INCH PITCH PROPELLER. PROPELLER LUSCOMBE 8E 14242 CONTINENTAL O-200-A ENGINE AND INSTALLATION OF CONTINENTAL O-200-A ENGINE AND MCCAULEY 1A105/SCM 71 INCH DIAMETER CONTINENTAL O-200-A BTCH MCCAULEY 1A105/SCM 71" x 46" x 46 INCH PITCH PROPELLER. PROPELLER LUSCOMBE 8E 14682 INSTALLATION OF GROVE HYDRAULIC Installation of Grove wheels and brakes in accordance with STC SA02466AK (wheel and brake CONTINENTAL O-200-A BTJA DISC BRAKE SYSTEM & WHEELS - assembly 61-104). REPLACE SHINN / FRESTONE LUSCOMBE 8E 15323 INSTALLATION OF BAS SHOULDER INERTIA REEL SHOULDER HARNESSES INSTALLED IAW FAA STC SA01256SE. CONTINENTAL O-200-A BTJA HARNESS SYSTEM - PILOT & PASSENGER

LUSCOMBE 8F 13122 ENGINE CHANGE TO CONTINENTAL C90- CONTINENTAL C90-14F ENGINE FITTED WITH MCCAULEY IB90/CM 71" X 52" PROPELLER. CONTINENTAL C90-14F LUSK 14F LUSCOMBE 8F 12936 SPIN OIL FILTER ADAPTOR FOR ADAPTOR FOR CONTINENTAL C90-8F TO ACCEPT SPIN-ON OIL FILTERS. CONTINENTAL C90-8F EITE CONTINENTAL C90-8F ACCEPTABLE FILTERS INCLUDE THE CHAMPION C138, BLUE PRINT ADT32109 OR BLUE PRINT ADD62104 . LUSCOMBE 8F 12620 ENGINE CHANGE TO CONTINENTAL O- CONTINENTAL O-200A ENGINE INSTALLED WITH MCCAULEY 1A100/MCM 69 INCH DIAMETER X 50 CONTINENTAL O-200-A BSHI 200-A INCH PITCH PROPELLER.. LUTON LA4A MINOR 13127 NEWTON 44RC 70" X 44" PROPELLER INSTALLATION OF NEWTON TYPE 44RC 70 INCH DIAMETER X 44 INCH PITCH PROPELLER. LYCOMING O-145-A2 ATCN LUTON LA4A MINOR 12509 MODIFICATION TO UNDERCARRIAGE MODIFICATION TO WHEEL AXLES TO ACCEPT LIGHTWEIGHT WHEELS AS FITTED TO CFM STREAK VW 1800 AWMN AXLE SHADOW AIRCRAFT LUTON LA4A MINOR 13069 REPLACE LUCAS MAGNETOS WITH STANDARD LEBURG SYSTEM FITTED, INCLUDING INSTALLED BATTERY INSTALLATION VW 1800 AWMN LEBERG ELECTRIC SYSTEM LUTON LA4A MINOR 12430 PROPELLER CHANGE TO NEWTON TYPE CHANGE OF PROPELLER TO NEWTON TYPE 15L, 58 INCH DIA X 34 INCH PITCH. VW 1834 ASML 15L, 58 X 34 LUTON LA4A MINOR 13402 GREAT PLANES VW 1834 ENGINE GREAT PLANES VW 1834 ENGINE FITTED USING EXISTING ENGINE MOUNT. ENGINE FITTED WITH VW 1834 AYDY LEBURG EI 10A IGNITION SYSTEM. LUTON LA4A MINOR 13403 PROPELLER CHANGE TO NEWTON NEWTON 21L38 57" DIAMETER X 33" PITCH PROPELLER FITTED. VW 1834 AYDY LUTON LA4A MINOR 12656 PROPELLER CHANGE TO NEWTON TYPE PROPELLER CHANGE TO NEWTON TYPE 10L 54" DIAMETER X 33" PITCH. VW (PEACOCK) 1600 BBCY 10L 54" X 33" MARQUART MA5 CHARGER 14704 HERCULES 7355711-S 73" x 55" INSTALLATION OF HERCULES 7355711-S 73 INCH DIAMETER x 55 INCH PITCH PROPELLER LYCOMING O-320-E2A BHBT PROPELLER INSTALLATION MARQUART MA5 CHARGER 12388 DROP DOWN DOOR DROP DOWN HINGED DOOR ADDED TO REAR COCKPIT PER APPLICANT'S DRAWING LYCOMING O-360-A3A BVJX

Prototype mods that have been approved since 1/1/2008 Page 62 30/11/20 LAA Technical Leaflet TL 3.17 MARQUART MA5 CHARGER 13092 HERCULES 7256264-S 72" X 46" INSTALLATION OF HERCULES 7256264-S 72 INCH DIAMETER X 46 INCH PITCH PROPELLER. LYCOMING O-360-A3A BVJX PROPELLER MAVERICK 430 12398 ENGINE AND PROP CHANGE AND ENGINE CHANGE TO JABIRU 2200A WITH GT-2/157/100 PROPELLER FITTED AND WING TIP JABIRU 2200A MZJJ INCREASE IN MAX AUTHORISED GROSS EXTENSIONS REMOVED TO ENABLE INCREASE IN MAXIMUM AUTHORISED GROSS WEIGHT TO WEIGHT. 430KG. MAVERICK 430 13189 WARP DRIVE RPM 2 BLADED 66 INCH WARP DRIVE PROPELLER FITED PITCH 12.5 DEGREES AT TIP FITTED ROTAX 582 CFWO DIAMETER PROPELLER MCR-01 13566 FLAPPERON DRIVE SCREW SYSTEM REPLACEMENT FLAPPERON DRIVE SCREW AND SHEAVE NUTS LOCALLY MANUFACTURED ROTAX 912 CCTE FOLLOWING WEAR PROBLEMS WITH ORIGINAL PARTS. PULLEY RETAINED BY WOODRUFF KEY FOR IMPROVED SECURITY MCR-01 13097 TREAT FUEL TANK WITH PHENOL FUEL TANK TREATED WITH PHENOL NOVOLAC SEALANT IN ACCORDANCE WITH MANUFACTURER'S ROTAX 912 CCTE NOVOLAC INSTRUCTIONS, AND IMMERSION TESTS CARRIED OUT ON THE FIRST INSTALLATION USING BOTH AVGAS AND UNLEADED MOGAS CONTAIING ETHANOL. MCR-01 12507 REPLACEMENT GLASS FIBRE FUEL TANK ORIGINAL DYN AERO CARBON FBRE FUEL TANK REPLACED BY CUSTOM MOULDED GRP TANK OF ROTAX 912 CCTE SAME EXTERNAL SHAPE, PER APPLICANT'S LAY-UP DRAWING AND REINFORCEMENT DETAILS TITLED 'MOD 12507 FUEL TANK' MCR-01 14938 LOWER ENGINE MOUNT SPACERS SPACERS / PACKERS 3mm THICK INTRODUCED ON FRONT FACE OF FIREWALL AT LOWER MOUNT ROTAX 912-UL PGAC RAIL PADS TO CORRECT ENGINE THRUSTLINE WITH NEW TYPE GEARBOX FITTED. MCR-01 13642 AUDIBLE STALL WARNING ACI STALL WARNING DEVICE FITTED TO PORT WING LEADING EDGE IN ACCORDANCE WITH ACI ROTAX 912-ULS CGHT INSTRUCTIONS. MCR-01 13507 BERINGER BRAKE MOD BERINGER HYDRAULIC DISC BRAKES, WHEELS, AXLES AND STANDARD FITTING KIT SUBSTITUTED ROTAX 912-ULS CUTE PER APPLICANT'S SUBMISSION MCR-01 13322 FLAPPERON DRIVE SCREWS & CARRIAGE REPLACEMENT FLAPPERON DRIVE SCREW AND SHEAVE NUTS LOCALLY MANUFACTURED ROTAX 912-ULS CCUI FOLLOWING WEAR PROBLEMS WITH ORIGINAL PARTS. PULLEY RETAINED BY WOODRUFF KEY FOR IMPROVED SECURITY. MCR-01 12507 REPLACEMENT GLASS FIBRE FUEL TANK ORIGINAL DYN AERO CARBON FBRE FUEL TANK REPLACED BY CUSTOM MOULDED GRP TANK OF ROTAX 912-ULS CCUI SAME EXTERNAL SHAPE, PER APPLICANT'S LAY-UP DRAWING AND REINFORCEMENT DETAILS TITLED 'MOD 12507 FUEL TANK' MCR-01 13376 FLAPPERON DRIVE SCREWS AND REPLACEMENT FLAPPERON DRIVE SCREWS AND CARRIAGE SHEAVE NUT PER MOD 13322 ROTAX 912-ULS TOMX SHEAVES MCR-01 13097 TREAT FUEL TANK WITH PHENOL FUEL TANK TREATED WITH PHENOL NOVOLAC SEALANT IN ACCORDANCE WITH MANUFACTURER'S ROTAX 912-ULS TOMX NOVOLAC INSTRUCTIONS, AND IMMERSION TESTS CARRIED OUT ON THE FIRST INSTALLATION USING BOTH AVGAS AND UNLEADED MOGAS CONTAIING ETHANOL. MCR-01 12633 STALL WARNER APERTURE INSTALLED ON LEADING EDGE OF STARBOARD WING WITH PLASTIC TUBING TO AN ROTAX 912-ULS CFSK ELECTRONIC PRESSURE SENSOR IN THE FUSELAGE. MCR-01 13051 REPLACE THROTTLE INNER CABLE AND PIANO WIRE TYPE THROTTLE INNER CABLE REPLACED WITH STANDARD ROTAX STRANDED INNER ROTAX 912-ULS MCRO CHANGE THROTTLE SPRING BIAS CABLE. THROTTLE ALTERED TO SPRING OPEN, AS PER STANDARD ROTAX SET-UP. MCR-01 CLUB 12780 BERINGER HYDRAULIC BRAKE KIT FOR BERINGER BRAKES INSTALLED IN ACCORDANCE WITH BERINGER INSTRUCTIONS ROTAX 912-ULS LMLV DYNAERO MCR01 MCR-01 CLUB 13097 TREAT FUEL TANK WITH PHENOL FUEL TANK TREATED WITH PHENOL NOVOLAC SEALANT IN ACCORDANCE WITH MANUFACTURER'S ROTAX 912-ULS CBNL NOVOLAC INSTRUCTIONS, AND IMMERSION TESTS CARRIED OUT ON THE FIRST INSTALLATION USING BOTH AVGAS AND UNLEADED MOGAS CONTAIING ETHANOL. MCR-01 CLUB 14683 ARPLAST PV50 160R130/3 PROPELLER INSTALLATION OF ARPLAST PV50 160R130/3 1600MM DIAMETER ELECTRIC IN-FLIGHT ADJUSTABLE ROTAX 912-ULS CBNL INSTALLATION PROPELLER MCR-01 CLUB 12507 REPLACEMENT GLASS FIBRE FUEL TANK ORIGINAL DYN AERO CARBON FBRE FUEL TANK REPLACED BY CUSTOM MOULDED GRP TANK OF ROTAX 912-ULS RESG SAME EXTERNAL SHAPE, PER APPLICANT'S LAY-UP DRAWING AND REINFORCEMENT DETAILS TITLED 'MOD 12507 FUEL TANK' MCR-01 CLUB 14448 WOODCOMP SR3000/3N 1625MM INSTALLATION OF WOODCOMP SR3000/3N 1625MM DIAMETER PROPELLER. ROTAX 912-ULS RESG DIAMETER PROPELLER INSTALLATION MCR-01 CLUB 12490 FLOWSCAN FUEL FLOW TRANSDUCER INSTALLATION OF FLOWSCAN FUEL FLOW TRANSDUCER IN FUEL SYSTEM BETWEEN FUEL RETURN ROTAX 912-ULS KARK AND CARBURETTORS. WIRING AND INSTRUMENTATION PRE-EXISTING. Prototype mods that have been approved since 1/1/2008 Page 63 30/11/20 LAA Technical Leaflet TL 3.17 MCR-01 CLUB 12305 SOFT START MODULE INSTALLATION OF CON-AIR SPORTS SOFT START MODULE TO ROTAX 912-ULS ENGINE IN ROTAX 912-ULS DGHI ACCORDANCE WITH CON-AIR SPORTS INSTRUCTIONS AND SM12305 LEAFLET. MCR-01 CLUB 13097 TREAT FUEL TANK WITH PHENOL FUEL TANK TREATED WITH PHENOL NOVOLAC SEALANT IN ACCORDANCE WITH MANUFACTURER'S ROTAX 912-ULS DGHI NOVOLAC INSTRUCTIONS, AND IMMERSION TESTS CARRIED OUT ON THE FIRST INSTALLATION USING BOTH AVGAS AND UNLEADED MOGAS CONTAIING ETHANOL. MCR-01 CLUB 12507 REPLACEMENT GLASS FIBRE FUEL TANK ORIGINAL DYN AERO CARBON FBRE FUEL TANK REPLACED BY CUSTOM MOULDED GRP TANK OF ROTAX 912-ULS CDWG SAME EXTERNAL SHAPE, PER APPLICANT'S LAY-UP DRAWING AND REINFORCEMENT DETAILS TITLED 'MOD 12507 FUEL TANK' MCR-01 CLUB 14601 DYNON HEATED PITOT/AoA PROBE INSTALLATION OF A DYNON HEATED PITOT/AOA PROBE MOUNTED WITH CUSTOM MADE BRACKET ROTAX 912-ULS DECO INSTALLATION TO SAME STARBOARD WING FLAP HANGER AS ORIGINAL PITOT TUBE IN ACCORDANCE WITH APPLICANT'S SUBMISSION V2 16 OCTOBER 2017. MCR-01 CLUB 13097 TREAT FUEL TANK WITH PHENOL FUEL TANK TREATED WITH PHENOL NOVOLAC SEALANT IN ACCORDANCE WITH MANUFACTURER'S ROTAX 912-ULS CDGG NOVOLAC INSTRUCTIONS, AND IMMERSION TESTS CARRIED OUT ON THE FIRST INSTALLATION USING BOTH AVGAS AND UNLEADED MOGAS CONTAIING ETHANOL. MCR-01 CLUB 12597 FLOSCAN FUEL FLOW TRANSDUCER AND INSTALLATION OF FLOSCAN 201B-6 FUEL FLOW TRANSDUCER AND VDO FUEL PRESSURE ROTAX 912-ULS CGCN FUEL PRESSURE TRANSDUCER TRANSDUCER CONNECTED TO MGL AVIONICS ELECTRONIC DISPLAY. INSTALLATION MCR-01 ULC 12305 SOFT START MODULE INSTALLATION OF CON-AIR SPORTS SOFT START MODULE TO ROTAX 912-ULS ENGINE IN ROTAX 912-ULS CCMM ACCORDANCE WITH CON-AIR SPORTS INSTRUCTIONS AND SM12305 LEAFLET. MCR-01 ULC 13097 TREAT FUEL TANK WITH PHENOL FUEL TANK TREATED WITH PHENOL NOVOLAC SEALANT IN ACCORDANCE WITH MANUFACTURER'S ROTAX 912-ULS CCMM NOVOLAC INSTRUCTIONS, AND IMMERSION TESTS CARRIED OUT ON THE FIRST INSTALLATION USING BOTH AVGAS AND UNLEADED MOGAS CONTAIING ETHANOL. MCR-01 ULC 13729 PROPELLER CHANGE TO ARPLAST PV50 PROPELLER CHANGE TO PV50 CONSTANT SPEED UNIT. WEIGHT REDUCTION EXERCISE INCLUDING ROTAX 912-ULS CDBY 162 X 130/3 LIGHTWEIGHT BATTERY INSTALLATION AND LIGHTWEIGHT INSTRUMENTATION FIT AND ADJUSTABLE RUDDER PEDAL OPTION REMOVED MCR-01 ULC 14731 WOODCOMP SR200/3 1620MM INSTALLATION OF WOODCOMP SR200/3 1620MM DIAMETER X 25 DEGREES PITCH PROPELLER ROTAX 912-ULS CDLL DIAMETER X 25 DEGREES PITCH MEASURED 170MM FROM TIP PROPELLER INSTALLATION MIDGET MUSTANG 14125 PROPELLER CHANGE TO ED STERBA PROPELLER CHANGE TO STERBA 60" x 70" AFTER SPINNER BROKE FREE IN FLIGHT AND BROKE CONTINENTAL O-200-A AWIR FIXED PITCH ORIGINAL PROPELLER. REPLACEMENT SPINNER MADE TO SUIT INCLUDING FRONT PLATE PREVIOUSLY LACKING MIDGET MUSTANG 13917 SPIN-ON OIL FILTER ADAPTER FOR INSTALLATION OF CUSTOM MADE SPIN-ON OIL FILTER ADAPTER P/N 79001003 WITH CHAMPION CONTINENTAL 0-200A (MODIFIED) IIHX CONTINENTAL PC60 (O-200) CH48108 OR C138 OR BLUE PRINT ADT32109 OIL FILTER.

AT ISSUE 4: APPLICABILITY EXTENDED TO CONTINENTAL C90-12 ENGINE. AT ISSUE 6: APPLICABILITY EXTENDED TO CONTINENTAL C85-12F ENGINE. AT ISSUE 7: APPLICABILITY EXTENDED TO CONTINENTAL C90-14F ENGINE. MIDGET MUSTANG 13817 PROPELLER CHANGE TO HERCULES INSTALLATION OF HERCULES 6282427-S 62 INCH DIAMETER X 82 INCH PITCH PROPELLER. LYCOMING O-320-E3D IIJC 6282427-S MILES M38 MESSENGER 2A 14528 INSTALLATION OF AUX ELECTRIC FUEL FACET 480545 ELECTRIC FUEL PUMP INSTALLED AS BACK UP TO ENGINE DRIVEN PUMP BLACKBURN CIRRUS MAJOR III AKBO PUMP AND SWITCH MILES M38 MESSENGER 2A 15228 ELECTRIC BACKUP PUMP & GASCOLATOR ELECTRIC BACK UP PUMP AND GASCOLATOR FITTED FOR ADDITIONAL FUEL SYSTEM INTEGRITY BLACKBURN CIRRUS MAJOR III AIEK

MILES M38 MESSENGER 2A 15229 DISC BRAKE CONVERSION HYDRAULIC DISC BRAKE SYSTEM FROM CHIPMUNK REPLACES AUSTER TYPE MECHANICAL DRUM BLACKBURN CIRRUS MAJOR III AIEK BRAKES MILES M65 GEMINI 1A 14606 HOFFMANN HO20-175-140L PROPELLERS INSTALLATION OF HOFFMANN HO20-175-140L PROPELLERS BLACKBURN CIRRUS MINOR 2A AKKH INSTALLATION MINICAB (JB01 STANDARD) 13734 ALTERNATIVE PAINT SYSTEM . CONTINENTAL C90-14F BGMR

Prototype mods that have been approved since 1/1/2008 Page 64 30/11/20 LAA Technical Leaflet TL 3.17 MINICAB (JB01 STANDARD) 14056 ENLARGED COMPOSITE FUEL TANK INSTALLATION OF NEW LARGER (70 LITRE) CAPACITY KEVLAR/CARBON FIBRE COMPOSITE FUEL CONTINENTAL C90-14F BGMR INSTALLATION TANK IN PLACE OF EXISTING ORIGINAL POLYESTER/CHOPPED STRAND MAT 60 LITRE TANK.

MINICAB (JB01 STANDARD) 14057 DYNON PITOT/AOA HEAD AND INSTALLATION OF DYNON PITOT/ANGLE OF ATTACK HEAD TO REPLACE ORIGINAL PITOT/STATIC CONTINENTAL C90-14F BGMR REPOSITIONED STATIC SOURCE TUBES. STATIC SOURCE PLATES INSTALLED IN BOTH FUSELAGE SIDES REAR OF COCKPIT AND INSTALLATION FITTED WITH DAMS TO REDUCE POSITION ERRORS. MINICAB (JB01 STANDARD) 13003 REPLACEMENT FUEL SELECTOR VALVE ANDAIR FS20 TYPE 2 FUEL SELECTOR VALVE FITTED. PLACARD REQUIRED SPECIFYING THAT TO CONTINENTAL C90-8F AWEP AVOID RISK OF FUEL STARVATION FRONT TANK MUST BE USED FOR TAKE OFF AND LANDING MINICAB (JB01 STANDARD) 14234 WHEEL AND BRAKE UPGRADE ORIGINAL WHEELS REPLACED AND DRUM BRAKES REPLACED WITH MATCO WHLF160L WHEEL AND CONTINENTAL C90-8F AWEP HYDRAULIC BRAKE KIT, USING VARIOUS OFF THE SHELF AND CUSTOM FITTINGS. MINICAB (JB01 STANDARD) 14340 FUEL TRANSFER PUMP INSTALLATION INSTALLATION OF FACET POSI-FLO 60300 FUEL TRANSFER PUMP WITH NON-RETURN VALVE CONTINENTAL C90-8F AWEP INCORPORATED AND ANDAIR FS22 DUPLEX FUEL SELECTOR VALVE TO ALLOW TRANSFER OF FUEL FROM THE 35 LITRE REAR MOUNTED AUXILIARY FUEL TANK TO THE 50 LITRE FORWARD MOUNTED MAIN FUEL TANK. MEASURED FLOW RATE WAS 75 LPH. ENGINE IS GRAVITY FED FROM THE MAIN FUEL TANK ONLY. TO PREVENT FRONT TANK OVER-FILL IN THE EVENT OF THE TRANSFER PUMP RUNNING WHEN THE FRONT TANK IS FULL, A FLOAT OPERATED 'SNORKEL' VALVE REDUCES TRANSFER FLOW RATE TO NOT EXCEED ENGINE CONSUMPTION. MINICAB (JB01 STANDARD) 14920 HERCULES 6852702-S 68" x 52" INSTALLATION OF HERCULES 6852702-S 68 INCH DIAMETER X 52 INCH PITCH PROPELLER. CONTINENTAL C90-8F AWEP PROPELLER INSTALLATION MINICAB (JB01 STANDARD) 14602 SPIN-ON OIL FILTER ADAPTER INSTALLATION OF A JPM AVIATION 79001002 SPIN-ON OIL FILTER ADAPTER ONTO CONTINENTAL CONTINENTAL C90-8F AWEP INSTALLATION C85-8F ENGINE AND FITTED WITH A BLUEPRINT ADT32109 OIL FILTER.

ISSUE 2 RAISED TO INCLUDE CONTINENTAL A65-8F ENGINE. ISSUE 3 RAISED TO INCLUDE CONTINENTAL C90-8F ENGINE. MINICAB (JB01 STANDARD) 13757 PROPELLER CHANGE TO CHRIS LODGE CJL LODGE CJL 110A 70 INCH DIAMETER X 50 INCH PITCH PROPELLER INSTALLATION. CONTINENTAL O-200-A ATPV 110A 70 X 50 MINICAB (JB01 STANDARD) 14233 CONTINENTAL O-200A ENGINE & INSTALLATION OF A CONTINENTAL O-200-A ENGINE WITH A HERCULES 6850448-S 68 INCH CONTINENTAL O-200-A ATPV HERCULES 6850448-S PROPELLER DIAMETER X 50 INCH PITCH PROPELLER. INSTALLATIONS MINICAB (JB01 STANDARD) 13977 TORQUE LINKS INSTALLATION ON MAIN MANUFACTURE AND INSTALLATION OF MAIN UNDERCARRIAGE TORQUE LINKS TO SUPPLEMENT CONTINENTAL O-200-A BRGW UNDERCARRIAGE LEGS THE ORIGINAL INTERNAL MATCHED SHAPE PISTON AND LEG DESIGN TO REDUCE WEAR RATE AND SO MINIMISE MAINTENANCE REQUIREMENT. MINICAB (JB01 STANDARD) 13018 PROPELLER CHANGE TO HERCULES 70" X INSTALLATION OF HERCULES 7049255 70 INCH DIAMETER X 49 INCH PITCH PROPELLER. CONTINENTAL PC60 BDGB 49" MINICAB GY 201 14834 HERCULES 7051449-S 70" x 51" INSTALLATION OF HERCULES 7051449-S 70 INCH DIAMETER x 51 INCH PITCH PROPELLER. CONTINENTAL A65-12 BCPD PROPELLER INSTALLAION MINICAB GY 201 13161 GENERATOR & ELECTRICAL SYSTEM GENNIPOD WIND-DRIVEN ALTERNATOR FITTED UNDER FUSELAGE BELLY PER APPLICANT'S CONTINENTAL A65-8F BGMJ SUBMISSION, TO PROVIDE POWER FOR SIMPLE 12V ELECTRICAL SYSTEM. ADDITIONAL PLACARD FITTED STATING VNE IS 96 KIAS WITH GENNIPOD FITTED. MINICAB GY201 (MODIFIED) 13323 HERCULES 6853319-S 68" X 53" INSTALLATION OF HERCULES 6853319-S 68 INCH DIAMETER X 53 INCH PITCH PROPELLER. CONTINENTAL C85-12F BBFL PROPELLER MISSION M108 14652 FUEL PUMP SYSTEM FUEL PUMP SELECTOR ROCKER SWITCH REPLACED WITH TWO SEPARATE ON-OFF SWITCHES, ONE ROTAX 912-iS STUZ FOR EACH PUMP. MONNETT SONERAI 1 13702 PROPELLER CHANGE TO STERBA 54" X INSTALLATION OF STERBA 54 INCH DIAMETER X 42 INCH PITCH PROPELLER. VW 1834 LOWE 42" MONNETT SONERAI 1 15156 INSTALLATION OF LEBURG ELECTRONIC STANDARD MAGNETOS REPLACED WITH LEBURG ELECTRONIC IGNITION MODULES. VW 1834 LOWE IGNITION INCORPORATES TWO YUASA BATTERIES, HONDA ALTERNATOR AND ASSOCIATED WIRING AND SWITCHING. INSTALLATION MADE IN ACCORDANCE WITH LEBURG INSTALLATION MANUAL DATED JAN 2013 WITH THE ADDITION OF CIRCUIT PROTECTION ON EACH IGNITION MODULE.

Prototype mods that have been approved since 1/1/2008 Page 65 30/11/20 LAA Technical Leaflet TL 3.17 MONNETT SONERAI 2 14015 INSTALLATION OF LEBURG IGNITION LEBURG EI10A DUAL ELECTRONIC IGNITION SYSTEM INSTALLED, INCORPORATING MAGNET AND REVMASTER R2100D BMIS SYSTEM SENSOR MOUNTS, REVMASTER ALTERNATOR, MAIN AND BACKUP BATTERIES AND ASSOCIATED ELECTRONICS AND WIRING. BATTERY STATES MONITORED BY VOLTMETERS. MONTGOMERIE-BENSEN B8MR 13859 PROPELLER CHANGE TO IVOPROP 52" INSTALLATION OF IVOPROP 3 BLADED 52 INCH DIAMETER GROUND ADJUSTABLE PROPELLER. ROTAX 532 BUJK

MONTGOMERIE-BENSEN B8MR 13639 TREATMENT OF FIBREGLASS FUEL TANK GLASS FIBRE FUEL TANKS REMOVED FROM , REINFORCED WITH FURTHER GLASS FIBRE ROTAX 582 BTIG WITH PHENOL EXTERNALLY AND SEALED INTERNALLY WITH PHENOL NOVOLAC TREATMENT, THEN REPLACED

MONTGOMERIE-BENSEN B8MR 12614 PROPELLER CHANGE TO IVOPROP 3 PROPELLER CHANGE TO IVOPROP 3 BLADED 60 INCH DIAMETER WITH MECHANICAL GROUND ROTAX 582 BXCL BLADED 60 INCH DIA GROUND ADJUSTMENT. ADJUSTABLE MONTGOMERIE-BENSEN B8MR 12730 ROTOR BLADE CHANGE TO MCCUTCHEN MAX GROSS WEIGHT INCREASED TO 295 Kg ROTAX 582 BWAH 23' DIAMETER MONTGOMERIE-BENSEN B8MR 12459 Drop Keel Conversion REAR PORTION OF KEEL REMOVED AND REPLACED WITH DROP KEEL. MODIFIED ENGINE ROTAX 582 CBFW SUPPORTS. GEARBOX INVERTED. REDUCED DIAMETER PROPELLER FITTED. MAIN WHEEL AXLE LINE RAISED BY 2" BY USE OF AXLE BLOCKS. DRAG LINKS AND ASSOCIATED BRACKETS FITTED. EXHAUST REPOSITIONED. CRICKET FIN AND RUDDER FITTED. MONTGOMERIE-BENSEN B8MR 13098 ALUMINIUM FUEL TANK ALUMINIUM FUEL TANK OF WELDED CONSTRUCTION FITTED AFTER ORIGINAL COMPOSITE TANK ROTAX 912-UL CBSV DEVELOPED LEAKS. MONTGOMERIE-BENSEN B8MR 14236 PROPELLER CHANGE TO WOODCOMP WOODCOMP SR200/3 1550mm DIA SUBSTITUTED ROTAX 912-UL CBNX SR200 MONTGOMERIE-BENSEN B8MR 13639 TREATMENT OF FIBREGLASS FUEL TANK GLASS FIBRE FUEL TANKS REMOVED FROM NACELLE, REINFORCED WITH FURTHER GLASS FIBRE ROTAX 912-UL BZOF WITH PHENOL EXTERNALLY AND SEALED INTERNALLY WITH PHENOL NOVOLAC TREATMENT, THEN REPLACED

MONTGOMERIE-PARSONS TWO 12550 ENGINE CHANGE TO ROTAX 618UL ENGINE CHAGED FOR ROTAX 618 USING EXSITING ENGINE MOUNT AS ON G-UNIV ROTAX 618 CDGT PLACE MORANE SAULNIER MS.315E D2 13260 ENGINE CHANGE TO ROTEC R3600 ROTEC R3600 ENGINE SUBSTITUTED USING CUSTOM DESIGNED ENGINE MOUNT ROTEC R3600 BZNK

MORANE SAULNIER MS.317 13679 PROPELLER CHANGE TO HERCULES CUSTOM MADE HERCULES PROPELLER INSTALLED DESIGNED AND MANUFACTURED USING CONTINENTAL W670-6A MOSA STANDARD HERCULES METHOD MOSLER N3 PUP 14002 CATEGORY CHANGE TO MICROLIGHT CATEGORY CHANGE TO MICROLIGHT FOLLOWING REVIEW AGAINST CURRENT MICROLIGHT MOSLER MMCB-35 BVEA DEFINITION, INCLUDING CALIBRATED STALL SPEED CHECKS. NOISE CERTIFICATE OBTAINED MURPHY ELITE 12881 ELEVATOR IMPROVEMENT TO CREATE SATISFACTORY ELEVATOR CENTERING CHARACTERISTICS, ELEVATOR AERODYNAMIC WILKSCH WAM-120 ONIG BALANCE DRASTICALLY REDUCED IN AREA AND ELEVATOR TRAILING EDGE THICKENED

MW5D SORCERER 12846 FITTING BRAKES TO MAIN WHEELS CONVENTIONAL WHEEL BRAKE SYSTEM FITTED TO BOTH MAIN WHEELS PER APPLICANT'S ROTAX 447 MYJZ SUBMISSION MW5D SORCERER 12847 ELECTRIC START SYSTEM STANDARD ROTAX ELECTRIC START INSTALLATION AND SUITABLE BATTERY INSTALLATION. ALL ROTAX 447 MYJZ POSITIVE CONNECTIONS TO BE INSULATED BY SUITABLE RUBBER BOOTS, MW6-S (MODIFIED) 14046 ENGINE CHANGE TO ROTAX 532UL ENGINE REPLACED BY ROTAX 532 AND PROPELLER BY IVOPROP 64" DIA THREE BLADED WITH 11 ROTAX 532 MZHG DEGREE PITCH SET MW6-S (MODIFIED) 12387 STRUCTURAL MODS TO ALLOW AN MW MISC 10/11/12/13 DRAWINGS INCORPORATED. ROTAX 582 MYDM INCREASE IN MAUW AIRCRAFT CURRENTLY ONLY CLEARED WITH MAUW OF 390 KG PENDING FLIGHT TEST PROGRAM AT INCREASED WEIGHT OF 415 KG. MW7 12558 ELECTRIC CARBURETTOR HEATING CYCLONE ELECTRIC CARBURETTOR HEATERS FITTED PER STANDARD CYCLONE INSTRUCTIONS ROTAX 503 BREE MW7 13231 ENGINE CHANGE TO ROTAX 503 WITH ROTX 503 ENGINE FITTED, WITH WARP DRIVE RPM 2 BLADED PROPELLER ROTAX 503 BWVN WARP DRIVE PROPELLER

Prototype mods that have been approved since 1/1/2008 Page 66 30/11/20 LAA Technical Leaflet TL 3.17 NICOLLIER HN 700 MENESTREL II 12568 INSTALL AIRWORLD SKYFLASH STROBE AIRWORLD SKYFLASH STROBE SYSTEM INSTALLED. ONE STREAMLINED STROBE UNIT SCREWED JABIRU 2200A CCCJ SYSTEM AND BONDED TO THE UPPER REAR FUSELAGE SECTION 48" AFT OF THE REAR OF THE TRANSPARENCY. A SECOND SCREWED TO THE LOWER REAR FUSELAGE 3" AFT OF THE TRAILING EDGE OF THE WING. POWER UNIT INSTALLED ON REAR BULKHEAD OF PARCEL SHELF. INCLUDES ASSOCIATED WIRING, SWITCH AND CIRCUIT BREAKER. NICOLLIER HN 700 MENESTREL II 13971 HARNESS RESTRAINT SHOULDER HARNESS ATTACHMENTS INSTALLED, CONSISTING OF A TANG ATTACHED TO THE JABIRU 2200A CHRE TAILWHEEL MOUNT ASSEMBLY AND P1 AND P2 TANGS MOUNTED ON THE REAR SHELF WITH ADDITIONAL LOCAL REINFORCEMENTS TO REAR SHELF. SHOULDER HARNESS ATTACHMENT TANGS CONNECTED TO TANG AT TAILWHEEL VIA TWO 1/8" 7X19 GALVANISED STEEL CABLES AND TURNBUCKLES. NICOLLIER HN 700 MENESTREL II 14629 PROPELLER CHANGE TO NEWTON 11R NEWTON 11R 60" X 44" INSTALLED JABIRU 2200A CHRE

NICOLLIER HN 700 MENESTREL II 12948 PROPELLER CHANGE TO NEWTON 09L INSTALLATION OF NEWTON TYPE 09L 54 INCH DIAMETER X 43 INCH PITCH PROPELLER REVMASTER R2300 VIVO 54" X 43" NICOLLIER HN 700 MENESTREL II 13043 PROPELLER CHANGE TO HERCULES INSTALLATION OF HERCULES 5742246 57 INCH DIAMETER X 42 INCH PITCH PROPELLER. REVMASTER R2300 VIVO 5742246 57" x 42" NICOLLIER HN 700 MENESTREL II 13659 INSTALLATION OF REVMASTER R2300 23- INSTALLATION OF REVMASTER R2300 23-0113 ENGINE AND HERCULES 5842379-S 58 INCH REVMASTER R2300 VIVO 0113 ENGINE AND HERCULES 5842379-S DIAMETER X 42 INCH PITCH PROPELLER. PROPELLER NICOLLIER HN 700 MENESTREL II 14351 FITTING OF ELEVATOR TRIM TAB MANUALLY OPERATED ELEVATOR TRIM TAB FITTED, USING HINGED TRIM TAB INSET INTO REVMASTER R2300 CIOR ELEVATOR AND ASSOCIATED CABLE AND HAND LEVER SYSTEM. NICOLLIER HN 700 MENESTREL II 14390 SHOULDER HARNESS ATTACH REAR ALTERNATIVE DESIGN OF REINFORCEMENT OF REAR SHELF TO ACCEPT SHOULDER HARNESS REVMASTER R2300 CIOR SHELF REINFORCEMENT FITTINGS AND ASSOCIATED CRASH CASE LOADS NICOLLIER HN 700 MENESTREL II 14047 ELEVATOR TRIM TAB ADDITION OF ELEVATOR TRIM TAB CONSISTING OF A WOOD AND FABRIC TAB MOUNTED ON A VW 2180 CCDS FALSE SPAR ON THE INBOARD END OF THE PORT ELEVATOR. CONTROLLED VIA A CABLE ACTUATED BY A CONTROL WHEEL LOCATED ON THE PORT SIDE OF THE COCKPIT. NICOLLIER HN 700 MENESTREL II 14048 BRAKE OPERATION FOOT OPERATED BRAKES INSTALLED BY INSERTING MDO MASTER CYLINDERS BETWEEN THE TOE- VW 2180 CCDS OPERATED SECTION OF EACH PILOT'S RUDDER PEDAL AND BRACKETS MOUNTED ON THE FLOOR FORWARD OF THE PEDALS. FLOOR IS LOCALLY REINFORCED USING PLYWOOD PLATES. NICOLLIER HN 700 MENESTREL II 14049 3 POINT HARNESS TRS 3-POINT HARNESSES HAVE BEEN INSTALLED USING A CUSTOM ARRANGEMENT TO SECURE THE VW 2180 CCDS UPPER ATTACHMENT POINT OF EACH. EACH HARNESS ATTACHES TO A TANG FASTENED TO A REINFORCED SECTION OF THE PARCEL SHELF BEHIND THE SEATS. THE LOWER PART OF EACH TANG ASSEMBLY ATTACHES VIA A TURNBUCKLE AND 1/8" 19 STRAND STEEL CABLE TO A TANG ATTACHED TO THE TAILWHEEL SPRING STRUCTURE.

NICOLLIER HN 700 MENESTREL II 14050 CANOPY TO CANOPY FRAME CANOPY BONDED TO WOOD AND CARBON COMPOSITE FRAME USING SIKAFLEX 295UV ADHESIVE. VW 2180 CCDS

NICOLLIER HN 700 MENESTREL II 14317 LEBURG IGNITION SYSTEM LEBURG ELECTRONIC DUAL IGNITION SYSTEM INSTALLED, CONSISTING OF IGNITION CONTROLLERS, VW 2180 CCDS COILS, SENSORS AND A TIMING DISC. SYSTEM INCORPORATES CURRENT PROTECTION OF IGNITION MODULES AND TWO BATTERIES INSTALLED ON FORWARD FACE OF FIREWALL. SYSTEM INSTALLED AS PER MANUFACTURER'S INSTRUCTIONS. NICOLLIER HN 700 MENESTREL II 12674 PROPELLER CHANGE TO NEWTON TYPE PROPELLER CHANGE TO NEWTON TYPE 15L 58" X 38" VW (AEROVEE) 2180 (MODIFIED) CDZR 15L 58" X 38" NICOLLIER HN 700 MENESTREL II 14086 PRINCE P-TIP 58" X 38" PROPELLER INSTALLATION OF PRINCE P-TIP 58 INCH DIAMETER X 38 INCH PITCH PROPELLER. VW (AEROVEE) 2180 (MODIFIED) CDZR INSTALLATION NICOLLIER HN 700 MENESTREL II 14178 AEROVEE UPGRADE, INSTALLATION OF INSTALLATION OF GREAT PLANES AIRCRAFT'S FORCE ONE PROPELLER HUB, ROTEC TBI-34-2 VW (AEROVEE) 2180 (MODIFIED) CDZR FORCE ONE PROP HUB & ROTEC TBI-34-2 THROTTLE BODY INJECTOR AND CABIN/CARBURETTOR HEATER.

Prototype mods that have been approved since 1/1/2008 Page 67 30/11/20 LAA Technical Leaflet TL 3.17 NICOLLIER MENESTREL 2 14402 INTERNAL CANOPY HINGES WITH GAS MANUFACTURE AND INSTALLATION OF INTERNALLY MOUNTED CANOPY HINGE ARMS AND JABIRU 2200A CKGJ STRUT ASSIST AND HOOK LATCHES CANOPY OVER-CENTRE HOOK-LATCH SYSTEM. TO AID RESCUE, SIMPLE SPRING SYSTEM CAUSES LATCH TO LOCK OPEN WHEN OPERATED FROM OUTSIDE. NICOLLIER MENESTREL 2 14403 MATERIAL ALTERATIONS FROM FRENCH USE OF SUBSTITUTE MATERIALS AS PER JODEL D18 LIST: 4130H IN PLACE OF ALL STEEL PARTS, JABIRU 2200A CKGJ SPEC 2024T3 IN PLACE OF AU64 AND 5754-0 IN PLACE OF A63. NICOLLIER MENESTREL 2 11954 ELEVATOR TRIM TAB FITTED ELEVATOR TRIM TAB FITTED DRIVEN BY MAC SERVO JABIRU 2200A CKGJ NICOLLIER MENESTREL 2 14050 CANOPY TO CANOPY FRAME CANOPY BONDED TO WOOD AND CARBON COMPOSITE FRAME USING SIKAFLEX 295UV ADHESIVE. JABIRU 2200A CKGJ

NICOLLIER MENESTREL 2 15055 3 POINT HARNESS 3 POINT HARNESSES FITTED TO BOTH SEATS, CONSISTING OF: JABIRU 2200A CKGJ - SPARCO 3-POINT HARNESSES FITTED (P/N MPN 4608BVS) - TANGS ON PARCEL SHELF AS PER MOD 14049 - PLY REINFORCEMENT ON PARCEL SHELF AS PER MOD 14390 - REAR ATTACHMENT TO TAILSKID SIMILAR TO MOD 14049 - 1/8" STEEL CABLES USED AS BOTH MOD 14390 AND 14049 NIPPER T.66 RA45 SERIES 3 13004 REPLACEMENT OF U/C NIEMAN RINGS NIEMAN RINGS REPLACED BY 2 OFF 1080 STANDARD (NOT HD) BUNGEES, DOUBLE-WRAPPED JABIRU 2200A AVKK WITH 1080 BUNGEES RINGS SO THAT EACH LEG IS SUPPORTED BY FOUR CORDS OF BUNGEE. NIPPER T.66 RA45 SERIES 3 12611 REPLACE MAINWHEEL BRAKE CALIPER MAINWHEEL BRAKES REPLACED WITH DISC BRAKE SYSTEM SAUER SE 1800 E2S AVKI NIPPER T.66 RA45 SERIES 3 13259 AILERON PUSHROD MODIFICATION AILERON PUSHROD REDESIGNED WITH CONVENTIONAL ROD END FITTINGS AT EACH END VW 1834 NIPP NIPPER T.66 RA45 SERIES 3 14837 FIT NEW FUEL TANK REPLACEMENT FUEL TANK MANUFACTURED IN WELDED ALUMINIUM, REPLACING FIBREGLASS VW 1834 AWJE COMPONENT NIPPER T.66 RA45 SERIES 3 12862 PROPELLER CHANGE LODGE CJL 125 56 x 34 PROPELLER SUBSTITUTED VW 1834 BRIK NIPPER T.66 RA45 SERIES 3 14662 LODGE CJL 125, 56" x 35" PROPELLER INSTALLATION OF LODGE CJL 125, 56 INCH DIAMETER X 35 INCH PITCH PROPELLER. VW 1834 BRIK INSTALLATION NIPPER T.66 RA45 SERIES 3 13241 NIPPER T66 LONG TIP TANKS NIPPER TIP TANKS FITTED PER ORIGINAL DRAWINGS VW (ARDEM) 4C02 MK.6 NIPR NIPPER T.66 RA45 SERIES 3 13004 REPLACEMENT OF U/C NIEMAN RINGS NIEMAN RINGS REPLACED BY 2 OFF 1080 STANDARD (NOT HD) BUNGEES, DOUBLE-WRAPPED VW (ARDEM) 4C02 MK.6 NIPR WITH 1080 BUNGEES RINGS SO THAT EACH LEG IS SUPPORTED BY FOUR CORDS OF BUNGEE. NIPPER T.66 RA45 SERIES 3 14065 CHANGE NOSE LEG NEIMAN RINGS FOR MINOR CHANGE TO NOSELEG TO ACCEPT BUNGEE CORD RINGS OF 1080 TYPE RATHER THAN VW (ARDEM) 4C02 MK.6 NIPR BUNGEE SHOCK CORD RING ORIGINAL NIEMAN RING SHOCK ELEMENTS. NIPPER T.66 RA45 SERIES 3 13004 REPLACEMENT OF U/C NIEMAN RINGS NIEMAN RINGS REPLACED BY 2 OFF 1080 STANDARD (NOT HD) BUNGEES, DOUBLE-WRAPPED VW (ARDEM) 4C02 MK.X BLMW WITH 1080 BUNGEES RINGS SO THAT EACH LEG IS SUPPORTED BY FOUR CORDS OF BUNGEE. NIPPER T.66 RA45 SERIES 3 14667 HERCULES 5636272-S 56" x 36" INSTALLATION OF HERCULES 5636272-S, 56 INCH DIAMETER X 36 INCH PITCH PROPELLER. VW (ARDEM) 4C02 MK.X BLMW PROPELLER INSTALLATION. NIPPER T.66 RA45 SERIES 3 13691 EXHAUST SYSTEM TWIN TWO-INTO-ONE EXHAUST PIPES FITTED INSTEAD OF FOUR SEPARATE STUBS, INCLUDING VW (ARDEM) 4C02 MK.X (MOD) AXLI EXPANSION SLIP JOINTS AND CARB HEAT MUFF NORD 1002 13902 INTRODUCTION OF CHT MONITORING WESTACH CHT GAUGE INSTALLED ON ALLOY BRACKET BELOW INSTRUMENT PANEL. CYLINDER RENAULT 6Q10B ATBG SELECTOR SWITCH MOUNTED ON INSTRUMENT PANEL. CHT PROBES MOUNTED UNDER EACH SPARK PLUG. WIRING TO CONNECT PROBES TO SWITCH AND GAUGE.

NOTE: IN FLIGHT, SELECTOR TO BE SET TO CYLINDER NUMBER 5.

THE FOLLOWING TEMPERATURE LIMITS ARE RECOMMENDED: MAXIMUM: 550°F (1 MINUTE OR LESS) CLIMB MAXIMUM: 525°F (5 MINUTES OR LESS) CRUISE MAXIMUM: 475°F (15 MINUTES OR LESS) MAXIMUM CONTINUOUS: 450°F NORD NC854 14773 FITTING FULL SEAT HARNESS TO PILOT ATTACHMENTS FOR SHOULDER HARNESSES INSTALLED TO TUBULAR STRUCTURE. CONTINENTAL A65-8F NORD AND PASSENGER POSITIONS NORD NC854S 12695 PROPELLER CHANGE TO YATES J3 C65 70" ORIGINAL YATES J3 C65 72" DIAMETER X 42" PITCH PROPELLER CROPPED TO 70" DIAMETER TO CONTINENTAL A65-8 BGEW X 42" INCREASE RPM.

Prototype mods that have been approved since 1/1/2008 Page 68 30/11/20 LAA Technical Leaflet TL 3.17 NORD NC854S 15041 GENI POD INSTALLATION GENNIPOD MOUNTED UNDER FUSELAGE BELLY USING SUITABLE BRACKET ARRANGEMENT. CONTINENTAL A65-8F BCGH ELECTRICAL SYSTEM MODIFIED TO INCLUDE GENNIPOD SYSTEM AND BATTERY NORD NC854S 12625 MODIFICATION OF ENGINE MOUNT TO ENGINE MOUNT MODIFIED BY REPLACING TWO STRAIGHT MEMBERS WITH CURVED MEMBERS OF CONTINENTAL C90-12F BIUP ACCEPT NEW ENGINE GREATER WALL THICKNESS AND THE ADDITION OF A NEW MEMBER, TO ACCOMMODATE A CHANGE IN ENGINE FROM A C65 TO A C90. NORD NC854S 12892 PROPELLER CHANGE TO SENSENICH W72GK PROPELLER SUBSTITUTED TO MATCH C90 ENGINE NOW FITTED CONTINENTAL C90-12F BIUP W72GK-50 NORD NC854S 13501 HERCULES 7046347-S 70" X 46" INSTALLATION OF HERCULES 7046347-S 70 INCH DIAMETER X 46 INCH PITCH PROPELLER CONTINENTAL C90-12F BIUP PROPELLER INSTALLATION NORD NC858S 14457 PROPELLER CHANGE TO CHRIS LODGE PROPELLER CHANGED TO LODGE CJL 100 72" X 47". CONTINENTAL C90-14F BPZD DRG100 PARNALL ELF II 14075 2M50 FUEL PUMP INSTALLATION INSTALLATION OF AN OVERHAULED 2M50 DOUBLE DIAPHRAGM FUEL PUMP AS USED ON THE CIRRUS HERMES II AAIN WALTER MINOR SERIES ENGINE FITTED WITH A CUSTOM MADE CIRRUS TO WALTER FUEL PUMP ADAPTOR. PAZMANY PL-2 12971 PROPELLER CHANGE TO HERCULES 68" X INSTALLATION OF HERCULES 6853244 68 INCH DIAMETER X 53 INCH PITCH PROPELLER LYCOMING O-235-C2C OPAZ 53" PELICAN CLUB 13245 WING STRUT IN REPAIRING ACCIDENT DAMAGE, SUBSTITUTE MATERIAL USED FOR WING STRUTS AS ORIGINAL ROTAX 912-UL BWWA MATERIAL NO LONGER AVAILABLE PELICAN PL 14748 ENGINE CHANGE TO ROTAX 912 ULS ROTAX 912-ULS ENGINE INSTALLED WITH WOODCOMP PROPULS AES 170 PROPELLER. ROTAX 912-ULS MPAC PIEL CP.1320 12729 CHANGE MATERIAL USED IN MAIN INSTALLATION OF GROVE GAC-6104-75 ALUMINIUM ALLOY UNDERCARRIAGE AND ASSOCIATED LYCOMING O-320-A2B CFIH UNDERCARRIAGE FITTINGS. PIEL CP301A 13917 SPIN-ON OIL FILTER ADAPTER FOR INSTALLATION OF CUSTOM MADE SPIN-ON OIL FILTER ADAPTER P/N 79001003 WITH CHAMPION CONTINENTAL C90-12F PIEL CONTINENTAL PC60 (O-200) CH48108 OR C138 OR BLUE PRINT ADT32109 OIL FILTER.

AT ISSUE 4: APPLICABILITY EXTENDED TO CONTINENTAL C90-12 ENGINE. AT ISSUE 6: APPLICABILITY EXTENDED TO CONTINENTAL C85-12F ENGINE. AT ISSUE 7: APPLICABILITY EXTENDED TO CONTINENTAL C90-14F ENGINE. PIEL CP301A 12767 PROPELLER CHANGE TO RWG 105 69" X PROPELLER CHANGE TO RWG 105 69" X 50" CONTINENTAL C90-14F ARRS 50" PIEL CP301A 12895 EVRA D.11.28.7.C PROPELLER CHANGE TO EVRA D.11.28.7.C CONTINENTAL C90-14F ARRS PIEL CP301A 13555 F & M ENTERPRISES T.A.F.-L SPIN ON OIL F&M ENTERPRISES T.A.F.-L OIL FILTER ADAPTER FITTED PER STC SE7559SW. FILTERS ACCEPTABLE CONTINENTAL C90-14F BDCI FILTER ADAPTOR FITMENT CHAMPION CH48108-1, TEMPEST AA-48108, CHALLENGER AVIATION CP-48108-C.

PIEL CP301A 14700 HERCULES 6950288-S 69" x 50" INSTALLATION OF HERCULES 6950288-S 69 INCH DIAMETER X 50 INCH PITCH PROPELLER CONTINENTAL C90-14F BDKH PROPELLER INSTALLATION PIEL CP301A 14876 C90 ALTERNATOR, ELECTRIC STARTER & Electrical system and spin on oil filter system CONTINENTAL C90-14F BHRR SPIN ON OIL FILTER PIEL CP301A 12560 FIT OIL BREATHER KIT AIRWORLD UK OIL BREATHER FITTED AS PREVIOUSLY APPPROVED ON JODEL D120 AIRCRAFT CONTINENTAL O-200-A AYTR PIEL CP301A 14074 ENGINE CHANGE TO CONTINENTAL O- CONTINENTAL 0-200A ENGINE WITH MCCAULEY 1A101/DCM 69" x 48" PROPELLER FITTTED CONTINENTAL O-200-A AYTR 200A & MCCAULEY PROPELLER PIEL CP301A 12982 PROPELLER CHANGE TO HERCULES INSTALLATION OF HERCULES 6850247 68 INCH DIAMETER X 50 INCH PITCH PROPELLER. CONTINENTAL O-200-A BIJU 6850247 68" X 50" PIEL CP301B 15140 HERCULES 6950288-S 69" x 50" INSTALLATION OF HERCULES 6950288-S 69 INCH DIAMETER x 50 INCH PITCH PROPELLER. CONTINENTAL C90-14F ASVG PROPELLER INSTALLATION PIEL CP301B (MODIFIED) 12982 PROPELLER CHANGE TO HERCULES INSTALLATION OF HERCULES 6850247 68 INCH DIAMETER X 50 INCH PITCH PROPELLER. CONTINENTAL O-200-A AXXC 6850247 68" X 50" PIEL CP328 SUPER-EMERAUDE 13049 PROPELLER CHANGE TO HERCULES 69" X INSTALLATION OF HERCULES 69 INCH DIAMETER X 54 INCH PITCH PROPELLER, S/N 6954254. LYCOMING O-235-L2A SAZZ 54" PIETENPOL AIR CAMPER 13117 U/C SAFETY STRAP. STRANDED STEEL SAFETY CABLE ADDED TO UNDERCARRIAGE SHOCK STRUT TO SUPPORT WEIGHT CONTINENTAL A65-8F ADRA OF AIRCRAFT IN THE EVENT OF A BUNGEE FAILURE OR WELD FAILURE. Prototype mods that have been approved since 1/1/2008 Page 69 30/11/20 LAA Technical Leaflet TL 3.17 PIETENPOL AIR CAMPER 12268 HOFFMANN HO14-178 120 PROPELLER INSTALLATION OF HOFFMANN HO14-178 120 PROPELLER CONTINENTAL O-200-A BWVB INSTALLATION PIETENPOL AIR CAMPER 13710 ENGINE CHANGE TO CONTINENTAL O- ENGINE REPLACED WITH CONTINENTAL 0-200A WITH JAMES 70" x 45" CONTINENTAL O-200-A PIET 200-A & PROPELLER CHANGE PIETENPOL AIR CAMPER 12897 ENGINE CHANGE TO CONTINENTAL O- ENGINE CHANGED TO CONTINENTAL 0-200A CONTINENTAL O-200-A BVYY 200 PIETENPOL AIR CAMPER 14729 STARTING AND CHARGING INSTALLATION OF SKY-TECH C12ST2/S STARTER, DELCO REMY GENERATOR, LUCAS NCB101 CONTINENTAL O-200-A BVYY INSTALLATION VOLTAGE REGULATOR, VARLEY LI5 LITHIUM IRON PHOSPHATE BATTERY, AND ASSOCIATED WIRING, SWITCHING, INDICATORS AND CIRCUIT PROTECTION. PIETENPOL AIR CAMPER 13895 JAMES AJ7045/SEN/C90 70 X 45 INSTALLATION OF ALAN JAMES AJ7045/SEN/C90 70 INCH DIAMETER X 45 INCH PITCH PROPELLER. CONTINENTAL O-200-A OHAL PROPELLER INSTALLATION PIETENPOL AIR CAMPER 12330 ADJUSTABLE FRONT LIFT STRUT ENDS SPECIAL THREADED FITTINGS INCORPORATED INTO FRONT LIGT STRUTS TO ALLOW LENGTH CONTINENTAL O-200-A RAGS ADJUSTMENT SIMILAR TO REAR STRUTS BUT OF UPRATED DESIGN. PIETENPOL AIR CAMPER 12617 PROPELLER CHANGE TO ALAN JAMES 70 PROPELLER CHANGE TO ALAN JAMES 70 INCH DIAMETER X 44 INCH PITCH. CONTINENTAL O-200-A RAGS INCH X 44 INCH PIETENPOL AIR CAMPER 13052 JURY STRUT TO REAR LIFT STRUT ADDITIONAL JURY STRYUT ADDED PER APPLICANT'S DRAWING. SHEET 1 AND 2 . SHEET 1 IS AT LYCOMING O-235-L2C OFFA REVISION A, SHEET 2 AT INITIAL ISSUE.

THIS MODIFICATION FOR PEACE OF MIND ONLY, NOT REQUIRED FOR STRUCTURAL REASONS PIETENPOL AIR CAMPER 13061 PREVENTION OF TOTAL COLLAPSE OF ADDITION OF SAFETY CABLE TO PREVENT UNDERCARRIAGE COLLAPSE IN THE EVENT OF A ROD END LYCOMING O-235-L2C OFFA U/C IN EVENT OF FAILURE FAILURE AT EITHER END OF THE SHOCK STRUT, PER APPLICANT'S DRAWING PIETENPOL AIR CAMPER 12773 ENGINE CHANGE TO ROTAX 912-ULS TOTAL REPLACEMENT OF ENGINE INSTALLATION IN ACCORDANCE WITH APPLICANT'S SUBMISSION. ROTAX 912-ULS BYFT WITH SENENICH EZ-PITCH PROPELLER PIETENPOL AIR CAMPER 13395 HERCULES 7448310-C 74" X 48" INSTALLATION OF HERCULES 7448310-C 74 INCH DIAMETER X 48 INCH PITCH PROPELLER. SUBARU EA81 DAYZ PROPELLER INSTALLATION. PIETENPOL AIR CAMPER 13350 PROPELLER CHANGE TO HERCULES HERCULES 7444304-C PROPELLER FITTED. SUBARU EA81 LEOD PIONEER 200 13048 ACI STALL WARNER INSTALLATION OF ACI STALL WARNER WITH BLADE SWITCH IN WING LEADING EDGE. ROTAX 912-UL CEWL PIONEER 200-M 13583 CATEGORY CHANGE TO MICROLIGHT AIRCRAFT FITTED WITH THE MODIFICATIONS LISTED IN TADS 334 NECESSARY FOR WEIGHT ROTAX 912-UL CEVJ REDUCTION WITH THE FOLLOWING EXCEPTIONS: MECHANICAL PITCH TRIM SYSTEM RETAINED. ORIGINAL WING TIPS RETAINED.

AIRFRAME COVERED WITH ORATEX UL600 MK3 TO REDUCE WEIGHT SUFFICIENT NOT TO INCLUDE ABOVE MENTIONED MODS. EMPTY WEIGHT 268KG. PIONEER 200-M 13338 ANDAIR GASIO-70 GASCOLATOR ANDAIR GASCOLATOR FITTED PER STANDARD PRACTISE TO FRONT OF FIREWALL WITH ROTAX 912-UL CGLI APPROPRIATE PROVISION FOR WATER DRAIN POINT THROUGH COWLINGS. PIONEER 200-M 14174 WARP DRIVE RPM 2 BLADED 66 INCH INSTALLATION OF WARP DRIVE RPM 2 BLADED 66 INCH DIAMETER X 19 DEGREES PITCH PROPELLER ROTAX 912-UL CGLI DIAMETER X 19 DEGREES PITCH PROPELLER INSTALLATION PIONEER 200-M 13243 AVEO POWER BURST NAV/STROBES FITMENT OF AVEO POWER BURST 05-04877 NAVIGATION LIGHTS/STROBES TO THE WING TIPS. ROTAX 912-UL OBRO INCLUDES ASSOCIATED WIRING, SWITCHING AND CIRCUIT PROTECTION. PIONEER 300 12967 AVTEK IDROVARIO 3 BAY BLADE INSTALLATION OF AVTEK IDROVARIO 3 BAY BLADE 3-BLADED IN-FLIGHT ADJUSTABLE 1664MM ROTAX 912-ULS DEWY PROPELLER DIAMETER PROPELLER. PIONEER 300 12587 TRIO EZ PILOT WING LEVELLER TRIO EZ PILOT SYSTEM INSTALLED IN ACCORDANCE WITH SUPPLIED DETAILS ROTAX 912-ULS PION INSTALLATION PIONEER 300 13967 TRIO PRO PILOT AUTO-PILOT (PITCH) INSTALLATION OF TRIO PRO PILOT AUTO-PILOT WITH PITCH SERVO, MOUNTED ONTO MOUNTING ROTAX 912-ULS PION INSTALLATION BRACKET OVER PRE-EXISTING ROLL SERVO. PIONEER 300 12996 PROPELLER CHANGE TO AVTEK INSTALLATION OF AVTEK IDROVARIO 3 BAY-BLADE 3 BLADED 1664MM DIA ROTAX 912-ULS XCIT IDROVARIO 3 BAY-BLADE 3 BLADED 1664MM DIA

Prototype mods that have been approved since 1/1/2008 Page 70 30/11/20 LAA Technical Leaflet TL 3.17 PIONEER 300 12587 TRIO EZ PILOT WING LEVELLER TRIO EZ PILOT SYSTEM INSTALLED IN ACCORDANCE WITH SUPPLIED DETAILS ROTAX 912-ULS CDYY INSTALLATION PIONEER 300 13967 TRIO PRO PILOT AUTO-PILOT (PITCH) INSTALLATION OF TRIO PRO PILOT AUTO-PILOT WITH PITCH SERVO, MOUNTED ONTO MOUNTING ROTAX 912-ULS CDYY INSTALLATION BRACKET OVER PRE-EXISTING ROLL SERVO. PIONEER 300 13421 REPLACE FUSELAGE WITH NEW SUPPLIED FUSEALGE REPLACED FOLLOWING ACCIDENT. NEW FUSELAGE SUPPLIED BY ALPI AS BARE FRAME. ROTAX 912-ULS IPKA BY ALPI PIONEER 300 13457 UNDERCARRIAGE PIVOT BRACKET RECTANGULAR STAINLESS STEEL WASHER PLATE FITTED TO REINFORCE MOUNTING POINT FOR ROTAX 912-ULS CDPA MOUNTING REINFORCEMENT RETRACTABLE UNDERCARIAGE TO WING SPAR BOX IN CENTRE FUSELAGE, AS ALREADY APPROVED ON G-EKIM UNDER LAA REPAIR NUMBER 0755 PIONEER 300 12996 PROPELLER CHANGE TO AVTEK INSTALLATION OF AVTEK IDROVARIO 3 BAY-BLADE 3 BLADED 1664MM DIA ROTAX 912-ULS VIXX IDROVARIO 3 BAY-BLADE 3 BLADED 1664MM DIA PIONEER 300 13746 MONITOR FUEL FLOW TO ENGINE INSTALLATION OF: ROTAX 912-ULS VIXX ELECTRONICS INTERNATIONAL FT-60 'RED CUBE' FUEL FLOW TRANSDUCER DOWNSTREAM OF RETURN LINE, WHICH IS RESTRICTED WITH A 0.35MM RESTRICTOR, TO PROVIDE DATA FOR FUEL FLOW COMPUTER WITHIN DYNON EFIS. FACET 20106 ELECTRIC FUEL PUMP FITTED IN SERIES DOWNSTREAM OF THE MECHANICAL PUMP. DYNON FUEL PRESSURE SENDER IN DISTRIBUTION MANIFOLD BETWEEN CARBURETTORS.

PIONEER 300 13130 SENSENICH 2A0J5R64ZN 64" DIAMETER INSTALLATION OF SENSENICH 2A0J5R64ZN 64" DIAMETER GROUND ADJUSTABLE PROPELLER. ROTAX 912-ULS EKIM PROPELLER PIONEER 300 13641 CHANGE TO FUEL SYSTEM RECONFIGURE FUEL SYSTEM FROM PUMPS IN PARALLEL TO PUMPS IN SERIES. ELECTRIC PUMP RE- ROTAX 912-ULS EKIM POSITIONED AHEAD OF GASCOLATOR AND LOCATED UNDER P2 SEAT. PIPEWORK ADJUSTED TO SUIT. PIONEER 300 13209 INSTALLATION OF MECAPLEX SLIDING INSTALLATION OF A MECAPLEX SLIDING WINDOW WITH HINGED SCOOP IN THE FRONT LOWER ROTAX 912-ULS CEAR WINDOWS WITH SCOOPS CORNER OF LEFT AND RIGHT SIDES OF THE CANOPY TO PROVIDE A MEANS OF VENTILATION AND DIRECT VISION IN THE EVENT OF AN EMERGENCY. PIONEER 300 13379 INSTALLATION OF FT-60 (RED CUBE) FUEL FT-60 FUEL FLOW SENSOR INSERTED IN FUEL SYSTEM BETWEEN POINT OF FLOW RETURN LINE AND ROTAX 912-ULS CGTL FLOW TRANSDUCER CARBURETTORS. SENSOR INSTALLED IN ACCORDANCE WITH MANUFACTURER'S GUIDELINES AND FIRE-SLEEVED. PIONEER 300 15380 DYNON SKYVIEW DUAL AXIS AUTO-PILOT INSTALLATION OF DYNON D700 SKYVIEW DUAL AXIS AUTO-PILOT. SERVO MOUNTING KIT ROTAX 912-ULS OWBA INSTALLATION SUPPLIED BY NORTHAIR AVIATION (ITALY). ROLL SERVO MOUNTED TO BRACKET BOLTED TO PLYWOOD BASE-PLATE SPANNING TWO WOODEN LONGERONS CENTRALLY BETWEEN CONTROL COLUMNS AND AND IMMEDIATELY AFT OF THE NOSE WHEEL VIEWING WINDOW. PITCH SERVO MOUNTED TO BRACKET ON OMEGA SHAPED BRACKET DIRECTLY ABOVE AND RIVETED TO ROLL SERVO MOUNTING BRACKET. PIONEER 300 HAWK 12722 INSTALLATION OF TRUTRAK ADI PILOT 1 EQUIPMENT INSTALLED AS SHOWN ON APPLICANT'S DRAWINGS/DETAILS ROTAX 912-ULS OPYO WING LEVELLING AUTO-PILOT PIONEER 300 HAWK 14152 MT-V-33-1-A/175-200 PROPELLER INSTALLATION OF MT-V-33-1-A/175-200 PROPELLER USING JIHOSTROJ HYDRAULIC GOVERNOR ROTAX 912-ULS ITBT INSTALLATION PIONEER 300 HAWK 14705 FITMENT OF RED CUBE FT-60 FUEL FLOW FT-60 FUEL FLOW TRANSDUCER INSTALLED BETWEEN FUEL RETURN 'T' AND CARBURETTORS. ROTAX 912-ULS ISBD SENSOR INSTALLED IN ACCORDANCE WITH MANUFACTURER'S INSTRUCTIONS ON THE FORWARD FACE OF THE FIREWALL. PIONEER 400 14420 ROTAX 912iS INSTALLATION ROTAX 912iS ENGINE INSTALLED AS PER ROTAX INSTRUCTIONS. ROTAX 912-iS NSKY

Prototype mods that have been approved since 1/1/2008 Page 71 30/11/20 LAA Technical Leaflet TL 3.17 PIONEER 400 13306 FLYMAP DUAL AXIS AUTO-PILOT INSTALLATION OF FLYMAP DUAL AXIS AUTO-PILOT INCORPORATING TRIO GOLD STANDARD ROTAX 914-UL CGVO INSTALLATION SERVOS. ROLL SERVO BOLTED TO FORWARD FACE OF WING SPAR, PUSH-ROD CONNECTED TO BASE OF STARBOARD COLUMN WITH 17MM PILLAR . PITCH SERVO BOLTED TO FORWARD BULKHEAD, PUSH-ROD ATTACHED TO VERTICAL BELLCRANK AT CENTRE OF TORQUE TUBE BETWEEN CONTROL COLUMNS USING 40MM PILLAR AT EACH END. LAA AIRWORTHINESS INFORMATION LEAFLET MOD/EQUIP/002 INCORPORATED ON BOTH SERVO DRIVE ARMS.

PIONEER 400 13306 FLYMAP DUAL AXIS AUTO-PILOT INSTALLATION OF FLYMAP DUAL AXIS AUTO-PILOT INCORPORATING TRIO GOLD STANDARD ROTAX 914-UL CIMD INSTALLATION SERVOS. ROLL SERVO BOLTED TO FORWARD FACE OF WING SPAR, PUSH-ROD CONNECTED TO BASE OF STARBOARD COLUMN WITH 17MM PILLAR . PITCH SERVO BOLTED TO FORWARD BULKHEAD, PUSH-ROD ATTACHED TO VERTICAL BELLCRANK AT CENTRE OF TORQUE TUBE BETWEEN CONTROL COLUMNS USING 40MM PILLAR AT EACH END. LAA AIRWORTHINESS INFORMATION LEAFLET MOD/EQUIP/002 INCORPORATED ON BOTH SERVO DRIVE ARMS.

PIONEER 400 14435 FIT TWO EXTRA FUEL TANKS UNDER TWO 17 LITRE FUEL TANKS OF WELDED ALUMINIUM ALLOY CONSTRUCTION INSTALLED IN ROTAX 914-UL CIMD REAR SEATS FUSELAGE TO REAR OF WING MAINSPAR, EITHER SIDE OF CENTRELINE, FEEDING INTO MAIN TANKS VIA ELECTRIC PUMP. ADDITIONAL FILLER ADDED TO REAR SECTION OF FUSELAGE. SUPPLEMENT TO POH REFERS PIPER J3C (MODIFIED) 13162 TOTAL LOSS ELECTRICAL SYSTEM AND B+C STARTER AND BATTERY INSTALLATION PLUS ASSOCIATED ELECTRICAL SYSTEM ADDED. CONTINENTAL C90-12F BMKC STARTER INSTALLATION PIPER J3C-65 13373 HERCULES 7242245 72" X 42" PROPELLER INSTALLATION OF HERCULES 7242245 72 INCH DIAMETER X 42 INCH PITCH PROPELLER. CONTINENTAL A65 AKAZ INSTALLATION. PIPER J3C-65 14761 INSTALL GROVE DISK BRAKE SYSTEM STC'd GROVE BRAKE INSTALLATION STC SA01704LA CONTINENTAL A65 BDOL PIPER J3C-65 14762 INSTALL THREE POINT FRONT SEAT . CONTINENTAL A65 BDOL HARNESS PIPER J3C-65 14763 INSTALL FOUR POINT INERTIA REEL REAR . CONTINENTAL A65 BDOL SEAT HARNESS PIPER J3C-65 14595 CONTINENTAL A65-8A ENGINE AND CONTINENTAL A65-8A ENGINE AND NEWTON 72" X 44" 2 BLADED WOODEN PROPELLER CONTINENTAL A65-8 BDHK NEWTON 72" X 44" 2 BLADED WOODEN INSTALLATIONS PROPELLER PIPER J3C-65 13095 TO INTRODUCE A REMOVABLE FUSELAGE SECOND DIAGONAL BRACE TUBE UNDER FUEL TANK MADE REMOVEABLE, SO TANK CAN BE CONTINENTAL A65-8 BGSJ STRUCTURE TUBE REMOVED DOWNWARDS FOR MAINTENANCE. THIS WAS THE STANDARD ARRANGEMENT ON MANY FACTORY BUILT J3C-65 AIRCRAFT. PIPER J3C-65 13543 PROPELLER CHANGED TO LODGE CJL 100 PROPELLER CHANGED TO LODGE CJL 100 72" x 42" CONTINENTAL A65-8 BGSJ 72" x 46" PIPER J3C-65 12972 HERCULES 7242245 72" X 42" PROPELLER INSTALLATION OF HERCULES 72 INCH DIAMETER X 42 INCH PITCH PROPELLER SERIAL NUMBER CONTINENTAL A65-8 BROR INSTALLATION 7242245. PIPER J3C-65 12464 PROPELLER CHANGE TO SENSENICH INSTALLATION OF SENSENICH S3097240 72 INCH DIAMETER X 40 INCH PITCH PROPELLER. THIS CONTINENTAL A65-8F BHPK S3097240 PROPELLER IS A W72CK42 WHERE THE PITCH WAS MODIFIED TO BE 40 INCHES. PIPER J3C-65 13516 HERCULES 7240342-S 72" X 40" INSTALLATION OF HERCULES 7240342-S 72 INCH DIAMETER X 40 INCH PITCH PROPELLER. CONTINENTAL A65-8F BHPK INSTALLATION. PIPER J3C-65 15092 GROVE DISC BRAKE AND WHEEL STC'd GROVE BRAKE INSTALLATION STC SA01704LA. CONTINENTAL A65-8F BHPK CONVERSION GROVE 40-208 WHEELS INSTALLED. PIPER J3C-65 14189 AIRWOLF REMOTE FILTER FOR A65 INSTALLATION OF AIRWOLF OIL FILTER ADAPTER IN ACCORDANCE WITH FAA STC SA000079NY. CONTINENTAL A65-8F BJAY

PIPER J3C-65 12357 SENSENICH W76CK-35 PROPELLER FITTED SENSENICH W76CK-35 PROPELLER SUBSTITUTED CONTINENTAL C85-14F NCUB

Prototype mods that have been approved since 1/1/2008 Page 72 30/11/20 LAA Technical Leaflet TL 3.17 PIPER J3C-65 15523 GROVE BRAKE INSTALLATION GROVE BRAKE INSTALLATION STC SA 01704LA CONTINENTAL C85-14F NCUB PIPER J3C-65 15524 CLEARANCE OF MODS FOUND OMNIBUS MODIFICATION TO RETROSPECTIVELY APPROVE VARIOUS MODIFICATIONS FOUND CONTINENTAL C85-14F NCUB EMBODIED DURING CAA ACAM EMBODIED AT AUDIT, INCLUDING REVISIONS CARRIED OUT AT THIS TIME TO BRING TO AN ACCEPTABLE STANDARD PIPER J3C-65 15538 EMBODIMENT OF STC SE00979AT WITH THIS MODIFICATION HAS BEEN RAISED TO APPROVE THE INCOPORATION OF 0-200 CRANKSHAFT, CONTINENTAL C85-14F NCUB ADDITIONAL CHANGES CONECTING RODS AND PISTONS UNDER STC SE00979AT, AND ALSO 0-200 CYLINDERS AND AND A CONTINENTAL C85-12 CRANKCASE WITH MODIFIED HOUSING FOR OIL SLINGER OF THE 0-200 CRANKSHAFT AS DETAILED IN THE STC ABOVE. PIPER J3C-65 15161 PROPELLER CHANGE TO HERCULES HERCULES PROPELLER OF TYPICAL HERCULES DESIGN, DESIGNED USING HERCULES CUSTOM CONTINENTAL C85-8 RCIE 7041372-S SOFTWARE PIPER J3C-65 14998 TAF-L SPIN-ON OIL FILTER ADAPTER INSTALLATION OF TAF-L SPIN-ON OIL FILTER ADAPTER WITH CHAMPION CH48108 FILTER PER STC CONTINENTAL C90-12 AJAD INSTALLATION SE7559SW. PIPER J3C-65 12861 ENGINE CHANGE TO CONTINENTAL C90- INSTALLATION OF CONTINENTAL C90-8F WITH EVRA D.11.28.7.C PROPELLER. CONTINENTAL C90-8F KURK 8F WITH EVRA D.11.28.7.C PROPELLER

PIPER J3C-65 13882 CONTINENTAL C90-8F ENGINE AND INSTALLATION OF CONTINENTAL C90-8F ENGINE AND LODGE CJL 100 72" X 47" PROPELLER. CONTINENTAL C90-8F BREB LODGE CJL 100 72" X 47" PROPELLER ENGINE MAXIMUM RPM LIMITED TO 2475 WITH THE LODGE CJL 100 PROPELLER FITTED. INSTALLATION PIPER J3C-65 14154 GROVE DISC BRAKE SYSTEM GROVE DISC BRAKE SYSTEM FITTED IN ACCORDANCE WITH FAA STC SA01704LA. CONTINENTAL C90-8F JCBS PIPER J3C-65 13584 MODIFICATION OF THROTTLE, RUDDER INSTALLATION OF LEVER ON LEFT SIDE OF COCKPIT TO PROVIDE LEFT HAND OPERATED RUDDER CONTINENTAL O-200-A BDEY AND BRAKE CONTROL CONTROL. RUDDER LEVER EQUIPPED WITH STYLE TWIST GRIP THROTTLE AND BRAKE LEVER FOR LEFT WHEEL BRAKE. SIMILAR BRAKE LEVER INSTALLED ON CONTROL COLUMN FOR THE RIGHT WHEEL BRAKE. PULL-PULL THROTTLE CABLES ATTACHED TO EXISTING FRONT SEAT THROTTLE LEVER. PIPER J3C-65 13585 CONTINENTAL O-200-A ENGINE AND INSTALLATION OF CONTINENTAL O-200-A ENGINE WITH SENSENICH W72GK-48 PROPELLER. CONTINENTAL O-200-A BDEY SENSENICH W72GK-48 PROPELLER INSTALLATIONS PIPER J3C-65 15083 CONTINENTAL A65-8F & SENSENICH A65 ENGINE SUBSTITUTED BY 0-200A WITH SENSENICH W72GK48 PROPELLER CONTINENTAL O-200-A BHVV W72GK48 PIPER J3C-65 12591 CRANKCASE BREATHER SETTLING TANK INSTALLATION OF 280CC ALUMINIUM TANK IN FRONT OF CARBURETTOR TO COLLECT OIL FROM CONTINENTAL O-200-A BHZU THE SUMP BREATHER WITH OUTLET HOSE AT BASE OF FIREWALL. PIPER J3C-65 13019 ENGINE CHANGE TO CONTINENTAL O- ENGINE CHANGED TO CONTINENTAL O-200A WITH SENSENICH W72GK-48 PROPELLER. CONTINENTAL O-200-A BPYN 200A PIPER J3C-65 12795 ENGINE CHANGE TO CONTINENTAL O200- ENGINE CHANGE TO CONTINENTAL O200-A WITH MCCAULEY 1A101/DCM 68 INCH DIAMETER CONTINENTAL O-200-A BTET A WITH MCCAULEY 1A101/DCM 68" X (CROPPED FROM 69 INCHES) X 48 INCH PITCH. 48" PIPER J3C-65 13823 PROPELLER CHANGE TO HERCULES INSTALLATION OF HERCULES 7045261-S 70 INCH DIAMETER X 45 INCH PITCH PROPELLER. CONTINENTAL C85-8F (MODIFIED) ATKI 7045261-S PIPER J3C-65 (MODIFIED) 12934 WINTERISATION BAFFLES INSTALLATION OF WINTERISATION BAFFLES TO C85-12F ENGINE CYLINDERS TO PREVENT CONTINENTAL C85-12F BBHJ EXCESSIVE OIL COOLING DURING COLD CONDITIONS. INSTALLATION OF ACCURATE OIL TEMPERATURE GAUGE AND CHT GAUGE THAT REGISTERS AT LEAST THE HOTTEST CYLINDER MANDATORY WITH BAFFLES FITTED. PIPER J3C-65 (MODIFIED) 12431 PROPELLER CHANGE PROPELLER CHANGED TO SENSENICH W72GK46 CONTINENTAL C85-8F BSVH PIPER J3C-65 (MODIFIED) 12432 ENGINE CHANGE TO CONTINENTAL C-85- ENGINE CHANGE TO CONTINENTAL C85-8F CONTINENTAL C85-8F BSVH 8F PIPER J3C-65 (MODIFIED) 12940 PROPELLER CHANGE TO SENSENICH EXISTING PROPELLER REPLACED WITH SENSENICH 69 CK-0-48L. CONTINENTAL O-200-A BPCF PIPER J3C-65 (MODIFIED) 13139 STRUT MOUNTED PYROTECHNICS - FOUR FLARE EFFECT PYROTECHNICS FITTED TO SHEET ALUMINIUM MOUNTING ATTACHED TO CONTINENTAL O-200-A BPCF FLARE EFFECT WING STRUTS OF EACH WING. MAXIMUM INDICATED AIRSPEED WHEN PYROTECHNICS STRUT MOUNTINGS FITTED: 90 KNOTS. ADDITIONAL COCKPIT PLACARD TO BE FITTED AS SPECIFIED IN LAA LETTER DATED 17.8.11

Prototype mods that have been approved since 1/1/2008 Page 73 30/11/20 LAA Technical Leaflet TL 3.17 PIPER J3C-65 (MODIFIED) 13140 WINGTIP PYROTECHNICS - SPARKLER TWIN SPARKLER EFFECT PYROTECHNICS FITTED TO WELDED STEEL TUBE WINGTIP MOUNTINGS. CONTINENTAL O-200-A BPCF EFFECT MAXIMUM INDICATED AIRSPEED WHEN PYROTECHNICS WINGTIP MOUNTINGS FITTED: 90 KNOTS. ADDITIONAL COCKPIT PLACARD TO BE FITTED AS SPECIFIED IN LAA LETTER DATED 17.8.11

PIPER J3C-65 (MODIFIED) 13700 ADDITION TO EXISTING PYROTECHNIC ADDITIONAL ROMAN CANDLE TYPE PYROTECHNICS FITTED TO UNDERCARRIAGE LEGS, CONTINENTAL O-200-A BPCF FIRING SYSTEM UNDERCARRIAGE LEGS STRIPPED OF FABRIC AND CUSTOM MOUNT FITTED. MAXIMUM INDICATED AIRSPEED WHEN PYROTECHNICS UNDERCARRIAGE MOUNTINGS FITTED : 90 KNOTS. ADDITIONAL COCKPIT PLACARD TO BE FITTED AS SPECIFIED IN LAA LETTER DATED 17.8.11

PIPER J3C-65 (MODIFIED) 14434 HERCULES 7045261-S 70" X 45" INSTALLATION OF HERCULES 7045261-S 70" X 45" PROPELLER. CONTINENTAL O-200-A BSFD PROPELLER INSTALLATION PIPER J3C-90 13466 HERCULES 7045261-S 70" X 45" INSTALLATION OF HERCULES 7045261-S 70 INCH DIAMETER X 45 INCH PITCH PROPELLER. CONTINENTAL C90-12F OCUB PROPELLER INSTALLATION PIPER J3C-90 12069 DISC BRAKE CONVERSION INSTALL GROVE DISC BRAKE CONVERSION PER STC SA01704LA CONTINENTAL C90-12F OCUB PIPER J3C-90 14522 MIXTURE CONTROL MIXTURE PUSH-PULL CONTROL MOVED TO SIDEWALL OF COCKPIT IN FUEL COCK APERTURE CONTINENTAL C90-12F OCUB PIPER J3C-90 12433 PROPELLER CHANGE TO EVRA D.11.28.7C INSTALLATION OF EVRA D.11.28.7C PROPELLER. CONTINENTAL C90-8F AKIB

PIPER J3C-90 12688 PROPELLER CHANGE TO MCCAULEY PROPELLER CHANGE TO MCCAULEY IB90/CM 71 INCH DIAMETER X 48 INCH PITCH. CONTINENTAL C90-8F AXGP IB90/CM 71" X 48" PIPER J5A 13423 OBSERVATION AIRCRAFT STYLE CABIN MORE EXTENSIVE CABIN GLAZING FITTED USING 3MM LEXAN PANELS ATTACHED USING AGS 4747- CONTINENTAL O-200-A BSXT GLAZING 408BS POP RIVETS PER APPLICANT'S SUBMISSION DETAILS PROVIDED IN MOD/2 FORM AND PHOTOGRAPHIC RECORD - REQUIREMENT FOR MOD 3 WAIVED ON THIS OCCASION PIPER J5A 13102 HERCULES 7246266-S 72" X 46" INSTALLATION OF HERCULES 7246266-S 72 INCH DIAMETER X 46 INCH PITCH PROPELLER. LYCOMING O-235-C1 BTKA PROPELLER MAXIMUM AUTHORISED ENGINE RPM RESTRICTED TO 2600. REF TCDS A-725 NOTE 307(F). PIPER L18C 13080 HERCULES 7045261 70" X 45" INSTALLATION OF HERCULES 7045261 70 INCH DIAMETER X 45 INCH PITCH PROPELLER. CONTINENTAL C90-8F AYPS PROPELLER. PIPER L18C 13495 REPLACE EXHAUST WITH VETTERMAN LEGEND CUB EXHAUST SYSTEM SUBSTITUTED, AS DIRECT REPLACEMENT FOR PIPER EXHAUST CONTINENTAL C90-8F AYPS "LEGEND CUB SYSTEM" SYSTEM PIPER L18C 14338 GROVE BRAKE CONVERSION STC SUBSTITUTE GROVE BRAKES PER STC SA01704LA CONTINENTAL C90-8F AYPS SA01704LA PIPER L18C 14580 ELECTRICAL INSTALLATION ELECTRICAL SYSTEM INSTALLED TO MAKE USE OF WIND-DRIVEN ALTERNATOR INSTALLED UNDER CONTINENTAL C90-8F BEUU SM10050. SYSTEM CONSISTS OF A 2.8AH BATTERY MOUNTED ON THE BAGGAGE COMPARTMENT FLOOR, AMMETER, VOLTMETER AND CIRCUIT BREAKERS MOUNTED IN THE STARBOARD WING ROOT, AND ASSOCIATED WIRING. PIPER L18C 12458 REPLACEMENT OF L18C EXHAUST STANDARD AFTER MARKET ALTERNATIVE EXHAUST BY AIRCRAFT EXHAUST INC CONTINENTAL C90-8F BIID SYSTEM PIPER L18C 14961 JPM 79001006 SPIN-ON OIL FILTER INSTALLATION OF JPM 79001006 OIL FILTER ADAPTER MOUNTED HORIZONTALLY TO CLEAR CONTINENTAL C90-8F BIID ADAPTER INSTALLATION EXHAUST SYSTEM AND WITH 30 DEGREE CRANK TO CLEAR ENGINE MOUNTING FRAME WITH BLUEPRINT ADT32109 OIL FILTER. PIPER L18C 12955 PROPELLER CHANGE TO MCCAULEY PROPELLER CHANGE TO MCCAULEY 1A105/SCM 71 INCH DIAMETER X 46 INCH PITCH. CONTINENTAL C90-8F BIZV 1A105/SCM 71" X 46" PIPER L18C 15311 GROVE DISC BRAKE CONVERSION STC STC'd GROVE BRAKE INSTALLATION STC SA01704LA. CONTINENTAL C90-8F BKET GROVE 40-208 WHEELS INSTALLED. PIPER L18C 13512 PROPELLER CHANGE TO SENSENICH W72 SENSENICH W72GK50 FITTED AT REBUILD CONTINENTAL C90-8F BKTA GK-50 PIPER L18C 13752 PROPELLER CHANGE TO HERCULES INSTALLATION OF HERCULES 6845406-S 68 INCH DIAMETER X 45 INCH PITCH PROPELLER. CONTINENTAL O-200-A PGEE 6845406-S

Prototype mods that have been approved since 1/1/2008 Page 74 30/11/20 LAA Technical Leaflet TL 3.17 PIPER L18C 13960 PROPELLER CHANGE TO HERCULES INSTALLATION OF HERCULES 7045261-S 70 INCH DIAMETER X 45 INCH PITCH PROPELLER. CONTINENTAL O-200-A PGEE 7045261-S PIPER L18C 14037 OMNIBUS SUNDRY CHANGES ALREADY ACCEPTED BY STC LYCOMING O-320-A2B ZPPY PIPER L18C (MODIFIED) 12318 PROPELLER CHANGE TO EVRA D11.28.7C PROPELLER CHANGE TO EVRA D11.28.7C 1760MM DIAMETER X 1260MM PITCH. CONTINENTAL C90-12F RCUB

PIPER L18C (MODIFIED) 13739 PROPELLER CHANGE TO LODGE CJL 110 LODGE CJL 110 70 INCH DIAMETER X 48 INCH PITCH PROPELLER INSTALLATION. CONTINENTAL C90-12F RCUB 70" X 48" PIPER L18C (MODIFIED) 13722 REBALANCING OF HOFFMANN BALANCING OF HOFFMAN PROPELLER FOLLOWING REFURBISHING BY HERCULES. PROPELLER CONTINENTAL C90-14F ZAZA PROPELLER AFTER REFURBISHING BALANCED USING METHOD OF INSERTING A SMALL SLUG OF LEAD INTO A SHALLOW HOLE (5mm DEEP x 12mm DIA) DRILLED IN THE FLAT FACE OF THE HUB. HOLE PLUGGED WITH A BEECH PLUG GLUED IN PLACE PER STANDARD HERCULES PROCEDURE PIPER L18C (MODIFIED) 13437 HERCULES 6943276-S 69" X 43" INSTALLATION OF HERCULES 6943276-S 69 INCH DIAMETER X 43 INCH PITCH PROPELLER. CONTINENTAL O-200-A BLPE PROPELLER INSTALLATION. PIPER L21B (MODIFIED) 15214 UNDER SEAT BATTERY RACK STC: SA02156AK (FAA) CONTINENTAL O-200-A BNXM UNDER SEAT BATTERY RACK MAX BATTERY WEIGHT 16 LB

4OFF RIVETS USED TO SUPPORT AFT FLANGE (INSTEAD OF 6OFF) AS LIMITED SPACE DUE SHOULDER HARNESS CABLE ATTACHMENT ODYSSEY PC680 BATTERY FITTED PIPER L4H 14020 NEWTON 07R 69" X 46" PROPELLER INSTALLATION OF NEWTON 07R 69 INCH DIAMETER X 46 INCH PITCH PROPELLER. CONTINENTAL A65-8 AHIP INSTALLATION PIPER L4H 12069 DISC BRAKE CONVERSION INSTALL GROVE DISC BRAKE CONVERSION PER STC SA01704LA CONTINENTAL C85-12 AISX PIPER L4H 14889 JAMES AJ7050/LC/A85 70" X 50" INSTALLATION OF JAMES AJ7050/LC/A85 70" X 50" PROPELLER, COPY IN BEECH OF LODGE CJL 110A CONTINENTAL C85-12 AISX PROPELLER INSTALLATION 70" X 50" MAHOGANY PROPELLER. PIPER L4J 14988 WINGTIP LEADING EDGE REPLACEMENT WINGTIP ALUMINIUM ALLOY SHEET LEADING EDGES REPLACED WITH GLASS FIBRE REINFORCED CONTINENTAL A65-8 AKTH PLASTIC MOULDINGS OF THE SAME SHAPE. PIPER PA-12 13171 FIT FLAPS FLAPS FITTED PER TCDS A.780 LYCOMING O-320-B2B ARTH PIPER PA-12 13196 ENGINE CHANGE TO LYCOMING O-320 ENGINE CHANGE TO LYCOMING 0-320 PER STC SA83AL. LYCOMING O-320-B2B ARTH B2B MAX PERMITTED RPM INCREASED TO 2700 TO SUIT THIS ENGINE PIPER PA-12 13197 CLEVELAND WHEELS/BRAKES CLEVELAND WHEELS AND BRAKES FITTED per STC SA2NE LYCOMING O-320-B2B ARTH PIPER PA-12 14698 HERCULES 7453712-S 74" X 53" INSTALLATION OF HERCULES 7453712-S 74 INCH DIAMETER X 53 INCH PITCH PROPELLER LYCOMING O-320-B2B ARTH PROPELLER INSTALLATION PIPER PA-12 15335 LYCOMING O-235-C2C ENGINE LYCOMING O-235-C2C SN 5641-15 ENGINE WITH SENSENICH M76AM-2-48 PROPELLER LYCOMING O-235-C CDCS INSTALLATION INSTALLATION. PIPER PA-12 15459 CASPER LABS 90 DEGREE OIL FILTER INSTALLATION OF CASPER LABS 90 DEGREE OIL FILTER HOUSING ADAPTER IN ACCCORDANCE WITH LYCOMING O-235-C CDCS ADAPTER STC THE CASPER LABS INSTALLATION MANUAL CL1000 REV. 8 AS A REPLACEMENT FOR LYCOMING ENGINES OIL FILTER ADAPTER AS PER FAA STC SE01930NY PIPER PA-15 12306 ENGINE CHANGE TO CONT O-200-A WITH ENGINE CHANGE TO CONTINENTAL O-200-A WITH EVRA D.11.28.4C (70 INCH DIAMETER X 45 INCH CONTINENTAL O-200-A ALGA EVRA D.11.28.4C PITCH) PROPELLER. PIPER PA-15 13524 UNDERCARRIAGE CONVERSION TO PA 17 SPRUNG PA-17 UNDERCARRIAGE STRUTS FITTED IN PLACE OF FIXED PA15 STRUT CONTINENTAL O-200-A BTOT

PIPER PA-15 13525 BRAKE UPGRADE GROVE DISC BRAKES FITTED IN PLACE OF EXISTING GOODRICH BRAKES CONTINENTAL O-200-A BTOT PIPER PA-15 13526 ELECTRIC TRIM CONVERSION MAC TRIM SERVO FITTED IN ELEVATOR CONNECTED BY SHORT PUSHROD TO ELEVATOR HORN CONTINENTAL O-200-A BTOT

PIPER PA-15 13643 FIT CAPACITANCE FUEL PROBE AND CAPACITANCE FUEL GAUGE FITTED CONTINENTAL O-200-A BTOT GUAGE PIPER PA-15 (MODIFIED) 13153 PROPELLER CHANGE TO WOODCOMP SR30 1800 MM DIA PROPELLER SUBSTITUTED ROTAX 912-UL ASHU PIPER PA-17 13509 HERCULES 7247330-S 72" X 47" INSTALLATION OF HERCULES 7247330-S 72 INCH DIAMETER X 47 INCH PITCH PROPELLER. CONTINENTAL A65-8 ALIJ PROPELLER INSTALLATION

Prototype mods that have been approved since 1/1/2008 Page 75 30/11/20 LAA Technical Leaflet TL 3.17 PIPER PA-17 13509 HERCULES 7247330-S 72" X 47" INSTALLATION OF HERCULES 7247330-S 72 INCH DIAMETER X 47 INCH PITCH PROPELLER. CONTINENTAL A65-8 BCVB PROPELLER INSTALLATION PIPER PA-17 14141 GROVE BRAKE KIT TO REPLACE EXISTING ORIGINAL BRAKES REPLACED BY DISC BRAKES IN ACCORDANCE WITH FAA STC SA01704LA. CONTINENTAL A65-8 BCVB SYSTEM INSTALLED USING GROVE INSTALLATION INSTRUCTIONS CDP2337-00024. ORIGINAL ELECTROL 459R MASTER CYLINDERS REPLACED WITH EQUIVALENT GROVE MASTER CYLINDERS 692-1. PIPER PA-17 14217 UPPER TORSO RESTRAINTS UPPER TORSO RESTRAINT FOR EACH OCCUPANT INSTALLED. BRACKET TO MOUNT UPPER TORSO CONTINENTAL A65-8 BCVB INSTALLATION RESTRAINT ATTACHMENT FITTING WELDED TO FUSELAGE UPPER TUBE CLUSTER AFT OF CABIN ON EACH SIDE. PIPER PA-17 12327 ANDAIR MINI GASCOLATOR INSTALLATION OF ANDAIR MINI GASCOLATOR SUPPORTED BY AN ALUMINIUM ALLOY BRACKET CONTINENTAL C85-12 BTBY BOLTED TO THE FIREWALL. PIPER PA-17 12969 EVRA 181/107 PROPELLER INSTALLATION INSTALLATION OF AN EVRA 181/107 PROPELLER. CONTINENTAL C85-12 BTBY

PIPER PA-17 13880 ELECTRICAL INSTALLATION B+C STARTER, B+C ALTERNATOR AND STARTER BATTERY INSTALLED USING PIPER SUPER CUB CONTINENTAL C90-12F BDVA BATTERY BOX MOUNTED ON FUSELAGE FRAME PIPER PA-17 14674 PROPELLER CHANGE TO SENSENICH PROPELLER CHANGED TO SENSENICH M76AK-2-42 CONTINENTAL C90-12F BDVA M76AK-2-42 PIPER PA-17 13315 ENGINE CHANGE TO CONTINENTAL C90- ENGINE CHANGED TO C90-8F, WITH MCCAULEY 1A90 71 x 46 PROPELLER. SINGLE WING ROOT CONTINENTAL C90-8F AWKD 8F, WING TANK FITTED, NOT FUEL TANK ADDED IN STARBOARD WING BUT NOT PLUMBED INTO SYSTEM AT THIS STAGE CONNECTED PIPER PA-17 13572 PROPELLER CHANGE TO HERCULES PROPELLER TYPE HERCULES 7046361-S SUBSTITUTED CONTINENTAL C90-8F AWKD 7046361-S PIPER PA-17 13572 PROPELLER CHANGE TO HERCULES PROPELLER TYPE HERCULES 7046361-S SUBSTITUTED CONTINENTAL C90-8F BDVB 7046361-S PIPER PA-17 10022 SPIN ON OIL FILTER TO IMPROVE ENGINE OIL FILTRATION, SPIN-ON OIL FILTER ADDED (FIREWALL MOUNTED) STCd CONTINENTAL C90-8F BLMP ITEM. PIPER PA-18-95 13436 G-HELN ELECTRIFICATION GENNIPOD UNIT FITTED TO AIRCRAFT UNDERCARRIAGE VEE STRUT ASSEMBLY USING CUSTOM CONTINENTAL C90-8F HELN BRACKET

AIRCRAFT VNE REDUCED TO 108 MPH WITH THIS INSTALLATION IN PLACE

A CLEAR PLACARD STATING THIS REDUCED VNE MUST BE PLACED ON THE INSTRUMENT PANEL ADJACENT TO THE ASI AND THE ASI RED LINE ALTERED ACCORDINGLY PIPER PA-18-95 13554 NEW INSTRUMENT PANEL NEW DEEPER CUSTOM INSTRUMENT PANEL FITTED TO ACCOMMODATE ADDITIONAL AVIONICS CONTINENTAL C90-8F HELN AND GENNIPOD SWITCHES ETC IN MORE RATIONAL ARRANGEMENT PIPER PA-18-95 14238 STC MOD SA01704LA CHANGE BRAKING SUBSTITUTE GROVE WHEELS AND BRAKES PER STC SA01704LA CONTINENTAL C90-8F HELN SYSTEM TO GROVE AVIATION PIPER PA-18-95 15061 INSTALLATION OF VENTRAL LED STROBE RAYLIGHT HERA SIMPLE LED STROBE LIGHT MOUNTED TO AFT LOWER FUSELAGE, INCLUDING CONTINENTAL C90-8F HELN CIRCUIT BREAKER, WIRING AND SWITCH. PITTS MODEL 12 14977 ENGINE CHANGE TO VEDENEYEV M14PF THE ENGINE HAS BEEN REPLACED BY THE MORE POWERFUL M14PF VARIANT WHICH HAS A VEDENEYEV M14PF PMIZ HIGHER GEAR RATIO SUPERCHARGER THAN THE M14P PITTS S-1 13047 ADDITION OF BATTERY ADDITION OF BATTERY MOUNTED TO REAR SEAT BACK FRAME LYCOMING IO-360-A1A INII

NOTE ADDITION OF BATTERY REDUCES AIRCRAFT PAYLOAD - CARRY OUT WEIGHT AND CG CHECK BEORE FLIGHT PITTS S-1C 12954 NEW TYPE OF CARBURETTOR ELLISON EFS-4A THROTTLE BODY INJECTOR INSTALLED IN PLACE OF STANDARD CARBURETTOR. LYCOMING O-320-A1A OSIC

PITTS S-1C 14115 HERCULES 7459410-S PROPELLER INSTALLATION OF HERCULES 7459410-S, 74 INCH DIAMETER X 59 INCH PITCH PROPELLER. LYCOMING O-320-A1A OSIC INSTALLATION PITTS S-1C 12649 SPRING GEAR UNDERCARRIAGE - GROVE GROVE CANTILEVER LEAF MAIN UNDERCARRIAGE SUBSTITUTED PER GROVE INSTRUCTIONS LYCOMING O-320-A2B BRAA

Prototype mods that have been approved since 1/1/2008 Page 76 30/11/20 LAA Technical Leaflet TL 3.17 PITTS S-1C 14696 SMOKE SYSTEM CONVENTIONAL SMOKE SYSTEM INSTALLATION OF MARVIN HOLMSLEY TYPE LYCOMING O-320-A2B BRAA PITTS S-1C 14767 SLIDING COCKPIT CANOPY INSTALLATION INSTALLATION OF STEEN AERO LABS SLIDING CANOPY WITH FRESH AIR VENT. LYCOMING O-320-A2B BRAA

PITTS S-1C 13675 BENDIX PS5 THROTTLE BODY CHANGED ROTEC TBI-40-4 TBI SUBSTITUTED FOR WORN BENDIX PS5 UNIT LYCOMING O-320-A2B BRJN TO ROTEC TB1-40-4 PITTS S-1C 13714 UPGRADE TO S-1S WINGS Pitts S-1S wings and interplane struts substituted on short fuselage S-1C. Undercarriage legs to LYCOMING O-320-A2B BRJN incorporate uprated to S-1S bungee carriers. Roots of cabane struts reinforced with welded finger plates at connection to upper longerons.

PITTS S-1C 13864 PROPELLER CHANGE TO HERCULES HERCULES TWO BLADE WOOD PROPELLER FITTED LYCOMING O-320-A2B BRJN 7256542-S PITTS S-1C (MODIFIED) 14592 SMOKE SYSTEM SMOKING AIRPLANES SYSTEM INSTALLED IN FORWARD FUSELAGE FORWARD OF CONTROL LYCOMING O-360-A4A BSRH COLUMN ASSEMBLY. SYSTEM ONLY CLEARED FOR FITMENT, NOT FOR CHARGING WITH SMOKE OIL (MODIFIED) OR FOR OPERATION, PENDING RE-WEIGHING OF AIRCRAFT AND SYSTEM TESTING PITTS S-1D 13295 PROPELLER CHANGE TO SENSENICH PROPELLER CHANGED TO SENSENICH 76EM8-0-60. ENGINE REBUILT AND RE CLASSIFIED AS 0-360- LYCOMING AEIO-360-A2A BLAG A2A (MODIFIED) WITH CHRISTEN OIL SYSTEM AND BENDIX INJECTION SYSTEM PITTS S-1D 13297 ENGINE & PROPELLER CHANGE LYCOMING 0-360 FITTED MODIFIED WITH BENDIX FUEL INJECTION AND CHRISTEN INVERTED OIL LYCOMING O-360-A3A PIII SYSTEM. SENSENICH 76EM8-0-60 PROPELLER FITTED. (MODIFIED) PITTS S-1E 13013 FUEL SYSTEM MODIFICATIONS MODIFICATIONS TO FUEL SYSTEM THAT INCLUDE: LYCOMING IO-360-B4A OKAY 1) INSTALLATION OF FLOSCAN 201B-6 FLOW TRANSDUCER CONNECTED TO MGL STRATOMASTER XTREME EFIS/FMS. 2) ANDAIR FUEL SELECTOR VALVE FS15-1. 3) ANDAIR WASHABLE FILTER FX375-M. PITTS S-1E 13666 MODIFICATIONS TO ENGINE INSTALLATION OF HIGH COMPRESSION PISTONS FROM NSF (NEED FOR SPEED) PISTONS TO RAISE LYCOMING IO-360-B4A OKAY THE COMPRESSION RATIO FROM 8.5:1 TO 9.5:1. PITTS S-1E 13811 PROPELLER CHANGE TO HERCULES INSTALLATION OF HERCULES 7559423-S 75 INCH DIAMETER X 59 INCH PITCH PROPELLER. LYCOMING O-360-B4A YOYO 7559423-S PITTS S-1E 12797 INSTALL SMOKE SYSTEM SMOKIN AIRPLANES SMOKE SYSTEM INSTALLED IN FORWARD FUSEALGE USING STANDARD SUPERIOR XP-IO-360-A1A FARL MANUFACTURER'S SCHEME FOR PITTS S1 VARIANTS. PITTS S-1S 13183 PROPELLER CHANGE TO PRINCE P TIP PRINCE P TIP 76" x 56" PROPELLER SUBSTITUTED. LYCOMING AEIO-360-B4A MINT PITTS S-1S 13498 E MAG ELECTRONIC IGNITION SINGLE E-MAG PLUS CONVENTIONAL MAGNETO FITTED. BUZZER FITTED TO WARN OF IGNITION LYCOMING AEIO-360-B4A WIGY BEING ACTIVATED WHEN ENGINE NOT RUNNING. TACHOMETER CHANGED TO SUIT INPUT AVAILABLE FOR E-MAG UNIT. PITTS S-1S 13608 DUAL EMAG ELECTRONIC IGNITION INSTALLATION OF P-MAG TO REPLACE LEFT HAND MAGNETO AND COMPLIMENT PREVIOUSLY LYCOMING AEIO-360-B4A WIGY FITTED P-MAG (MOD 13498 REFERS). BOTH P-MAGS SET TO CURVE 'B' WITH NO MANIFOLD PRESSURE CONNECTION TO RESULT IN NEAR MAGNETO . PITTS S-1S 12538 PROPELLER CHANGE TO SENSENICH PROPELLER CHANGE TO SENSENICH W76HM8-60, 76 INCH DIAMETER X 60 INCH PITCH. LYCOMING IO-360-B4A BKDR W76HM8-60, 76" X 60" PITTS S-1S 13513 SMOKE SYSTEM CUSTOM MADE SMOKE SYSTEM INSTALLED PER APPLICANT'S SUBMISSION LYCOMING IO-360-B4A BKDR PITTS S-1S 13811 PROPELLER CHANGE TO HERCULES INSTALLATION OF HERCULES 7559423-S 75 INCH DIAMETER X 59 INCH PITCH PROPELLER. LYCOMING IO-360-B4A BKDR 7559423-S PITTS S-1S 14191 INSTALLATION OF VARLEY LI-5 BATTERY INSTALLATION OF VARLEY Li-5 LiFePO4 LITHIUM-ION BATTERY IN PLACE OF ODYSSEY PC545 AGM LYCOMING IO-360-B4A HOON BATTERY MOUNTED BEHIND P1 SEAT. PITTS S-1S 13449 AEROVOLTZ 12 CELL LIFEPO4 LITHIUM AEROVOLTZ 12 CELL LIFEPO4 LITHIUM BATTERY CONTAINED IN ALUMINIUM BATTERY BOX LYCOMING O-360-A3A FORZ BATTERY INSTALLATION ON ENGINE MOUNTED TO PORT SIDE OF ENGINE MOUNTING FRAME WITH STAINLESS STEEL P-CLIPS. MOUNTING FRAME PITTS S-1S 13828 SMOKE SYSTEM PITTS SMOKE SYSTEM FITTED BUT WITH ALTERNATIVE SMOKE PUMP, ALTERNATIVE SMOKE OIL LYCOMING O-360-A3A FORZ SOLENOID AND ALTERNATIVE MOUNTING ARRANGEMENT FOR SMOKE PUMP PITTS S-1S 14301 HEADER TANK INSTALLATION OF A RAVEN 10 LITRE CAPACITY HEADER TANK SECURED BELOW MAIN FUEL TANK LYCOMING O-360-A3A FORZ WITH CUSTOM MADE STRAPS. FLOP TUBE TRANSFERRED FROM MAIN TANK TO HEADER TANK. Prototype mods that have been approved since 1/1/2008 Page 77 30/11/20 LAA Technical Leaflet TL 3.17 PITTS S-1S 14346 DUAL P-MAGS INSTALLATION INSTALLATION OF DUAL P-MAG 114 MODEL ELECTRONIC IGNITION UNITS IN PLACE OF MAGNETOS LYCOMING O-360-A3A FORZ PER MANUFACTURER'S INSTRUCTIONS. PITTS S-1S 14347 WHIRLWIND 200AC 80 INCH DIAMETER INSTALLATION OF WHIRLWIND 200AC, 80 INCH DIAMETER, 2 COMPOSITE BLADED CONSTANT LYCOMING O-360-A3A FORZ PROPELLER INSTALLATION SPEED PROPELLER WITH JIHOSTROJ P-940-010/AL GOVERNOR

ISS 2 RAISED TO INCLUDE WOODWARD GOVERNOR. PITTS S-1S 13344 ENGINE CHANGE TO LYCOMING 0-360- 0-360-A4M ENGINE SUBSTITUTED COMPLETE WITH BENDIX FUEL INJECTION SYSTEM AND LYCOMING O-360-A4A BOXH A4M CHRISTEN INVERTED OIL SYSTEM PITTS S-1S 13368 ANDAIR FUEL PUMP ANDAIR ELECTRIC BACK-UP FUEL PUMP IN LIEU OF MANUAL WOBBLE PUMP ARRANGEMENT LYCOMING O-360-A4A BOXH PITTS S-1S 12797 INSTALL SMOKE SYSTEM SMOKIN AIRPLANES SMOKE SYSTEM INSTALLED IN FORWARD FUSEALGE USING STANDARD LYCOMING O-360-A4A PARG MANUFACTURER'S SCHEME FOR PITTS S1 VARIANTS. PITTS S-1S 12997 MODIFY FUEL TANK FUEL TANK PICK-UP MOUNTIN RAISED 70mm ON FRONT FACE OF TANK SO THAT FLOP TUBE LYCOMING O-360-A4A PARG REACHES HIGHER UP TANK HEN INVERTED, REDUCING MINIMUM FUEL UEABLE WHEN INVERTED. PITTS RECOMMENDED PROHIITION ON AEROBATICS AT LOW LEVEL WITH LESS THAN 1/4 TANK FULL, NOT AFFECTED BY THIS MOD PITTS S-1S 13275 SINGLE LIGHTSPEED PLASMA III SINGLE LIGHTSPEED PLASMA III SYSTEM INSTALLED WITH CONVENTIONAL MAGNETO REMAINING SUPERIOR XP-IO-320-A3AD2 BRZX ELECTRONIC IGNTION IN PLACE FOR OTHER IGNITION SOURCE. PITTS S-1S 13788 ENGINE CHANGE TO SUPERIOR XP-IO-320-INSTALLATION OF A SUPERIOR XP-IO-320-A3AD2 ENGINE BUILT BY CFS AERO LTD WITH A SUPERIOR XP-IO-320-A3AD2 BRZX A3AD2 HOFFMANN HO23C HM-B188 156 PROPELLER. PITTS S-1S 13969 CATTO ACRO 3 BLADED 70" X 61" INSTALLATION OF CATTO ACRO 3 BLADED 70 INCH DIAMETER X 61 INCH PITCH PROPELLER SUPERIOR XP-IO-320-A3AD2 BRZX PROPELLER INSTALLATION PITTS S-1S 14300 CATTO ACRO 70" X 63.5"PROPELLER INSTALLATION OF CATTO ACRO 70 INCH DIAMETER X 63.5 INCH PITCH PROPELLER. SUPERIOR XP-IO-320-A3AD2 BRZX INSTALLATION PITTS S-1S 14993 ENGINE & PROP CHANGE TO SUPERIOR ENGINE & PROP CHANGE TO SUPERIOR IO 360 & MT186R160-4G SUPERIOR XP-IO-360-A1HC3 BOXV IO 360 & MT186R160-4G PITTS S-1T 14146 SKY DYNAMICS MAXI-SUMP WITH COLD INSTALLATION OF SKY DYNAMICS MAXI-SUMP WITH COLD AIR INDUCTION SYSTEM. LYCOMING AEIO-360-A1A BKPZ AIR INDUCTION SYSTEM INSTALLATION

PITTS S-1T 14147 SKYDYNAMICS 4-1 EXHAUST SYSTEM INSTALLATION OF SKYDYNAMICS 4 INTO 1 EXHAUST SYSTEM. LYCOMING AEIO-360-A1A BKPZ INSTALLATION PITTS S-2AE 13314 RACING BATTERIES RBA-300 2 OFF RACING BATTERIES RBA-300 LITHIUM IRON PHOSPHATE BATTERIES INSTALLED IN A LYCOMING AEIO-360-A1A JIIL INSTALLATION CUSTOMISED HOUSING WITHIN THE EXISTING BATTERY BOX. PITTS S-2S 12251 PROPELLER CHANGE TO MTV-9-B-C/C203- CHANGE OF PROPELLER TO MTV-9-B-C/C203-20d, 80 INCH DIAMETER LYCOMING AEIO-540-D4A5 EWIZ 20d PITTS S-2S 12252 INSTALLATION OF ELECTRONIC IGNITION INSTALLATION OF PLASMA III CDI IGNITION SYSTEM IN PLACE OF THE RIGHT HAND MAGNETO. LYCOMING AEIO-540-D4A5 EWIZ

PITTS S-2S 13465 REVISIONS TO ENGINE INSTALLATION ALTERNATIVE SKY DYNAMICS COLD AIR INDUCTION SUMP, SKY DYNAMICS EXHAUST, API FUEL LYCOMING AEIO-540-D4A5 EWIZ INJECTION AND WOLF COWLING FITTED FITTED PITTS S-2S 13476 MAIN LANDING GEAR CHANGE TO RV MAIN UNDERCARRIAGE REPLACED WITH HARMON ROCKET STYLE LEGS FITTED TO MODIFIED LYCOMING AEIO-540-D4A5 EWIZ STYLE HARMON ROCKET ENGINE MOUNT PITTS S-2S 13492 NEW FIN AND TAILPLANE WITH FIN AND RUDDER, TAILPLANE AND ELEVATORS RESTYLED TO INCLUDE AERODYNAMIC HORN LYCOMING AEIO-540-D4A5 EWIZ ENLARGED, HORN BALANCED RUDDER BALANCE, ELEVATOR MASS BALANCE, INCREASED ELEVATOR AND RUDDER AREA AND TO LOOK AND ELEVATORS SIMILAR TO PITTS S2C. MOD RAISED TO ISSUE 2 TO INCLUDE REVISED TAILPLANE AND ELEVATORS WHICH WERE INCORPORATED AT PHASE 2. PLUMB BGP-1 14043 LIQUID COOLED CYLINDER HEADS ROTEC ENGINEERING'S LIQUID COOLED CYLINDER HEADS (LCH) KIT FITTED IN ACCORDANCE WITH JABIRU 2200A (MODIFIED) BGPI INSTALLATION THE MANUFACTURER'S INSTRUCTIONS TO THE PREVIOUSLY INSTALLED JABIRU 2200A ENGINE WITH ASSOCIATED RADIATOR AND ELECTRIC COOLANT PUMP. POLIKARPOV PO-2 13568 HERCULES 9364299 93" X 64" HERCULES 9364299 92.5 INCH DIAMETER X 64.47 INCH PITCH PROPELLER INSTALLATION SHVETSOV M-11D BSSY PORTERFIELD CP50 13341 FITTING GENIPOD GENERATOR GENNIPOD FITTED TO UNDERCARRIAGE LEGS PER APLICANT'S DRAWING CONTINENTAL A65-8F AFZL PORTERFIELD CP50 13815 ENGINE AND PROPELLER CHANGE DUE TO LACK OF SPARE PARTS FOR CONTINENTAL A50, ENGINE CHANGED FROM CONTINENTAL CONTINENTAL A65-8F AFZL A50 TO CONTINENTAL A65-8 AS FITTED TO PORTERFIELD CP65 VARIANT Prototype mods that have been approved since 1/1/2008 Page 78 30/11/20 LAA Technical Leaflet TL 3.17 PORTERFIELD CP65 12883 PROPELLER CHANGE TO SENSENICH 74CK- PROPELLER CHANGE TO SENSENICH 74CK-0-46, 74 INCH DIAMETER X 46 INCH PITCH METAL CONTINENTAL A65-8 BVWY 0-46 PROPELLER. PRACTAVIA SPRITE SERIES 2 14180 ENGINE & PROPELLER CHANGE CONTINENTAL 0-300D ENGINE AND MCCAULEY 1A170/EM 73" x 53" PROPELLER SUBSTITUTED CONTINENTAL O-300-D BCVF PULSAR 13001 ENGINE REPLACEMENT - SUBFRAME LATER TYPE JABIRU 2200A FITTED, WITH MINOR CHANGE TO ENGINE MOUNT TO SUIT SUMP OF JABIRU 2200A BXDU MODIFICATION LATER TYPE ENGINE, ALSO AIR INTAKE SYSTEM ALTERED TO SUIT PULSAR 13111 WARP DRIVE RPM 2 BLADED 56" INSTALLATION OF WARP DRIVE RPM 2 BLADED 56 INCH DIAMETER PROPELLER. ROTAX 582 BTWY DIAMETER PROPELLER PULSAR 14438 FLAP LEVER REPAIR SCHEME ' ROTAX 582 LWNG PULSAR 13326 PROPELLER CHANGE TO WARP DRIVE WARP DRIVE RPM 2 BLADED 56" DIAMETER PROPELLER SUBSTITUTED ROTAX 582 BTRF PULSAR 13405 ADDITION OF NOSE BALLAST 8 LBS OF LEAD BALLAST WEIGHT BOLTED AND BONDED TO FRONT INSIDE OF ENGINE COWL. ROTAX 582 CHEX PULSAR 13036 IMPROVEMENTS TO FUEL SYSTEM INSTALLATION OF ALUMINIUM FUEL PIPE FROM TANK THROUGH FIREWALL TO GASCOLATOR, ROTAX 582 BVTW ADDITION OF FUEL DRAIN TAP FROM TEE FITTING AT GASCOLATOR INLET, RE-ARRANGEMENT OF PNEUMATIC AND ELECTRIC PUMPS IN PARALLEL, ADDITION OF FUEL FLOW TRANSDUCER IN PARALLEL WITH A BYPASS VALVE THAT WOULD OPERATE IN THE CASE WHERE THE TRANSDUCER BECOMES BLOCKED AND INSTALLATION OF PURPOSE MADE FUEL DISTRIBUTION MANIFOLD/CABLE OPERATED PRIMER VALVE. PULSAR 13037 COOLING SYSTEM CHANGES INSTALLATION OF COOLANT COLLECTION TANK MADE FROM AN ALUMINIUM AUTOMOTIVE ROTAX 582 BVTW 'SWIRLPOT' MODIFIED WITH THE WELDED ON ADDITION OF APPROPRIATE HOSE FITTINGS AND MOUNTING BRACKET, INSTALLATION OF MOULDED PLASTIC AUTOMOTIVE PRESSURISED COOLANT OVERFLOW BOTTLE MOUNTED TO FIREWALL WITH ANTI-VIBRATION MOUNTS, ELIMINATION OF COOLANT BYPASS HOSE AND THERMOSTAT AND ADDITION OF AIR VENT FROM CYLINDER HEAD TO COLLECTION TANK AND INSTALLATION OF BRASS PURPOSE MADE FLOW GUIDE/O-RING RETAINER INTO CYLINDER HEAD AT COOLANT OUTLET. PULSAR 13137 OIL TANK MOUNTING IMPROVEMENTS INSTALLATION OF CUSTOM MADE ALUMINIUM ENGINE OIL TANK WITH INTEGRAL MOUNTINGS ROTAX 582 BVTW ATTACHED TO REAR OF ENGINE VIA FABRIC REINFORCED RUBBER ANTI-VIBRATION STRIPS.

PULSAR 13792 FIT MERIN BLADDER TANKS WITHIN MERIN BLADDER TANKS FITTED WITHIN EXISTING TANK SPACES IN WINGS. PLACARD MUST BE ROTAX 582 RMAN EXISTING FUEL TANKS FITTED CLOSE TO FUEL SELECTOR STATING 'CAUTION - IF BOTH TANKS ARE SELECTED, THE ENGINE WILL STOP AS SOON AS EITHER TANK BECOMES EMPTY.' PULSAR 3 14726 MGL XTREME DUAL AXIS AUTO-PILOT INSTALLATION OF MGL DUAL AXIS AUTO-PILOT CONTROLLED VIA MGL XTREME EFIS. ROTAX 912-ULS BYJL INSTALLATION BUZZER, MOUNTED TO CENTRAL SECTION OF INSTRUMENT PANEL, CONNECTED TO PIN NO. OF MGL XTREME UNIT TO PROVIDE AURAL WARNING OF SERVO DISENGAGEMENT.

PITCH SERVO MOUNTED TO AFT END OF CENTRAL TUNNEL STARBOARD SIDE-WALL WITH SHORT PUSH-ROD DRIVING ELEVATOR AFT PUSH-ROD AT ITS CONNECTION WITH THE ELEVATOR FORWARD PUSH-ROD.

ROLL SERVO MOUNTED ON CUSTOM MADE BRACKET FITTED TO CENTRAL TUNNEL STARBOARD SIDE-WALL AFT OF SEAT BACK BULKHEAD WITH PUSH-ROD DRIVING PRIMARY AILERON BELLCRANK GANGED WITH REARMOST PRIMARY AILERON PUSH-ROD ROD-END WITH LONGER BOLT.

PULSAR XP 13534 PROPELLER CHANGE TO WOODCOMP WOODCOMP KLASSIC 1600MM (63") DIA THREE BLADED PROPELLER FITTED. ROTAX 912-UL BUZB KLASSIC 1600MM PULSAR XP 13535 PITCH TRIM ACTUATOR RAY ALLEN SERVO FITTED ACTING ON TRIM BIAS SPRING TO REPLACE MECHANICAL SYSTEM ROTAX 912-UL BUZB REPLACEMENT/RELOCATION PULSAR XP 14309 OIL COOLER LOCATION A DOCKING 013-1 OIL COOLER IS LOCATED ABOVE THE ENGINE ON THE PORT SIDE, INCLUDING A ROTAX 912-UL CISE SHROUD TO PASS AIR FROM THE ADJACENT COWL OPENING OVER THE COOLER MATRIX. THE SHROUD INCORPORATES A DEFLECTOR FLAP, CONTROLLED BY A PUSH-PULL LEVER IN THE COCKPIT, TO VARY THE AMOUNT OF AIR FLOWING THROUGH THE MATRIX.

Prototype mods that have been approved since 1/1/2008 Page 79 30/11/20 LAA Technical Leaflet TL 3.17 PULSAR XP 14310 CABIN HEAT CABIN HEAT PROVIDED BY AN ALLOY MUFF AROUND A STRAIGHT SECTION OF THE ENGINE ROTAX 912-UL CISE EXHAUST SYSTEM. AIR DUCTED FROM FRONT FACE OF COWLING THROUGH MUFF AND VIA A SCAT HOSE TO AN ALLOY MIXER BOX ON THE FRONT FACE OF THE FIREWALL. A COCKPIT-OPERATED FLAP ALLOWS THE FOR THE AIR FLOW TO BE CONTROLLED OR STOPPED. A CARBON MONOXIDE MONITOR IN THE COCKPIT CHECKS THE AIR QUALITY. PULSAR XP 14311 TAIL SPRING MOUNTING TAIL SPRING MOUNTED TO REAR FUSELAGE VIA A COMPOSITE TUBE RATHER THAN DIRECTLY, TO ROTAX 912-UL CISE ENABLE EASY REMOVAL OF A DAMAGED TAIL SPRING. TUBE IS CONSTRUCTED OF GLASS CLOTH WITH EPOXY RESIN WRAPPED AROUND TAIL SPRING. THE TUBE IS BONDED IN POSITION AS PER THE BUILD MANUAL. TAIL SPRING RETAINED IN TUBE USING AN AN3 BOLT. QAC QUICKIE TRI-Q 12516 NEW NOSE LEG WITH EXTENDED NEW NOSE LEG WITH VERTICAL SECTION THREE INCHES LONGER THAN PREVIOUS LEG TO ALLOW VW 2276 FARY LENGTH. SHORTER TAKE-OFF RUN. QAC QUICKIE TRI-Q 12929 PRINCE P-TIP 52" X 49" PROPELLER CHANGE TO PRINCE P-TIP 52 INCH DIAMETER X 49 INCH PITCH. VW 2276 FARY QAC QUICKIE TRI-Q 13947 ENGINE CHANGE TO GREAT PLAINS LIMBACH ENGINE REPLACED WITH GREAT PLAINS VW2276 UNIT VW 2276 FARY AIRCRAFT VW 2276 QUAD CITY CHALLENGER II 12281 PROPELLER CHANGE TO IVOPROP 3 CHANGE OF PROPELLER TO IVOPROP 3 BLADED 60 INCH DIAMETER GROUND ADJUSTABLE SET TO ROTAX 503 MYAG BLADED 60 INCH DIA 13 DEGREES PITCH AT TIP QUAD CITY CHALLENGER II 12799 REVISED MAIN UNDERCARRIAGE COMPOSITE MAIN UNDERCARRIAGE LEGS FITTED AS PREVIOUSLY APPROVED ON G-CAMR, WITH ROTAX 503 MYTT IMPROVED WHEELS AND HYDRAULIC BRAKE QUICKIE TRI-Q 200 14266 T.A.F.-L SPIN ON OIL FILTER ADAPTER INSTALLATION OF A T.A.F.-L SPIN-ON OIL FILTER ADAPTER IN ACCORDANCE WITH STC SE7559SW CONTINENTAL O-200-A BWIZ INSTALLATION USING TEMPEST AA48108 OIL FILTER AS PERMITTED BY FAA-PMA NO. PQ1206CE SUPPLEMENT NO. 90. RAF 2000 14262 IMPROVED CARB HEAT MUFF CARB HEAT MUFF OF IMPROVED DESIGN FITTED USING A LONGER AIR PATH TO INCREASE SUBARU EA82 BVSM TEMPERATURE RISE RAF 2000 GTX-SE 14335 OIL COOLER AND THERMOSTATIC OIL INSTALLATION OF OIL COOLER WITH CUSTOM MADE BRACKETS TO REAR OF COCKPIT BELOW SUBARU EJ22 BXAC VALVE INSTALLATION BATTERY CARRIER AND WITH 80°C THERMOSTATIC OIL VALVE SANDWICHED BETWEEN OIL FILTER AND ORIGINAL OIL FILTER ATTACHMENT POSITION. RAF 2000 GTX-SE 12311 TAILPLANE, TIP FINS, DOOR PIP PINS TAILPLANE ADDED INCLUDING TIP FINS AND RUDDER CENTERING SPRINGS. 'PRODUCTION SUBARU EJ22 BXDE AND RUDDER CENTERING SPRINGS VERSION OF MODIFICATION 11838. PIP PINS ALSO SUBSTITUTED FOR CABIN DOOR HINGE PINS AND CABIN DOOR PLACARDS ALTERED ACORDINGLY RAF 2000 GTX-SE 12973 INSTALL STROBE LIGHTS TO INCREASE INSTALLATION OF TWO OFF SKYFLASH STROBE HEADS, MOUNTED ABOVE EACH DOOR, CONTROL SUBARU EJ22 BYJA VISUAL SAFETY BOX AND ASSOCIATED WIRING AND SWITCHES. RAF 2000 GTX-SE 13768 FUEL INJECTION WITH SDS ENGINE THIS MODIFICATION CONSISTS OF SEVERAL ELEMENTS. PART 1 CONVERT ENGINE FROM SUBARU EJ22 BXAC MANAGEMENT SYSTEM AND SWIRL POT CARBURRED TO FUEL INJECTED. PART 2 FIT SDS ENGINE MANAGEMENT SYSTEM, TIMING TRIGGER MAGNETS AND TIMING SENSOR, OXYGEN SENSOR AND FUEL/AIR RATIO INDICATOR. PART 3 FIT SWIRL POT TO FUEL SYSTEM ON OUTLET SIDE OF FUEL RAIL TO AVOID PUMP CAVITATION. PART 4 SET UP SDS SYSTEM WITH APPROPRIATE FUEL AND IGNITION MAPS. OXYGEN SENSOR TO BE USED TO DISPLAY AIR/FUEL RATIO ONLY, SYSTEM NOT TO BE USED IN CLOSED LOOP MODE, THIS MOD APPROVES OPEN LOOP OPERATION ONLY. AFTER INITIAL SETUP, MIXTURE CONTROL KNOB MUST BE PROGRAMMED TO BE LOCKED OUT AND MIXTURE CONTROL KNOB REMOVED BEFORE FLIGHT. ALL FOUR PARTS HAVE BEEN CARRIED OUT ON G-BYIN. FOR RAF 2000 GTX-SE ALREADY FITTED WITH THE RAF FACTORY-SUPPLIED FUEL INJECTION SYSTEM, ONLY PARTS 2, 3 AND 4 ARE REQUIRED. THE SYSTEM IS USER-PROGRAMMED. THE SYSTEM USES THE SUBARU MANIFOLD, INJECTORS AND THROTTLE BODY BUT DISPENSES WITH THE MASS AIRFLOW SENSOR, KNOCK SENSOR, CAMSHAFT POSITION SENSOR AND IDLE AIR CONTROL VALVE AND ALL THE ASSOCIATED WIRING AND ELECTRONICS, OXYGEN SENSOR USED ONLY TO DISPLAY F/A RATIO.

Prototype mods that have been approved since 1/1/2008 Page 80 30/11/20 LAA Technical Leaflet TL 3.17 RAF 2000 GTX-SE 13768 FUEL INJECTION WITH SDS ENGINE THIS MODIFICATION CONSISTS OF SEVERAL ELEMENTS. PART 1 CONVERT ENGINE FROM SUBARU EJ22 BYIN MANAGEMENT SYSTEM AND SWIRL POT CARBURRED TO FUEL INJECTED. PART 2 FIT SDS ENGINE MANAGEMENT SYSTEM, TIMING TRIGGER MAGNETS AND TIMING SENSOR, OXYGEN SENSOR AND FUEL/AIR RATIO INDICATOR. PART 3 FIT SWIRL POT TO FUEL SYSTEM ON OUTLET SIDE OF FUEL RAIL TO AVOID PUMP CAVITATION. PART 4 SET UP SDS SYSTEM WITH APPROPRIATE FUEL AND IGNITION MAPS. OXYGEN SENSOR TO BE USED TO DISPLAY AIR/FUEL RATIO ONLY, SYSTEM NOT TO BE USED IN CLOSED LOOP MODE, THIS MOD APPROVES OPEN LOOP OPERATION ONLY. AFTER INITIAL SETUP, MIXTURE CONTROL KNOB MUST BE PROGRAMMED TO BE LOCKED OUT AND MIXTURE CONTROL KNOB REMOVED BEFORE FLIGHT. ALL FOUR PARTS HAVE BEEN CARRIED OUT ON G-BYIN. FOR RAF 2000 GTX-SE ALREADY FITTED WITH THE RAF FACTORY-SUPPLIED FUEL INJECTION SYSTEM, ONLY PARTS 2, 3 AND 4 ARE REQUIRED. THE SYSTEM IS USER-PROGRAMMED. THE SYSTEM USES THE SUBARU MANIFOLD, INJECTORS AND THROTTLE BODY BUT DISPENSES WITH THE MASS AIRFLOW SENSOR, KNOCK SENSOR, CAMSHAFT POSITION SENSOR AND IDLE AIR CONTROL VALVE AND ALL THE ASSOCIATED WIRING AND ELECTRONICS, OXYGEN SENSOR USED ONLY TO DISPLAY F/A RATIO.

RAF 2000 GTX-SE 14335 OIL COOLER AND THERMOSTATIC OIL INSTALLATION OF OIL COOLER WITH CUSTOM MADE BRACKETS TO REAR OF COCKPIT BELOW SUBARU EJ22 BYIN VALVE INSTALLATION BATTERY CARRIER AND WITH 80°C THERMOSTATIC OIL VALVE SANDWICHED BETWEEN OIL FILTER AND ORIGINAL OIL FILTER ATTACHMENT POSITION. RAF 2000 GTX-SE 12779 INSTALL VTB FUEL COMPUTER OWN-DESIGNED FUEL FLOW METER / COMPUTER FITTED, USING FLOSCAN FUEL FLOW SUBARU EJ22 CBJE TRANSDUCER RAF 2000 GTX-SE 12578 REPLACE STUB AXLES AND FIT DISC MATCO M6HB WHEELS AND MATCHING AXLES AND HYDRAULIC DISC BRAKES FITTED AS INSTALLED SUBARU EJ22 YROJ BRAKES ON G-BYIN EXCEPT DUAL MASTER CYLINDERS AND ALUMIUM ALLOY BRAKE PIPES FITTED. SECOND MASTER CYLINDER MADE FROM PIPER CYLINDER p/n 17000 RAND KR-2 12728 PROPELLER CHANGE TO GT INSTALLATION OF GT-2/142/VVU PROPELLER ON JABIRU 2200A ENGINE. JABIRU 2200A CEHT RAND KR-2 13835 ENGINE CHANGE TO JABIRU 2200A ENGINE CHANGE FROM VW TO JABIRU 2200A PER G-BSTL INSTALLATION JABIRU 2200A BYLP RANS S10 13108 ENGINE CHANGE TO ROTAX 582 WITH INSTALLATION OF ROTAX 582 ENGINE WITH IVOPROP 2 BLADED 66 INCH DIAMETER GROUND ROTAX 582 BSMT IVOPROP 2 BLADE 66" DIA PROPELLER. ADJUSTABLE PROPELLER SET 12.5 DEGREES PITCH AT THE TIP TO PROVIDE 6300 MAXIMUM STATIC RPM. RANS S10 12483 PROPELLER CHANGE TO WARP DRIVE 2 WARP DRIVE 2 BLADED 66" DIAMETER GROUND ADJUSTABLE PROPELLER INSTALLED. ROTAX 582 BTCR BLADED 66" DIAMETER GROUND ADJUSTABLE RANS S10 13079 AILERON SPADES RANS STANDARD OPTIONAL AILERON SPADES ADDED ROTAX 582 BUAX RANS S10 12262 PROPELLER CHANGE TO WARP DRIVE 66 CHANGE OF PROPELLER TO WARP DRIVE RPM 3 BLADED 66 INCH DIAMETER ROTAX 912-UL BTWZ INCH DIA 3 BLADE RANS S6 13062 ENGINE CHANGE TO ROTAX 582 2-V CHANGE OF ENGINE TO ROTAX 582 2-V WITH WARP DRIVE RPM 2 BLADED 66 INCH DIAMETER X ROTAX 582 BSMU 12.5 DEGREES PITCH PROPELLER. RANS S6 14092 CATEGORY CHANGE FROM GROUP A TO CATEGORY CHANGE PER AAN PFA-204-191 issue 2 ROTAX 582 BSSI MICROLIGHT RANS S6-116 12452 ENGINE CHANGE TO ROTAX 912-UL. CHANGE OF ENGINE TO ROTAX 912-UL. ROTAX 912-UL BVUM RANS S6-116 12453 PROPELLER CHANGE TO WARP DRIVE CHANGE OF PROPELLER TO WARP DRIVE RPM 2 BLADED 66" DIAMETER. ROTAX 912-UL BVUM RPM 2 BLADED 66" DIAMETER. RANS S6-116 12555 REMOVABLE UPPER PART OF ENGINE THE CUTTING OFF OF THE UPPER PART OF THE ENGINE COWLING NOSE BOWL AND USING EIGHT ROTAX 912-UL BWYR COWLING NOSE BOWL. 1/4 TURN FASTENERS FOR ITS RE-ATTACMENT TO THE LOWER PART. RANS S6-116 14940 PROPELLER CHANGE TO WOODCOMP PROPELLER CHANGE TO WOODCOMP KLASSIC 160/3/R. ROTAX 912-UL BXCU KLASSIC 160-3R RANS S6-116 13163 PROPELLER CHANGE TO WOODCOMP WOODCOMP KLASSIC 170/3/R INSTALLED ON ROTAX 912-UL ENGINE. ROTAX 912-UL CDGB KLASSIC 170/3/R RANS S6-ES 12439 HKS700E ENGINE INSTALLATION HKS700E ENGINE INSTALLED USING MODIFIED ROTAX 912 ENGINE MOUNT AND STANDARD RANS HKS 700E CFDK ENGINE COWLINGS. RANS S6-ES 11388 PROPELLER CHANGE GT-2/157/98 PROPELLER FITTED JABIRU 2200A BYPT Prototype mods that have been approved since 1/1/2008 Page 81 30/11/20 LAA Technical Leaflet TL 3.17 RANS S6-ES 14041 INSTALLATION OF EFIS/EMS MGL AVIONICS XTREAM EFIS/EMS SYESTEM FITTED TO FACILITATE CHT MONITORING JABIRU 2200A BYRG INSTRUMENT SYSTEM RANS S6-ES 14042 PASSIVE HEATING SYSTEM CARB BODY HEATER FITTED, HEATED BOTH BY CIRCULATING ENGINE OIL THROUGH IT AND WITH JABIRU 2200A BYRG AN EMBEDDED ELECTRIC HEATER ELEMENT. PILOT'S NOTES SUPPLEMENT PAGE 08 REFERS

RANS S6-ES 14080 ENGINE AND PROPELLER CHANGE INSTALLATION OF JABIRU 2200A ENGINE AND GT-2/157/NO-FW101SRTC PROPELLER. JABIRU 2200A SOOZ RANS S6-ES 12249 PROPELLER CHANGE TO GT-2/157/95 CHANGE OF PROPELLER TO GT-2/157/95 157CM DIAMETER X 95CM PITCH JABIRU 2200A BZGR RANS S6-ES 15026 SKIN REPLACEMENT ORIGINAL DACRON SKINS REPLACED WITH NEW SKINS MANUFACTURED BY TOP FLIGHT SAILS LTD. JABIRU 2200A BZMJ SKINS REPLACED ON: FUSELAGE, WINGS, FLAPS, AILERONS, ELEVATORS, TAILPLANE, FIN AND RUDDER.

NEW SKINS USE IDENTICAL MATERIALS, THREAD, PATTERNS AND STITCHING AS THE ORIGINALS.

RANS S6-ES 14328 JABIRU 2200A ENGINE AND GT-2/157/NO-INSTALLATION OF JABIRU 2200A ENGINE AND GT2/157/NO-FW101SRTC PROPELLER. JABIRU 2200A CBUY FW101SRTC PROPELLER INSTALLATIONS

RANS S6-ES 14838 CATEGORY CHANGE FROM MICROLIGHT MAX GROSS WEIGHT INCREASED TO 454 Kg JABIRU 2200A TSOB TO GROUP A VFE INCREASED TO 80 MPH DESIGNATION CHANGED TO RANS S6-ESA CLASSIFICATION CHANGED TO SEP AEROPLANE RANS S6-ES 15463 CATEGORY CHANGE TO MICROLIGHT CATEGORY CHANGE TO MICROLIGHT, MTWA REDUCED TO 450 KG JABIRU 2200A TSOB RANS S6-ES 14941 VARLEY LI-5 LITHIUM IRON PHOSPHATE INSTALLATION OF A VARLEY LI-5 LITHIUM IRON PHOSPHATE (LiFePO4) BATTERY IN CUSTOM MADE JABIRU 2200A CITH BATTERY INSTALLATION BATTERY BOX THAT ALSO SUPPORTS A KEY OPERATED BATTERY ISOLATING SWITCH, MOUNTED TO FUSELAGE STRUCTURE IMMEDIATELY AFT OF P2 SEAT BACK.

6.3KG OF BALLAST AND TRAY MOUNTED IN FUSELAGE REAR TO REPLACE REMOVED BATTERY.

RANS S6-ES 13374 ADDITION OF COAMING BETWEEN TOP INSTALLATION OF ALUMINIUM SHEET COAMING FROM UNDER LIP AT TOP OF INSTRUMENT PANEL JABIRU 2200A SBAP OF INSTRUMENT PANEL AND FIREWALL TO FIREWALL. SECURED TO FUSELAGE FRAME MEMBERS WITH CUSHIONED P-CLIPS. OPTIONAL BRACE TUBE AT TOP OF INSTRUMENT PANEL MUST NOT BE FITTED. RANS S6-ES 13610 JURY STRUT FIXING REPLACEMENT OF 1 OFF STIFF NUT ON EACH JURY STRUT WITH SAFETY-PIN LOCKED CASTELLATED JABIRU 2200A SBAP NUTS AND 1 OFF BOLT REPLACED WITH DRILLED EQUIVALENT AND WIRE-LOCKED TO FACILITATE REPEATED RIGGING/DE-RIGGING. RANS S6-ES 13827 OIL COOLER MOUNTED WITH RUBBER INSTALLATION OF OIL COOLER USING MERLIN M6 RUBBER MOUNTING BOBBINS BETWEEN EACH JABIRU 2200A SBAP BOBBINS MOUNTING HOLE AND ORIGINAL, REVERSED P-CLIP. ADDITIONAL ALUMINIUM SUPPORT BRACKET ATTACHED TO INBOARD FLANGE OF OIL COOLER FITTED TO SUPPORT BOTH INLET AND OUTLET OIL HOSES AGAINST VIBRATION USING FOUR MINIMUM STRONG TIE WRAPS. RANS S6-ES 14107 ADDITION OF COAMING INSTALLATION OF ALUMINIUM SHEET COAMING FROM UNDER LIP AT TOP OF INSTRUMENT PANEL JABIRU 2200A GWFT TO FIREWALL. SECURED TO FIREWALL USING 3 OFF SCREWS AND NUT PLATES. OPTIONAL BRACE TUBE AT TOP OF INSTRUMENT PANEL MUST NOT BE FITTED. RANS S6-ES 14982 INSTRUMENT PANEL COAMING INSTALLATION OF ALUMINIUM SHEET COAMING FROM TOP OF INSTRUMENT PANEL TO FIREWALL. JABIRU 2200A TBLC SECURED TO FUSELAGE FRAME MEMBERS WITH CUSHIONED P-CLIPS. INCORPORATES RECESSED DOCUMENT TRAYS. OPTIONAL BRACE TUBE AT TOP OF INSTRUMENT PANEL MUST NOT BE FITTED.

RANS S6-ES 14107 ADDITION OF COAMING INSTALLATION OF ALUMINIUM SHEET COAMING FROM UNDER LIP AT TOP OF INSTRUMENT PANEL JABIRU 2200A EGCA TO FIREWALL. SECURED TO FIREWALL USING 3 OFF SCREWS AND NUT PLATES. OPTIONAL BRACE TUBE AT TOP OF INSTRUMENT PANEL MUST NOT BE FITTED.

Prototype mods that have been approved since 1/1/2008 Page 82 30/11/20 LAA Technical Leaflet TL 3.17 RANS S6-ES 13187 FUEL SELECTOR VALVE REMOVAL OF TWO INDIVIDUAL FUEL ON/OFF TAPS BEHIND SEATS FOR EACH WING TANK AND ROTAX 582/48 MZMS INSTALLATION OF SINGLE FUEL SELECTOR VALVE WITH LEFT/OFF/RIGHT SELECTION IN LOWER FRONT OF COCKPIT. COCKPIT PLACARD MUST BE INSTALLED IN CLEAR VIEW OF THE PILOT STATING 'CAUTION: PROLONGED SIDE SLIPPING WITH FUEL TANK OF LOWER WING SELECTED MAY CAUSE FUEL STARVATION'. RANS S6-ES 13232 GRP PROPELLER SPINNER WITH FRONT MANUFACTURE AND INSTALLATION OF GRP PROPELLER SPINNER WITH FRONT AND BACK PLATE ROTAX 582/48 BYCN AND BACK PLATE MANUFACTURE AND INSTALLATION. RANS S6-ES 15238 CATEGORY CHANGE TO GROUP A INCREASED MTWA TO 454 KG, NARROW CHORD FLAPS AND AILERONS. REPLACEMENT WEIGHT ROTAX 582/48 BYJO AND BALANCE REPORT RANS S6-ES 15445 CATEGORY CHANGE TO MICROLIGHT CATEGORY CHANGE BACK TO MICROLIGHT ROTAX 582/48 BYJO RANS S6-ES 13853 WARP DRIVE RPM 2 BLADED 64" X 13 WARP DRIVE RPM 2 BLADED 64 INCH DIAMETER X 13 DEGREES AT TIP PROPELLER INSTALLATION ROTAX 582/48 BZEW DEG PROPELLER INSTALLATION RANS S6-ES 15026 SKIN REPLACEMENT ORIGINAL DACRON SKINS REPLACED WITH NEW SKINS MANUFACTURED BY TOP FLIGHT SAILS LTD. ROTAX 582/48 BZEW SKINS REPLACED ON: FUSELAGE, WINGS, FLAPS, AILERONS, ELEVATORS, TAILPLANE, FIN AND RUDDER.

NEW SKINS USE IDENTICAL MATERIALS, THREAD, PATTERNS AND STITCHING AS THE ORIGINALS.

RANS S6-ES 12571 RANS S6 CENTRE FUEL TANK CENTRE FUEL TANK ADDED PER EARLIER MODEL RANS S6 ACTING AS HEADER TANK ROTAX 582/48 BZGF RANS S6-ES 13477 RANS S6 ELECTRIC TRIM PROPOSAL CUSTOM ELECTRIC ELEVATOR TRIM TAB SERVO FITTED OPERATING CUSTOM TRIM TAB, ROTAX 582/48 BZGF ASSOCIATED ELECTRICAL SWITCH AND POSITION INDICATOR UNIT RANS S6-ES 12571 RANS S6 CENTRE FUEL TANK CENTRE FUEL TANK ADDED PER EARLIER MODEL RANS S6 ACTING AS HEADER TANK ROTAX 582/48 CCTV RANS S6-ES 12716 ENGINE CHANGE TO ROTAX 912-F4 WITH ENGINE CHANGE TO ROTAX 912-F3 MODIFIED TO -F4 USING ROTAX PARTS AND WITH WARP DRIVE ROTAX 912-F4 BZKF WARP DRIVE RPM 2 BLADED 66" DIA PRO RPM 2 BLADED 66" DIA PROPELLER.

RANS S6-ES 12133 HYDRAULIC DISC BRAKES INSTALLATION OF BX-1000 BLACK MAX WHEELS AND HYDRAULIC DISC BRAKE SYSTEM WITH HAND ROTAX 912-F4 BZKF LEVER AND MASTER CYLINDER MOUNTED ON P1 CONTROL COLUMN. RANS S6-ES 12380 PROPELLER CHANGE WARP DRIVE RPM 2 BLADED 66 x 14.5 DEGREES FITTED ROTAX 912-UL CCTX RANS S6-ES 12555 REMOVABLE UPPER PART OF ENGINE THE CUTTING OFF OF THE UPPER PART OF THE ENGINE COWLING NOSE BOWL AND USING EIGHT ROTAX 912-UL CCTX COWLING NOSE BOWL. 1/4 TURN FASTENERS FOR ITS RE-ATTACMENT TO THE LOWER PART. RANS S6-ES 13213 ROTAX 912-UL WITH WARP DRIVE RPM 2 INSTALLATION OF ROTAX 912-UL ENGINE FITTED WITH WARP DRIVE RPM 2 BLADED 66 INCH ROTAX 912-UL BXWK BLADED 66" DIA X 14.5 DEG PROPELLER DIAMETER X 14.5 DEGREES PITCH PROPELLER.

RANS S6-ES 12555 REMOVABLE UPPER PART OF ENGINE THE CUTTING OFF OF THE UPPER PART OF THE ENGINE COWLING NOSE BOWL AND USING EIGHT ROTAX 912-UL RTHS COWLING NOSE BOWL. 1/4 TURN FASTENERS FOR ITS RE-ATTACMENT TO THE LOWER PART. RANS S6-ESA 15118 REMOVABLE RH STICK MODIFICATION MODIFICATION TO RIGHT HAND CONTROL COLUMN TO ENABLE ITS REMOVAL AND RE- ROTAX 582/48 CCOF INSTALLATION WITHOUT SPECIAL TOOLS. STEEL SLEEVE RIVETED TO BASE OF CUT-DOWN CONTROL COLUMN TO LOCATE ONTO REMAINING STUB. CONTROL COLUMN SECURED WITH SINGLE BOLT, CASTELLATED NUT AND SAFETY PIN.

RANS S6-ESA 13200 CHANGE ENGINE TO ROTAX 912-UL WITH INSTALLATION OF ROTAX 912-UL ENGINE WITH WARP DRIVE RPM 2 BLADED 66 INCH DIAMETER ROTAX 912-UL MZOZ WARP DRIVE 2 BLADED 66" DIA PROP PROPELLER AT 14.5 DEGREES PITCH.

RANS S6-ESA 14392 CATEGORY CHANGE FROM MICROLIGHT NO PHYSICAL CHANGE TO AIRCRAFT, CATEGORY CHANGED TO SEP WITH 1000 LBS MAX GROSS ROTAX 912-UL MZOZ TO GROUP A WEIGHT RANS S6-ESA 14888 KIEV 273/1700 PROPELLER INSTALLATION INSTALLATION OF KIEV 273/1700, 1700 MM DIAMETER PROPELLER. ROTAX 912-UL MZOZ

Prototype mods that have been approved since 1/1/2008 Page 83 30/11/20 LAA Technical Leaflet TL 3.17 RANS S6-ESA 15338 ELECTRIC FUEL PUMP INSTALLATION FACET 40106 ELECTRIC FUEL PUMP INSTALLED ON SHELF FORWARD OF FUSELAGE MOUNTED FUEL ROTAX 912-UL MZOZ TANK. INCORPORATES APPROPRIATE WIRING, CIRCUIT PROTECTION AND AN ILLUMINATED SWITCH. RANS S6-ESA 14397 CATEGORY CHANGE TO GROUP A CATEGORY CHANGE FROM MICROLIGHT TO GROUP A. NO PHYSICAL CHANGE TO AIRCRAFT. MAX ROTAX 912-UL WZOY GROSS WEIGHT INCREASED TO 1000 LBS RANS S6-ESD 12796 LEADING EDGE ATTACHMENT POINT DOUBLER PLATES ADDED TO SPAR TUBES AT ROOT ATTACHMENT, WITH REPLACEMENT INNER ROTAX 503 MWUL REPAIR SLEEVE, RIVETTED IN PLACE PER APPLICANT'S DRAWING . APPLICABLE TO ONE OR BOTH WINGS AS REQUIRED RANS S6-ESD 12837 FUEL TANK REPLACEMENT TWIN RANS S6-ES WING TANKS FITTED INSTEAD OF S6-ESD TYPE FUSELAGE TANK. ROTAX 503 MYHK RANS S6-ESD (MODIFIED) 12405 ELECTRIC STARTER GPL ELECTRIC STARTER FITTED TO ROTAX ENGINE. ROTAX 503 MYIS EMPTY WEIGHT OF MODIFIED AIRCRAFT MUST NOT EXCEED MAX PERMITTED EMPTY WEIGHT OF 243 Kg. NOTE THAT THE FITTING OF THE STARTER MAY ADVERSELY AFFECT THE ENGINE WARRANTY, IF APPLICABLE. RANS S6-ESD (MODIFIED) 12427 WEIGHT INCREASE TO 430KG INSTALLATION OF AREA 1 AILERONS AND FLAPS, UPRATED FRONT WING STRUTS, PURPOSE MADE ROTAX 503 MYLD GUSSET PLATES TO ATTACH EXISTING REAR STRUTS AND INCREASING FLAP DEPLOYMENT ANGLE TO BETWEEN 40 AND 43 DEGREES. RANS S6-ESD (MODIFIED) 12434 ENGINE CHANGE TO ROTAX 582 WITH CHANGE OF ENGINE TO ROTAX 582 WITH TENNESSEE 66 INCH DIAMETER X 44 INCH PITCH ROTAX 582 MYBA TENNESSEE 66 X 44 PROPELLER PROPELLER FITTED. RANS S6-ESD (MODIFIED) 14229 WARP DRIVE RPM 2 BLADED 66" X 12.5 INSTALLATION OF WARP DRIVE RPM 2 BLADED 66 INCH DIAMETER X 12.5 DEGREES AT THE TIP ROTAX 582 MYBA DEGREES PROPELLER INSTALLATION PROPELLER. RANS S6-ESD (MODIFIED) 13701 ENGINE CHANGE TO ROTAX 582 INSTALLATION OF A ROTAX 582 DCDI ENGINE WITH A WARP DRIVE RPM 2 BLADED 66 INCH ROTAX 582 MYJD DIAMETER X 12.5 DEGREES PITCH PROPELLER. RANS S6-ESD (MODIFIED) 13701 ENGINE CHANGE TO ROTAX 582 INSTALLATION OF A ROTAX 582 DCDI ENGINE WITH A WARP DRIVE RPM 2 BLADED 66 INCH ROTAX 582 MYVP DIAMETER X 12.5 DEGREES PITCH PROPELLER. RANS S6-ESD (MODIFIED) 15302 FITTING OF WING TANKS FACTORY-SUPPLIED WING TANKS FITTED IN CONJUNCTION WITH PREVIOUSLY INSTALLED ROTAX 582 MYVP FUSELAGE TANK. SELECTOR VALVE INSTALLED BETWEEN SEATS. INCORPORATES VALVE TO PREVENT CROSS-FLOW BETWEEN WING TANKS ON THE GROUND. RANS S6-ESD (MODIFIED) 15404 REMOVABLE UPPER PART OF ENGINE THE CUTTING OFF OF THE UPPER PART OF THE ENGINE COWLING NOSE BOWL AND USING THREE ROTAX 582 MYVP COWLING NOSE BOWL 1/4 TURN FASTENERS EACH SIDE FOR ITS RE-ATTACHMENT TO THE LOWER PART. RANS S6-ESD (MODIFIED) 12508 ENGINE CHANGE AND WEIGHT INCREASE ROTAX 582 ENGINE AND WEIGHT UPGRADE TO 450 Kg ROTAX 582 MZEN

RANS S6-ESD (MODIFIED) 13226 IVOPROP 3 BLADED 66" DIAMETER X IVOPROP 3 BLADED GROUND ADJUSTABLE 66 INCH DIAMETER X 12.5 DEGREES PITCH PROPELLER ROTAX 582 MZEN 12.5° PITCH PROPELLER. INSTALLATION. RANS S6-ESD (MODIFIED) 13151 FUEL SYSTEM VENT REARRANGED TO FUEL SYSTEM HEADER TANK VENTED TO TOP OF SITE GAUGE RATHER THAN SEPARATE VENT ROTAX 582/48 MWSC PREVENT SPILLLAGE ON TRANSPAENCY WHICH TENDS TO LEAK OVER TRANSPARNCY, CAUSING CRAZING RANS S6-ESD (MODIFIED) 12677 ENGINE CHANGE TO 582/48 WITH ENGINE CHANGE TO 582/48 WITH ARPLAST ECOPROP 168 104/3 X 14.5 DEGREES PITCH AT 75% ROTAX 582/48 MYDX ARPLAST ECOPROP 168 104/3 PROPELLER RADIUS PROPELLER TO ENABLE GROSS WEIGHT INCREASE TO 450KG.

RANS S6-ESD (MODIFIED) 12743 INSTRUMENT PANEL ENLARGED HOLES RANSD S6-116 / SUPER SIX TYPE INSTRUMENT PANEL FITTED ROTAX 582/48 MYDX RANS S6-ESD (MODIFIED) 12379 ENGINE CHANGE TO ROTAX 912-UL ENGINE CHANGED TO ROTAX 912-UL USING STANDARD RANS INSTALLATION ROTAX 912-UL MYGH RANS S6-ESD (MODIFIED) 12380 PROPELLER CHANGE WARP DRIVE RPM 2 BLADED 66 x 14.5 DEGREES FITTED ROTAX 912-UL MYGH RANS S6-ESD (MODIFIED) 12941 ENGINE CHANGE ROTAX 912 ROTAX 912-UL ENGINE FITTED USING RANS FIREWALL FORWARD KIT ALONG WITH CHANGE TO 450 ROTAX 912-UL SHUC KG CONFIGURATION RANS S6-ESD (MODIFIED) 14361 CHANGE TO RANS ELEVATOR TRIM STANDARD RANS PITCH TRIM SYSTEM REPLACED WITH X'AIR HAWK SYSTEM, CONSISTING OF: X'AIR ROTAX 912-UL SHUC HAWK TRIM TAB MOUNTED TO STANDARD RANS ELEVATOR IN SAME MANNER AS X'AIR HAWK; X'AIR HAWK CONTROL LEVER/PULLEY; X'AIR HAWK CONTROL CABLES; BESPOKE TRIM LEVER MOUNTING IN PORT WING RIB; CONTROL STOPS PROVIDED BY CABLE CLAMPS ADJACENT TO TRIM LEVER. RANS S6-ESD (MODIFIED) 14958 CATEGORY CHANGE FROM GROUP A TO CATEGORY CHANGE FROM GROUP A TO MICROLIGHT ROTAX 912-UL SHUC MICROLIGHT Prototype mods that have been approved since 1/1/2008 Page 84 30/11/20 LAA Technical Leaflet TL 3.17 RANS S6-ESD XL 13396 ROTAX 912-UL ENGINE AND WARP DRIVE INSTALLATION OF ROTAX 912-UL ENGINE AND WARP DRIVE RPM 2 BLADED 66 INCH DIAMETER X ROTAX 912-UL MZNV RPM 2 BLADED 66" X 14.5 ° PROP INST 14.5 DEGREES PITCH PROPELLER.

RANS S6-ESD XL (MODIFIED) 15080 INSTALLATION OF M5 AVIATION M5 AVIATION PRODUCTS ELECTRIC STARTER FITTED TO ROTAX 503. ROTAX 503 2-V MYYV PRODUCTS STARTER FITTED IN ACCORDANCE WITH THE MANUFACTURER'S INSTRUCTIONS, INCLUDING ALLOY ANGLE BRACKET TO SUPPORT THE MOTOR ASSEMBLY BY ATTACHING TO THE ENGINE CRANKCASE.

RANS S6-ESD XL (MODIFIED) 12736 ENGINE CHANGE TO ROTAX 582 AND ENGINE CHANGED TO ROTAX 582 UL DCDI MOD99. PROPELLER CHANGED TO WARPDRIVE 2- ROTAX 582/48 MZIY WARP DRIVE PROPELLER BLADED 64" DIAMETER. RANS S6S-116 SUPER SIX 13589 AUXILLARY ELECTRIC FUEL PUMP ELECTRIC BACK-UP FUEL PUMP FITTED IN SERIES WITH MECHANICAL PUMP, TO REAR OF FIREWALL. ROTAX 912-UL RDNS FUEL PRESSURE GAUGE. RANS S6S-116 SUPER SIX 14515 KIEV 273/1700 PROPELLER INSTALLATION INSTALLATION OF KIEV 273/1700, 1700MM DIAMETER X 28 DEGREES AT 350MM RADIUS PITCH, 3 ROTAX 912-UL RDNS BLADED PROPELLER. RANS S6S-116 SUPER SIX 15193 KIEV 263/1700 PROPELLER INSTALLATION INSTALLATION OF KIEV 263/1700 3 BLADE PROPELLER. ROTAX 912-ULS XALZ

RANS S7 13192 MOD TO AXLE SUPPORT SOCKET REINFORCING STRIP ADDED TO UNDERCARRIAGE SOCKETS. ROTAX 912-UL OJKM RANS S7 12660 ELEVATOR TRIM REPLACE STANDARD PITCH TRIM SYSTEM WITH TRIM WHEEL MOUNTED IN COCKPIT LINKED BY ROTAX 912-ULS CBNF CABLES TO A BELLCRANK AT STATION 6 IN THE REAR FUSELAGE. TRIM TAB OPERATED BY 'PIANO' WIRE FROM BELLCRANK. RANS S7 13094 FUEL COLLECTOR MOD TWIN CYLINDRICAL FUEL HEADER TANKS ADDED IN VICINITY OF REAR DOOR PILLAR TUBES TO ROTAX 912-ULS CBNF ENSURE SUSTAINED FUEL FLOW IN SIDE SLIPPING FLIGHT RANS S7S 12349 LONGITUDINAL STABILITY INSTALLATION OF SHOCK CORDS TO APPLY FORWARD FORCE ON CONTROL STICK AND REVISING ROTAX 912-ULS CEEJ AUGMENTATION RANGE OF TRIM TAB MOVEMENT TO PREVENT LONGITUDINAL INSTABILITY RANS S7S 13785 WOODCOMP KLASSIC 170/3/R INSTALLATION OF WOODCOMP KLASSIC 170/3/R 1720MM DIAMETER PROPELLER. ROTAX 912-ULS CEEJ PROPELLER INSTALLATION RANS S7S 14519 SUBSTITUTE LITHIUM ION BATTERY AND BATTERY RE-LOCATED TO AFT FACE OF FIREWALL IN A BOX FABRICATED FROM 60601-T6 ALLOY. ROTAX 912-ULS CINI MOVE TO REAR OF FIREWALL BATTERY IS A VARLEY LI-5 LITHIUM IRON PHOSPHATE, INSTALLED IN ACCORDANCE WITH SM14337 ISSUE 4. RANS S7S 13943 PROPELLER CHANGE TO SENSENICH INSTALLATION OF SENSENICH 3B0R5R68C 3 BLADED 68 INCH DIAMETER GROUND ADJUSTABLE ROTAX 912-ULS CHTO 3B0R5R68C PROPELLER. REARWIN 175 11919 UPPER TORSO RESTRAINT ADDITION OF UPPER TORSO RESTRAINT FOR BOTH OCCUPANTS ATTACHED TO CLAMP BRACKETS CONTINENTAL A75-8 BTGI ALIGNED WITH AVERAGE OCCUPANT SHOULDER HEIGHT AND SECURED TO UPPER CROSS MEMBER ADJACENT TO WELD CLUSTER PP13R OR PP13L AS APPROPRIATE (REF DRG 16-001). CLAMP BRACKETS SECURED TO CROSS MEMBER WITH 1/8" MONEL RIVET OR ROSETTE WELD.

REARWIN 8125 CLOUDSTER 14452 TRIM PULLEY UPGRADE IMPROVED DESIGN OF TRIM PULLEY USING GREATER ANGLE OF ENGAGEMENT AND IDLER PULLEY WARNER SCARAB 145 EVLE TO PREVENT CABLE SLIPPAGE REARWIN 8500 13646 TRIM INDICATING SYSTEM MECHANICAL, CABLE TYPE TRIM INDICATOR SYSTEM ADDED TO PITCH TRIM SYSTEM LE BLOND AE 5DF AEOF REBEL 14599 PROP CHANGE TO HERCULES 73 X 53 . LYCOMING O-320-A2B DIKY REBEL 13460 TAILPLANE STRUT ATTACHMENTS AN3 BOLTS ATTACHING TAILPLANE STRUTS TO TAILPLANE REPLACED WITH AN4SIZE LYCOMING O-320-C2A BZFT EQUIVALENTS, WITH APPROPRIATE NUTS AND WASHERS, TO ELIMINATE WEAR IN BOLT HOLES. BOLT HOLES DRILLED AND REAMED TO PROVIDE LIGHT PRESS FIT ON ASSEMBLY. REBEL 13456 PROPELLER CHANGE TO HOFFMANN HOFFMANN PROPELLER FIXED PITCH FITTED LYCOMING O-320-D2A MRPH HO23C HM-B188 156C REBEL 13548 HERCULES 6958353-S 69" X 58" INSTALLATION OF HERCULES 6958353-S 69 INCH DIAMETER X 58 INCH PITCH PROPELLER ROTAX 912-ULS BUTK PROPELLER INSTALLATION RENEGADE 912 12305 SOFT START MODULE INSTALLATION OF CON-AIR SPORTS SOFT START MODULE TO ROTAX 912-ULS ENGINE IN ROTAX 912 BWPE ACCORDANCE WITH CON-AIR SPORTS INSTRUCTIONS AND SM12305 LEAFLET. RENEGADE SPIRIT UK 13357 ENGINE CHANGE TO BOXER RT1200 BMW R100 ENGINE REPLACED BY BMW RT1200 USING SAME ENGINE MOUNT REDUCTION GEAR BMW RT1200 MWNF AND PROPELLER AAN PFA 195-0161 sup 6 REFERS Prototype mods that have been approved since 1/1/2008 Page 85 30/11/20 LAA Technical Leaflet TL 3.17 RENEGADE SPIRIT UK 14596 ENGINE & PROPELLER CHANGE - JABIRU POWERPLANT INSTALLED IS A JABIRU 2200A AND HERCULES 6033343-S PROPELLER. INSTALLED ON JABIRU 2200A RNGD 2200A A JABIRU UK ENGINE MOUNT. RENEGADE SPIRIT UK 15099 REMOVABLE REAR WINDSCREEN GRP MOULDED FRAME WITH POLYCARBONATE SCREEN FITTED FORWARD OF REAR COCKPIT JABIRU 2200A MYUF POSITION USING QUICK-RELEASE FASTENERS. RENEGADE SPIRIT UK 12825 PROPELLER CHANGE TO NEWTON TYPE PROPELLER CHANGE TO NEWTON TYPE 23L 65" X 41" ROTAX 582 MVZP 23L 65" X 41" RENEGADE SPIRIT UK 13307 BLACK MAX BX-1320 AXLES, WHEELS INSTALLATION OF BLACK MAX BX-1320 AXLES, WHEELS AND HEEL OPERATED BRAKES. ROTAX 582 MZIZ AND BRAKES REPLICA AVRO 504K 14684 HERCULES 9432705-C 94" x 32" INSTALLATION OF HERCULES 9432705-C 94 INCH DIAMETER X 32 INCH PITCH PROPELLER. ROTEC R3600 EROE PROPELLER INSTALLATION REPLICA BE2C 13699 SMOKE SYSTEM CONVENTIONAL SMOKE SYSTEM FITTED WITH ELECTRIC FUEL PUMP, OIL TANK, NON RETURN DE HAVILLAND GIPSY MAJOR 10 MK AWYI VALVE, NOZZLE AND ASSOCIATED PIPEWORK, CIRCUIT BREAKER AND MOMENTARY SWITCH 1 (MODIFIED) REPLICA BRISTOL M1C 13616 REPLACEMENT OF LE RHONE 110HP REPLACEMENT PISTON ASSEMBLIES MANUFACTURED TO PATTERN USING SUBSTITUTE MATERIALS LE RHONE 110 HP BWJM ENGINE PISTON ASSEMBLIES AND PROCESSES REPLICA BRISTOL SCOUT MODEL 14628 REPLACEMENT LE RHONE 80HP PISTON PISTON ASSEMBLIES CONSISTING OF PISTONS, PISTON RINGS, GUDGEON PINS AND RETAINING LE RHONE 80 HP FDHB C ASSEMBLIES BOLTS,REPLACED WITH NEW PARTS MANUFACTURED BY TVAL IN NEW ZEALAND REPLICA CAMPBELL CRICKET 12769 REPLACE NOSEWHEEL, FRONT FORKS & FRONT WHEEL REPLACED WITH 9.5" MONTGOMERIE ENGINEERING WHEEL. HOPE TECHNOLOGY ROTAX 503 BRLF BRAKING SYSTEM, NOSEWHEEL SPAT DISC BRAKE SYSTEM WITH ASSOCIATED SPACERS AND FIXINGS INSTALLED. FRONT FORKS ADDED MANUFACTURED IAW P LOVEGROVE DRAWING FOR CRICKET MK IV. OPTIONAL NOSEWHEEL SPAT ADDED OF FIBREGALSS MANUFACTURE REPLICA FOKKER DR1 13380 HERCULES 8355308-S PROPELLER INSTALLATION OF HERCULES 8355308-S 83 INCH DIAMETER X 55 INCH PITCH PROPELLER. LYCOMING AIO-360-A2B BVGZ INSTALLATION REPLICA FOKKER DR1 13821 ENGINE AND PROP CHANGE ENGINE CHANGED TO LYCOMING HIO-360-B1B WITH HERCULES 8449397-S PROPELLER LYCOMING H10-360-BIB FOKK REPLICA HAWKER CYGNET 13087 MODIFICATIONS TO JAP ENGINE AEROVEE CARBURETTOR AND LEBURG IGNITION SUBSTITUTED J.A.P. J.99 EBJI REPLICA JODEL DR1050 12534 FUEL SELECTOR VALVE CHANGE AND INSTALLATION OF ANDAIR FUEL SELECTOR VALVE FS20X3F ONTO PILOT'S SIDE SPAR MOUNTED CONTINENTAL O-200-A CESA RELOCATION BRACKET. REPLICA JODEL DR200 13868 INSTALLATION OF AUTOPILOT b CONTINENTAL O-200-A DANA REPLICA JODEL DR200 13869 INSTALLATION OF A THIRD FUEL TANK n CONTINENTAL O-200-A DANA AND A 3 TANK SELECTION SYSTEM REPLICA JODEL DR200 13870 MODIFYING BRAKES TO HEEL OPERATED b CONTINENTAL O-200-A DANA BRAKES REPLICA JODEL DR200 13871 INSTALLATION OF SERVO POWERED k CONTINENTAL O-200-A DANA TRIM MANAGEMENT SYSTEM REPLICA JODEL DR200 13872 INSTALLATION OF WING FLAPS k CONTINENTAL O-200-A DANA REPLICA SE5A 13514 HERCULES 7244346-C 72" X 43" INSTALLATION OF HERCULES 7244346-C 72 INCH DIAMETER X 43 INCH PITCH PROPELLER. CONTINENTAL C90-14F BUOD INSTALLATION REPLICA SE5A 14737 SMOKE SYSTEM INSTALLATION SMOKE SYSTEM INSTALLED CONSISTING OF A 1.5 LITRE STEEL OIL TANK ATTACHED TO THE CONTINENTAL C90-14F BUOD FORWARD FACE OF THE FIREWALL, A FACET 17PO3 PUMP AND A STAND-ALONE EXIDE ELTZ5S BATTERY. INCLUDES ASSOCIATED OIL PIPES, EXHAUST INJECTORS, ELECTRICAL WIRING, SWITCHES AND CIRCUIT PROTECTION. REPLICA SE5A 13514 HERCULES 7244346-C 72" X 43" INSTALLATION OF HERCULES 7244346-C 72 INCH DIAMETER X 43 INCH PITCH PROPELLER. CONTINENTAL C90-8F BDWJ INSTALLATION REPLICA SE5A 12423 SMOKE SYSTEM INSTALLATION CONVENTIONAL SMOKE SYSTEM FITTED USING ELECTRIC PUMP FEEDING SMOKE OIL FROM CONTINENTAL C90-8F BDWJ DEDICATED TANK INTO EXHAUST SYSTEM VIA ASSOCIATED REINFORCED BRAIDED RUBBER PIPEWORK AND NOZZLE REPLICA SE5A 12423 SMOKE SYSTEM INSTALLATION CONVENTIONAL SMOKE SYSTEM FITTED USING ELECTRIC PUMP FEEDING SMOKE OIL FROM CONTINENTAL O-200-A BMDB DEDICATED TANK INTO EXHAUST SYSTEM VIA ASSOCIATED REINFORCED BRAIDED RUBBER PIPEWORK AND NOZZLE REPLICA SE5A 12567 MACHINE GUN NOISE SIMULATOR PROPANE/OXYGEN SYSTEM INSTALLED BASED ON WELDING TORCH TECHNOLOGY WITH CONTINENTAL O-200-A BMDB ELECTRONIC IGNITION / SPARK PLUG IGNITOR AND SAFETY PRESSURE RELIEF VALVE

Prototype mods that have been approved since 1/1/2008 Page 86 30/11/20 LAA Technical Leaflet TL 3.17 REPLICA SE5A 12565 ENGINE AND PROPELLER CHANGE CONTINENTAL 0-200A ENGINE FITTED IN PLACE OF C90-14F. NO ELECTRIC START OR ALTERNATOR CONTINENTAL O-200-A BMDB FITTED. PROPELLER FITTED IS A LODGE CJL 110A 70" X 48" REPLICA SE5A 12565 ENGINE AND PROPELLER CHANGE CONTINENTAL 0-200A ENGINE FITTED IN PLACE OF C90-14F. NO ELECTRIC START OR ALTERNATOR CONTINENTAL O-200-A SEVA FITTED. PROPELLER FITTED IS A LODGE CJL 110A 70" X 48" REPLICA SE5A 13890 ROMAIN 72" X 45" PROPELLER INSTALLATION OF ROMAIN 72 INCH DIAMETER X 45 INCH PITCH PROPELLER. CONTINENTAL O-200-A SEVA INSTALLATION REPLICA SE5A 13469 PROPELLER CHANGE TO HEGY 78 X 40 HEGY 78" x 40" PROPELLER OF CONVENTIONAL WOODEN DESIGN FITTED, AS PREVIOUSLY USED ON CONTINENTAL O-200-A CCBN THIS AIRCRAFT PRIOR TO IMPORT TO THE UK REPLICA SE5A 12423 SMOKE SYSTEM INSTALLATION CONVENTIONAL SMOKE SYSTEM FITTED USING ELECTRIC PUMP FEEDING SMOKE OIL FROM CONTINENTAL O-200-A CCBN DEDICATED TANK INTO EXHAUST SYSTEM VIA ASSOCIATED REINFORCED BRAIDED RUBBER PIPEWORK AND NOZZLE REPLICA SE5A 14934 HERCULES 7244346-C 72" x 44" HERCULES 7244346-C 72 INCH DIAMETER X 44 INCH PITCH PROPELLER INSTALLATION. CONTINENTAL O-200-A CCBN PROPELLER INSTALLATION REPLICA SE5A 13852 INSTALLATION OF MAGNETO DRIVE MANUFACTURE AND INSTALLATION OF MAGNETO DRIVE ADAPTOR SCREWED INTO REAR END OF HISPANO SUIZA TYPE E 180 BHP ERFC ADAPTOR TO CRANKSHAFT OF HISPANO CRANKSHAFT OF A HISPANO SUIZA ENGINE , SECURED BY TORQUE LOADING TO 60 LB.FT., LOCTITE SUIZA ENGINE 648 ON THE THREAD AND A 6MM GRADE A2 STAINLESS STEEL PIN WITHIN THE CRANKSHAFT WEB THROUGH THE ADAPTOR SHAFT. REPLICA SOPWITH CAMEL F.1 13806 REPLACEMENT CLERGET 130/150HP REPLACEMENT GUDGEON PINS MADE TO PATTERN CLERGET 9BF BZSC ENGINE GUDGEON PINS REPLICA SOPWITH CAMEL F.1 13839 REPLACEMENT CLERGET 130/150HP REPLACEMENT ROCKER ARMS MANUFACTURED TO PATTERN CLERGET 9BF BZSC ENGINE REPLICA SOPWITH TRIPLANE 13619 REPLACEMENT CLERGET ENGINE PISTON REPLACEMENT CLERGET PISTON ASSEMBLIES MADE TO PATTERN USING APPROPRIATE MODERN CLERGET 9B BOCK ASSEMBLIES EQUIVALENT MATERIALS REPLICA SOPWITH TRIPLANE 13839 REPLACEMENT CLERGET 130/150HP REPLACEMENT ROCKER ARMS MANUFACTURED TO PATTERN CLERGET 9B BOCK ENGINE ROCKER ARM REPLICA WAR FW190 13669 PROPELLER CHANGE TO CATTO 3 BLADED PROPELLER CHANGE TO CATTO 3 BLADED 60" x 62". CONTINENTAL O-200-A SYFW 60" X 62" RETROSPECTIVE CHANGE PROPELLER FOUND FITTED AFTER SALE OF AIRCRAFT TO NEW OWNER

RL 5A-XP SHERWOOD RANGER 13591 ADDITION OF AERO CONVERSIONS SMOKIN AIRPLANES SMOKE SYSTEM INSTALLED ON FRONT SEAT JABIRU 2200A SWAB SMOKE SYSTEM RL5A LW SHERWOOD RANGER 12321 PROPELLER CHANGE TO GT-2/157/98 CHANGE OF PROPELLER TO GT-2/157/98 JABIRU 2200A GKFC RUTAN LONG EZ 13424 MAIN WING TRAILING EDGE FENCES TRAILING EDGE FENCES FITTED AS PREVIOUSLY TESTED ON G-WILY CONTINENTAL O-240 ICON RUTAN LONG EZ 12097 PROPELLER CHANGE TO HERTZLER 62 X CHANGE OF PROPELLER TO HERTZLER 62 INCH DIAMETER X 68 INCH PITCH. CONTINENTAL O-240 ICON 68 RUTAN LONG-EZ 14456 HERCULES 6474538-S 64" X 74" HERCULES 6474538-S 64 INCH DIAMETER X 74 INCH PITCH PROPELLER INSTALLATION CONTINENTAL O-240-A RAFT PROPELLER INSTALLATION RUTAN LONG-EZ 13085 ENGINE CHANGE TO LYCOMING IO-320 ENGINE CHANGE TO LYCOMING IO-320 B1A WITH BRUCE TIFT 63" X 75" PROPELLER LYCOMING IO-320-B1A RAEM B1A RUTAN LONG-EZ 13175 WILHELMSON ELECTRIC NOSEGEAR ELECTRIC NOSEGEAR SYSTEM WITH ELECTRICAL EMERGENCY LOWERING PROVISION LYCOMING IO-320-B1A RAEM RETRACTION/EXTENSION SYSTEM RUTAN LONG-EZ 13175 WILHELMSON ELECTRIC NOSEGEAR ELECTRIC NOSEGEAR SYSTEM WITH ELECTRICAL EMERGENCY LOWERING PROVISION LYCOMING IO-320-B1A BZMF RETRACTION/EXTENSION SYSTEM RUTAN LONG-EZ 13316 ROLLOVER BAR ROLL-OVER BAR FITTED AS DEVELOPED BY BILL ALLEN LYCOMING IO-320-B1A BZMF RUTAN LONG-EZ 14766 TRIO EZ3 AUTO-PILOT (PITCH) INSTALLATION OF TRIO EZ3 AUTO-PILOT (PITCH) SYSTEM LYCOMING IO-320-B1A BZMF INSTALLATION RUTAN LONG-EZ 15239 INCREASE of MTWA TO 1600 LBS. INCREASE OF MAXIMUM TOTAL WEIGHT AUTHORISED (MTWA) TO 1600 LBS. LYCOMING IO-320-B1A BZMF RUTAN LONG-EZ 15183 INCREASE MTWA TO 1450 LBS INCREASE TO MAXIMUM TOTAL WEIGHT AUTHORISED FROM 1325 LBS TO 1450 LBS. LYCOMING O-235-C1 BLMN RUTAN LONG-EZ 14899 MGL AUTO-PILOT (ROLL) INSTALLATION REPLACEMENT OF NAVAID-1 AUTO-PILOT (ROLL) SERVO WITH MGL SERVO CONTROLLED BY MGL LYCOMING O-235-C2A MUSO EFIS.

Prototype mods that have been approved since 1/1/2008 Page 87 30/11/20 LAA Technical Leaflet TL 3.17 RUTAN LONG-EZ 13533 GO PRO HERO HD CAMERA MOUNTS PROVISION FOR MOUNTING UP TO FOUR GO-PRO CAMERAS, LYCOMING O-235-L2A BOOX ABOVE AND BELOW WING MUST BE OPERATED PER 'PILOT'S NOTES ASSOCIATED WITH LAA MOD 13533 GO PRO CAMERA FIT'

RUTAN LONG-EZ 14987 HERTZLER 62" X 68" PROPELLER INSTALLATION OF HERTZLER 62" X 68" 'SILVER BULLET' PROPELLER LYCOMING O-235-L2C HAIG INSTALLATION RUTAN LONG-EZ 13412 OIL SYSTEM MODIFICATIONS INSTALLATION ON UPPER FIREWALL OF MOCAL RFH3 REMOTELY MOUNTED SPIN-ON OIL FILTER LYCOMING O-235-L2C LUKE ADAPTOR WITH K&N HP-3001 FILTER, MOCAL TYPE A THERMOSTATICALLY CONTROLLED OIL COOLER BYPASS VALVE AND MOCAL 10 ROW OIL COOLER MOUNTED TO PORT SIDE LOWER COWLING. THE K&N HP-3001 IS EQUIPPED WITH A BYPASS VALVE AND AN ANTI DRAIN-BACK VALVE. RUTAN LONG-EZ 12397 ELECTRIC NOSE LIFT AND UPPER FITTING INSTALLATION OF AN ELECTRICALLY POWERED SCREW-JACK ACTUATOR TO EXTEND AND RETRACT LYCOMING O-235-L2C OMJT WITH TAPERED ROLLER BEARINGS THE NOSE LEG WITH OCCUPANTS ON BOARD AND A NOSE LEG UPPER FITTING WITH TAPERED ROLLER BEARINGS INSTALLED. RUTAN LONG-EZ 12882 NAVAID DEVICES AP-1 WING LEVELLING NAVAID DEVICES WING LEVELLING AUTO-PILOT WITH SERVO MOUTED TO REAR FACE OF LYCOMING O-235-L2C OMJT AUTO-PILOT STARBOARD SIDE WING SPAR. RUTAN LONG-EZ 11257 INSTALLATION OF ROLL BAR ROLL BAR OF APPLICANT'S OWN DESIGN INCORPORATED. LYCOMING O-235-L2C OMJT RUTAN LONG-EZ 12723 TRIO EZ PILOT WING LEVELLING AUTO- INSTALLATION OF TRIO EZ PILOT WING LEVELLING AUTO-PILOT WITH SERVO MOUNTED ON LYCOMING O-235-L2C CBLZ PILOT STARBOARD AFT FACE OF CENTRE SECTION SPAR DRIVING AILERON PUSH ROD ADJACENT TO AILERON TORQUE TUBE BELLCRANK VIA CLAMP ATTACHMENT. RUTAN LONG-EZ 14230 HERTZLER 63" X 69" PROPELLER INSTALLATION OF HERTZLER 'SILVER BULLET' 63 INCH DIAMETER X 69 INCH PITCH PROPELLER. LYCOMING O-290-G BRFB INSTALLATION RUTAN LONG-EZ 12457 PROPELLER CHANGE TO CATTO 3 BLADED CATTO 3 BLADED 60" X 80" PROPELLER FITTED AS ALTERNATIVE TO HERTZLER 66" X 75" PITCH LYCOMING O-320-D3G LGEZ 60" X 80" USED PREVIOUSLY. (MODIFIED) RUTAN LONG-EZ 12484 PROPELLER CHANGE TO HERTZLER 65" X PROPELLER CHANGE TO HERTZLER 65 INCH DIAMETER X 80 INCH PITCH. LYCOMING O-320-D3G LGEZ 80" (MODIFIED) RUTAN LONG-EZ 12602 WING MOUNTED BAGGAGE PODS INSTALLATION OF WING MOUNTED BAGGAGE PODS MANUFACTURED BY FEATHER LITE INC. OF LYCOMING O-320-D3G LGEZ CALIFORNIA. (MODIFIED) EACH BAGGAGE POD TO BE PLACARDED 'MAX LOAD 30LB'. COCKPIT PLACARD TO BE INSTALLED WHEN BAGGAGE PODS ARE FITTED STATING 'WITH BAGGAGE PODS FITTED CHECK WEIGHT & CG BEFORE FLIGHT'. RUTAN LONG-EZ 12713 CONVERT ENGINE FROM CONVERSION TO FUEL INJECTION USING PRECISION AIRMOTIVE RSA-5AD1 FUEL SERVO WITH LW- LYCOMING O-320-D3G LGEZ CARBURETTORED TO INJECTED 15473 ENGINE DRIVEN HP PUMP AND ANDAIR PX375-TC ELECTRIC BACK-UP PUMP. (MODIFIED) RUTAN LONG-EZ 12714 MAXIMUM GROSS WEIGHT INCREASE TO INCREASE OF MAXIMUM GROSS WEIGHT TO 1650 LBS WITH A MAXIMUM LANDING WEIGHT OF LYCOMING O-320-D3G LGEZ 1650 LBS (748 KG). 1600 LBS. AIRCRAFT PERFORMANCE AT 1650 LBS SATISFACTORY WITH HERZLER 65" X 80" (MODIFIED) PROPELLER. RUTAN LONG-EZ 12715 TRIO AVIONICS 'PRO PILOT' DUAL AXIS INSTALLATION OF TRIO AVIONICS 'PRO PILOT' DUAL AXIS AUTO-PILOT WITH ROLL SERVO BOLTED LYCOMING O-320-D3G LGEZ AUTOPILOT TO FIREWALL BELOW WING SPAR LEVEL AND PUSH-ROD DRIVING CS124 AILERON BELLCRANK AND (MODIFIED) PITCH SERVO MOUNTED TO A BASE PLATE THAT IS SECURED TO FUSELAGE STARBOARD INSIDE WALL USING 'CLICK BOND' STUDS AND PUSH-ROD DRIVING NC-12A ELEVATOR BELLCRANK.

RUTAN LONG-EZ 14690 CATTO CPX 2 BLADED 66" X 76" INSTALLATION OF CATTO CPX 2 BLADED 66 INCH DIAMETER X 76 INCH PITCH PROPELLER. LYCOMING O-320-D3G LGEZ PROPELLER INSTALLATION DESIGNATION CPX MEANS 'CATTO PROPELLERS EXPERIMENTAL' TO DIFFERENTIATE IT FROM THE (MODIFIED) CATTO ASTM CERTIFIED PROPELLERS. RUTAN LONG-EZ 14164 NOSE EXTENSION NEW 15 INCH LONGER NOSE FITTED IN ACCORDANCE WITH RUTAN INSTRUCTIONS. WILKSCH WAM-120 LEZE RUTAN LONG-EZ 14165 HEATED PITOT HEAD INSTALLED IN NOSE INSTALLATION OF A FALCON AN5812 HEATED PITOT HEAD IN NOSE SECTION. WILKSCH WAM-120 LEZE

RUTAN LONG-EZ 13175 WILHELMSON ELECTRIC NOSEGEAR ELECTRIC NOSEGEAR SYSTEM WITH ELECTRICAL EMERGENCY LOWERING PROVISION WILKSCH WAM-120 LEZE RETRACTION/EXTENSION SYSTEM RUTAN LONG-EZ 14166 CABIN HEAT INSTALLATION IN NOSE SECTION OF TWO EVANS COOLANT FILLED AND BUNDED WITH DRAINS T7 WILKSCH WAM-120 LEZE DESIGN MICRO HEATER/BLOWERS HEATED BY ENGINE OIL CIRCULATED BY ELECTRIC PUMP VIA A CALORIFIER INSTALLED IN ENGINE SUMP. Prototype mods that have been approved since 1/1/2008 Page 88 30/11/20 LAA Technical Leaflet TL 3.17 RUTAN LONG-EZ 14167 ELECTRIC PITCH TRIM REPLACEMENT OF STANDARD SPRING AND CABLE PITCH TRIM SYSTEM WITH ELECTRIC PITCH TRIM WILKSCH WAM-120 LEZE INCORPORATING A FIRGELLI L16-100-12 ELECTRIC LINEAR ACTUATOR ANCHORED TO NOSE WHEEL COVER AND CONNECTED TO A GLASS FIBRE LEAF SPRING BONDED AND RIVETTED TO THE ELEVATOR TORQUE TUBE RUTAN LONG-EZ 14168 HEATED SEAT INSTALLATION OF ROSTRA ELECTRIC HEATING ELEMENTS INSERTED UNDER SEAT COVERS OF P1 WILKSCH WAM-120 LEZE SEAT WITH TWO HEAT SETTINGS VIA A TWO POSITION SWITCH RUTAN LONG-EZ 14169 FUEL SENDERS INSTALLATION IN BOTH FUEL TANKS OF A CAPACITANCE PROBE TO PROVIDE FUEL QUANTITY WILKSCH WAM-120 LEZE INFORMATION TO A DYNON EFIS VIA PRINCETON TECHNOLOGY INC. DATA CONVERTER UNITS MOUNTED ON FRONT OF FIREWALL BEHIND PASSENGER HEADREST. RUTAN LONG-EZ 14187 DYNON SKYVIEW DUAL AXIS AUTO-PILOT INSTALLATION OF DYNON SKYVIEW DUAL AXIS AUTO-PILOT. WILKSCH WAM-120 LEZE

ROLL SERVO INSTALLED ON THE STARBOARD REAR OF THE SPAR INBOARD OF THE WING ROOT VIA WELDED STAINLESS STEEL BRACKET ATTACHED TO BONDED ON STUDS AND CONNECTED VIA PUSH- ROD WITH ROD-ENDS DIRECTLY TO THE ROLL BELLCRANK CS24.

PITCH SERVO MOUNTED TO ALUMINIUM BRACKET BONDED AND RIVETED TO PLATE BONDED TO UNDERSIDE AND CONNECTED TO THE FORMER ELEVATOR PITCH TRIM BRACKET CS2 VIA RIVETED AND BOLTED ON ALUMINIUM BELLCRANK. RUTAN LONG-EZ (MODIFIED) 12394 WING LEVELLER INSTALLATION INSTALLATION OF NAVAID DEVICES WING LEVELLER WITH SERVO MOUNTED TO REAR OF CONTINENTAL O-240-E BPWP FIREWALL RUTAN VARIEZE 12916 B & T 56" X 69" PROPELLER B & T 56 INCH DIAMETER X 69 INCH PITCH PROPELLER INSTALLED. CONTINENTAL O-200-A LASS RUTAN VARIEZE 12949 PROPELLER CHANGE TO HERCULES 59" X INSTALLATION OF HERCULES 5971250 59 INCH DIAMETER X 71 INCH PITCH PROPELLER CONTINENTAL O-200-A LASS 71" RUTAN VARIEZE 11780 COMPRESSION RATIO OF ENGINE COMPRESSION RATIO OF ENGINE INCREASED TO 8:1. CONTINENTAL O-200-A LASS INCREASED ENGINE MAY CONTINUE TO BE OPERATED TO NORMAL TBO OR IAW AIRWORTHINESS NOTICE 35 SUBJECT TO RESULTS OF REGULAR AN 35 CONDITION CHECKS REMAINING SATISFACTORY.

RUTAN VARIEZE 12363 INSTALLATION OF WING LEVELLING TRIO EZ-PILOT WING LEVELLER INSTALLED WITH SERVO ON FIREWALL AND PUSH-ROD CONNECTED CONTINENTAL O-200-A VEZE AUTO-PILOT TO AILERON BELLCRANK CS124. RUTAN VARIEZE 12479 COMPOSITE LEAF SPRING PITCH TRIM ALTERNATIVE DESIGN OF PITCH TRIM BIAS SPRING OF COMPOSITE CONSTRUCTION, PER CONTINENTAL O-200-A VEZE APPLICANT'S DRAWING M12479-1 and -2 RYAN ST3KR 12726 PROPELLER CHANGE TO SENSENICH W90 CHANGE TO SENSENICH W90 HASP-86 90 INCH DIAMETER X 86 INCH PITCH PROPELLER. KINNER R56 BTBH HASP-86 SCINTEX CP1310-C3 12300 STROBE AND VENTRAL PANEL MOD INSTALLATION OF AIRWORLD STROBE SYSTEM, WITH ONE STROBE HEAD ON THE FIN TIP, THE CONTINENTAL O-200-A BGVE OTHER UNDERNEATH THE FUSELAGE WITH THE AMPLIFIER UNIT IN THE REAR FUSELAGE. IN ADDITION, REMOVABLE PANEL FITTED IN LOWER FUSELAGE FOR ACCESS TO LOWER STROBE ATTACHMENTS AND AMPLIFIER UNIT. SCINTEX CP1310-C3 14052 HERCULES 6850247-S INSTALLATION INSTALLATION OF HERCULES 6850247 68 INCH DIAMETER X 50 INCH PITCH PROPELLER. CONTINENTAL O-200-A BJVS SCINTEX CP301-C3 12521 PROPELLER CHANGE TO RWG 107 70 PROPELLER CHANGE TO RWG 107 70 INCH DIA X 47 INCH PITCH CONTINENTAL C90-14F BIVF INCH DIA X 47 INCH PITCH SCINTEX CP301-C3 14721 HERCULES 6950288-S 69" x 50" INSTALLATION OF HERCULES 6950288-S 69 INCH DIAMETER X 50 INCH PITCH PROPELLER. CONTINENTAL C90-14F BIVF PROPELLER INSTALLATION SHADOW SERIES DD 13504 NOSE WHEEL INSPECTION HATCH STANDARD CROSBIE OPTION INSPECTION PANEL TO FACILITATE INSECTION OF NOSEWHEEL LEG ROTAX 582/47 MYZP MOUNTINGS SHADOW SERIES DD 12282 RETROSPECTIVE MODIFICATION/REPAIR REPAIR BOOM TUBE AT TAILPLANE ATTACHMENTS TO SUIT HOLE LOCATIONS ON REPLACEMENT ROTAX 582/47 CCMW SCHEME TAILPLANE, PER APPLICANT'S SUBMISSION SHERWOOD RANGER ST 14280 DMOTOR INSTALLATION DMOTOR LF26 ENGINE INSTALLED ON JABIRU ENGINE MOUNT WITH ASSOCIATED ANCILLARIES. D-MOTOR LF26 CIWD FITTED WITH A HERCULES 6332515-S PROPELLER. INSTALLED IN ACCORDANCE WITH TLAC INSTRUCTIONS. SHERWOOD RANGER ST 12698 PROPELLER CHANGE TO GT-2/157/98 GT-2/157/98 PROPELLER FITTED AS REPLACEMENT JABIRU 2200 CDPH Prototype mods that have been approved since 1/1/2008 Page 89 30/11/20 LAA Technical Leaflet TL 3.17 SHERWOOD RANGER ST 14100 HERCULES 6234441-S, 62" X 34" INSTALLATION OF HERCULES 6234441-S, 62 INCH DIAMETER X 34 INCH PITCH PROPELLER. JABIRU 2200 CDPH PROPELLER INSTALLATION SHERWOOD RANGER ST 14932 CAMIT FLYWHEEL CLAMP REVISED CLAMP ARRANGEMENT TO BETTER RETAIN FLYWHEEL JABIRU 2200 CDPH

NOTE: APPLICABLE TO 1/4" AND 5/16", BUT NOT 3/8", BOLT CRANKSHAFTS SHERWOOD RANGER XP 14426 WING LIGHTS AND TAIL STROBE WHELEN MICROBURST NAVIGATION AND STROBE LIGHTS INSTALLED ON WING TIPS AND RUDDER, D-MOTOR LF26 TSOG IN ACCORDANCE WITH AIRCRAFT MANUFACTURER'S RECOMMENDATIONS. INCLUDES ASSOCIATED WIRING, SWITCH AN 10A CIRCUIT BREAKER. SHERWOOD RANGER XP 14419 LOCKER AND ACCESS PANEL BAGGAGE LOCKER PROVIDED BY ADDITION OF HINGED PANEL TO LOWER CENTRAL WING SURFACE JABIRU 2200A CIYY ON UPPER WING. PANEL IS HINGED ABOUT FORWARD EDGE AND CLOSED BY 2 OFF CAMLOC FASTENERS ON AFT EDGE.

ACCESS TO REAR COCKPIT FACILITATED BY INCLUSION OF DROP-DOWN PANEL ON PORT SIDE. PANEL IS CUT FROM THE GLASS FIBRE FUSELAGE COMBING AND HINGED ON LOWER EDGE. 2 OFF CAMLOC FASTENERS SECURE THE PANEL IN THE CLOSED POSITION. SHERWOOD SCOUT 14948 ENHANCED GROUND PLANE GROUND PLANE CONSISTING OF 1MM THICK 6082T6 ALUMINIUM ALLOY SHEET APPROX 1500MM ROTAX 912-ULS OUAV LONG INSTALLED ABOVE FABRIC COVERING IN BASE OF REAR FUSELAGE. SHERWOOD SCOUT 14927 CABIN HEATER CABIN HEAT SYSTEM INSTALLED CONSISTING OF ALLOY MUFF AROUND EXHAUST SILENCER ROTAX 912-ULS INYS CONNECTED TO A DIVERTER VALVE CONTROLLED BY A BOWDEN CABLE/COCKPIT PUSH-PULL CONTROL. CARBON MONOXIDE MONITOR MOUNTED IN COCKPIT. SHERWOOD SCOUT 14928 FUEL TAPS AUXILIARY FUEL TAPS FITTED BETWEEN EACH WING TANK AND THE MAIN FUEL VALVE TO ENABLE ROTAX 912-ULS INYS INDIVIDUAL FUEL TANKS TO BE ISOLATED FOR MAINTENANCE, PARKING ON UNEVEN GROUND OR IN THE EVENT OF A LINE LEAK. VALVES LOCATED ON TOP FUSELAGE LONGERONS ABOVE AND BEHIND THE SEATING POSITIONS. SHERWOOD SCOUT 14929 BUNGEE COVERS BUNGEE COVERS (2 OFF) ARE FITTED TO THE LANDING GEAR, CONSISTING OF SHAPED BALSA END- ROTAX 912-ULS INYS CAPS AND AN ALLOY WRAP. TOP ENDS ARE CLAMPED TO TOP STRUT, LOWER ENDS ARE FREE TO SLIDE OVER LOWER STRUT. SHERWOOD SCOUT 15153 FUEL SYSTEM CHANGES INSTALLATION OF FT60 RED CUBE FUEL FLOW TRANSDUCER AND FUEL PRESSURE TRANSDUCER TO ROTAX 912-ULS INYS FORWARD FACE OF FIREWALL. INSTALLATION OF MGL FF4 FUEL COMPUTER TO INSTRUMENT PANEL. INCLUDES ASSOCIATED FUEL SYSTEM FITTINGS, ATTACHMENT BRACKETS AND ELECTRICAL WIRING, INCLUDING APPROPRIATE CIRCUIT PROTECTION. SILENCE TWISTER 13068 HERCULES 56" X 53" PROPELLER INSTALLATION OF HERCULES 56 INCH DIAMETER X 53 INCH PITCH PROPELLER, S/N 5653260. JABIRU 2200A TWSS SILENCE TWISTER 12054 SMOKE SYSTEM INSTALLED SMOKE SYSTEM INSTALLED IN ACORDANCE WITH APPLICANT'S SUBMISSION, CONSISTING OF JABIRU 2200A TWSS MOULDED COMPOSITE REAR FUSELAGE SMOKE OIL TANK, ELECTRIC PUMP, VALVE AND ASSOCIATED PIPEWORK AND SWITCH. OIL FED TO NOZZLE IN EXHAUST PIPE. SILENCE TWISTER 14064 REPLACE JABIRU 2200A WITH CAMIT CAMIT CAE 2200 ENGINE FITTED AS A SUBSTITUTE FOR JABIRU 2200A JABIRU 2200A TWSS 2200 ENGINE SILENCE TWISTER 14333 FIT WING TIE-DOWN & ACCESS PANEL REINFORCED CIRCULAR HOLE AND ASSOCIATED ACCESS PANELS INTRODUCED IN WING SKIN JABIRU 2200A TWSS UNDERSURFACE, WITH ASSOCIATED TE-DOWN FITTINGS SILENCE TWISTER 12910 WINGTIP PYROTECHNICS - SPARKLER TWIN WATERFALL SPARKLERS FITTED TO WELDED STEEL TUBE WINGTIP MOUNTINGS, ADDITIONAL JABIRU 2200A TWSS EFFECT COCKPIT PLACARD TO BE FITTED AS SPECIFIED IN LAA LETTER DATED 16.8.10 SILENCE TWISTER 14776 FUSELAGE MOUNTED 'LED' LIGHTING LED LIGHTING STRIPS BONDED TO FUSELAGE, 4 STRIPS EACH SIDE. CONTROL ELECTRONICS JABIRU 2200A TWSS STRIPS MOUNTED IN FUSELAGE WITH ASSOCIATED SWITCHING AND CIRCUIT PROTECTION. SILENCE TWISTER 13014 HERCULES 5853241 58" X 53" PROPELLER INSTALLATION OF HERCULES 5853241 58 INCH DIAMETER X 53 INCH PITCH PROPELLER. UL POWER 260iSA TWST

SILENCE TWISTER 12910 WINGTIP PYROTECHNICS - SPARKLER TWIN WATERFALL SPARKLERS FITTED TO WELDED STEEL TUBE WINGTIP MOUNTINGS, ADDITIONAL UL POWER 260iSA TWST EFFECT COCKPIT PLACARD TO BE FITTED AS SPECIFIED IN LAA LETTER DATED 16.8.10 SILENCE TWISTER 13613 ENGINE & PROPELLER CHANGE ENGINE CHANGED TO UL260iSA AS PREVIOUSLY APPROVED FOR G-SWIP, WITH HERCULES WOOD UL POWER 260iSA TWSR PROPELLER 58" x 33" SILENCE TWISTER 12519 CHANGE OF POWER PLANT UL POWER 260i ENGINE INSTALLED, INCLUDING MODIFIED ENGINE MOUNT, NEW COWLINGS, UL POWER 260iSA RIOT MODIFIED FUEL AND ELECTRICAL SYSTEMS AND RE-POSITIONED BATTERY. Prototype mods that have been approved since 1/1/2008 Page 90 30/11/20 LAA Technical Leaflet TL 3.17 SILENCE TWISTER 12910 WINGTIP PYROTECHNICS - SPARKLER TWIN WATERFALL SPARKLERS FITTED TO WELDED STEEL TUBE WINGTIP MOUNTINGS, ADDITIONAL UL POWER 260iSA RIOT EFFECT COCKPIT PLACARD TO BE FITTED AS SPECIFIED IN LAA LETTER DATED 16.8.10 SILENCE TWISTER 13014 HERCULES 5853241 58" X 53" PROPELLER INSTALLATION OF HERCULES 5853241 58 INCH DIAMETER X 53 INCH PITCH PROPELLER. UL POWER 260iSA RIOT

SILENCE TWISTER 14379 NEW COWLING AND OIL COOLER SCOOP CUSTOM MADE COWLINGS WITH LO-PRESTI STYLE INTAKES AND BELLY MOUNTED OIL COOLER UL POWER 260iSA FUUN WITH RAM INTAKE AND FLUSH OUTLET WITH COCKPIT CONTROLLED COWL FLAP. SILENCE TWISTER 14380 TAILPLANE SECURING FAIL SAFE ADDITION OF CFRP TAB TO TAILPLANE ROOT THAT ENTERS SLOT IN FUSELAGE FAIRING ALLOWING UL POWER 260iSA FUUN BOLT AND STIFF NUT TO SECURE THE TWO PARTS TOGETHER TO PROVIDE A SECONDARY FORM OF TAILPLANE RETENTION. SILENCE TWISTER 13633 FITTING OF MOUNTING FOR EXTERNAL UNDER BELLY MOUNTING PROVIDED FOR EXTERNAL STREAMLINED FUEL TANK AND PYRO RACK, UL POWER 260iSA JINX FUEL TANK AND UNDERBELLY PYRO RACK WITH QUICK RELEASE ATTACHMENT, QUICK DISCONNECT FUEL FITTINGS AND ASSOCIATED ELECTRICAL SWITCHES AND WIRING. USE OF PYRO RACK APPROVED ONLY. USE OF EXTERNAL FUEL TANK NOT APPROVED AT THIS STAGE. SIPA 903 12582 PROPELLER CHANGE TO EVRA PROPELLER CHANGE TO EVRA D.11.28.7.C, 70 INCH DIAMETER X 47 INCH PITCH. CONTINENTAL C90-12F BBDV D.11.28.7.C SKY ARROW 650 T 14692 PROPELLER CHANGE TO HOFFMAN PROPELLER CHANGE TO HOFFMAN HO17F HM-167 148 LD ON ROTAX 912-UL ENGINE. ROTAX 912-UL BXGT HO17F HM-167 148 LD SKY ARROW 650 T 14999 HELICES E-PROPS EXCALIBUR 3-130-L INSTALLATION OF HELICES E-PROPS EXCALIBUR 3-130-L 168CM DIAMETER PROPELLER ROTAX 912-UL CIAO PROPELLER INSTALLATION SKY ARROW 650 T 12305 SOFT START MODULE INSTALLATION OF CON-AIR SPORTS SOFT START MODULE TO ROTAX 912-ULS ENGINE IN ROTAX 912-ULS BZVT ACCORDANCE WITH CON-AIR SPORTS INSTRUCTIONS AND SM12305 LEAFLET. SKY ARROW 650 T 13425 ROTAX 912 ULS ENGINE INSTALL INSTALLATION OF ROTAX 912-ULS ENGINE WITH AIRMASTER AP332 68 INCH DIAMETER ROTAX 912-ULS IOIA AIRMASTER AP332 68" DIA PROPELLER PROPELLER. SKY ARROW 650 T 12270 PROPELLER CHANGE TO NSI CAP 140 PROPELLER CHANGE TO NSI CAP 140 3 BLADED 68 INCH DIAMETER. ROTAX 914-UL BYCY SKY ARROW 650 T 12271 ENGINE CHANGE TO ROTAX 914 UL. ENGINE CHANGE TO ROTAX 914 UL. ROTAX 914-UL BYCY SKY ARROW 650 T 13527 ULPOWER UL260IS ENGINE & HERCULES UL POWER 260I ENGINE INSTALLATION UL POWER 260iS DGMT PROP SKYSTAR KITFOX MK5 12859 ROTAX 912-ULS ENGINE RETROFITTED STANDARD FACTORY OPTIONAL ROTAX 912-ULS ENGINE FITTED, WITH GSC TECH III 68" DIAMETER ROTAX 912-ULS LESZ PROPELLER. SKYSTAR KITFOX MK5 12956 PROPELLER CHANGE TO KIEV 263/1700 - PROPELLER CHANGE TO KIEV 263/1700 - 1710MM DIA ROTAX 912-ULS LESZ 1710MM DIA SLEPCEV STORCH 12382 PROPELLER CHANGE TO WARP DRIVE 3 CHANGE OF PROPELLER TO WARP DRIVE 3 BLADED 72" DIAMETER GROUND ADJUSTABLE. ROTAX 912-ULS BZOB BLADED 72" DIA SMITH DSA-1 MINIPLANE 14869 EVRA D.11.28.4.C PROPELLER INSTALLATION OF EVRA D.11.28.4.C PROPELLER. CONTINENTAL C90-9-8 BTGJ INSTALLATION SNS-7 HIPERBIPE 13054 INSTALLATION OF DIGITAL SYSTEMS ON PROVISIONS ADDED FOR FLIGHT TESTING ADDITIONAL RADIO EQUIPMENT. THIS MODIFICATIN LYCOMING IO-360-B1E HIPE PASSENGERS STATION COVERS MECHANICAL INSTALALTION OF EQUIPMENT AND DOES NOT CONFER APPROVAL TO OPERATE THE EQUIPMENT IN FLIGHT. SNS-7 HIPERBIPE 13377 INSTALLATION OF ON-BOARD DATA DATA PROCESSING EQUIPMENT INSTALLED IN ACCORDANCE WITH APPLICATION DETAILS, LYCOMING IO-360-B1E HIPE PROCESSING INCLUDING EXTERNAL FIN SNS-7 HIPERBIPE 14209 AIRCRAFT DATA PROCESSING AND WIFI AIRCRAFT DATA PROCESSING UNIT MOUNTED ON CENTRAL COAMING LYCOMING IO-360-B1E HIPE INSTALLATION EXTERNAL ANTENNA HOUSING ADDED CONTAINING WI FI DATA MODEM CONNECTION TO AIRCRAFT DATA SOURCES SONEX 12632 ELECTRONIC PITCH TRIM INDICATOR PITCH TRIM POSITION IS INDICATED ON THE STRATOMASTER ENIGMA EFIS UNIT. THE POSITION AEROVEE 2180 ZONX INFORMATION IS PROVIDED BY A LINEAR POTENTIOMETER ATTACHED TO THE TRIM MECHANISM.

SONEX 14951 SPLIT P1 & P2 SEATING - LOWER SEAT SINGLE 0.025" ALUMINIUM 'SLING' SEAT DIVIDED INTO SEPARATE SEATS AND STARBOARD SEAT AEROVEE 2180 CIDP OPTION P2 ONLY INSTALLED PER FACTORY LOWER SEAT OPTION. SONEX 14738 TRIM POSITION INDICATOR PITCH TRIM POSITION INDICATOR CONSISTING OF A LINEAR POTENTIOMETER ATTACHED TO THE AEROVEE 2180 YCMI PITCH TRIM CONTROL DRIVING A DIAL INDICATOR ADJACENT TO THE THIS CONTROL.

Prototype mods that have been approved since 1/1/2008 Page 91 30/11/20 LAA Technical Leaflet TL 3.17 SONEX 13995 CONVERT JABIRU 3300 NO 1817 TO CAMIT SOLID LIFTER CONVERSION KIT USING HONDA LIFTERS AND FLOOD FEED, SIMILAR TO JABIRU 3300A CEFJ SOLID LIFTER CONFIGURATION PREVIOUSLY ACCEPTED MOD ON G-PHCJ. THROUGH BOLTS UPRATED TO 7/16" DIA USING CAMIT CONVERSION KIT. SONEX 12632 ELECTRONIC PITCH TRIM INDICATOR PITCH TRIM POSITION IS INDICATED ON THE STRATOMASTER ENIGMA EFIS UNIT. THE POSITION JABIRU 3300A SONX INFORMATION IS PROVIDED BY A LINEAR POTENTIOMETER ATTACHED TO THE TRIM MECHANISM.

SONEX 15357 FUEL TANK OUTLET FITTING ORIGINAL FUEL TANK OUTLET FITTING REPLACED WITH BRASS FITTING BONDED IN TAPPED HOLE JABIRU 3300A EEHA WITH 3M DP 8005 ADHESIVE. FINGER STRAINER SOLDERED TO REDUCER. FUEL VALVE SCREWED TO EXTERNAL END OF FITTING. SONEX 12848 VW 2180 ENGINE VW 2180 ENGINE INSTALLED INCORPORATING DIEHL ACCESSORY CASE PACKAGE, GREAT PLAINS VW 2180 CGPL ELECTRONIC IGNITION AND MODIFIED ENGINE MOUNTING ARRANGEMENT. SONEX 12909 PITCH TRIM INDICATION PITCH TRIM INDICATION SYSTEM ADDED TO PITCH TRIM CONTROL UNIT, CONSISTING OF A SERIES VW 2180 CGPL OF MICROSWITCHES CORRESPONDING WITH A SERIES OF LEDS ON THE INSTRUMENT PANEL REPRESENTING TRIM POSITION. SOPWITH PUP 14742 REPLACEMENT LE RHONE 80HP PISTON REPLACEMENT PISTON ASSEMBLIES MANUFACTURED IN ALUMINIUM ALLOY REPLACING ORIGINAL LE RHONE 80 HP EBKY ASSEMBLIES CAST IRON PISTONS (SOME LATER LE RHONE 80 BHP ENGINES WERE ORIGINALLY FITTED WITH ALUMINIUM ALLOY PISTONS. USED IN CONJUNCTION WITH REPLACEMENT CYLINDER LINERS MOD 15063 SOPWITH PUP 14833 REPLACEMENT LE RHONE 80HP INLET & REPLACEMENT INLET AND EXHAUST VALVES MANUFACTURED BY G+S VALVES LTD LE RHONE 80 HP EBKY EXHAUST VALVES SOPWITH PUP 15063 LE RHONE 80HP REPLACEMENT REPLACEMENT CYLINDER LINERS MANUFACTURED AND FITTED LE RHONE 80 HP EBKY CYLINDER LINERS SPARTAN ARROW 13427 REPLACEMENT OF VALVE GUIDE REPLACEMENT OF VALVE GUIDES OVERHAUL AND RE-FACING OF CYLINDER HEADS CIRRUS HERMES II ABWP MATERIAL WITH COLISBRO ALLOY SPARTAN ARROW 14439 PROPELLER CHANGE TO HERCULES PROPELLER IS A REPLICA OF THE ORIGINAL Z630/1 MADE FROM THE SAME MATERIALS AND THE CIRRUS HERMES II ABWP Z630/1 SAME DESIGN AS THE ORIGINAL. SPITFIRE MK 26 14469 RUDDER PEDAL BELL CRANKS AND RUDDER PEDALS LINKED BY SYSTEM CONSISTING OF TWO BELLCRANKS AND THREE PUSHRODS, IN JABIRU 5100A CENI PUSHROD SYSTEM ADDITION TO THE EXISTING CABLE AND TWO PULLEYS, TO PREVENT SPRING IN RUDDER CIRCUIT AND BRAKES, AND AVOID OVERLOADING RUDDER, RUDDER HINGES AND RUDDER HORN UNDER BRAKING ACTION. SPITFIRE MK 26 14469 RUDDER PEDAL BELL CRANKS AND RUDDER PEDALS LINKED BY SYSTEM CONSISTING OF TWO BELLCRANKS AND THREE PUSHRODS, IN JABIRU 5100A CEPL PUSHROD SYSTEM ADDITION TO THE EXISTING CABLE AND TWO PULLEYS, TO PREVENT SPRING IN RUDDER CIRCUIT AND BRAKES, AND AVOID OVERLOADING RUDDER, RUDDER HINGES AND RUDDER HORN UNDER BRAKING ACTION. SPITFIRE MK 26 13407 HERCULES 6862294-S 68" X 61.98" INSTALLATION OF HERCULES 6862294-S PROPELLER JABIRU 5100A RORB PROPELLER SPITFIRE MK26 13105 PROPELLER CHANGE TO SENSENICH SENSENICH W68SJ6-70G FIXED PITCH TWO BLADE WOOD PROPELLER FITTED JABIRU 5100A HABT SPRINT 160 12650 REVISION OF C OF G RANGE NON-AEROBATIC CG AFT LIMIT INTRODUCED OF 78.1 " AOD. AEROBATIC AFT CG LIMIT 77.4 " AOD. LYCOMING AEIO-320-D1B OAGI BAGGAGE WEIGHT LIMIT REDUCED TO 50 LBS AND CARRRIAGE OF BAGGAGE DURING AEROBATICS PROHIBITED. STAAKEN Z-21 FLITZER 12745 PROPELLER CHANGE TO NEWTON 11L 60 PROPELLER CHANGE FOLLOWING MINOR ACCIDENT VW 1834 FLIZ x 31 STAAKEN Z-21 FLITZER 12908 HERCULES 5932236 58.5" x 32" HERCULES 593236 58.5 INCH DIAMETER X 32 INCH PITCH PROPELLER. VW 1834 FLIZ PROPELLER STAAKEN Z-21 FLITZER 13624 PROPELLER CHANGE TO HERCULES INSTALLATION OF HERCULES 6534377-S 65 INCH DIAMETER X 34 INCH PITCH PROPELLER. VW (AEROVEE) 2180 ERIW 6534377-S MAXIMUM ENGINE RPM REDUCED TO 3050 WITH THIS PROPELLER DUE TO PROPELLER TIP SPEED CONSIDERATIONS STAMPE SV4C 13715 REPLACEMENT OF FUEL SELECTOR FUEL SELECTOR VALVES AND FILTER REPLACED WITH ANDAIR VALVES, MODERN AN FITTINGS AND RENAULT 4P-03 AXNW VALVES AND FILTER ASSOCIATED PIPEWORK USING CUSTOM MADE ADAPTORS STAMPE SV4C 13716 REPLACEMENT OF ORIGINAL WESTACH TACHO, OIL PRESSURE AND FUEL PRESSURE GAUGES SUBSTITUTED RENAULT 4P-03 AXNW INSTRUMENTS Prototype mods that have been approved since 1/1/2008 Page 92 30/11/20 LAA Technical Leaflet TL 3.17 STAMPE SV4C 14128 INTRODUCTION OF CHT MONITORING WESTACH CHT GAUGE INTRODUCED SELECTABLE BETWEEN ALL FOUR CYLINDER HEADS. RENAULT 4P-05 AMPI IN THE ABSENCE OF ANY ENGINE MANUFACTURER'S RECOMMENDATION, RED LINE SET AT 550 DEGREES F WHICH IS CONSISTENT WITH RESULTS OBTAINED ON TEST STAMPE SV4C (MODIFIED) 15405 HERCULES HL2011/HP LEGERE SERIE HERCULES HL2011/HP LEGERE SERIE 2011 COPY 199 CM DIAMETER X 150.6 CM PITCH PROPELLER RENAULT 4P-05 HJSS 2011 COPY PROPELLER INSTALLATION INSTALLATION STARDUSTER TOO 12368 LYCOMING HIO-360E1AD ENGINE FITTED LYCOMING HIO-360-E1AD ENGINE FITTED IN PLACE OF PREVIOUS 0-320 ENGINE. WALKER 76 x 56 LYCOMING HIO-360-E1AD BTGS WOOD PROPELLER FITTED (MODIFIED) STARDUSTER TOO 13819 PROPELLER CHANGE TO ALAN JAMES INSTALLATION OF ALAN JAMES AJ7656/WC/180 76 INCH DIAMETER X 56 INCH PITCH PROPELLER. LYCOMING HIO-360-E1AD BTGS AJ7656/WC/180 76" X 56" (MODIFIED) STARDUSTER TOO 14118 REPLACE PISTON TO LYC/HIO-30- PISTONS CHANGED TO SL10207-S TO GIVE 8.7:1 COMPRESSION RATIO IDENTICAL TO HIO-360-C1A, LYCOMING HIO-360-E1AD BTGS E1AD/8.7:1 YIELDING 205 BHP AT 2900 RPM. RPM LIMITED TO 2700 IN THIS INSTALLATION ONLY DUE TO LACK (MODIFIED) OF INFORMATION REGARDING ACCEPTABILITY OF THE JAMES PROPELLER FOR USE ABOVE 2700 RPM OR 180 BHP. MINIMUM FUEL GRADE NOW 100LL. STARDUSTER TOO SA300 14464 SENSENICH W76HZ5M8-58 76" x 58" INSTALLATION OF SENSENICH W76HZ5M8-58 76 INCH DIAMETER X 58 INCH PITCH PROPELLER. LYCOMING IO-360-C1C6 CDBR PROPELLER INSTALLATION STARDUSTER TOO SA300 12763 SECOND ELECTRIC FUEL PUMP INSTALLATION OF TWO FACET 478-360 ELECTRIC FUEL PUMPS, PLUMBED IN SERIES FROM LYCOMING O-360-C2D WINN INSTALLATION DEDICATED TANK OUTLET, TO PROVIDE SUFFICIENT FUEL FLOW WHEN FUEL TANK CONTENTS ARE LOW. 3-WAY SWITCH INSTALLED TO ISOLATE AND OPERATE EACH PUMP SEPARATELY. GRAVITY FEED FUEL LINE, PLUMBED FROM DEDICATED FUEL TANK OUTLET, FITTED WITH ANDAIR CK-375 NON-RETURN VALVE TO PREVENT RECIRCULATING FLOW WHEN ELECTRIC PUMP IS OPERATING. STARDUSTER TOO SA300 13709 GROVE UNDERCARRIAGE INSTALLATION GROVE UNDERCARRIAGE SUBSTITUTED DUE TO CONCERNS OVER INTEGRITY OF ORIGINAL LYCOMING IO-540-C4B5 KEEN UNDERCARRIAGE STARDUSTER TOO SA300 13352 ADDITION OF TUBULAR SOCKET TO EASE LIFTING TUBE ADDED TO REAR FUSELAGE TRUSS TO EASE GROUND HANDLING LYCOMING 0-360-A1F6 BOBT MANUAL GROUND HANDLING ATTENTION-GETTING WARNING PLACARD MUST BE FITTED ADJACENT TO LIFTING BAR SOCKET (MODIFIED) STATING 'WARNING - REMOVE LIFTING BAR BEFORE FLIGHT' STARLET SA500 12455 PROPELLER CHANGE EVRA D11.28.7B PROPELLER FITTED TO CONTINENTAL C90-8F ENGINE. CONTINENTAL C90-8F AZTV STARSTREAK SHADOW SA-II 14539 ENGINE CHANGE TO ROTAX 618 UL engine change to ROTAX 618 per AAN PFA 161-0172 Supp 6 issue 3 ROTAX 582/48 BYFI STEEN SKYBOLT 13984 ANTIGRAVITY LiFePO4 BATTERY AND INSTALLATION OF ANTIGRAVITY ATX12-20 LITHIUM ION (LiFePO4) BATTERY FITTED TO FIREWALL LYCOMING IO-360-A1A IIPI PLANE POWER ALTERNATOR IN CUSTOM BATTERY BOX AND PLANE POWER SAL12-70 ALTERNATOR INSTALLATION. INSTALLATIONS STEEN SKYBOLT 13985 LIGHTSPEED PLASMA III ELECTRONIC INSTALLATION OF LIGHTSPEED PLASMA III ELECTRONIC IGNITION LYCOMING IO-360-A1A IIPI IGNITION INSTALLATION STEEN SKYBOLT 14616 FITTING A SMOKING AIRPLANES SMOKE SMOKIN AIRPLANES UNIT INSTALLED ON FRONT SEAT IN A MANNER THAT ALLOWS REMOVAL LYCOMING IO-360-A1A IIPI SYSTEM WHEN AIRCRAFT to BE FLOWN WITH A PASSENGER. SINGLE EXHAUST INJECTOR (G-IIPI) OR DUAL INJECTOR (G-IIPI) MAY BE USED TO SUIT EXHAUST SYSTEM CONFIGURATION STEEN SKYBOLT 14617 WHIRLWIND 200AC 80" DIAMETER INSTALLATION OF WHIRLWIND 200AC 80 INCH DIAMETER C/S PROPELLER USING JIHOSTROJ P-940- LYCOMING IO-360-A1A IIPI PROPELLER INSTALLATION 010/AL GOVERNOR STEEN SKYBOLT 14543 ENGINE CHANGE TO LYCOMING IO-360- LYCOMING IO-360-A1A INSTALLED. LYCOMING IO-360-A1A SKIE A1A STEEN SKYBOLT 12670 EXTERNAL RELEASE OF FULL SKYBOLT STEEN AEROLAB CANOPY FITTED WITH PIP-PIN EMERGENCY RELEASE. PIP-PIN REVERSED SO LYCOMING IO-360-A1B6 SBOL CANOPY HANDLE IS EXTERNAL FOR EMERGENCY OPENING. PLACARDS FITTED TO INDICATE OPERATE ARRANGEMENT AND NEED TO PREVIEW BEFORE FLIGHT. STEEN SKYBOLT 13952 INSTALLATION OF FUEL FLOW INSTALLATION OF ELECTRONICS INTERNATIONAL FT-60 'RED CUBE' FUEL FLOW MONITORING LYCOMING IO-360-A1B6 SBOL MONITORING SYSTEM TRANSDUCER. STEEN SKYBOLT 14424 PROP CHANGE TO SENSENICH 76EM8S5- PROP CHANGE TO SENSENICH 76EM8S5-0-62. AEROBATICS PERMITTED ONLY SUBSEQUENTLY LYCOMING IO-360-C1C BUXI 0-62 AFTER IMPROVEMENT TO MODIFIED ENGINE MOUNT THAT WAS FORMERLY ONLY CLEARED WITH WOODEN PROPELLER. STEEN SKYBOLT 13302 FULL CANOPY WITH EXTERNAL RELEASE STEEN CANOPY OPTION WITH ADDITIONAL PROVISIONS FOR EMERGENCY EGRESS AND SUITABLE LYCOMING IO-360-C1C RODC INSTALLATION INSTRUCTION PLACARDS STEEN SKYBOLT 14621 REAR COCKPIT BUBBLE CANOPY BUBBLE CANOPY FITTED SIMILAR TO G-IIPI LYCOMING IO-360-C1C IPII Prototype mods that have been approved since 1/1/2008 Page 93 30/11/20 LAA Technical Leaflet TL 3.17 STEEN SKYBOLT 15298 CONSPICUITY LIGHTS INSTALLATION INSTALLATION OF TWO CONSPICUITY LIGHTS TO FUSELAGE UNDERSIDE IMMEDIATELY AFT OF THE LYCOMING IO-360-C1C IPII LOWER COWLING, ONE EACH SIDE OF THE AIRCRAFT CENTRE-LINE. STEEN SKYBOLT 14616 FITTING A SMOKING AIRPLANES SMOKE SMOKIN AIRPLANES UNIT INSTALLED ON FRONT SEAT IN A MANNER THAT ALLOWS REMOVAL LYCOMING IO-360-C1C IPII SYSTEM WHEN AIRCRAFT to BE FLOWN WITH A PASSENGER. SINGLE EXHAUST INJECTOR (G-IIPI) OR DUAL INJECTOR (G-IIPI) MAY BE USED TO SUIT EXHAUST SYSTEM CONFIGURATION STINSON HW-75 13917 SPIN-ON OIL FILTER ADAPTER FOR INSTALLATION OF CUSTOM MADE SPIN-ON OIL FILTER ADAPTER P/N 79001003 WITH CHAMPION CONTINENTAL C90-12F AFYO CONTINENTAL PC60 (O-200) CH48108 OR C138 OR BLUE PRINT ADT32109 OIL FILTER.

AT ISSUE 4: APPLICABILITY EXTENDED TO CONTINENTAL C90-12 ENGINE. AT ISSUE 6: APPLICABILITY EXTENDED TO CONTINENTAL C85-12F ENGINE. AT ISSUE 7: APPLICABILITY EXTENDED TO CONTINENTAL C90-14F ENGINE. STINSON HW-75 14423 HERCULES 6943276-S 69" x 43" INSTALLATION OF A HERCULES 6943276-S 69 INCH DIAMETER x 43 INCH PITCH PROPELLER CONTINENTAL O-200-A BMSA PROPELLER INSTALLATION STITS PLAYBOY SA3A 14902 PROPELLER CHANGE TO HERCULES PROPELLER CHANGED TO HERCULES 72454785-S CONTINENTAL A65-8 BVVR 72454785-S STITTS PLAYBOY SA3A 13955 ENGINE CHANGE TO CONTINENTAL A65- A65-8 ENGINE AND LODGE CJL 100 72 x 47 PROPELLER FITTED. CONTINENTAL A65-8 BGLZ 8 STREAK SHADOW 12302 CATEGORY CHANGE TO MICROLIGHT CATEGORY CHANGE INCLUDING PROPELLER CHANGE TO 3 BLADED ARPLAST ROTAX 582 BONP STREAK SHADOW 12303 PROP CHANGE TO ARPLAST 152/132 CHANGE OF PROPELLER TO ARPLAST 3 BLADED 152/132 DAM 48/3 SET AT 21.5 DEGREES AT 10CM ROTAX 582 BONP DAM48/3 X 21.5 DEG FROM TIP STREAK SHADOW 12680 CATEGORY CHANGE TO GROUP A ELEVATOR GAR SEAL REMOVED AND PLACARDS CHANGED TO REFLECT GROUP A STATUS ROTAX 582 BONP STREAK SHADOW 13312 ALUMINIUM ALLOY FUEL TANKS BY JEDI INSTALLATION OF ALUMINIUM ALLOY MAIN AND/OR SLIPPER TANKS FABRICATED BY JEDI RACING ROTAX 582 BONP RACING LTD CARS LTD IN PLACE OF ORIGINAL TANKS. TANKS COVERED BY THIS MODIFICATION ARE 23 LITRE NARROW MAIN TANK, 33 LITRE WIDE MAIN TANK, 27 LITRE SLIPPER TANK, AND 23 LITRE SLIPPER TANK FOR ROTAX 912 INSTALLATIONS. STREAK SHADOW 14858 CATEGORY CHANGE FROM GROUP A TO ELEVATOR GAP SEAL FITTED, MTWA REDUCED TO 390 KG AS NARROW BODY EXAMPLE. VNE ROTAX 582 BSMN MICROLIGHT REDUCED TO 125 MPH AS THIS WAS FASTEST SPEED ACHIEVED IN TEST AND HIGHER SPEEDS REQUIRE GREATER THAN DESIRABLE FORWARD STICK FORCE. NOISE CERTIFICATE ISSUED. STREAK SHADOW 12348 PROPELLER CHANGE TO ARPLAST INSTALLATION OF ARPLAST 152/132 DAM 3 52" DIA X 21° AT 75% RADIUS ROTAX 582 BTKP 152/132 DAM 3 52" DIA STREAK SHADOW 14474 FITTING OF M4 ELECTRIC STARTER M4 ELECTRIC STARTER FITTED IN PLACE OF MANUAL RECOIL START. INCLUDES BATTERY TRAY, 17.2 ROTAX 582 BTZZ Ah BATTERY AND ASSOCIATED WIRING, SWITCHING AND CIRCUIT PROTECTION. START IS MOUNTED WITH AN ADDITIONAL ANGLE BETWEEN THE MOTOR HOUSING AND THE EXISTING EXHAUST BRACKET TO REDUCE VIBRATIONS. CIRCUIT INCLUDES COCKPIT-OPERATED BATTERY ISOLATION SWITCH. STREAK SHADOW 15196 CATEGORY CHANGE TO MICROLIGHT CHANGE TO MICROLIGHT CONFIGURATION WITH 390 KG MTWA ROTAX 582 BTZZ STREAK SHADOW 13067 CATEGORY CHANGE FROM GROUP A TO ELEVATOR GAP SEAL FITTED AND WING FLAP TRAVEL TO BE CHECKED PER AAN PFA 161 0172 SUP ROTAX 582 BUGM MICROLIGHT 10. MAX GROSS WIGHT LIMITED TO 390 Kg WITH NARROW BODY COCKPIT. STREAK SHADOW 12514 ARPLAST 3 BLADED 152/132 DAM 48/3 ARPLAST 3 BLADED PROPELLER FITTED TYPE 152/132 DA 48/3 PITCHED TO 21 DEGREES AT 4" FROM ROTAX 582 BUIL PROPELLER FITTED BLADE TIP, IN ACCORDANCE WITH ARPLAST FITTING INSTRUCTIONS. STREAK SHADOW 12831 CATEGORY CHANGE TO GROUP A ELEVATOR GAP SEAL REMOVED, MAX GROSS WEIGHT RAISED TO 408 KG ROTAX 582 BUOB STREAK SHADOW 13904 CATEGORY CHANGE TO MICROLIGHT CATEGORY CHANGE TO MICROLIGHT WITH ADDITION OF ELEVATOR GAP SEAL AND ENSURING ROTAX 582 BUVX FULL FLAP TRAVEL ACHIEVED. MAX GROSS WEIGHT REDUCED TO 390 Kg. NOISE CERTIFICATE ISSUED STREAK SHADOW 12561 CATEGORY CHANGE TO MICROLIGHT CATEGORY CHANGE. ELEVATOR GAP SEAL FITTED. FLAP TRAVEL CHECKED. WEIGHT AND BALANCE ROTAX 582 BVFR CHECK. PLACARD ADDED. STREAK SHADOW 12562 PROPELLER CHANGE TO ARPLAST ARPLAST 152/132 DAM 3 BLADED PROPELLER FITTED WITH PITCH 21.5° AT 4" FROM TIP. ROTAX 582 BVFR STREAK SHADOW 14244 CATEGORY CHANGE TO MICROLIGHT NARROW BODY STREAK CONVERTED TO MICROLIGHT TWO SEATER WITH 390 KG MTWA, ROTAX 582 BVTD ELEVATOR GAP SEAL FITTED, FLAP DEFLECTION CHECKED, NOISE CERTIFICATE ISSUED STREAK SHADOW 15095 CATEGORY CHANGE TO MICROLIGHT . ROTAX 582 BWAI Prototype mods that have been approved since 1/1/2008 Page 94 30/11/20 LAA Technical Leaflet TL 3.17 STREAK SHADOW 14883 Category change from Group A to ALREADY ACCEPTED CONFIGURATION - NARROW BODY FUSELAGE, ELEVATOR GAP SEAL, 30 ROTAX 582 GORE Microlight DEGREE FLAP TRAVEL AND 390 Kg MTWA, NOISE CERTIFICATE ISSUED STREAK SHADOW 14884 ENGINE CHANGE TO ROTAX 582 . ROTAX 582 GORE STREAK SHADOW 12499 CATEGORY CHANGE TO GROUP A CATEGORY CHANGE. ROTAX 582 MWPP STREAK SHADOW 12822 PROPELLER CHANGE TO WARP DRIVE PROPELLER CHANGE TO WARP DRIVE RPM 4 BLADED 52" DIAMETER X 15 DEGREES AT TIP. ROTAX 582 DOTT RPM 4 BLADED 52" DIAMETER STREAK SHADOW 13244 CATEGORY CHANGE TO GROUP A CATEGORY CHANGE TO GROUP A BY REMOVING ELEVATOR GAP SEAL ROTAX 582 DOTT STREAK SHADOW 14490 WARP DRIVE RPM 3 BLADED 52 INCH INSTALLATION OF WARP DRIVE RPM 3 BLADED 52 INCH DIAMETER PROPELLER ROTAX 582 DOTT DIAMETER PROPELLER INSTALLATION STREAK SHADOW 12436 PROPELLER CHANGE PRECISION PROPS 4 BLADED 52" DIAMETER GROUND ADJUSTABLE PROPELLER FITTED. ROTAX 618 WHOG STREAK SHADOW 12264 PROPELLER CHANGE TO ARPLAST CHANGE OF PROPELLER TO ARPLAST ECOPROP 133L130/3 ROTAX 912-UL BXFK ECOPROP 133L130/3 STREAK SHADOW 14871 Category change from microlight to CATEGORY CHANGE TO GROUP A - NO PHYSICAL CHANGE REQUIRED BUT ELEVATOR GAP SEAL ROTAX 912-UL BYOO group A NOW OPTIONAL STREAK SHADOW 12601 CONVERSION OF CARBS & FUEL SYSTEM SEE WORKSHEET G-ENEE/2 (SAME AS G-MYTY). SINGLE POLYTHENE TANK FITTED IN REAR COCKPIT ROTAX 912-UL ENEE REPLACING MAIN AND SLIPPER TANK ARRANGEMENT STREAK SHADOW SA 14750 ENGINE CHANGE TO ROTAX 582 UL DCDI ROTAX 582 ENGINE SUBSTITUTED ROTAX 582 BWPS

STREAK SHADOW SA 14574 ENGINE CHANGE TO ROTAX BLUE TOP 99 . ROTAX 582 MGGT

STREAK SHADOW SA 12814 PROPELLER CHANGE TO ARPLAST 3 ARPLAST 3 BLADED DAM 4875/3 PROPELLER FITTED ROTAX 582 CEZU BLADE STREAK SHADOW SA 12329 CATEGORY CHANGE FROM MICROLIGHT REMOVAL OF REAR COCKPIT BLOCKING BAR AND INSTALLATION OF REAR SEAT BELTS TO ALLOW ROTAX 618 MYNX TO GROUP A USE AS GROUP 'A' CATEGORY AIRCRAFT WITH MAXIMUM GROSS WEIGHT OF 408 KG. STREAK SHADOW SA 13100 CATEGORY CHANGE TO MICROLIGHT CATEGORY CHANGE. ELEVATOR GAP SEAL ADDED, FLAP TRAVEL CONFIRMED PER MANUAL. ROTAX 618 WYAT WEIGHT CHECKED AND PLACARD FITTED. STREAK SHADOW SA-M 13141 REPLACEMENT FUEL SYSTEM SINGLE FUEL TANK FOUNTED IN REAR SEAT POSITION PER G-MYTY NAD G-ENEE ROTAX 582 BUXC STREAK SHADOW SA-M 13766 CATEGORY CHANGE TO MICROLIGHT CATEGORY CHANGE TO MICROLIGHT AS SINGLE SEATER WITH MAX GROSS WEIGHT OF 350 Kg AND ROTAX 582 BUXC DESIGNATION CHANGED TO SA-M STREAK SHADOW SA-M 13015 CATEGORY CHANGE TO GROUP A CATEGORY CHANGE TO GROUP A. ROTAX 912-UL TEHL STREAK SHADOW SA-M 14176 CATEGORY CHANGE TO MICROLIGHT CATEGORY CHANGE TO SINGLE SEAT MICROLIGHT WITH 350 Kg MAX GROSS WEIGHT. ROTAX 912-UL TEHL SPITFIRE MK26 14428 BRAKE CYLINDER RELOCATION RELOCATION OF THE LOWER ATTACHMENT POINT OF THE BRAKE CYLINDERS FROM RUDDER ISUZU V6 CIEN ASSEMBLY TO FIXED POINTS ON THE FUSELAGE. MK26 14527 ROTEC LIQUID COOLED CYLINDER HEADS INSTALLATION OF ROTEC LIQUID COOLED CYLINDER HEADS AND ASSOICATED RADIATORS, PUMPS JABIRU 5100A CJWW FITTED TO JABIRU 5100A ENGINE AND CONTROLS TO JABIRU 5100A ENGINE.

SUPERMARINE SPITFIRE MK26 14545 ROTEC ALTERNATOR CONVERSION INSTALLATION OF BELT DRIVEN DENSO 12196N 45 AMP ALTERNATOR MOUNTED TO REAR OF JABIRU 5100A CJWW ENGINE WITH MOUNTING KIT DESIGNED AND SUPPLIED BY ROTEC AEROSPORT. SUPERMARINE SPITFIRE MK26 12766 RUDDER CABLE TENSION ADJUSTMENT 2 OFF MS21251-B3S TURNBUCKLES AND ASSOCIATED FITTINGS ADDED TO RUDDER CABLE SYSTEM JABIRU 5100A CEFC TO ENABLE CORRECT CABLE TENSION AND ADJUSTMENTS TO BE MADE. ONE TURNBUCKLE INSTALLED IN EACH RUDDER CABLE IN AFT FUSELAGE SECTION, LOCATED BEHIND THE ACCESS HATCH. SUPERMARINE SPITFIRE MK26 14123 THROTTLE FRICTION EXISTING THROTTLE FRICTION DEVICE SUPPLEMENTED BY ADDING A DELRIN CAM FASTENED TO JABIRU 5100A CEFC THE THROTTLE SUPPORT STRUCTURE. A SPRING-LOADED FOLLOWER IS FASTENED TO THE THROTTLE LEVER, WHICH FOLLOWS THE CAM WITH A PVC FRICTION PAD. SPRING TENSION MAY BE ADJUSTED TO VARY THE FRICTION. CAM ARC IS OFFSET BY 4MM AFT TO CREATE INCREASED FRICTION TOWARDS IDLE THROTTLE. SUPERMARINE SPITFIRE MK26 14466 UNDERCARRIAGE LEG REBUILD UNDERCARRIAGE MAIN LEGS REDESIGNED USING STRONGER UPPER TUBE MATERIAL, SCISSORS JABIRU 5100A CEFC RATHER THAN SPLINES, REDUCED TOE-IN AND SUNDRY MINOR DETAIL CHANGES

Prototype mods that have been approved since 1/1/2008 Page 95 30/11/20 LAA Technical Leaflet TL 3.17 SUPERMARINE SPITFIRE MK26 14469 RUDDER PEDAL BELL CRANKS AND RUDDER PEDALS LINKED BY SYSTEM CONSISTING OF TWO BELLCRANKS AND THREE PUSHRODS, IN JABIRU 5100A CEFC PUSHROD SYSTEM ADDITION TO THE EXISTING CABLE AND TWO PULLEYS, TO PREVENT SPRING IN RUDDER CIRCUIT AND BRAKES, AND AVOID OVERLOADING RUDDER, RUDDER HINGES AND RUDDER HORN UNDER BRAKING ACTION. TAYLOR MONOPLANE 12480 ENGINE CHANGE INSTALLATION OF JABIRU 2200A USING CORBY STARLET ENGINE MOUNT AND FIREWALL JABIRU 2200A OBJM REINFORCEMENTS. TAYLOR MONOPLANE 12526 AILERON MASS BALANCING AILERON MASS BALANCES ADDED AS PER TAYLOR TITCH DRAWINGS, EXCEPT ARM IS WELDED TO JABIRU 2200A OBJM BRACKET RATHER THAN BRAZED. TAYLOR MONOPLANE 12527 PENDANT RUDDER PEDALS PENDANT RUDDER PEDALS WITH TOE BRAKES INSTALLED IN PLACE OF BOTTOM-HINGED RUDDER JABIRU 2200A OBJM PEDALS. PEDALS HINGED FROM NYLON BLOCKS MOUNTED ON FORWARD COCKPIT UPRIGHTS.

TAYLOR MONOPLANE 15231 HERCULES 5842799-S 58'' X 42'' INSTALLATION OF HERCULES 5842799-S 58 INCH DIAMETER X 42 INCH PITCH PROPELLER JABIRU 2200A OBJM PROPELLER INSTALLATION TAYLOR MONOPLANE 12746 WING TIP SHAPE WING TIP RE-MODELLED TO PROVIDE INTERMEDIATE AREA BETWEEN EXISTING LONG AND SHORT VW 1600 AYSH SPAN OPTIONS, ELLYPITICAL TIP SHAPE REPLACED BY SHEARED TIPS. TAYLOR MONOPLANE 12498 PROPELLER CHANGE TO LODGE CJL 129 PROPELLER CHANGE TO LODGE CJL 129 54 INCH DIAMETER X 33 INCH PITCH. VW 1600 BGCY 54 INCH DIAMETER X 33 INCH PITCH. TAYLOR MONOPLANE 12898 PROPELLER CHANGE TO NEWTON 10L PROPELLER CHANGE TO NEWTON 10L 54 INCH DIAMETER X 33 INCH PITCH. VW 1600 BLDB 54" X 33" TAYLOR MONOPLANE 14433 PROP CHANGE TO NEWTON 09L NEWTON 09L 54 x 36 propeller fitted. VW 1600 BMET TAYLOR MONOPLANE 14072 NEWTON 09L 54" X 33" PROPELLER INSTALLATION OF NEWTON 09L 54 INCH DIAMETER X 33 INCH PITCH PROPELLER. VW 1600 BRUO INSTALLATION TAYLOR MONOPLANE 13381 NEWTON 10L 54" X 34" PROPELLER INSTALLATION OF NEWTON 10L 54 INCH DIAMETER X 34 INCH PITCH PROPELLER. VW 1700 BDAD INSTALLATION. TAYLOR MONOPLANE 12863 PROPELLER CHANGE TO SAXON 56" X 36" PROPELLER CHANGE TO SAXON 11885636 56" X 36" VW 1834 BDNG

TAYLOR MONOPLANE 13065 PROPELLER CHANGE TO C J LODGE LODGE CJL 124 57 x 32 PROPELLER SUBSTITUTED. VW 1834 BDNG TAYLOR MONOPLANE 12800 LEBURG ELECTRIC DUAL IGNITION LEBURG SYTEM FITTED, BATTERIES MOUNTED BEHIND MAIN SPARINCOCKPIT PER APPLICANT'S VW 1834 BEVS SYSTEM SUBMISSION TAYLOR MONOPLANE 12315 PROPELLER CHANGE TO NEWTON TYPE CHANGE OF PROPELLER TO NEWTON TYPE 09L 54 X 33 VW (PEACOCK) 1600 AXYK 09L 54 X 33 TAYLOR MONOPLANE 14416 AUXILIARY FUEL PUMP ELECTRIC FUEL PUMP FITTED AS A BACK-UP FOR ENGINE DRIVEN PUMP VW (PEACOCK) 1600 AXYK TAYLOR TITCH 12269 PROPELLER CHANGE TO RWG 61" X 64.5" INSTALLATION OF RWG 61" X 64.5" PROPELLER CONTINENTAL C90-12F BARN

TAYLOR TITCH 13628 MODIFICATION TO ONE PIECE WING FOLLOWING ACCIDENT IN 2004, TWO-PIECE WING RE-CONFIGURED AS ONE PIECE WING BY CONTINENTAL O-200-A BABE MAKING MAINSPAR SPLICE INSERT. MAINSPAR TO FUSELAGE ATTACHMENTS REVISED TO SUIT

TAYLOR TITCH 13629 MODIFICATION TO TAILPLANE DOUBLERS ADDED TO TAILPLANE FRONT AND REAR SPARS, MOUNTING ARRANGEMENT ALTERED CONTINENTAL O-200-A BABE TO SUIT RESULTING THICKER SPARS TAYLOR TITCH 13630 MODIFICATION TO ENGINE 0-200 C85 PISTONS FITTED CONFERRING AN INCREASED CR of 8.5. CONTINENTAL O-200-A BABE TAYLOR TITCH 13631 PROPELLER CHANGE TO HERCULES 62" X HERCULES 62 x 68.49 PROPELLER SUBSTITUTED, USING 4" SABRE EXTENSION TO MATCH EXISTING CONTINENTAL O-200-A BABE 68.49" COWLINGS ORIGINALLY BUILT FOR MT PROPELLER TAYLOR TITCH 12342 BRAKE RUDDER PEDAL SYSTEM ORIGINAL PLYWOOD PEDALS AND CABLE BRAKE SYSTEM REPLACED WITH ALLOY RUDDER PEDALS CONTINENTAL O-200-A TICH ON ALLOY SUPPORT BRACKETS. TOE-OPERATED LEVERS ACT ON MATCO MC-4A MASTER CYLINDERS. TAYLOR TITCH 12343 UNDERCARRIAGE CLAMPING SYSTEM ONE-PIECE UNDERCARRIAGE SPRING ATTACHED TO FUSELAGE USING CUSTOM DESIGNED 6082-T6 CONTINENTAL O-200-A TICH ANGLES. TAYLOR TITCH 12344 FLAP LEVER SYSTEM FLAP LEVER MOVED FROM ORIGINAL LOCATION UNDER PILOT'S RIGHT ELBOW TO ATTACHMENT CONTINENTAL O-200-A TICH ON MAIN SPAR. TAYLOR TITCH 12345 PROPELLER CHANGE TO KF6165/S2/RR CHANGE OF PROPELLER TO TERRY GARDNER MANUFACTURED COPY OF KEN FERN KF6165/S2/RR CONTINENTAL O-200-A AYZH 61" X 65" COPY 61 INCH DIAMETER X 65 INCH PITCH Prototype mods that have been approved since 1/1/2008 Page 96 30/11/20 LAA Technical Leaflet TL 3.17 TAYLORCRAFT BC12-65 12875 PROPELLER CHANGE KEN FERN KF 7242 UL-S2-RR PROPELLER SUBSTITUTED FOLLOWING ACCIDENT CONTINENTAL A65-8F BPHP TAYLORCRAFT BC12D 12838 PROPELLER CHANGE TO MCCAULEY PREVIOUSLY FITTED MCCAULEY 1B90/CM 74" X 47" RE-PITCHED TO 45". CONTINENTAL A65-8 BVXS 1B90/CM 74" X 45" TAYLORCRAFT BC12D 13577 PROPELLER CHANGE TO SENSENICH SENSENICH W72CK42 PROPELLER SUBSTITUTED CONTINENTAL A65-8F BTFK W72CK42 TAYLORCRAFT BC12D 14019 ENGINE CHANGE TO CONTINENTAL C85- ENGINE REPLACED WITH A CONTINENTAL C85-12F, RETAINING A LODGE CJL 100 72"X47". CONTINENTAL C85-12F BPHO 12F OCCUPANCY RESTRICTED TO SINGLE-SEAT OPERATION. TAYLORCRAFT BC12D 14389 INCORPORATION OF PART 2 OF STC SA1- INCORPORATION OF FAA STC SA1-210. THIS CONSISTS OF REINFORCED STRUT FITTINGS TO ALLOW CONTINENTAL C85-12F BPHO 210 TO INCREASE MAUW TO 1280 LBS AN INCREASE MAUW TO 1280 LBS.

TEAM HIMAX 1700R 13366 STREAMLINED STRUT FAIRINGS FOR STREAMLINED STRUT FAIRINGS, OF SOLID BASLSA WOOD CONSTRUCTION, ATTACHED TO ROTAX 447 CBNZ MAINPLANE, TAILPLANE & EXISTING ROUND SECTION ALUMINIUM TUBE STRUTS AND COVERED WITH DACRON FABRIC. UNDERCARRIAGE TEAM MINIMAX 12707 FITTING ELECTRIC TRIM ELECTRIC DIGITAL ELEVATOR TRIM SYSTEM INSTALLED OF OWNER'S OWN CUSTOM DESIGN ROTAX 447 MWFD TEAM MINIMAX 91 12559 ENGINE & PROPELLER CHANGE HUMMEL 1/2 VW ENGINE AND NEWTON 2-BLADE 54" X 29" PROPELLER FITTED. HUMMEL 1/2 VW 45 HP MYBM TEAM MINIMAX 91 13184 MECHANICAL DISC BRAKE CALLIPER DISC BRAKE CALLIPER UNITS REPLACED BY EQUIVALENT CLARK CMD-8 CALLIPER UNIT ROTAX 447 MYYR UPGRADE P2002 SIERRA DELUXE 12979 THROTTLE FRICTION DEVICE INSTALLATION OF ROTARY KNOB TYPE THROTTLE FRICTION CONTROL CONCENTRIC WITH PLUNGER ROTAX 912-ULS OTEC THROTTLE ON CENTRAL THROTTLE CONTROL (SIMILAR TO MOD 12258). DELUXE 12751 ANDAIR NON-RETURN VALVE AT EACH INSTALLATION OF ANDAIR CK375H NON-RETURN VALVE IN FUEL HOSE BETWEEN EACH TANK ROTAX 912-ULS OTEC TANK OUTLET OUTLET AND FUEL SELECTOR VALVE TO PREVENT FUEL TRANSFER BETWEEN TANKS WHEN AIRCRAFT IS PARKED ON SLOPING GROUND WITH ONE WING LOWER THAN THE OTHER. TECNAM P2002-EA SIERRA 12781 FUEL TANK DRAINS INSTALLATION OF FUEL TANK DRAINS IN ACCORDANCE WITH TECNAM DOCUMENT NO. 108. ROTAX 912-ULS TESI ACCEPTABLE ON ALL VARIANTS OF TECNAM SIERRA. TECNAM P2002-EA SIERRA 12258 ALTERNATIVE THROTTLE FRICTION REMOVAL OF TECNAM SUPPLIED THROTTLE FRICTION DEVICE AND INSTALLATION OF ROTARY ROTAX 912-ULS TESI DEVICE KNOB TYPE THROTTLE FRICTION CONTROL CONCENTRIC WITH PLUNGER THROTTLE ON ONE THROTTLE ONLY. TECNAM P2002-EA SIERRA 12248 PROPELLER CHANGE TO GT-2 VEB/GT-2 CHANGE OF PROPELLER TO GT-2 VEB/GT-2 V14S177RFW80SRTC WITH SMART AVIONICS CSC 1/G ROTAX 912-ULS SRRA V14S177RFW80SRTC CONTROLLER. TECNAM P2002-EA SIERRA 12248 PROPELLER CHANGE TO GT-2 VEB/GT-2 CHANGE OF PROPELLER TO GT-2 VEB/GT-2 V14S177RFW80SRTC WITH SMART AVIONICS CSC 1/G ROTAX 912-ULS CDTV V14S177RFW80SRTC CONTROLLER. TECNAM P2002-EA SIERRA 11789 TRIO WING LEVELLER AUTO PILOT TRIO WING LEVELLER AUTO PILOT ROTAX 912-ULS SDOB TECNAM P2002-EA SIERRA 11880 TRIO ALTITUDE HOLD INSTALLATION OF TRIO EZ-2 ALTITUDE HOLD WITH PITCH CONTROL SERVO LOCATED UNDER P2 ROTAX 912-ULS SDOB SEAT. AUTO-TRIM FEATURE NOT ENABLED. TECNAM P2002-EA SIERRA 15097 HERCULES 7059797-S 70" x 59" INSTALLATION OF HERCULES 7059797-S 70" x 59" PROPELLER ROTAX 912-ULS SDOB PROPELLER INSTALLAION TECNAM P2002-EA SIERRA 13549 IVOPROP MEDIUM 3 BLADED 68" INSTALLATION OF IVOPROP MEDIUM 3 BLADED 68 INCH DIAMETER GROUND ADJUSTABLE ROTAX 912-ULS RLMW DIAMETER 9° PITCH PROPELLER PROPELLER SET TO 9 DEGREES PITCH AT 70% RADIUS. INSTALLATION. TECNAM P2002-EA SIERRA 15219 HERCULES 7059797-S 70" X 59" INSTALLATION OF HERCULES 7059797-S 70 INCH DIAMETER X 59 INCH PITCH PROPELLER ROTAX 912-ULS CEOC PROPELLER INSTALLATION TECNAM P2002-EA SIERRA 13764 WOODCOMP SR3000/3N 1720MM INSTALLATION OF WOODCOMP SR3000/3N 1720MM DIAMETER PROPELLER ROTAX 912-ULS TSAC DIAMETER PROPELLER INSTALLATION TECNAM P2002-EA SIERRA 13838 SMART AVIONICS CSC-1/G CONSTANT INSTALLATION OF SMART AVIONICS CSC-1/G ELECTRONIC CONSTANT SPEED PROPELLER ROTAX 912-ULS TSAC SPEED PROPELLER CONTROLLER CONTROLLER TO REPLACE MANUAL PITCH CHANGE SWITCHES. INSTALLATION TECNAM P2002-EA SIERRA 13973 INSTALLATION OF TRUTRAK ROLL INSTALLATION OF TRUTRAK ROLL SERVO UNDER THE SEATS DRIVEN BY A VIZION 380. ROTAX 912-ULS TSAC AUTOPILOT

Prototype mods that have been approved since 1/1/2008 Page 97 30/11/20 LAA Technical Leaflet TL 3.17 TECNAM P2002-EA SIERRA 14087 TRUTRACK PITCH SERVO (VIZION 380) INSTALLATION OF TRUTRAK PITCH SERVO MOUNTED IN CUSTOM MADE TRAY UNDER COCKPIT ROTAX 912-ULS TSAC INSTALLATION FLOOR WITH SHORT PUSH-ROD DRIVING PITCH PUSH-ROD VIA CUSTOM MADE CLAMPED TAB. AUTO-PILOT STATIC PORT OPEN TO COCKPIT PRESSURE TO AVOID PITCH OVER-SENSITIVITY DURING TURNS.

TECNAM P2002-EA SIERRA 14702 IMPROVED NOSEWHEEL SPINDLE ORIGINAL 2-PIECE NOSEWHEEL SPINDLE REPLACED WITH A SINGLE STRAIGHT-THROUGH STEEL ROTAX 912-ULS TSAC ASSEMBLY SPINDLE. TECNAM P2002-EA SIERRA 12255 HINGED TOP ENGINE COWLING ENGINE TOP COWL MADE IN THREE PIECES WITH CENTRAL PART FIXED AND SIDES HINGED FOR ROTAX 912-ULS NFLY ADDITIONAL CONVENIENCE. WATER SEAL ADDED AT LAA SUGGESTION. TECNAM P2002-EA SIERRA 12258 ALTERNATIVE THROTTLE FRICTION REMOVAL OF TECNAM SUPPLIED THROTTLE FRICTION DEVICE AND INSTALLATION OF ROTARY ROTAX 912-ULS CEVM DEVICE KNOB TYPE THROTTLE FRICTION CONTROL CONCENTRIC WITH PLUNGER THROTTLE ON ONE THROTTLE ONLY. TECNAM P2002-EA SIERRA 13124 ONE THROTTLE CONTROL PORT-SIDE THROTTLE CONTROL REMOVED, LEAVING ONE CENTRAL THROTTLE CONTROL. ROTAX 912-ULS CGUW TECNAM P2002-EA SIERRA 12258 ALTERNATIVE THROTTLE FRICTION REMOVAL OF TECNAM SUPPLIED THROTTLE FRICTION DEVICE AND INSTALLATION OF ROTARY ROTAX 912-ULS CGUW DEVICE KNOB TYPE THROTTLE FRICTION CONTROL CONCENTRIC WITH PLUNGER THROTTLE ON ONE THROTTLE ONLY. TECNAM P2002-EA SIERRA 12751 ANDAIR NON-RETURN VALVE AT EACH INSTALLATION OF ANDAIR CK375H NON-RETURN VALVE IN FUEL HOSE BETWEEN EACH TANK ROTAX 912-ULS CGUW TANK OUTLET OUTLET AND FUEL SELECTOR VALVE TO PREVENT FUEL TRANSFER BETWEEN TANKS WHEN AIRCRAFT IS PARKED ON SLOPING GROUND WITH ONE WING LOWER THAN THE OTHER. TECNAM P2002-EA SIERRA 12759 ANDAIR FUEL SHUT OFF VALVE INSTALLATION OF ANDAIR TYPE 20 FUEL TANK SELECTOR/SHUT OFF VALVE, REPLACING ORIGINAL ROTAX 912-ULS CGUW TECNAM FUEL VALVES. TECNAM P2002-RG SIERRA 12406 ALTERNATIVE THROTTLE FRICTION INSTALLATION OF ROTARY KNOB TYPE THROTTLE FRICTION CONTROL CONCENTRIC WITH PLUNGER ROTAX 912-ULS TESR DEVICE THROTTLE ON LEFT HAND THROTTLE ONLY. TECNAM P2002-RG SIERRA 12409 MOVE POSITION OF FUEL TAPS FUEL SHUT OFF VALVES REPOSITIONED 6" AFT OF ORIGINAL POSITION ROTAX 912-ULS TESR TECNAM P2002-RG SIERRA 12440 UNDERCARRIAGE RETRACTION LEVER INSTALLATION OF A SPRUNG LATCH TO PREVENT INADVERTANT OPERATION OF UNDERCARRIAGE ROTAX 912-ULS TESR SAFETY LATCH RETRACTION LEVER. TECNAM P2002-RG SIERRA 12748 FUEL FLOW MONITORING SYSTEM FUEL FLOW MONITORING SYSTEM USING FLOSCAN 201B-6 TRANSDUCER AND DYNON D180 EFIS ROTAX 912-ULS TESR UNIT INSTALLED IN ACCORDANCE WITH MANUFACTURER'S INSTRUCTIONS. TECNAM P2002-RG SIERRA 12751 ANDAIR NON-RETURN VALVE AT EACH INSTALLATION OF ANDAIR CK375H NON-RETURN VALVE IN FUEL HOSE BETWEEN EACH TANK ROTAX 912-ULS TESR TANK OUTLET OUTLET AND FUEL SELECTOR VALVE TO PREVENT FUEL TRANSFER BETWEEN TANKS WHEN AIRCRAFT IS PARKED ON SLOPING GROUND WITH ONE WING LOWER THAN THE OTHER. TECNAM P2002-RG SIERRA 12781 FUEL TANK DRAINS INSTALLATION OF FUEL TANK DRAINS IN ACCORDANCE WITH TECNAM DOCUMENT NO. 108. ROTAX 912-ULS TESR ACCEPTABLE ON ALL VARIANTS OF TECNAM SIERRA. TECNAM P2002-RG SIERRA 12915 COOLANT THERMOSTAT FOR ROTAX 91X INSTALLATION OF CONAIR SPORTS SUPPLIED COOLANT THERMOSTAT TO ROTAX 91X SERIES ROTAX 912-ULS TESR SERIES ENGINES ENGINE INSTALLATIONS. INSTALLATION CARRIED OUT IN ACCORDANCE WITH CONAIR SPORTS INSTRUCTIONS. TECNAM P2002-RG SIERRA 11789 TRIO WING LEVELLER AUTO PILOT TRIO WING LEVELLER AUTO PILOT ROTAX 912-ULS TESR TECNAM P2002-RG SIERRA 11880 TRIO ALTITUDE HOLD INSTALLATION OF TRIO EZ-2 ALTITUDE HOLD WITH PITCH CONTROL SERVO LOCATED UNDER P2 ROTAX 912-ULS TESR SEAT. AUTO-TRIM FEATURE NOT ENABLED. TECNAM P2002-RG SIERRA 12759 ANDAIR FUEL SHUT OFF VALVE INSTALLATION OF ANDAIR TYPE 20 FUEL TANK SELECTOR/SHUT OFF VALVE, REPLACING ORIGINAL ROTAX 912-ULS CFSB TECNAM FUEL VALVES. TECNAM P2002-RG SIERRA 12258 ALTERNATIVE THROTTLE FRICTION REMOVAL OF TECNAM SUPPLIED THROTTLE FRICTION DEVICE AND INSTALLATION OF ROTARY ROTAX 912-ULS CFSB DEVICE KNOB TYPE THROTTLE FRICTION CONTROL CONCENTRIC WITH PLUNGER THROTTLE ON ONE THROTTLE ONLY. TECNAM P2002-RG SIERRA 12781 FUEL TANK DRAINS INSTALLATION OF FUEL TANK DRAINS IN ACCORDANCE WITH TECNAM DOCUMENT NO. 108. ROTAX 912-ULS CFSB ACCEPTABLE ON ALL VARIANTS OF TECNAM SIERRA. -EA ECHO 15077 CATEGORY CHANGE TO GROUP A CATEGORY CHANGE WITH TECNAM STANDARD STEEL MAIN UNDERCARRIAGE FITTED, MTWA JABIRU 2200A TECM INCREASED TO 500 KG. DESIGNATION CHANGED TO -EA VARIANT

Prototype mods that have been approved since 1/1/2008 Page 98 30/11/20 LAA Technical Leaflet TL 3.17 TECNAM P92-EA ECHO 13567 HEATER KIT FOR TECNAM ECHO STANDARD TECNAM HEATER SELECTOR BOX FITTED TO FIREWALL, WITH MANUAL CONTROL FROM JABIRU 2200A CBGE COCKPIT. HEAT SUPPLIED BY STANDARD JABIRU EXHAUST HEAT MUFF FED TO SELECTOR BOX VIA SCAT HOSE TECNAM P92-EA ECHO 13567 HEATER KIT FOR TECNAM ECHO STANDARD TECNAM HEATER SELECTOR BOX FITTED TO FIREWALL, WITH MANUAL CONTROL FROM JABIRU 2200A BZWT COCKPIT. HEAT SUPPLIED BY STANDARD JABIRU EXHAUST HEAT MUFF FED TO SELECTOR BOX VIA SCAT HOSE TECNAM P92-EA ECHO 12798 CATEGORY CHANGE TO GROUP A CATEGORY CHANGED TO GROUP A. AAN PFA-318-419 SUPPLEMENT 1 REFERS. JABIRU 2200A CBAX TECNAM P92-EA ECHO 12855 FLOSCAN SERIES 200 FUEL FLOW FLOSCAN SERIES 200 FUEL FLOW TRANSDUCER INSTALLED JABIRU 2200A CBAX TRANSDUCER TECNAM P92-EA ECHO 12856 TRIO PRO PILOT DUAL AXIS AUTO-PILOT INSTALLATION OF TRIO PRO PILOT DUAL AXIS AUTO-PILOT WITH SERVOS MOUNTED TO ANGLE JABIRU 2200A CBAX BRACKETS, THE ROLL SERVO ON THE COCKPIT ROOF AND THE PITCH SERVO ON TO FUSELAGE FLOOR AFT AND ADJACENT TO THE PITCH CONTROL IDLER BELLCRANK. TECNAM P92-EA ECHO 13136 REPLACEMENT OF POROUS GRP FUEL REPLACEMENT WING TANKS FABRICATED FROM ALUMINIUM PER STANDARD AVIATION JABIRU 2200A CBLB TANKS WITH SHEET ALUMINIUM TANKS PRACTICES, APPLICANTS DRAWING SHOWS FABRICATION DETAILS. SIGHT TUBE ADDED AT ROOT END. TECNAM P92-EA ECHO 13332 CATEGORY CHANGE TO GROUP A REINFORCED MAIN UNDERCARRIAGE REQUIRED JABIRU 2200A CBLB TECNAM P92-EA ECHO 12841 CATEGORY CHANGE FROM MICROLIGHT INSTALLATION OF TECNAM SUPPLIED STEEL MAIN UNDERCARRIAGE LEGS WITH MARCO INGENGO UL POWER 260i CCAL TO GROUP A 5 X 5.00 WHEELS AND BRAKES TO ENABLE OPERATION AT INCREASED MAXIMUM GROSS WEIGHT OF 500KG. TECNAM P92-EA ECHO 13077 ENGINE CHANGE TO UL POWER UL POWER 260i FITTED USING STANDARD JABIRU ENGINE MOUNT, MODIFIED COWLINGS AND UL POWER 260i CCAL STANDARD GT PROPELLER FOR JABIRU ENGINE. SINGLE BATTERY INSTALLATION USED. HEADER TANK FITTED TO ACCOMMODATE VAPOUR RETURN LINE. TECNAM P92-EA ECHO 13190 GT-2/160/VZR-FW101SRTC 160CM X INSTALLATION OF GT-2/160/VZR-FW101SRTC 160CM DIAMETER X 105CM PITCH PROPELLER. UL POWER 260i CCAL 105CM PROPELLER TECNAM P92-EA ECHO 13136 REPLACEMENT OF POROUS GRP FUEL REPLACEMENT WING TANKS FABRICATED FROM ALUMINIUM PER STANDARD AVIATION UL POWER 260i CCAL TANKS WITH SHEET ALUMINIUM TANKS PRACTICES, APPLICANTS DRAWING SHOWS FABRICATION DETAILS. SIGHT TUBE ADDED AT ROOT END. TECNAM P92-EM ECHO 13136 REPLACEMENT OF POROUS GRP FUEL REPLACEMENT WING TANKS FABRICATED FROM ALUMINIUM PER STANDARD AVIATION JABIRU 2200A WHEN TANKS WITH SHEET ALUMINIUM TANKS PRACTICES, APPLICANTS DRAWING SHOWS FABRICATION DETAILS. SIGHT TUBE ADDED AT ROOT END. TECNAM P92-EM ECHO 14279 VARLEY LI-5 LIFEPO4 BATTERY INSTALLATION OF VARLEY LI-5 LIFEPO4 (LITHIUM FERROUS PHOSPHATE) BATTERY TO FRONT OF JABIRU 2200A CBDM INSTALLATION TO FIREWALL FIREWALL IN CUSTOM MADE ALUMINIUM BATTERY BOX. TECNAM P92-EM ECHO 13136 REPLACEMENT OF POROUS GRP FUEL REPLACEMENT WING TANKS FABRICATED FROM ALUMINIUM PER STANDARD AVIATION ROTAX 912-ULS CBUG (MODIFIED) TANKS WITH SHEET ALUMINIUM TANKS PRACTICES, APPLICANTS DRAWING SHOWS FABRICATION DETAILS. SIGHT TUBE ADDED AT ROOT END. TECNAM P92-EM ECHO 13409 HERCULES 6860325-S 68" X 60" INSTALLATION OF HERCULES 6860325-S 68 INCH DIAMETER X 60 INCH PITCH PROPELLER. ROTAX 912-ULS PGFG (MODIFIED) PROPELLER INSTALLATION. TEVERSON BISPORT 15316 SENSENICH 76EM8-0-60 76" X 60" INSTALLATION OF SENSENICH 76EM8-0-60 76 INCH DIAMETER X 60 INCH PITCH PROPELLER. LYCOMING IO-360-C1E6 CBGH PROPELLER INSTALLATION THORP T-18 13749 PROPELLER CHANGE TO AYMAR DEMUTH AYMAR DEMUTH 68" X 68" PROPELLER INSTALLED ON LYCOMING O-290-G4. LYCOMING O-290-G4 BSVN 2900 68" X 68" TIPSY NIPPER T.66 SERIES 2 12284 PROPELLER CHANGE TO LODGE CJL 147 CHANGE OF PROPELLER TO LODGE CJL 147 56 INCH DIA X 38 INCH PITCH JABIRU 2200A CCFE 56 X 38 TIPSY NIPPER T.66 SERIES 2 13004 REPLACEMENT OF U/C NIEMAN RINGS NIEMAN RINGS REPLACED BY 2 OFF 1080 STANDARD (NOT HD) BUNGEES, DOUBLE-WRAPPED JABIRU 2200A CCFE WITH 1080 BUNGEES RINGS SO THAT EACH LEG IS SUPPORTED BY FOUR CORDS OF BUNGEE. TIPSY NIPPER T.66 SERIES 2 13735 VW REVMASTER ENGINE AND HERCULES REVMASTER 2100D ENGINE RETROFITTED WITH STROMBERG CD150 CARBURETTOR AND REVMASTER R2100D NIPS 57352685 PROPELLER HERCULES PROPELLER. TWIN PUMPS AND FUEL PRESSURE REGULATOR FITTED. TIPSY NIPPER T.66 SERIES 2 13004 REPLACEMENT OF U/C NIEMAN RINGS NIEMAN RINGS REPLACED BY 2 OFF 1080 STANDARD (NOT HD) BUNGEES, DOUBLE-WRAPPED REVMASTER R2100D NIPS WITH 1080 BUNGEES RINGS SO THAT EACH LEG IS SUPPORTED BY FOUR CORDS OF BUNGEE. TIPSY NIPPER T.66 SERIES 2 13004 REPLACEMENT OF U/C NIEMAN RINGS NIEMAN RINGS REPLACED BY 2 OFF 1080 STANDARD (NOT HD) BUNGEES, DOUBLE-WRAPPED VW 1834 ARFV WITH 1080 BUNGEES RINGS SO THAT EACH LEG IS SUPPORTED BY FOUR CORDS OF BUNGEE. Prototype mods that have been approved since 1/1/2008 Page 99 30/11/20 LAA Technical Leaflet TL 3.17 TIPSY NIPPER T.66 SERIES 2 12549 HOPE BRAKE CONVERSION INSTALLATION OF HOPE BRAKES LTD DISC BRAKES WITH CALIPERS MOUNTED ON PURPOSE MADE VW 1834 ASZV BRACKETS WELDED TO AXLE AND BICYCLE TYPE BRAKE OPERATING LEVER MOUNTED TO CONTROL COLUMN. TIPSY NIPPER T.66 SERIES 2 14228 IGNITION SYSTEM REPLACEMENT OF MAGNETOS WITH TWIN LEBURG ELECTRONIC IGNITION SYSTEM, INCLUDING VW (PEACOCK) 1835 ARXN THE INSTALLATION OF A KUBOTA ALTERNATOR, TWO BATTERIES AND ASSOCIATED WIRING, CIRCUIT PROTECTION AND SWITCHING. TIPSY NIPPER T.66 SERIES 2 14746 INSTALLATION OF ELECTRICAL FUEL AUTOMOTIVE-TYPE FUEL SENDER MOUNTED ON REAR FACE OF FUEL TANK DRIVING GAUGE ON VW (PEACOCK) 1835 ARXN GAUGE & SENDER INSTRUMENT PANEL. TIPSY NIPPER T.66 SERIES 3 12631 ENGINE CHANGE TO VW 2180 INSTALLATION OF VW 2180 WITH GREAT PLAINS PARTS, INCLUDING 'FORCE 1' HUB AND A VW 2180 ONCS COMPRESSION RATIO OF 8:1, AND INSTALLATION OF STERBA 56" X 40" PROPELLER. TIPSY NIPPER T.66 SERIES 3 13861 BRAKE CONVERSION (HYDRAULIC) HYDRAULIC DISK BRAKES FITTED OPERATED BY HAND LEVER ON STICK GRIP VW 2180 ONCS TIPSY NIPPER T.66 SERIES 3 13004 REPLACEMENT OF U/C NIEMAN RINGS NIEMAN RINGS REPLACED BY 2 OFF 1080 STANDARD (NOT HD) BUNGEES, DOUBLE-WRAPPED VW 2180 ONCS WITH 1080 BUNGEES RINGS SO THAT EACH LEG IS SUPPORTED BY FOUR CORDS OF BUNGEE. TIPSY NIPPER T.66 SERIES 3 12922 NEWTON 21L E40 57" X 33" PROPELLER PROPELLER CHANGE TO NEWTON 21L E40 57 INCH DIAMETER X 33 INCH PITCH VW (PEACOCK) 1834 ENIE TIPSY NIPPER T.66 SERIES 3 13004 REPLACEMENT OF U/C NIEMAN RINGS NIEMAN RINGS REPLACED BY 2 OFF 1080 STANDARD (NOT HD) BUNGEES, DOUBLE-WRAPPED VW (PEACOCK) 1834 ENIE WITH 1080 BUNGEES RINGS SO THAT EACH LEG IS SUPPORTED BY FOUR CORDS OF BUNGEE. TIPSY NIPPER T.66 SERIES 3 14855 DUAL LEBURG IGNITION DUAL LEBURG IGNITION FITTED. INCLUDES FITTING TWO BATTERIES IN ASSOCIATED MOUNTINGS, VW (PEACOCK) 1834 ENIE ADJUSTMENT OF ENGINE MOUNTING, ALTERNATOR, REGULATOR/RECTIFIER, ASSOCIATED WIRING, CIRCUIT BREAKERS AND SWITCHES. TIPSY NIPPER T66 SERIES 2 12868 ARDEM 4C02 MK XI 1600 CC ENGINE INSTALLATION OF ROLLASON ARDEM MK XI 1600 CC ENGINE WITH LEGURGH IGNITION ARDEM 4CO2 MK XI ARBG INSTALLATION INTEGRATED WITH ORIGINALLY FITTED STAMO ENGINE MOUNT. (MODIFIED) TIPSY NIPPER T66 SERIES 2 13004 REPLACEMENT OF U/C NIEMAN RINGS NIEMAN RINGS REPLACED BY 2 OFF 1080 STANDARD (NOT HD) BUNGEES, DOUBLE-WRAPPED ARDEM 4CO2 MK XI ARBG WITH 1080 BUNGEES RINGS SO THAT EACH LEG IS SUPPORTED BY FOUR CORDS OF BUNGEE. (MODIFIED) TIPSY TRAINER 1 12325 PROPELLER CHANGE TO NEWTON COPY CHANGE OF PROPELLER TO NEWTON COPY OF FAIREY LA553 MADE USING BEECH INSTEAD OF WALTER MIKRON 2 AISA OF FAIREY LA553 MAHOGONY AS IN THE ORIGINAL PROPELLER. PROPELLER IS DESIGNATED A NEWTON 04L05 WITH A DIAMETER REDUCED TO 59.5" FROM AN INITIAL DIAMETER OF 61", AND A PITCH OF 45.6".

TIPSY TRAINER 1 14677 HERCULES 6536710-S 65" x 36" INSTALLATION OF HERCULES 6536710-S 65 INCH DIAMETER x 36 INCH PITCH PROPELLER. WALTER MIKRON 2 AISA PROPELLER INSTALLATION TITAN T-51 MUSTANG 14026 REPLICA GUNS ON T51 TITAN OPTIONAL DUMMY GUN BARRELS FITTED TO WING LEADING EDGES HONDA J35A6 CIFD TITAN T-51 MUSTANG 13028 PROPELLER CHANGE TO MTV-21-A/180- INSTALLATION OF MTV-21-A/180-05 2 BLADED PROPELLER USING JIHOSTROJ GOVERNOR ROTAX 912-ULS MUZY 05 TITAN T-51 MUSTANG 12890 CHANGING TITAN LIMIT SWITCHES UNLIKE THE UK FIRST OF TYPE G-MUZY, G-TSIM USES SUITABLY RATED HIGH POWER SUZUKI V6 MINI MERLIN TSIM MICROSWITCHES IN THE UNDERCARRIAGE CIRCUIT RATHER THAN LOW POWER MICROSWITCHES AND A SEMICONDUCTOR HIGH POWER SWITCH UNIT. TITAN T-51 MUSTANG 12891 FITTING ACCESS PANELS ACCESS PANELS AND ASSOCIATED DOUBLERS INTRODUCED INTO FUSELAGE SIDE SKINS TO ACCESS SUZUKI V6 MINI MERLIN TSIM HYDRAULIC MOTOR, BATTERY AND CONTROL SYSTEM COMPONENTS. TITAN T-51 MUSTANG 13109 APPLICATION TO FIT FACET RED TOP FACET RED TOP FUEL PUMP FITTED SUZUKI V6 MINI MERLIN TSIM FUEL PUMP TITAN T-51 MUSTANG 13561 RELOCATION OF AIRCRAFT BATTERY TO BATTERY RELOCATED TO FORWARD TURTLEDECK COMPARTMENT TO IMPROVE AIRCRAFT'S EMPTY SUZUKI V6 MINI MERLIN TSIM FORWARD LOCATION CG POSITION TITAN T-51 MUSTANG 14026 REPLICA GUNS ON T51 TITAN OPTIONAL DUMMY GUN BARRELS FITTED TO WING LEADING EDGES SUZUKI V6 MINI MERLIN TSIM TITAN T-51 MUSTANG 13891 RELOCATION OF FUEL PUMPS ELECTRIC FUEL PUMPS RELOCATED FROM FIREWALL TO WING MAIN SPAR IN WHEEL BAY AREA, TO SUZUKI V6 MINI MERLIN DHYS REDUCE HEAD OF FUEL FOR PRIMING PUMPS AND REDUCE TEMPERATURES TITAN T-51 MUSTANG 14954 MAIN LANDING GEAR TORQUE LINKS MACHINED ALUMINIUM ALLOY TORQUE LINKS MANUFACTURED REPLACING FOLDED AND WELDED SUZUKI V6 MINI MERLIN DHYS SHEET STEEL ORIGINALS AFTER OVERLOAD FAILURE OF ORIGINAL LINKS ON LANDING

TL 2000UK STING CARBON 13082 RELOCATION OF FACET ELECTRIC FUEL FACET PUMP RELOCATED TO COOL LOCATION IN COCKPIT AREA RATHER THAN INSIDE ENGINE ROTAX 912-ULS CGLJ PUMP COMPARTMENT WHERE VAPOUR LOCKING HAS BEEN EXPERIENCED DUE TO LOCAL HEATING OF FUEL SYSTEM

Prototype mods that have been approved since 1/1/2008 Page 100 30/11/20 LAA Technical Leaflet TL 3.17 TL 2000UK STING CARBON 13082 RELOCATION OF FACET ELECTRIC FUEL FACET PUMP RELOCATED TO COOL LOCATION IN COCKPIT AREA RATHER THAN INSIDE ENGINE ROTAX 912-ULS CGML PUMP COMPARTMENT WHERE VAPOUR LOCKING HAS BEEN EXPERIENCED DUE TO LOCAL HEATING OF FUEL SYSTEM TL 2000UK STING CARBON 13082 RELOCATION OF FACET ELECTRIC FUEL FACET PUMP RELOCATED TO COOL LOCATION IN COCKPIT AREA RATHER THAN INSIDE ENGINE ROTAX 912-ULS SACM PUMP COMPARTMENT WHERE VAPOUR LOCKING HAS BEEN EXPERIENCED DUE TO LOCAL HEATING OF FUEL SYSTEM TL 2000UK STING CARBON 13042 TRIO EZ PILOT WING LEVELLER FULL APPROVAL WITH SERVO NOW CONNECTED, APPROVED FOLLOWING SUCCESSFUL FLIGHT ROTAX 912-ULS CGPO TESTING. TL 2000UK STING CARBON 13066 NOSELEG AXLE BUSHING NOSELEG FORK HOLES FOR AXLE BORED OUT OVER-SIZE TO LINE UP HOLE CENTRELINES AND ROTAX 912-ULS STUN FITTED WITH 20MM DIAMETER, 17MM LONG MILD STEEL BUSHES TIG WELDED IN POSITION. TL 2000UK STING CARBON 13362 TRUTRAK ADI PILOT II DUAL AXIS AUTO INSTALLATION OF TRUTRAK ADI DUAL AXIS AUTO-PILOT IN ACCORDANCE WITH TL INSTRUCTIONS. ROTAX 912-ULS STUN PILOT INSTALLATION TL 2000UK STING CARBON 12878 CHANGE TO NOSEWHEEL FAIRING AFT SECTION OF FACTORY-SUPPLIED FAIRING SPLIT TO ENABLE REMOVAL WITHOUT DISMANTLING ROTAX 912-ULS STIN OTHER AIRCRAFT PARTS. FLANGE MOULDED ON ONE HALF OF SPILT USING 2 LAYERS OF 50MM GLASS TAPE AND EPOXY RESIN. SPEED NUTS MOULDED IN AT 75MM INTERVALS. ALUMINIUM STRIP RIVETED IN TO VERTICAL SECTION TO PROVIDE OVERLAP. TL-3000 SIRIUS 13862 PROPELLER CJHANGE TO TL-ULTRALIGHT . ROTAX 912-ULS CIAF POWERMAX TL-3000 SIRIUS 15252 REMOVAL OF BALLISTIC RECOVERY REMOVAL OF BALLISTIC PARACHUTE RECOVERY SYSTEM. INSTALLATION OF LEAD SHEET WEIGHT IN ROTAX 912-ULS CIAF SYSTEM PARACHUTE BOX TL2000 UK STING CARBON S4 14193 PROPELLER CHANGE TO POWERMAX POWERMAX ELECTRICAL CONSTANT SPEED PROPELLER FITTED 1748MM DIAMETER ROTAX 912-iS ZIZY 1748 DIA TRI KIS 14271 LYLE HENDRICKS MK3 NOSE LEG LYLE HENDRICKS MK 3 NOSELEG FITTED SIMILAR TO THAT PREVIOUSLY ACCEPTED BY PFA ON TRI-R CONTINENTAL IO-240-A1B BZDR ASSEMBLE COMPLETE KIS G-OKPW TRI KIS 13372 HERCULES 6474311-S 64" X 74" INSTALLATION OF HERCULES 6474311-S 64 INCH DIAMETER X 74 INCH PITCH PROPELLER. CONTINENTAL IO-240-B1B BVZD PROPELLER INSTALLATION TRI R-KIS 13365 HERCULES 6474311-S PROPELLER INSTALLATION OF HERCULES 6474311-S 64 INCH DIAMETER X 74 INCH PITCH PROPELLER. CONTINENTAL IOF-240-B OKMA INSTALLATION TSW-2 12747 PROPELLER CHANGE TO LODGE CJL 104 PROPELLER CHANGE TO LODGE CJL 104 74 INCH DIAMETER X 54 INCH PITCH. LYCOMING O-320-A1A BLPB 74" X 54" VANS RV-10 12551 HEATED PITOT/AOA DYNON HEATED PITOT HEAD MOUNTED ON UNDERSIDE OF PORT WING IN BAY OUTBOARD OF LYCOMING IO-540-D4A5 RVVY AILERON CRANK USING A SAFEAIR1 MAST. HEATER CONTROLLER MOUNTED ON AILERON INSPECTION PLATE. INCLUDES ASSOCIATED AIR LINES, WIRING AND CIRCUIT PROTECTION. VANS RV-10 12552 LIGHTING AND STROBE SYSTEM WHELEN LN SYS6 NAVIGATION AND STROBE LIGHT SYSTEM INSTALLED. THIS CONSISTS OF WINGTIP LYCOMING IO-540-D4A5 RVVY POSITION AND STROBE LIGHTS, TAIL LIGHT/STROBE, POWER SUPPLY PACK AND ASSOCIATED WIRING AND CIRCUIT PROTECTION. POWER PACK MOUNTED ON PORT SIDE OF REAR FUSELAGE USING VANS F10112-L BRACKET. VANS RV-10 12553 STATIC PORT SAFEAIR1 STATIC PORTS INSTALLED AS PER MANUFACTURER'S INSTRUCTIONS IN THE STANDARD LYCOMING IO-540-D4A5 RVVY RV-10 LOCATIONS. VANS RV-10 12554 DYNON SKYVIEW DUAL AXIS AUTO PILOT DYNON 2-AXIS AUTOPILOT SYSTEM INSTALLED, CONSISTING OF DYNON SV42 SERVOS ATTACHED LYCOMING IO-540-D4A5 RVVY TO THE STARBOARD AILERON BELLCRANK AND PITCH IDLER ARMS RESPECTIVELY, IN ACCORDANCE WITH THE DYNON INSTRUCTIONS. THESE ARE CONTROLLED BY A DYNON SKYVIEW EFIS. INCLUDES ASSOCIATED WIRING AND CIRCUIT PROTECTION. RAY ALLEN G07 STICK GRIPS ENABLE READY DISCONNECT OF THE AUTOPILOT SYSTEM.

SYSTEM PARAMETER SETTINGS ARE AS RECORDED IN FLIGHT TEST SCHEDULE LAA/FT-AP DATED 18/7/15. VANS RV-10 13044 BAGGAGE RESTRAINT ANCHOR POINTS INSTALLATION OF FOUR VANS SUPPLIED CA BAGGAGE TIE DOWN ATTACHMENT RINGS INTO THE LYCOMING IO-540-D4A5 RVVY INSTALLATION BAGGAGE BAY FLOOR.

Prototype mods that have been approved since 1/1/2008 Page 101 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-10 12417 FUEL FILTRATION AND VALVE STANDARD VANS FUEL VALVE REPLACED WITH ANDAIR FS20 EQUIVALENT. STANDARD VANS IN- LYCOMING IO-540-D4A5 RVVY LINE FUEL FILTER REPLACED WITH ANDAIR GASCOLATOR PN 375 AND RELOCATED FROM FLOOR OF CENTRAL TUNNEL TO WALL OF CENTRAL TUNNEL. VANS RV-10 13059 TRUTRACK DIGIFLIGHT IIVS DUAL AXIS INSTALLATION OF TRUTRAK DIGIFLIGHT IIVS DUAL AXIS AUTO-PILOT WITH ROLL SERVO INSTALLED LYCOMING IO-540-D4A5 CGJP AUTO-PILOT IN STARBOARD WING AND PUSH-ROD ATTACHED TO UPPER SURFACE OF SERVO ARM SO ALLOWING USE OF 0.35" LONG SPACER INSTEAD OF THE 0.89" LONG SPACER AS SUPPLIED WITH TRUTRAK INSTALLATION KIT. PITCH SERVO IS A CAPSTAN TYPE MOUNTED ON TRUTRAK BRACKET USING SHORT CABLE DRIVING FABRICATED PUSH-ROD ATTACHED TO PITCH CONTROL IDLER BELLCRANK. VANS RV-10 14084 GARMIN GAP-26 HEATED PITOT/AOA INSTALLATION OF GARMIN GAP-26 HEATED PITOT/AOA PROBE ON SAFEAIR1 MAST MOUNTED TO LYCOMING IO-540-D4A5 CGJP PROBE ON SAFEAIR1 MAST PORT WING UNDERSIDE OUTBOARD OF AILERON BELLCRANK ACCESS HOLE PER SAFEAIR1 AND GARMIN INSTRUCTIONS. VANS RV-10 14084 GARMIN GAP-26 HEATED PITOT/AOA INSTALLATION OF GARMIN GAP-26 HEATED PITOT/AOA PROBE ON SAFEAIR1 MAST MOUNTED TO LYCOMING IO-540-D4A5 TOPP PROBE ON SAFEAIR1 MAST PORT WING UNDERSIDE OUTBOARD OF AILERON BELLCRANK ACCESS HOLE PER SAFEAIR1 AND GARMIN INSTRUCTIONS. VANS RV-10 15249 GARMIN G3X AUTOPILOT INSTALLATION OF GARMIN DUAL AXIS AUTO-PILOT DRIVEN BY A GARMIN G3X EFIS UNIT AND LYCOMING IO-540-D4A5 TOPP CONTROLLED VIA A GARMIN GMC 307 INTERFACE. GARMIN GSA 28 SERVOS INSTALLED USING GARMIN MOUNTING HARDWARE IN ACCORDANCE WITH GARMIN DOCUMENT 190-01115-01 REV. AK VANS RV-10 12415 TRIO EZ PILOT INSTALLATION OF TRIO EZ PILOT. SERVO IS MOUNTED ON THE WING SPAR. INSTALLATION LYCOMING IO-540-V4A5D RVIO INCLUDES ELECTRICAL PROVISION, SERVO DISCONNECT BUTTON ON CONTROL STICK AND A WARNING LIGHT ON THE INSTRUMENT PANEL. INSTALLED AS PER MANUFACTURER'S INSTRUCTIONS, REV 2.3. VANS RV-10 12416 TRIO EZ ALTITUDE CONTROL INSTALLATION OF TRIO EZ ALTITUDE CONTROL SYSTEM. SERVO MOUNTED IN REAR FUSELAGE ON LYCOMING IO-540-V4A5D RVIO CUSTOM-MADE MOUNTING. INCORPORATES ASSOCIATED ELECTRICAL INSTALLATION, SERVO DISCONNECT SWITCH ON CONTROL STICK AND A WARNING LIGHT ON THE INSTRUMENT PANEL. INSTALLATION OTHERWISE AS PER MANUFACTURER'S INSTRUCTIONS.

VANS RV-10 12417 FUEL FILTRATION AND VALVE STANDARD VANS FUEL VALVE REPLACED WITH ANDAIR FS20 EQUIVALENT. STANDARD VANS IN- LYCOMING IO-540-V4A5D RVIO LINE FUEL FILTER REPLACED WITH ANDAIR GASCOLATOR PN 375 AND RELOCATED FROM FLOOR OF CENTRAL TUNNEL TO WALL OF CENTRAL TUNNEL. VANS RV-10 12418 CENTRAL CONSOLE VANS STANDARD GLOVE BOX AND PANEL SPACE FOR TWO MECHANICAL FUEL GAUGES PROVIDED LYCOMING IO-540-V4A5D RVIO BETWEEN CENTRE CONSOLE AND INSTRUMENT PANEL LOWER SURFACE. VANS RV-10 12419 PLENUM & COWL INSTALLATION OF JAMES COWL AND PLENUM. INSTALLED AS PER MANUFACTURER'S LYCOMING IO-540-V4A5D RVIO INSTRUCTIONS AND INCORPORATING ACCESS TO THE OIL FILLER. VANS RV-10 12420 LOW LEVEL FUEL SENSOR & FUEL TABS AIRCRAFT EXTRAS 'LOW FUEL WARNING SYSTEM' FITTED WITH AN OPTICAL SENSOR IN EACH TANK LYCOMING IO-540-V4A5D RVIO AND WARNING LIGHT FOR EACH ON INSTRUMENT PANEL. ALLOY TABS FITTED TO FUEL TANKS TO PROVIDE VISUAL INDICATION OF APPROX 2/3 FULL TANKS. VANS RV-10 13786 FALCON HEATED PITOT TUBE INSTALLATION OF FALCON HEATED PITOT TUBE MOUNTED WITH FALCON MOUNTING BRACKET TO LYCOMING IO-540-V4A5D RVIO INSTALLATION RV10 PORT WING UNDERSIDE OUTBOARD OF AILERON BELLCRANK ACCESS HOLE. VANS RV-10 13786 FALCON HEATED PITOT TUBE INSTALLATION OF FALCON HEATED PITOT TUBE MOUNTED WITH FALCON MOUNTING BRACKET TO LYCOMING YIO-540-D4A5 XRVX INSTALLATION RV10 PORT WING UNDERSIDE OUTBOARD OF AILERON BELLCRANK ACCESS HOLE. VANS RV-10 14819 INSTALL 2 AXIS AUTOPILOT TRUTRAK 2-AXIS AUTOPILOT FITTED. THIS CONSISTS OF A TRUTRAK PICTORIAL PILOT CONTROLLING LYCOMING YIO-540-D4A5 XRVX A TRUTRAK DSB-C SERVO MOUNTED IN THE STARBOARD WING, CONNECTED TO THE AILERON BELLCRANK, AND A TRUTRAK ALTRAK CONTROLLING A TRUTRAK DSP-C SERVO MOUNTED IN THE AFT FUSELAGE, CONNECTED TO THE ELEVATOR IDLER CRANK. INCLUDES ASSOCIATED SWITCHES, WIRING AND CIRCUIT PROTECTION. VANS RV-10 12569 LUGGAGE COMPARTMENT FORWARD INSTALLATION OF RESTRAINING HINGES TO PREVENT FORWARD MOVEMENT OF REAR SEAT BACKS LYCOMING YIO-540-D4A5 RRVX BULKHEAD RESTRAINT AND A BLANKING PANEL TO PREVENT SMALL ITEMS MOVING FORWARD UNDER CRASH LOAD CONDITIONS.

Prototype mods that have been approved since 1/1/2008 Page 102 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-10 12901 DYNON SKYVIEW AUTO PILOT INSTALLATION OF DYNON SKYVIEW AUTOPILOT INCORPORATING SV32 ROLL SERVO IN STARBOARD LYCOMING YIO-540-D4A5 RRVX WING AND SV42 PITCH SERVO IN FUSELAGE, USING DYNON-SUPPLIED MOUNTING HARDWARE, ASSOCIATED STICK-GRIP SWITCHES AND DYNON SKY VIEW EFIS UNIT.

VANS RV-10 12902 OVERHEAD CABIN CONSOLE INSTALLATION OF STEINAIR INC GFRP PANEL IN CABIN ROOF USING ARALDITE 2014-1 ADHESIVE. LYCOMING YIO-540-D4A5 RRVX

VANS RV-10 12903 MAIN WHEEL AXLE NUT EXTENSIONS INSTALLATION OF RIVETHEAD AXLE NUT EXTENSION AT EACH OUTBOARD MAIN WHEEL POSITION, LYCOMING YIO-540-D4A5 RRVX WITH CORRESPONDING CAPS MOULDED INTO EACH SPAT. VANS RV-10 12904 MATCO NOSE WHEEL AXLE ASSEMBLY FITMENT OF MATCO WHLAXLE24 NOSE WHEEL AXLE ASSEMBLY AND MATCO WHLA24SPKIT LYCOMING YIO-540-D4A5 RRVX SPACER KIT. VANS RV-10 12905 DOOR LATCH BLOCKS AND BOLTS REPLACE NYLON DOOR LATCH BLOCKS WITH ALUMINIUM ALLOY EQUIVALENTS (RIVETHEAD DRBLK- LYCOMING YIO-540-D4A5 RRVX 10). FIT DOME ENDED STAINLESS STEEL DOOR BOLT ENDS (WITH SENSOR MAGNETS). VANS RV-10 12906 DOOR LOCKS LOCK MECHANISM FITTED TO EACH CABIN DOOR TO PREVENT DOOR RELEASE HANDLE FROM LYCOMING YIO-540-D4A5 RRVX MOVING WHEN IN THE LOCKED POSITION. VANS RV-10 12931 HEATED PITOT HEAD AERO INSTRUMENT AN5812 ELECTRICALLY HEATED PITOT HEAD INSTALLED USING GRETZ AERO LYCOMING YIO-540-D4A5 RRVX MOUNTING BRACKET. UNIT INSTALLED ON PORT WING, 15 INCHES AFT OF WING LEADING EDGE AT A POSITION 57 INCHES INBOARD OF THE OUTER RIB. VANS RV-10 14831 INCORPORATION OF TWO ANDAIR FUEL ANDAIR FX375-M FUEL FILTER (1 PER SIDE) INCORPORATED IN FUEL SYSTEM BETWEEN FUEL TANK LYCOMING YIO-540-D4A5 RRVX FILTERS AND SELECTOR VALVE. ELEMENT FROM EXISTING FUEL FILTER (SAME PART NUMBER) REMOVED TO ALLOW FREE PASSAGE OF FUEL FROM SELECTOR TO ENGINE. VANS RV-10 14227 DYNON SKYVIEW AUTO-PILOT INSTALLATION OF DYNON SKYVIEW DUAL AXIS AUTO-PILOT WITH OPTIONAL SV-AP-PANEL. SERVOS LYCOMING YIO-540-D4A5 ORVX INSTALLATION ARE DYNON SV42 FOR ROLL FUNCTION AND SV42T FOR PITCH FUNCTION. VANS RV-10 14246 SHELF FOR ADAHRS UNITS SHELF FOR MOUNTING TWO ADAHRS UNITS FABRICATED FROM 0.032" ALLOY AND RIVETTED TO LYCOMING YIO-540-D4A5 ORVX THE UPPER FUSELAGE LONGERONS IN THE REAR FUSELAGE AFT OF FRAME F-1006A. VANS RV-10 14247 TWIN DYNON PITOTS IN WINGS INSTALLATION OF A DYNON PITOT/AOA HEAD, ONE HEATED, MOUNTED WITH A GRETZ MAST, TO LYCOMING YIO-540-D4A5 ORVX THE UNDERSIDE OF EACH WING PER GRETZ AERO INSTRUCTIONS. VANS RV-10 14252 ANDAIR FUEL VALVE AND FILTER ACCESS STANDARD VANS-SUPPLIED FUEL VALVE REPLACED WITH ANDAIR FS20 VALVE MOUNTED IN TOP LYCOMING YIO-540-D4A5 ORVX FLAP OF CENTRAL TUNNEL. AIRWARD 'RV-10 TUNNEL SCO' ACCESS PANEL MOUNTED TO PORT SIDE OF CENTRAL TUNNEL TO ALLOW ACCESS TO FUEL AND CONTROL SYSTEMS FOR MAINTENANCE. INSTALLED IN ACCORDANCE WITH AIRWARD INSTRUCTIONS. VANS RV-10 14666 SECOND ALTERNATOR & ASSOCIATED B&C SD-8 8 AMP SECONDARY ALTERNATOR INSTALLED ON ENGINE. INCLUDES ASSOCIATED LYCOMING YIO-540-D4A5 ORVX SWITCHES/WIRING BATTERY, SWITCHES, FUSES AND WIRING. VANS RV-10 13597 DYNON AUTO PILOT AND MOUNTING OF DYNON SV42 ROLL SERVO MOUNTED IN RIGHT HAND WING IN ACCORDANCE WITH LYCOMING YIO-540-D4A5 OMRC ADAHRS UNIT MANUFACTURER'S INSTRUCTIONS. DYNON SV42T PITCH SERVO MOUNTED IN REAR FUSELAGE CONNECTING TO ELEVATOR IDLER CRANK IN ACCORDANCE WITH MANUFACTURER'S INSTRUCTIONS. DYNON ADAHRS UNIT MOUNTED ON ALLOY SHELF MOUNTED JUST AFT OF BAGGAGE BAY, ATTACHED TO FUSELAGE LONGERONS AND STEADIED VIA A BRACKET CONNECTING ITS MID-SPAN TO THE CENTRAL STRUT OF THE BAGGAGE BAY AFT SUPPORT STRUCTURE. SERVOS CONTROLLED BY A DYNON SKYVIEW SVD1000 SYSTEM. DOUBLE THROW SWITCH FITTED TO SWITCH OFF ELECTRIC PITCH TRIM WHEN AUTO-PILOT IS SWITCHED ON. MOMENTARY PUSH BUTTON PITCH TRIM ENABLE SWITCH FITTED TO ALLOW PITCH TRIMMING WITH AUTO-PILOT ON.

VANS RV-10 13667 AIRWORLD STROBES/NAV LIGHTS AIRWORLD SKYFLASH POWER UNIT P/N 300300-2P MOUNTED ON ALLOY PLATE MOUNTED TO Z- LYCOMING YIO-540-D4A5 OMRC SECTION STRINGERS ON LEFT SIDE OF FUSELAGE FLOOR AFT OF BAGGAGE BAY. 302956 AND 302957 NAV/STROBE UNITS MOUNTED TO LEFT AND RIGHT WING TIPS RESPECTIVELY USING SELF- TAPING SCREWS INTO GFRP TIP, REINFORCED WITH AN EPOXY/FLOCK PLUG. VANS RV-10 15221 LANDING LIGHT ON BASE OF ENGINE INSTALLATION OF SMOOTH AVIATION SMOKER LANDING/TAXI/CONSPICUITY LIGHT ON BASE OF LYCOMING YIO-540-D4A5 OMRC COWL ENGINE COWL

Prototype mods that have been approved since 1/1/2008 Page 103 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-10 14324 DYNON HEATED AoA PITOT PROBE DYNON HEATED ANGLE OF ATTACK PITOT PROBE MOUNTED ON GRETZ MOUNT IN ACCORDANCE LYCOMING YIO-540-D4A5 MCLK WITH MANUFACTURERS' INSTRUCTIONS. INCLUDES ASSOCIATED WIRING, SWITCHING AND CIRCUIT PROTECTION. ANGLE OF ATTACK INFORMATION DISPLAYED ON DYNON SKYVIEW UNIT. VANS RV-10 14326 DYNON AUTOPILOT SYSTEM DYNON DUAL AXIS AUTOPILOT SYSTEM INSTALLED USING STANDARD DYNON SERVO BRACKETS LYCOMING YIO-540-D4A5 MCLK FOR THE TYPE IN THE WING AND AFT FUSELAGE. SYSTEM CONTROLLED BY A DYNON SKYVIEW UNIT WITH AUXILIARY SV-AP-PANEL. SYSTEM PROVIDES AUTOTRIM FUNCTIONALITY.

VANS RV-10 13023 FIBREGLASS WING FAIRINGS FIBREGLASS WING ROOT FILLET FAIRINGS MANUFACTURED BY SAINT AVIATION INSTALLED OVER LYCOMING YIO-540-D4A5 RVGO THE STANDARD METAL FAIRINGS. VANS RV-10 13041 INSTALLATION OF REAR NACA DUCTS INSTALLATION OF REAR NACA DUCTS TO IMPROVE CABIN VENTILATION. NACA DUCTS LYCOMING YIO-540-D4A5 RVGO FOR CABIN VENTILATION INTRODUCED TO FUSELAGE SIDEWALLS AFT OF BAGGAGE COMPARTMENT. DUCTING WITH SERVO CONTROLLED VALVE TO OUTLETS IN OVERHEAD CONSOLE IN THE REAR PASSENGER AREA. VANS RV-10 13298 180 DEGREE DOOR HANDLES 'PLANE AROUND' 180 DEGREE TURN DOOR LATCH SYSTEM WITH 3RD LATCH INSTALLED INSTEAD LYCOMING YIO-540-D4A5 RVGO OF VANS SECONDARY DOOR LATCH (SB 10-1-4). VANS RV-10 13655 ANGLE OF ATTACK SYSTEM FIT ADVANCED FLIGHT SYSTEM (AFS) ANGLE OF ATTACK SYSTEM. PRESSURE PORTS ADDED TO LYCOMING YIO-540-D4A5 RVGO PORT WING IN ACCORDANCE WITH MANUFACTURER'S INSTRUCTIONS. PRESSURE PORTS CONNECTED TO AF-4500 EFIS. VANS RV-10 13657 ADVANCED FLIGHT SYSTEM AUTOPILOT FIT ADVANCED FLIGHT SYSTEM (TRUTRAK) AUTOPILOT PROVIDING TWO-AXIS CONTROL. LYCOMING YIO-540-D4A5 RVGO INCORPORATES AUTOMATIC PITCH TRIM. INSTALLED IN ACCORDANCE WITH MANUFACTURER'S INSTRUCTIONS AND CONTROLLED USING AFS-4500 EFIS UNIT. VANS RV-10 13041 INSTALLATION OF REAR NACA DUCTS INSTALLATION OF REAR NACA DUCTS TO IMPROVE CABIN VENTILATION. NACA DUCTS LYCOMING YIO-540-D4A5 TENN FOR CABIN VENTILATION INTRODUCED TO PORT AND STARBOARD FUSELAGE SIDEWALLS AFT OF BAGGAGE COMPARTMENT. DUCTING WITH SERVO CONTROLLED VALVE TO OUTLETS IN OVERHEAD CONSOLE IN THE REAR PASSENGER AREA. VANS RV-10 14253 GARMIN G3X TOUCH DUAL AXIS AUTO- INSTALLATION OF GARMIN DUAL AXIS AUTO-PILOT DRIVEN BY A GARMIN G3X EFIS UNIT AND LYCOMING YIO-540-D4A5 TENN PILOT WITH GMC 307 CONTROL PANEL CONTROLLED VIA A GARMIN GMC 307 INTERFACE. GARMIN GSA 28 SERVOS INSTALLED USING INSTALLATION GARMIN MOUNTING HARDWARE IN ACCORDANCE WITH GARMIN DOCUMENT 190-01115-01 REV. U. VANS RV-12 12983 INSTALLATION OF MECHANICAL FUEL INSTALLATION OF ROCHESTER 05-16700 FLOAT ACTUATED MECHANICAL FUEL CONTENTS GAUGE ROTAX 912-ULS TWLV CONTENTS GAUGE INTO TOP OF FUEL TANK USING ASSOCIATED WELDED FITTING. VANS RV-12 12984 INSTALLATION OF FUEL DRAIN VALVE IN INSTALLATION OF A CAV110 SAF-AIR FUEL DRAIN VALVE INTO TANK OUTLET LINE VIA A.N. FITTINGS ROTAX 912-ULS TWLV TANK OUTLET LINE TEED OFF FROM FUEL OUTLET LINE. ACCESS TO DRAIN THROUGH HOLE IN PRE-EXISTING ACCESS PANEL. VANS RV-12 13255 RUDDER PEDAL EXTENSIONS INSTALLATION OF RUDDER PEDAL EXTENSIONS FOR SHORTER LEGGED PILOT. ROTAX 912-ULS TWLV VANS RV-12 13257 FAIRINGS FOR MAIN UNDERCARRIAGE INSTALLATION OF NON STRUCTURAL ABS PLASTIC FAIRINGS; ONE BETWEEN EACH MAIN ROTAX 912-ULS TWLV AND ENTRANCE STEP UNDERCARRIAGE LEG AND FUSELAGE SIDE, ONE BETWEEN EACH MAIN UNDERCARRIAGE LEG AND WHEEL SPAT AND ONE BETWEEN EACH STEP AND FUSELAGE SIDE. VANS RV-12 13033 WING LATCH INDICATOR ALTERNATIVE WING LATCH PIN INDICATOR USING MICROSWITCHES RATHER THAN ROTAX 912-ULS CGYI ELECTROMAGNETS AS SENSORS VANS RV-12 13218 MECHANICAL FUEL CONTENTS GUAGE INSTALLATION OF ROCHESTER 05-16700 FLOAT ACTUATED MECHANICAL FUEL CONTENTS GAUGE ROTAX 912-ULS RVIZ INTO TOP OF FUEL TANK USING ASSOCIATED WELDED FITTING. VANS RV-12 13222 INSTALLATION OF FUEL DRAIN VALVE IN INSTALLATION OF A CAV110 SAF-AIR FUEL DRAIN VALVE INTO TANK OUTLET LINE VIA A.N. FITTINGS ROTAX 912-ULS RVIZ TANK OUTLET LINE TEED OFF FROM FUEL OUTLET LINE. ACCESS TO DRAIN THROUGH HOLE IN PRE-EXISTING ACCESS PANEL. VANS RV-12 13033 WING LATCH INDICATOR ALTERNATIVE WING LATCH PIN INDICATOR USING MICROSWITCHES RATHER THAN ROTAX 912-ULS CHTI ELECTROMAGNETS AS SENSORS VANS RV-12 12984 INSTALLATION OF FUEL DRAIN VALVE IN INSTALLATION OF A CAV110 SAF-AIR FUEL DRAIN VALVE INTO TANK OUTLET LINE VIA A.N. FITTINGS ROTAX 912-ULS VRRV TANK OUTLET LINE TEED OFF FROM FUEL OUTLET LINE. ACCESS TO DRAIN THROUGH HOLE IN PRE-EXISTING ACCESS PANEL. Prototype mods that have been approved since 1/1/2008 Page 104 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-12 12984 INSTALLATION OF FUEL DRAIN VALVE IN INSTALLATION OF A CAV110 SAF-AIR FUEL DRAIN VALVE INTO TANK OUTLET LINE VIA A.N. FITTINGS ROTAX 912-ULS DOUZ TANK OUTLET LINE TEED OFF FROM FUEL OUTLET LINE. ACCESS TO DRAIN THROUGH HOLE IN PRE-EXISTING ACCESS PANEL. VANS RV-12 14794 INSTALLATION OF GARMIN G3X SYSTEM INSTALLATION OF VANS GARMIN DUAL SCREEN G3X EFIS OPTION WITH DUAL AXIS AUTOPILOT. ROTAX 912-ULS DOUZ & NEW INSTRUMENT PANEL ARRANGEMENT MODIFIED FROM STANDARD BY USING SINGLE-PIECE INSTRUMENT PANEL WITH SUB-PANEL, DELETION OF STANDARD VANS FUSE PANEL AND USE OF CIRCUIT BREAKERS. ARRANGEMENT INCORPORATES AUTOPILOT/TRIM MASTER SWITCH TO ALLOW RAPID ISOLATION OF THE PITCH TRIM SERVO MOTOR.

VANS RV-12 14795 INSTALLATION OF MAIN GEAR LEG AND INSTALLATION OF KNOTS2U CABIN STEP INTERFACE FAIRINGS. ROTAX 912-ULS DOUZ ENTRY STEP FAIRINGS INSTALLATION OF RVBITS MAIN GEAR TRANSITION FAIRINGS AT TOP AND BOTTOM OF EACH MAIN GEAR LEG, ALONG WITH VANS GEAR LEG FAIRINGS. VANS RV-12 15046 ON OFF SWITCH FOR AUX FUEL PUMP AN ADDITIONAL SWITCH IS MOUNTED ON THE INSTRUMENT PANEL TO ENABLE THE AUXILIARY ROTAX 912-ULS CKZH FUEL PUMP TO BE INDEPENDENTLY SWITCHED ON AND OFF. POH AMENDED TO REFLECT ADDITIONAL FUEL SYSTEM CONTROL. VANS RV-3 13814 FUEL TANK OUTLET PLUMBING MINOR AMENDMENT TO FUEL TANK OUTLET PLUMBING TO RELIEVE STRESS ON OUTLET FITTING LYCOMING O-235-F2B BVDC BOSS, AND PREVENT CRACKING IN TANK BASE AROUND BOSS. FP5 FUEL FLOWMETER INSTALLED.

VANS RV-4 13540 FIT REAR THROTTLE AND PROPELLER REAR THROTTLE AND RPM CONTROLS FITTED CONNECTED TO FRONT CONTROLS VIA PUSHRODS LYCOMING IO-360-B1B MAXV QUADRANT VANS RV-4 11909 SMOKE SYSTEM INSTALLATION OF SMOKE SYSTEM INCORPORATING OIL TANK AND PUMP ASSEMBLY FASTENED LYCOMING IO-360-B1B MAXV ONTO BAGGAGE BAY FLOOR VIA REMOVABLE ANGLE BRACKETS VANS RV-4 15023 WHIRLWIND 74HRT PROPELLER INSTALLATION OF WHIRLWIND 74HRT 3 BLADE 74 INCH DIAMETER CONSTANT SPEED PROPELLER LYCOMING IO-360-B1B MAXV INSTALLATION WITH JIHOSTROJ P-920 GOVERNOR. VANS RV-4 14723 SENSENICH 2G0M8/C72RG-5-0 INSTALLATION OF SENSENICH 2G0M8/C72RG-5-0 72 INCH DIAMETER LYCOMING IO-360-B4A RVDX PROPELLER INSTALLATION 2 COMPOSITE BLADED GROUND-ADJUSTABLE PROPELLER. (MODIFIED) VANS RV-4 13337 CATTO 3 BLADED 68" X 70" PROPELLER INSTALLATION OF CATTO 3 BLADED 68 INCH DIAMETER X 70 INCH PITCH PROPELLER. LYCOMING O-320-B2C RVNS VANS RV-4 14305 MT-V-11-C/183-59 PROPELLER INSTALLATION OF AN MT-V-11-C/183-59 PROPELLER. LYCOMING O-320-B2C RVNS INSTALLATION VANS RV-4 14623 FALCON HEATED PITOT PROBE FALCON HEATED PITOT PROBE MOUNTED TO GRETZ MAST INSTALLED IN SAME LOCATION AS VANS LYCOMING O-320-D1A RVJW MOUNTED TO GRETZ MAST STANDARD PITOT HEAD. INSTALLATION VANS RV-4 14624 LANDING LIGHT INSTALLATION INSTALLATION OF VANS LEADING EDGE LANDING LIGHT KIT LL DW-2 RV-4/6/7/8 IN STARBOARD LYCOMING O-320-D1A RVJW WING OUTBOARD BAY, EXCEPT 100W FILAMENT BULB LAMP SUBSTITUTED BY TELEDYNE 2307055- 1 ALPHABEAM LED LAMP. VANS RV-4 14625 POSITION/NAV/STROBE LIGHTS INSTALLATION OF AVEOFLASHLP LSA POSITION/NAV/STROBE LIGHTS TO WING TIPS. LYCOMING O-320-D1A RVJW INSTALLATION VANS RV-4 13893 REPLACEMENT OF CARBURETTOR WITH ORIGINAL MARVEL SCHLEBLER CARBURETOR REPLACED BY ROTEC TBI, FED BY RECIRCULATING LYCOMING O-320-D1A IKON ROTEC TBI FUEL SYSTEM VIA ANDAIR DUPLEX VALVE TO SELECTED TANK. FUEL PUMP COOLING AIR INCREASED AND HEAT SHIELD AND FLOW STRAIGHTENERS FITTED. VANS RV-4 14009 USE OF MOGAS AIRCRAFT MODIFIED TO ALLOW USE OF E5 MOGAS INCLUDING ADDITION OF VAPOUR RETURN LYCOMING O-320-D1A IKON LINE, TWIN ELECTRIC FUEL PUMPS INSTEAD OF SINGLE ELECTRIC PLUS MECHANICAL PUMP, ROTEC TBI SUBTITUTED VANS RV-4 14384 REPAIR TO REAR SPAR AT AILERON REINFORCEMENT BRACKET ADDED TO BACK UP REAR WING SPAR AT INBOARD AILERON HINGE LYCOMING O-320-D1A IKON BRACKET LOWER RIVETS POINT AT LOWER RIVET, DUE TO KNOWN CRAKING PROBLEM ON RV SERIES AIRCRAFT AT THIS POINT. AFTER TWO RIVETS CAME LOOSE IN SERVICE, AT ISSUE TWO OF THIS MOD THESE TWO RIVETS REPLACED WITH HILOC FASTENERS SEE AMENDED DRAWING ATTACHED. VANS RV-4 14385 SEAT BELT ANCHOR ADDITIONAL SEAT BELT ANCHORAGE POINTS FITTED FOR A BACK-UP HOOKER TYPE DUAL LAP LYCOMING O-320-D1A IKON STRAP IN FRONT SEAT POSITION COCKPIT

Prototype mods that have been approved since 1/1/2008 Page 105 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-4 14133 SMOKE SYSTEM SA-200 INSTALLATION SMOKING AIRPLANES SA-200 SMOKE SYSTEM INSTALLED AS PER MANUFACTURER'S LYCOMING O-320-D2A SPRX INSTRUCTIONS. THE 5.5 US GALLON SMOKE OIL TANK IS LOCATED ON FLOOR OF REAR LUGGAGE BAY AND IS ATTACHED TO THE FUSELAGE LONGERONS VIA ALUMINIUM ALLOY ANGLES ON FOUR SIDES AND A 2024-T3 REINFORCING/DOUBLER PLATE. THE TANK IS ATTACHED TO THE ANGLES USING THE SUPPLIED SCREWS; THE ANGLES ARE ATTACHED TO THE LONGERONS USING CHERRYMAX CR-3213-5 RIVETS. THE PUMP IS LOCATED AFT OF THE FIREWALL BETWEEN THE RUDDER PEDALS. AN INJECTOR NOZZLE ON EACH EXHAUST STACK INTRODUCES THE OIL INTO THE EXHAUST GASES. THE PUMP IS PROTECTED BY A 15 CIRCUIT BREAKER AND OPERATED BY A SWITCH ON THE INSTRUMENT PANEL AND A PUSH-BUTTON MOUNTED ON THE CONTROL STICK.

VANS RV-4 14560 EXTERNAL LED STRIPS INSTALLATION INSTALLATION OF MULTIPLE LED STRIPS TO FUSELAGE OUTER SURFACE ALIGNED LENGTHWISE, LYCOMING O-320-D2A SPRX CONTROLLED VIA 12 VOLT CONTROL UNIT AND SWITCHING RELAY MOUNTED BEHIND THE INSTRUMENT PANEL. VANS RV-4 14600 ADDITION OF REAR SEAT THROTTLE ADDITION OF REAR THROTTLE LEVER LINKED TO THE FRONT THROTTLE MECHANISM VIA A 3/16" LYCOMING O-320-D2A SPRX CONTROL STEEL PUSHROD AND FORK ATTACHMENT, SUPPORTED BY STRUCTURAL MEMBERS F405 AND F406.

VANS RV-4 14812 CATTO 3BRV67X68NLE-320 3 BLADED INSTALLATION OF CATTO 3BRV67X68NLE-320 3 BLADED PROPELLER WITH NICKEL LEADING EDGES. LYCOMING O-320-D2A SPRX PROPELLER INSTALLATION VANS RV-4 13545 SEALED PLENUM WITH CIRCULAR COWL COWL MODIFIED AND CUSTOM-BUILT PLENUM INTRODUCED TO PROVIDE IMPROVED COOLING. LYCOMING O-320-E2A BVLR AIR INTAKES UPPER REAR OF COWL FIXED USING SKYBOLT FASTENERS. (MODIFIED) VANS RV-4 13719 WHELAN STROBES AND POSITION LIGHTS WHELAN STROBES AND POSITION LIGHTS INSTALLED ON WING TIPS AND RUDDER. SYSTEM LYCOMING O-320-E2A BVLR CONSISTS OF A-413A-HDA-CF-14 POWER SUPPLY, A650PG-14 GREEN LIGHT AND STROBE, A650PR- (MODIFIED) 14 RED LIGHT AND STROBE, A555-14 WHITE TAIL POSITION LIGHT AND HD-60-1 INSTALLATION PACKAGE (VANS LN SYS1-B1). POWER SUPPLY FASTENED TO REAR FUSELAGE. VANS RV-4 14267 DUAL P-MAG 114 MODEL ELECTRONIC INSTALLATION OF TWO P-MAG 114 MODEL ELECTRONIC IGNITION UNITS AND EI COMMANDER LYCOMING O-320-E2A BVLR IGNITION UNITS INSTALLATION IGNITION MONITORING SYSTEM. (MODIFIED) VANS RV-4 14827 REAR THROTTLE CONTROL REAR THROTTLE QUADRANT ADDED LYCOMING O-320-E2B BOHW VANS RV-4 12566 PROPELLER CHANGE SENSENICH 70CMS16-0-79 PROPELLER FITTED. MAX RPM REDUCED TO 2600 AS REQUIRED BY LYCOMING O-320-E2C IIGI SENSENICH DATA VANS RV-4 13063 STRENGTHENED LOWER FIREWALL SKIN TWO 12" X 3/4" 26 GAUGE SS304 STAINLESS STEEL ANGLES RIVETTED TO LOWER FIREWALL SKIN LYCOMING O-320-E2C IIGI USING 23 OFF AN426AD3 COUNTERSUNK RIVETS ON EACH ANGLE. VANS RV-4 14095 WINGTIP PYROTECHNICS PIROTECHNICS FITTED TO STEEL FRAMES ATTACHED TO WING TIPS LYCOMING O-320-E2D SPRK MANDATORY COCKPIT PLACARD REQUIRED AS STATED IN LAA eMAIL DATED 20.4.16 STATING SPECIAL LIMITATIONS AND REQUIREMENTS VANS RV-4 14131 ROUTING OF WIRES THROUGH SPAR 1 INCH DIAMETER HOLE THROUGH BULKHEAD F-404 AND SPAR WEBS APPROXIMATELY 5" FROM LYCOMING O-320-E2D SPRK WEB STARBOARD FUSELAGE SIDE AND 4" ABOVE FLOOR, TO ACCOMMODATE WIRING LOOM. PLASTIC CONDUIT LOCATED IN HOLE, RETAINED WITH NUTS AND USING A PACKING PLATE TO ENSURE ALIGNMENT OF AFT NUT. VANS RV-4 14132 MICRO AERODYNAMICS VORTEX MICRO AERODYNAMICS INC MICRO KIT (RV) FITTED IN ACCORDANCE WITH LYCOMING O-320-E2D SPRK GENERATORS MANUFACTURER'S INSTRUCTIONS (INSTALLATION MANUAL MA2114 INITIAL RELEASE). 12 PAIRS OF VORTEX GENERATORS MOUNTED TO THE UPPER SURFACE OF EACH WING AND 6 PAIRS MOUNTED TO THE UNDER SURFACE OF THE TAILPLANE.

Prototype mods that have been approved since 1/1/2008 Page 106 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-4 14133 SMOKE SYSTEM SA-200 INSTALLATION SMOKING AIRPLANES SA-200 SMOKE SYSTEM INSTALLED AS PER MANUFACTURER'S LYCOMING O-320-E2D SPRK INSTRUCTIONS. THE 5.5 US GALLON SMOKE OIL TANK IS LOCATED ON FLOOR OF REAR LUGGAGE BAY AND IS ATTACHED TO THE FUSELAGE LONGERONS VIA ALUMINIUM ALLOY ANGLES ON FOUR SIDES AND A 2024-T3 REINFORCING/DOUBLER PLATE. THE TANK IS ATTACHED TO THE ANGLES USING THE SUPPLIED SCREWS; THE ANGLES ARE ATTACHED TO THE LONGERONS USING CHERRYMAX CR-3213-5 RIVETS. THE PUMP IS LOCATED AFT OF THE FIREWALL BETWEEN THE RUDDER PEDALS. AN INJECTOR NOZZLE ON EACH EXHAUST STACK INTRODUCES THE OIL INTO THE EXHAUST GASES. THE PUMP IS PROTECTED BY A 15 CIRCUIT BREAKER AND OPERATED BY A SWITCH ON THE INSTRUMENT PANEL AND A PUSH-BUTTON MOUNTED ON THE CONTROL STICK.

VANS RV-4 14142 DUAL P-MAGS INSTALLATION OF E-MAG P-114 ELECTRONIC IGNITION UNITS IN PLACE OF BOTH LEFT AND RIGHT LYCOMING O-320-E2D SPRK MAGNETOS. UNITS INSTALLED AS PER MANUFACTURER'S INSTRUCTIONS (INSTALLATION AND OPERATING GUIDE LC114.26), INCLUDING APPROPRIATE COOLING. VANS RV-4 14560 EXTERNAL LED STRIPS INSTALLATION INSTALLATION OF MULTIPLE LED STRIPS TO FUSELAGE OUTER SURFACE ALIGNED LENGTHWISE, LYCOMING O-320-E2D SPRK CONTROLLED VIA 12 VOLT CONTROL UNIT AND SWITCHING RELAY MOUNTED BEHIND THE INSTRUMENT PANEL. VANS RV-4 14811 CATTO 3BRV67X68NLE-320 3 BLADED INSTALLATION OF CATTO 3BRV67X68NLE-320 3 BLADED PROPELLER WITH NICKEL LEADING EDGES. LYCOMING O-320-E2D SPRK PROPELLER INSTALLATION VANS RV-4 12469 PROPELLER CHANGE TO SENSENICH CHANGE OF PROPELLER TO SENSENICH 70CM6S16-0-79, 70 INCH DIAMETER X 79 INCH PITCH. LYCOMING O-320-E3D BULG 70CM6S16-0-79 VANS RV-4 13099 PROPELLER CHANGE TO HERCULES HERCULES 7078267-S 70" x 78" PROP FITTED LYCOMING O-360-A1A CDJB VANS RV-4 13354 FT-60 FUEL FLOW TRANSDUCER FT-60 ('RED CUBE') FUEL FLOW TRANSDUCER INSERTED IN FUEL SYSTEM DOWN-STREAM OF THE LYCOMING O-360-A1A RVER FUEL VALVE, FILTER AND BOOST PUMP. MOUNTED IN THE FORWARD COCKPIT AREA. (MODIFIED) VANS RV-4 14418 APPROVAL OF NON STANDARD ITEMS . LYCOMING O-360-A1A RVER (MODIFIED) VANS RV-4 12951 FASTBACK FASTBACK FUSELAGE INCORPORATED USING HARMON ROCKET II PLANS. INCLUDES ALTERNATIVE LYCOMING AEIO-360-H1B RVIL TURTLE DECK ARRANGEMENT AND ROLL-OVER PROTECTION. VANS RV-4 14461 FLY BOY RV ROCKET STEERING LINK INSTALLATION OF RV ROCKET TAILWHEEL STEERING LINK P/N 1200. LYCOMING AEIO-360-H1B RVIL VANS RV-4 14462 JAMES AIRCRAFT PLENUM CHAMBER & INSTALLATION OF JAMES PLENUM CHAMBER AND COWL IN ACCORDANCE WITH LYCOMING AEIO-360-H1B RVIL COWL MANUFACTURER'S INSTRUCTIONS. VANS RV-4 14478 DUAL L114.27 MODEL P-MAGS INSTALLATION OF DUAL L114.27 MODEL P-MAGS TO LYCOMING AEIO-360-H1B ENGINE. LYCOMING AEIO-360-H1B RVIL INSTALLATION VANS RV-4 14586 WHIRLWIND 200RV 72" PROPELLER INSTALLATION OF WHIRLWIND 200RV 72 INCH DIAMETER CONSTANT SPEED PROPELLER USING LYCOMING AEIO-360-H1B RVIL INSTALLATION AERO TECHNOLOGIES PCU 5000 P/NATFS-58-1 FRONT MOUNTED CSU. VANS RV-4 13756 SMOKE SYSTEM INSTALLATION INSTALLATION OF SMOKING AIRPLANES SA101 SMOKE SYSTEM IN REAR BAGGAGE BAY. SUPERIOR XP-IO-360-B1A2 ORCA VANS RV-4 12395 INSTALLATION OF TRIO AVIONICS EZ1 INSTALLATION OF TRIO AVIONICS EZ1 AUTOPILOT USING THE SAFEAIR1 WING TIP INSTALLATION SUPERIOR XP-IO-360-B1C2 MUMY AUTOPILOT KIT INCLUDING AN ADDITIONAL BOLT IN EACH LOWER CORNER OF THE MOUNTING PLATE.

VANS RV-6 12985 PROPELLER CHANGE TO CATTO 3 BLADED INSTALLATION OF CATTO 3 BLADED 70 INCH DIAMETER X 75 INCH PITCH PROPELLER. LYCOMING IO-360-A2B NPKJ 70" X 75" VANS RV-6 11650 Engine Mount Modification 1.625" OD UNDERCARRIAGE LEG SOCKETS ON ENGINE MOUNT REPLACED BY 1.875" OD LYCOMING IO-360-A2B NPKJ UNDERCARRIAGE LEG SOCKETS.

WELDING TO BE CARRIED OUT BY CAA APPROVED WELDER, WITH DUE RECARD TO PRECAUTIONS WHEN WELDING THIN WALL TUBING TO THICK WALL TUBING.

ALL OTHER DETAILS ON ENGINE MOUNT REMAIN UNCHANGED.

AT ISSUE 2: MOUNT MAY OPTIONALLY ALSO BE MODIFIED TO INCLUDE GUSSET 'B' FROM MOD 11076.

Prototype mods that have been approved since 1/1/2008 Page 107 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-6 15171 INSTALLATION OF A SINGLE E-MAG P114 INSTALLATION OF AN E-MAGS P-114 MODEL ELECTRONIC IGNITION UNIT TO REPLACE STARBOARD LYCOMING IO-360-A2B NPKJ MODEL ELECTRONIC IGNITION UNIT MAGNETO.

VANS RV-6 11076 ENGINE MOUNT REINFORCEMENT TO ADD FOUR 0.125 INCH THICK 4130N GUSSETS TO RV6 ENGINE FRAME BY WELDING AS SHOWN LYCOMING O-320-B2B GLUC ON ASSOCIATED SKETCHES, INCLUDING QUALIFYING COMMENTS IN JOHN TEMPEST'S LETTER TITLED 'PFA MOD 11076 VANS RV-6 ENGINE MOUNT REINFORCEMENT'.

ISSUE 2 RAISED TO INCLUDE REPAIR TO CRACKS IN WELD BETWEEN LEG SOCKET AND MOUNTING FRAME IN ACCORDANCE WITH AC43.13-1B PARA 4-88 PRIOR TO INSTALLATION OF REINFORCEMENT GUSSETS. VANS RV-6 13933 DUAL E-MAG P-114 SERIES IGNITION INSTALLATION OF DUAL E-MAG P-114 IGNITION UNITS IN PLACE OF STANDARD MAGNETOS. LYCOMING O-320-B2C BVCG SYSTEM INSTALLATION VANS RV-6 12621 PROPELLER CHANGE TO WARNKE 68 X 74 PROPELLER CHANGE TO WARNKE 68 INCH DIAMETER X 74 INCH PITCH LYCOMING O-320-B2C KELL

VANS RV-6 14455 TRIO PRO PILOT AUTO-PILOT PITCH INSTALLATION OF TRIO PITCH SERVO IN ACCORDANCE WITH TRIO INSTRUCTIONS WITH AN LYCOMING O-320-B2C EYOR SERVO INSTALLATION ADDITIONAL SUPPORT BRACKET UNDER SERVO TRAY TO COMPLETE TRIO PRO PILOT DUAL AXIS AUTO-PILOT SYSTEM. VANS RV-6 15408 INCREASE LOADING LIMITATIONS MTWA INCREASE IN MTWA FROM 1600 LBS TO 1650 LBS ON RV-6 WHEN AIRCRAFT IS FITTED WITH RV-7 LYCOMING O-320-B2C EYOR TO 748 KG (1650 LB) STANDARD OF ENGINE/UNDERCARRIAGE MOUNT. VANS RV-6 11650 Engine Mount Modification 1.625" OD UNDERCARRIAGE LEG SOCKETS ON ENGINE MOUNT REPLACED BY 1.875" OD LYCOMING O-320-D1A RVIN UNDERCARRIAGE LEG SOCKETS.

WELDING TO BE CARRIED OUT BY CAA APPROVED WELDER, WITH DUE RECARD TO PRECAUTIONS WHEN WELDING THIN WALL TUBING TO THICK WALL TUBING.

ALL OTHER DETAILS ON ENGINE MOUNT REMAIN UNCHANGED.

AT ISSUE 2: MOUNT MAY OPTIONALLY ALSO BE MODIFIED TO INCLUDE GUSSET 'B' FROM MOD 11076. VANS RV-6 12462 SENSENICH 70CM7S9-0-80 PROPELLER ALTERNATIVE PROPELLER FITTED AS ABOVE. WITH THIS PROPELLER, WHICH IS A STANDARD VANS LYCOMING O-320-D1A GPAG FITTED OPTION, MAX PERMITTED RPM IS REDUCED TO 2600 VANS RV-6 14016 OWN DESIGN CENTRE CONSOLE CENTRE CONSOLE CONSTRUCTED FROM GFRP USED TO MOUNT THROTTLE, MIXTURE, FLAP AND LYCOMING O-320-D1A RVTE FUEL CONTROLS. VANS RV-6 14054 PROPRIETARY SOFTWARE SYSTEMS ANGLE OF ATTACK INDICATOR/WARNING SYSTEM INSTALLED, CONSISTING OF: PRESSURE PORTS LYCOMING O-320-D1A RVTE ANGLE OF ATTACK INDICATOR ON UPPER AND LOWER STARBOARD WING SURFACE, 'SPORT' COCKPIT INDICATOR, PROCESSOR UNIT, ASSOCIATED CONNECTION TUBES AND ELECTRICAL CONNECTORS. A SWITCH IS MOUNTED ON A CUSTOM-MADE BRACKET ATTACHED TO THE FUSELAGE BULKHEAD, ARRANGED SO THAT THE SWITCH IS ACTUATED AS THE FLAPS ARE LOWERED. INSTALLATION IN ACCORDANCE WITH MANUFACTURER'S INSTRUCTIONS.

VANS RV-6 14055 JP FS450 FUEL FLOW COMPUTER JP FS450 FUEL FLOW METER INSTALLED IN COCKPIT. JP 700900-1 (FXT-201) FUEL FLOW LYCOMING O-320-D1A RVTE TRANSDUCER MOUNTED ON BRACKET ON FORWARD FACE OF FIREWALL IN ACCORDANCE WITH MANUFACTURER'S INSTRUCTIONS. ASSOCIATED WIRES AND FUSE FITTED. VANS RV-6 11108 STALL WARNER REDDISH TYPE STALL WARNING INSTALLED IN ACCORDANCE WITH MANUFACTURER'S LYCOMING O-320-D1A CCJI INSTRUCTIONS. VANS RV-6 13565 RV-7 STYLE WING TIP FUEL TANKS MANUFACTURE OF WING TIP FUEL TANKS IN THE SHAPE OF RV-7 STYLE WING TIPS. EACH TIP TANK LYCOMING O-320-D1A CCJI HAS ITS OWN FILLER AND VENT TUBE AND A MAXIMUM CAPACITY OF 35 LITRES. FUEL FROM EACH TIP TANK FEEDS THE SAME WING'S MAIN FUEL TANK BY GRAVITY. A NON-RETURN VALVE IN THE LINE BETWEEN THE TANKS PREVENTS FUEL FROM GOING FROM THE MAIN TANK INTO THE TIP TANK.

Prototype mods that have been approved since 1/1/2008 Page 108 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-6 12860 TRUTAK DIGIFLIGHT II VS AUTO PILOT REPLACEMENT OF TRUTRAK DIGITRAK AUTO-PILOT CONTROL HEAD WITH TRUTRAK DIGIFLIGHT II LYCOMING O-320-D1A CCJI VS HEAD AND INSTALLATION OF PITCH SERVO. NOTE: ROLL SERVO PREVIOUSLY MOUNTED TO TRUTRAK BRACKETRY INSTALLED IN PORT WING ADJACENT TO AILERON BELLCRANK. VANS RV-6 14654 MTOW INCREASE MTWA INCREASED TO 818 Kg, (1800 Lbs), MAX LANDING WEIGHT OF 726 Kg (1600 Lbs) LYCOMING O-320-D1A GDRV INTRODUCED, WITH ADDITIONAL RESTRICTIONS ON FLIGHT AT MORE THAN 726 Kg. VANS RV-6 14689 NIGHT/IFR CLEARANCE . LYCOMING O-320-D1A GDRV VANS RV-6 14691 GARMIN G3X DUAL AXIS AUTO-PILOT INSTALLATION OF GARMIN G3X DUAL AXIS AUTO-PILOT USING GARMIN GDU460 WITH GARMIN LYCOMING O-320-D1A GDRV INSTALLATION GMC305 CONTROLLER AND GARMIN GSA28 SERVOS, IN PLACE OF TRUTRAK AUTO-PILOT. ORIGINAL SERVO MOUNTINGS AND CONTROL CONNECTIONS UTILISED. GARMIN G5 EFIS CONNECTED TO ACT AS BACK-UP CONTROLLER. VANS RV-6 14694 INSTRUMENTATION UPGRADE INSTALLATION OF GARMIN GDU460 WITH GARMIN G5 AS BACK-UP ASI, ALTIMETER AND . LYCOMING O-320-D1A GDRV INSTRUMENT PANEL SUPPORT MODIFIED TO ACCOMMODATE EFIS UNITS. EXISTING HEATED PITOT PROBE REPLACED WITH GARMIN GAP26 HEATED PITOT PROBE. VANS RV-6 12760 REPLACEMENT OF NAVAID WING INSTALLATION OF TRIO PRO PILOT DUAL AXIS AUTO-PILOT INCORPORATING EXISTING NAVAID LYCOMING O-320-D1A CDVT LEVELLER WITH TRIO PRO PILOT WING LEVELLER SERVO INSTALLATION. PITCH CONTROL SERVO INSTALLED ON PLATFORM ATTACHED TO SUPPORT STRUCTURE FOR PITCH SYSTEM IDLER BELLCRANK. VANS RV-6 14547 NAVIGATION AND STROBE LIGHTS INSTALLATION OF 'AVEO POWERBURST DAYLITE' NAVIGATION AND STROBE LIGHTS, P/NOS. AVE- LYCOMING O-320-D2B REVE INSTALLATION ON WING TIPS WPSTG-20D AND AVE-WPSTR-20D, TO WING TIPS MOUNTED ON CUSTOM MADE COMPOSITE MOUNTS PER APPLICANT'S SUBMISSION. VANS RV-6 14548 GARMIN G5 DUAL AXIS AUTO-PILOT INSTALLATION OF GARMIN G5 DUAL AXIS AUTO-PILOT WITH GMC 507 CONTROLLER INSTALLED IN LYCOMING O-320-D2B REVE INSTALLATION ACCORDANCE WITH GARMIN G5 INSTALLATION MANUAL 190-02072-01 REV. 2. GSA 28 ROLL SERVO INSTALLED USING MOUNTING KIT 011-02952-10. GSA 28 PITCH SERVO INSTALLED USING MOUNTING KIT 011-02952-14. VANS RV-6 14514 DYNON SKYVIEW DUAL AXIS AUTO-PILOT INSTALLATION OF DYNON SKYVIEW DUAL AXIS AUTO-PILOT WITH ROLL SERVO UNDER P2 SEAT LYCOMING O-320-D2J ORVI INSTALLATION THIGH SUPPORT IN ACCORDANCE WITH DYNON AUTO-PILOT SERVO INSTALLATION GUIDE RV6 ROLL DOCUMENT 101046-001 REV F AND PITCH SERVO INSTALLED IN ACCORDANCE WITH DYNON AUTO-PILOT SERVO INSTALLATION GUIDE RV6, RV7, RV9 PITCH DOCUMENT 101046-005 REV F.

VANS RV-6 15517 MAIN WHEEL TYRE SIZE INCREASE SLIGHTLY LARGER TYRES FITTED TO IMPROVE OPERATION FROM SOFT GROUND LYCOMING O-320-D2J NMRV 15 INCH DIAMETER TYRES FITTED TO MAIN WHEELS IN PLACE OF 13.5 INCH DIAMETER ORIGINALS

TYRE TYPE: AERO CLASSIC AA4AA 3-PART TYRE DESCRIPTOR: 15x6.00-5 TESTED INFLATION PRESSURE: 25 PSI

MAIN WHEEL SPATS NOT FITTED EXISTING MAIN WHEEL RIMS USED UNCHANGED

VANS RV-6 12896 CATTO 3 BLADED 68" X 70" PROPELLER CHANGE TO CATTO 3 BLADED 68 INCH DIAMETER X 70 INCH PITCH. LYCOMING O-320-E2A KELX VANS RV-6 12001 NAVAID AUTO-PILOT INSTALLATION OF NAVAID DEVICES WING LEVELLING AUTO-PILOT WITH SERVO FITTED UNDER P2 LYCOMING O-320-E2A KELX SEAT VANS RV-6 11076 ENGINE MOUNT REINFORCEMENT TO ADD FOUR 0.125 INCH THICK 4130N GUSSETS TO RV6 ENGINE FRAME BY WELDING AS SHOWN LYCOMING O-320-E2A KELX ON ASSOCIATED SKETCHES, INCLUDING QUALIFYING COMMENTS IN JOHN TEMPEST'S LETTER TITLED 'PFA MOD 11076 VANS RV-6 ENGINE MOUNT REINFORCEMENT'.

ISSUE 2 RAISED TO INCLUDE REPAIR TO CRACKS IN WELD BETWEEN LEG SOCKET AND MOUNTING FRAME IN ACCORDANCE WITH AC43.13-1B PARA 4-88 PRIOR TO INSTALLATION OF REINFORCEMENT GUSSETS. VANS RV-6 10432 FIT TRIO EZ-PILOT TO REPLACE NAVAID INSTALLATION OF TRIO EZ-PILOT CONTROL UNIT TO SUBSTITUTE NAVAID AP-1. NAVAID SERVO LYCOMING O-320-E2A RVIB DEVICES AP-1 AUTO-PILOT REMAINS. Prototype mods that have been approved since 1/1/2008 Page 109 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-6 12754 TRUTRAK ALTRAK VS ALTITUDE HOLD TRUTRAK ALTRAK VS ALTITUDE HOLD AUTO-PILOT WITH CLIMB AND DESCENT FUNCTION. LYCOMING O-320-E2A RVIB AUTO-PILOT VANS RV-6 12950 PROPELLER CHANGE TO CATTO 70" x 72" INSTALLATION OF CATTO 70 INCH DIAMETER X 72 INCH PITCH 2 BLADED PROPELLER. LYCOMING O-320-E2A RVIB

VANS RV-6 13964 FIT JOHANSON WING TIP FUEL TANKS JOHANSON WING TIP FUEL TANKS FITTED, PLUMBED TO FOUR WAY FUEL VALVE. LOW FUEL LYCOMING O-320-E2A RVIB WARNING ALERTS FITTED. COCKPIT PLACARD ADDED PROHIBITING USE OF TIP TANKS FOR TAKE OFF OR LANDING, AND PROHIBITING AEROBATICS WITH ANY FUEL IN THE TIP TANKS VANS RV-6 13433 HARTZELL C2YL-1BF/F7663-4 PROPELLER INSTALLATION OF HARTZELL C2YL-1BF/F7663-4 72 INCH DIAMETER HYDRAULIC CONSTANT SPEED LYCOMING O-320-E2A RVSE INSTALLATION. PROPELLER. VANS RV-6 13644 SMOKE SYSTEM INSTALLATION INSTALLATION OF SMOKE SYSTEM WITH SMOKE OIL TANK SITUATED IN BAGGAGE BAY BEHIND LYCOMING O-320-E2D JSRV PASSENGER SEAT, OIL PUMP BEHIND PILOT'S SEAT AND SOLENOID OIL CUT-OFF VALVE JUST AFT OF FIREWALL. VANS RV-6 14306 WHIRLWIND GA200L-716-72 PROPELLER INSTALLATION OF WHIRLWIND GA200L-716-72, 72 INCH DIAMETER GROUND ADJUSTABLE, 2 LYCOMING O-320-E2D JSRV INSTALLATION COMPOSITE BLADED PROPELLER WITH ALUMINIUM HUB. VANS RV-6 14117 ENGINE CHANGE TO LYCOMING O-320 ENGINE CHANGE TO LYCOMING 0-320-E2D MODIFIED BY FITTING FUEL PUMP (p/n 40295) AND LYCOMING O-320-E2D ORVE E2D ASSOCIATED ACCESSORY CASE, MAG DRIVE IDLER GEAR AND FUEL PUMP OPERATING PUSHROD. NO CHANGE TO COMPRESSION RATIO VANS RV-6 14514 DYNON SKYVIEW DUAL AXIS AUTO-PILOT INSTALLATION OF DYNON SKYVIEW DUAL AXIS AUTO-PILOT WITH ROLL SERVO UNDER P2 SEAT LYCOMING O-320-E3D BZWZ INSTALLATION THIGH SUPPORT IN ACCORDANCE WITH DYNON AUTO-PILOT SERVO INSTALLATION GUIDE RV6 ROLL DOCUMENT 101046-001 REV F AND PITCH SERVO INSTALLED IN ACCORDANCE WITH DYNON AUTO-PILOT SERVO INSTALLATION GUIDE RV6, RV7, RV9 PITCH DOCUMENT 101046-005 REV F.

VANS RV-6 11076 ENGINE MOUNT REINFORCEMENT TO ADD FOUR 0.125 INCH THICK 4130N GUSSETS TO RV6 ENGINE FRAME BY WELDING AS SHOWN LYCOMING O-320-E3D BZWZ ON ASSOCIATED SKETCHES, INCLUDING QUALIFYING COMMENTS IN JOHN TEMPEST'S LETTER TITLED 'PFA MOD 11076 VANS RV-6 ENGINE MOUNT REINFORCEMENT'.

ISSUE 2 RAISED TO INCLUDE REPAIR TO CRACKS IN WELD BETWEEN LEG SOCKET AND MOUNTING FRAME IN ACCORDANCE WITH AC43.13-1B PARA 4-88 PRIOR TO INSTALLATION OF REINFORCEMENT GUSSETS. VANS RV-6 12437 PROPELLER CHANGE PROPELLER CHANGE TO SENSENICH 70CM6S16-0-79 LYCOMING O-320-E3D TNGO VANS RV-6 14122 DYNON D10A DUAL AXIS AUTO-PILOT INSTALLATION OF DYNON D10A DUAL AXIS AUTO-PILOT. LYCOMING O-320-H2AD RRRV INSTALLATION DYNON SV32 ROLL SERVO INSTALLED UNDER LEFT SEAT THIGH SUPPORT STRUCTURE DRIVING BOTTOM OF P1 CONTROL COLUMN IN ACCORDANCE WITH DYNON SERVO MOUNTING INSTRUCTIONS - RV-6 FUSELAGE ROLL KIT 101046-001 REV D. DYNON SV32 PITCH SERVO INSTALLED IN REAR FUSELAGE DRIVING PITCH SYSTEM IDLER IN ACCORDANCE WITH DYNON SERVO MOUNTING INSTRUCTIONS - RV-6/7/9 PITCH KIT 101046-005 REV D. VANS RV-6 12335 PROPELLER CHANGE TO HARTZELL HC- CHANGE OF PROPELLER TO HARTZELL HC-C2YK-1BF LYCOMING O-360-A1A OTRV C2YK-1BF VANS RV-6 11650 Engine Mount Modification 1.625" OD UNDERCARRIAGE LEG SOCKETS ON ENGINE MOUNT REPLACED BY 1.875" OD LYCOMING O-360-A1A OTRV UNDERCARRIAGE LEG SOCKETS.

WELDING TO BE CARRIED OUT BY CAA APPROVED WELDER, WITH DUE RECARD TO PRECAUTIONS WHEN WELDING THIN WALL TUBING TO THICK WALL TUBING.

ALL OTHER DETAILS ON ENGINE MOUNT REMAIN UNCHANGED.

AT ISSUE 2: MOUNT MAY OPTIONALLY ALSO BE MODIFIED TO INCLUDE GUSSET 'B' FROM MOD 11076. VANS RV-6 12598 INSTALLATION OF TRUTRAK A/P & ROLL STANDARD INSTALLATION PER TRUTRAK MANUAL LYCOMING O-360-A1A OBUZ SERVO Prototype mods that have been approved since 1/1/2008 Page 110 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-6 12599 INSTALLATION OF DYNON AOA PITOT INSTALLED IN ACCORDANCE WITH DYNON AND SAFEAIR INSTRUCTIONS LYCOMING O-360-A1A OBUZ PROBE AND SAFEAIR MAST VANS RV-6 11687 MAIN UNDERCARRIAGE SOCKET ADDITIONAL BRACING TUBES ADDED TO ENGINE MOUNT TO STIFFEN ATTACHMENT OF MAIN LYCOMING O-360-A1A OBUZ BRACING GEAR LEG SOCKETS TO PREVENT CRACKING IN THIS VICINITY CAUSED BY REPEATED LANDING LOADS VANS RV-6 12851 PROPELLER CHANGE TO AYMAR- PROPELLER CHANGE TO AYMAR-DEMUTH 68 INCH DIAMETER X 78 INCH PITCH. LYCOMING O-360-A1D RVIT DEMUTH 68" X 78" VANS RV-6 12276 INSTALLATION OF 'BELL' TAILWHEEL INSTALLATION OF 'BELL' TAILWHEEL FORK TO INCREASE GROUND CLEARANCE OF FUSELAGE REAR LYCOMING O-360-A3A ORVG FORK IN ACCORDANCE WITH DRAWINGS STATED BELOW. VANS RV-6 12407 PROPELLER CHANGE TO SENSENICH CHANGE OF PROPELLER TO SENSENICH 72FM8S9-1(85). LYCOMING O-360-A4A RVCL 72FM8S9-1(85) VANS RV-6 13325 TRUTRAK DIGIFLIGHT IIVS DUAL AXIS INSTALLATION OF TRUTRAK DIGIFLIGHT IIVS DUAL AXIS AUTO-PILOT SYSTEM WITH ROLL SERVO LYCOMING O-360-A4A RVCL AUTO-PILOT INSTALLATION MOUNTED UNDER P2 SEAT THIGH SUPPORT AND PITCH SERVO MOUNTED TO BRACKET ATTACHED TO RIB ADJACENT TO PITCH IDLER BELLCRANK. VANS RV-6 13570 PROPELLER CHANGE CATTO 3 BLADED INSTALLATION OF CATTO 3 BLADED 68 INCH DIAMETER X 74 INCH PITCH PROPELLER. LYCOMING O-360-A4A RVCL 68" x 74" VANS RV-6 13467 STROBE ON VERTICAL STABILISER KUNTZLEMAN SC103 STROBE UNIT INSTALLED IN COMPOSITE FAIRING JUST AHEAD OF RUDDER LYCOMING YIO-320-D1A OPAR FAIRING HINGE LINE, WITH ASSOCIATED WIRING, FUSE AND SWITCH. VANS RV-6 14248 GARMIN G3X DUAL AXIS AUTO-PILOT INSTALLATION OF GARMIN G3X DUAL AXIS AUTO-PILOT WITH GMC 307 CONTROLLER AND GSA 28 LYCOMING YIO-320-D1A OPAR INSTALLATION SERVOS INSTALLED USING GARMIN MOUNTING KITS IN ACCORDANCE WITH GARMIN INSTALLATION MANUALS 011-02952-10 REV K (ROLL) AND 011-02952-11 REV K (PITCH). VANS RV-6 14249 RV-7 WING TIP FUEL TANKS MANUFACTURE AND INSTALLATION OF WING TIP FUEL TANKS IN THE SHAPE OF RV-7 STYLE WING LYCOMING YIO-320-D1A OPAR TIPS.

MODIFICATION APPROVAL DOES NOT INCLUDE AUTHORISATION FOR FUEL TO BE CARRIED IN TIP TANKS.

EACH TIP TANK HAS ITS OWN FILLER AND VENT TUBE AND A MAXIMUM CAPACITY OF 35 LITRES. FUEL FROM EACH TIP TANK FEEDS THE SAME WING'S MAIN FUEL TANK BY A DEDICATED ELECTRIC FUEL PUMP, TYPE FACET 40105, MANUALLY SWITCHED FROM THE COCKPIT. A NON-RETURN VALVE IN THE LINE BETWEEN THE TANKS PREVENTS FUEL FROM GOING FROM THE MAIN TANK INTO THE TIP TANK. A FLOAT SWITCH IS INSTALLED IN EACH TIP TANK WHICH TRIGGERS A RED INDICATOR LAMP WHEN ITS CONTENTS ARE NEARLY EXHAUSTED, OTHERWISE A GREEN LAMP IS ILLUMINATED.

VANS RV-6 13361 INSTALLATION OF ELECTRONICS ELECTRONICS INTERNATIONAL FT-60 FLOW TRANSDUCER FITTED DOWNSTREAM OF ELECTRIC FUEL LYCOMING YO-320-D1A CHFG INTERNATIONAL FT-60 FUEL FLOW PUMP AND FILTER. TRANSDUCER VANS RV-6 14156 SUPERIOR XP-IO-360-B1AC2 ENGINE AND INSTALLATION OF SUPERIOR XP-IO-360-B1AC2 ENGINE WITH HARTZELL HC-C2YK-1BF/F7666A-4 72 SUPERIOR XP-IO-320-B1AC2 BZVN HARTZELL HC-C2YK-1BF/F7666A-4 72 INCH DIAMETER PROPELLER. INCH DIAMETER PROPELLER INSTALLATIONS VANS RV-6 14924 TRUTRAK VIZION 385 AUTOPILOT TRUTRAK VISION 385 DUAL AXIS AUTOPILOT INSTALLED IN ACCORDANCE WITH THE SUPERIOR XP-IO-320-B1AC2 BZVN MANUFACTURER'S INSTRUCTIONS AND USING MANUFACTURER'S HARDWARE. ROLL SERVO INSTALLED BENEATH PASSENGER SEAT; PITCH SERVO INSTALLED IN AFT FUSELAGE.

Prototype mods that have been approved since 1/1/2008 Page 111 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-6 11575 RV/ROCKET TAILWHEEL STEERING LINK RV/ROCKET TAILWHEEL STEERING LINK FITTED BETWEEN STEERING ARMS ON RUDDER AND SUPERIOR XP-O-320-A1AC2 UNES TAILWHEEL.

INSTALLATION CARRIED OUT IN ACCORDANCE WITH INSTRUCTION SHEETS PROVIDED BY COMPONENT MANUFACTURER.

COMPONENT MANUFACTURER DETAILS ARE: TERRY JANTZI, PO BOX 20052, PIONEER PARK POSTAL OUTLET, KITCHENER, ON CADAN, N2P 2B4. VANS RV-6 12276 INSTALLATION OF 'BELL' TAILWHEEL INSTALLATION OF 'BELL' TAILWHEEL FORK TO INCREASE GROUND CLEARANCE OF FUSELAGE REAR SUPERIOR XP-O-320-A1AC2 UNES FORK IN ACCORDANCE WITH DRAWINGS STATED BELOW. VANS RV-6 12860 TRUTAK DIGIFLIGHT II VS AUTO PILOT REPLACEMENT OF TRUTRAK DIGITRAK AUTO-PILOT CONTROL HEAD WITH TRUTRAK DIGIFLIGHT II SUPERIOR XP-O-360-B1A2 PWUL VS HEAD AND INSTALLATION OF PITCH SERVO. NOTE: ROLL SERVO PREVIOUSLY MOUNTED TO TRUTRAK BRACKETRY INSTALLED IN PORT WING ADJACENT TO AILERON BELLCRANK. VANS RV-6 13847 SLIDING CANOPY FITMENT WITH VANS SLIDING CANOPY TRANSPARENCY BONDED IN PLACE USING SIKAFLEX 295 ADHESIVE IN SUPERIOR XP-IO-320-A3A2 DCOE ADHESIVE PLACE OF SCREWS. ALUMINIUM ALLOY 'SKIRTS' RETAINED FOR ADDITIONAL SECURITY. VANS RV-6A 13303 TRIO EZ PILOT AUTO-PILOT INSTALLATION OF TRIO EZ PILOT AUTO-PILOT (ROLL) INSTALLATION BY SUBSTITUTION OF NAVAID LYCOMING IO-320-D1A TOGO INSTALLATION AP1 SERVO WITH NAVAID SERVO ONTO EXISTING MOUNTING TRAY UNDER P2 SEAT THIGH SUPPORT. VANS RV-6A 12865 REPLACEMENT OF NAVAID WING INSTALLATION OF TRIO PRO PILOT DUAL AXIS AUTO-PILOT, THE ROLL SERVO BEING MOUNTED IN LYCOMING IO-320-D2A RVGA LEVELLER WITH TRIO PRO PILOT AUTO- AN IDENTICAL MANNER TO THE PREVIOUSLY INSTALLED NAVAID SERVO. PILOT PITCH SERVO MOUNTED ON TRIO TRAY ADJACENT TO PITCH IDLER IN FUSELAGE REAR. VANS RV-6A 13217 LIGHT SPEED PLASMA III CD IGNITION SUBSTITUTION OF RIGHT HAND SLICK MAGNETO WITH A LIGHT SPEED ENGINEERING PLASMA III LYCOMING IO-320-D2A RVGA RETROFIT CD ELECTRONIC IGNITION UNIT. VANS RV-6A 12279 TRUTRAK ALTRAK VS INSTALLATION OF TRUTRAK ALTRAK VS ACCORDING TO TRUTRAK INSTALLATION INSTRUCTIONS LYCOMING O-320-D1A CDAE

VANS RV-6A 14268 GRETZ PITOT MOUNT & DYNON PITOT DYNON UNHEATED PITOT/ANGLE OF ATTACK HEAD P/N 100141-000 MOUNTED ON GRETZ AERO LYCOMING O-320-D1A CBCP HEAD WITH AOA PORT CBK-12 PITOT MOUNT. THIS IS LOCATED ON THE UNDERSIDE OF THE PORT WING OUTBOARD OF THE INSPECTION HATCH, IN ACCORDANCE WITH THE MANUFACTURER'S INSTRUCTIONS. ANGLE OF ATTACK PORT CONNECTED TO DYNON D180 EFIS.

AT ISSUE 2, DYNON SKYVIEW UNIT ADDED AS ACCEPTABLE ALTERNATIVE ANGLE OF ATTACK DISPLAY/WARNING DEVICE.

VANS RV-6A 13281 TRUTRAK DIGIFLIGHT II VS AUTO PILOT TRUTRAK DIGIFLIGHT II VS DUAL AXIS AUTO-PILOT SYSTEM WHERE ROLL SERVO IS MOUNTED LYCOMING O-320-D2A RVNI UNDER P2 SEAT THIGH SUPPORT AND PITCH SERVO IS MOUNTED TO TRUTRAK BRACKET ADJACENT TO PITCH IDLER BELLCRANK. VANS RV-6A 14805 HEATED PITOT TUBE PIPER HEATED PITOT PROBE MOUNTED TO PORT WING FORWARD OF AILERON BELLCRANK LYCOMING O-320-D2J RKID INSPECTION HATCH. VANS RV-6A 12377 NOSEWHEEL MODIFICATION 5.00 x 5 NOSEWHEEL TYRE FITTED USING MODIFIED FORK AND SPAT PER BILL KNOTT LYCOMING O-320-D3G RVGC MODIFICATION ON G-RVSA. VANS RV-6A 12648 GROUND POWER SOCKET GROUND POWER SOCKET INSTALLED IN FUSELAGE SIDE IMMEDIATELY FORWARD OF FRAME F-602 LYCOMING O-320-D3G RVGC AND BELOW UPPER ON STARBOARD SIDE. VANS RV-6A 13035 INSTRUMENT PANEL AND ELECTRICAL INSTALLATION OF NEW INSTRUMENT PANEL WITH ADVANCED FLIGHT SYSTEMS AF4500 LARGE LYCOMING O-320-E2D CSPR SYSTEM UPGRADE DISPLAY EFIS AND UPGRADE TO ELECTRICAL SYSTEM. VANS RV-6A 13114 COWLING AIR EXIT LOUVRES INSTALLATION OF TWO GLOSTER AIR PARTS 4685 AFT EXITING LOUVRES IN THE LOWER COWLING LYCOMING O-320-E2D CSPR BOTTOM SURFACE, ONE EACH SIDE OF THE EXHAUST OUTLET BLISTER IN ACCORDANCE WITH DRAWINGS SKETCH 1 AND SKETCH 2 IN THE MODIFICATION APPLICATION, TO INCREASE AIR OUTFLOW FROM THE ENGINE COWLING. VANS RV-6A 13274 'ANTI-SPLAT' NOSE LEG STIFFENER INSTALLATION OF 'ANTI-SPLAT' NOSE LEG STIFFENER WITH ASSOCIATED NOSE LEG FAIRING. LYCOMING O-320-E2D CSPR

Prototype mods that have been approved since 1/1/2008 Page 112 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-6A 13300 TRUTRAK DIGIFLIGHT II VS DUAL AXIS INSTALLATION OF DIGIFLIGHT II VS DUAL AXIS AUTO-PILOT WITH ROLL SERVO INSTALLED UNDER LYCOMING O-320-E2D CSPR AUTO-PILOT STARBOARD SEAT THIGH SUPPORT IN ACCORDANCE WITH TRUTRAK RV-6 FUSELAGE ROLL INSTALLATION AND PITCH SERVO MOUNTED TO RIB THAT SUPPORTS THE PITCH SYSTEM IDLER BELLCRANK IN ACCORDANCE WITH RV-6, 7, 9 PITCH SERVO INSTALLATION. VANS RV-6A 14354 HERCULES 6876517-S 68" x 76" INSTALLATION OF HERCULES 6876517-S 68 INCH DIAMETER X 76 INCH PITCH PROPELLER LYCOMING O-320-E2D CSPR PROPELLER INSTALLATION VANS RV-6A 13292 TRIO/NAVAID AUTOPILOT/WING WING LEVELLER INSTALLATION WITH TRIO EZ WING LEVELLER WITH NAVAID DEVICES SERVO IN LYCOMING O-320-H2AD CGYO LEVELLER WING AILERON BELLCRANK ZONE VANS RV-6A 14802 ELECTRONIC IGNITION ELECTROAIR EIS-1 ELECTRONIC IGNITION SYSTEM REPLACING RIGHTHAND MAGNETO. LYCOMING O-360-A1A CKTF

AVOID CONTINUOUS OPERATION BETWEEN 2000 AND 2250 RPM. OPERATION ABOVE 2600 RPM IS LIMITED TO TAKEOFF. AS SOON AS PRACTICAL AFTER TAKEOFF THE RPM SHOULD BE REDUCED TO 2600 RPM OR LESS. THE PROPELLER BLADES ARE LIFE LIMITED AND MUST BE RETIRED UPON REACHING 8700 HOURS.

VANS RV-6A 14803 S-TEC 30 AUTOPILOT INSTALLATION OF S-TEC 30 DUAL AXIS AUTOPILOT SYSTEM, CONSISTING OF AN INSTRUMENT LYCOMING O-360-A1A CKTF PANEL MOUNTED CONTROL UNIT, A ROLL SERVO MOUNTED IN THE WING ATTACHED TO THE AILERON BELLCRANK, A CAPSTAN-TYPE PITCH SERVO MOUNTED ON A LOWER LONGERON IN THE AFT FUSELAGE AND ASSOCIATED MOUNTING BRACKETS AND ELECTRICAL CONNECTIONS. VANS RV-6A 14825 WING TIP TANKS FLYMORE WING TIP TANKS INSTALLED IN ACCORDANCE WITH MANUFACTURER'S INSTRUCTIONS. LYCOMING O-360-A1A CKTF NOTE THAT THIS MODIFICATION DOES NOT INCLUDE USING THESE TANKS TO CARRY FUEL. TANKS MUST REMAIN EMPTY AND ISOLATED FROM THE AIRCRAFT'S FUEL SYSTEM.

TANK FILLERS TO BE PLACARDED 'DO NOT USE'.

VANS RV-6A 13559 INSTALLATION OF DYNON HEATED INSTALLATION OF DYNON HEATED AOA/PITOT TUBE WITH GRETZ MOUNT AND MAST. LYCOMING O-360-A4M RVSA AOA/PITOT TUBE WITH GRETZ MOUNT AND MAST VANS RV-6A 14561 MGL DUAL AXIS AUTO-PILOT MGL DUAL AXIS AUTO-PILOT INSTALLATION WITH ROLL SERVO INSTALLED IN ACCORDANCE WITH LYCOMING O-360-A4M RVSA DYNON RV6 ROLL INSTRUCTIONS DOC 101046-001 REV F AND PITCH SERVO INSTALLED IN ACCORDANCE WITH DYNON RV6, RV7, RVP PITCH INSTRUCTIONS 101046-005 REV F. VANS RV-6A 14736 NIGHT/IFR CLEARANCE NIGHT IFR CLEARANCE LYCOMING O-360-A4M RVSA VANS RV-6A 14997 AVMAP ULTRA EFIS INSTALLATION OF AVMAP ULTRA EFIS AND SMARTPACK BATTERY BACKUP IAW MANUFACTURER'S LYCOMING O-360-A1AD RVSH INSTRUCTIONS. SOFTWARE FOR AVMAP IS 5.21.6C1 OR GREATER, PROVIDING BETTER READABILITY (MODIFIED) OF ASI AND ALT INFORMATION ON THE HSI PAGE. VANS RV-6A 13462 NAVAID AUTO-PILOT (ROLL) INSTALLATION OF NAVAID AP-1 WITH SERVO MOUNTED ON CUSTOM MADE TRAY IN STARBOARD SUPERIOR XP-IO-360-B1A2 CCVS INSTALLATION WING ADJACENT TO AILERON BELLCRANK. (MODIFIED) VANS RV-6A 13308 MODIFIED CENTRE CONSOLE EXISTING CENTRE CONSOLE MODIFIED TO ACCEPT VANS 'CT-83F DELUX' THROTTLE QUADRANT SUPERIOR XP-IO-360-B1AA2 RVIC WITH BRACKETS BEHIND PANEL TO ACCOMMODATE CABLE ATTACHMENTS. VANS RV-6A 13309 TRIO EZ PILOT AND EZ-3 AUTO-PILOT INSTALLATION OF TRIO EZ PILOT AUTO-PILOT (ROLL) SYSTEM USING CUSTOM BRACKET FOR SERVO SUPERIOR XP-IO-360-B1AA2 RVIC INSTALLATIONS AND TRIO EZ-3 AUTO-PILOT (PITCH) SYSTEM USING TRIO MOUNTING BRACKET FOR SERVO.

VANS RV-6A 14463 TRUTRAK VIZION 385 DUAL AXIS AUTO- TRUTRAK VIZION 385 DUAL AXIS AUTO-PILOT WITH AUTO-TRIM INSTALLATION. ROLL SYSTEM SUPERIOR XP-IO-360-B1AA2 RVIC PILOT INSTALLATION INSTALLED IN ACCORDANCE WITH RV-6 FUSELAGE ROLL INSTALLATION INSTRUCTIONS AND PITCH SYSTEM IN ACCORDANCE WITH RV-6,7,9 PITCH SERVO INSTALLATION INSTRUCTIONS.

VANS RV-6A 15349 CHANGE OF NOSE WHEEL TO BERINGER INSTALLATION OF BERINGER RA-015(A) WHEEL ASSEMBLY, ASSOCIATED AXLE AND SPACER, AND SUPERIOR XP-IO-360-B1AA2 RVIC PAC01 11X4.00X5" TYRE IN PLACE OF STANDARD VANS ITEMS.

Prototype mods that have been approved since 1/1/2008 Page 113 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-6A 14430 DYNON D10A AUTO-PILOT WITH AP74 INSTALLATION OF DYNON DUAL AXIS AUTO-PILOT WITH AN AP74 CONTROLLER. SUPERIOR XP-O-360-B1A2 OMDB CONTROLLER INSTALLATION ROLL SERVO INSTALLED UNDER P1 SEAT ACCORDING TO DYNON INSTRUCTIONS IN DOCUMENT 101046-001 REVISION F. PITCH SERVO INSTALLED IN FUSELAGE REAR IN ACCORDANCE WITH DYNON INSTRUCTIONS IN DOCUMENT 101046-005 REVISION F. VANS RV-6A 12288 INSTRUMENT PANEL SEGMENTED PANEL FITTED SUPERIOR XP-IO-320-B1XC2 TJDM VANS RV-6A 12289 CANOPY FIXING CANOPY BONDED RATHER THAN RIVETED/BOLTED IN PLACE SUPERIOR XP-IO-320-B1XC2 TJDM VANS RV-6A 12290 RV-7 WING TIPS INSTALLATION ALTERNATIVE RV-7 WING TIPS (W-715) SUBSTITUTED SUPERIOR XP-IO-320-B1XC2 TJDM VANS RV-6A 12291 ENGINE PLENUM TOP AND COWLING PLENUM CHANGED TO EXTERNAL TYPE RATHER THAN INTEGRAL SUPERIOR XP-IO-320-B1XC2 TJDM VANS RV-6A 12292 FUEL FLOW TRANDUCER FLOSCA201 FUEL FLOW TRANSDUCER INSTALLED SUPERIOR XP-IO-320-B1XC2 TJDM VANS RV-6A 12293 STROBE LIGHTS SKYFLASH TWIN HEAD STROBE LIGHT SYSTEM FITTED SUPERIOR XP-IO-320-B1XC2 TJDM VANS RV-6A 12294 MODIFIED STEP INSTALLATION STEP INSTALLED IN A NEATER FASHION SUPERIOR XP-IO-320-B1XC2 TJDM VANS RV-6A 12295 STALL WARNER ELECTRICAL STALL WARNER FITTED SUPERIOR XP-IO-320-B1XC2 TJDM VANS RV-6A 13728 ENGINE CHANGE TO SUPERIOR XP-IO-320-ENGINE CHANGED TO SUPERIOR IO-320-B1XC2 WITH DUAL P MAG IGNITION SUPERIOR XP-IO-320-B1XC2 TJDM B1XC2 VANS RV-7 14110 ELECTRONIC IGNITION STANDARD MAGNETOS REPLACED WITH A LIGHTSPEED PLASMA III ELECTRONIC IGNITION ON ONE ECI TITAN DIOX-370- TERO SIDE AND A E-MAG P-114 ELECTRONIC IGNITION ON THE OTHER SIDE. LIGHTSPEED CONTROL A4L2T MODULE MOUNTED ON CUSTOM BRACKETS IN THE AVIONICS BAY. BOTH UNITS FITTED IN ACCORDANCE WITH THE MANUFACTURERS' INSTRUCTIONS. VANS RV-7 14111 PNEUMATIC TAIL WHEEL ANDAIR WH7 TAILWHEEL INSTALLED IN PLACE OF STANDARD VANS TAILWHEEL. MOUNTED ON A ECI TITAN DIOX-370- TERO JD AIRPARTS TAILWHEEL FORK AND USING JD AIRPARTS TAILWHEEL YOKE AND TAILWHEEL A4L2T STEERING LINK. VANS RV-7 15255 GRETZ GA-1000 PITOT HEAD ON GRETZ GA-1000 HEATED PITOT TUBE MOUNTED ON GRETZ MAST FITTED IN ACCORDANCE WITH ECI TITAN IOX-370- CKTX MAST MANUFACTURER'S INSTRUCTIONS ON PORT WING. ADD7T8 VANS RV-7 13999 B&C SD-8 STANDBY ALTERNATOR INSTALLATION OF A B&C SD-8 ALTERNATOR FITTED TO VACUUM PUMP PAD WITH PMR1C ECI TITAN IOX-370- CKTX INSTALLATION VOLTAGE REGULATOR ADD7T8 VANS RV-7 14507 GARMIN DUAL AXIS AUTO-PILOT INSTALLATION OF GARMIN DUAL AXIS AUTO-PILOT WITH GARMIN G3X TOUCH AND GNC 307 ECI TITAN IOX-370- CKTX INSTALLATION INTERFACE ADD7T8 VANS RV-7 11575 RV/ROCKET TAILWHEEL STEERING LINK RV/ROCKET TAILWHEEL STEERING LINK FITTED BETWEEN STEERING ARMS ON RUDDER AND LYCOMING AEIO-320-D1B CDYZ TAILWHEEL.

INSTALLATION CARRIED OUT IN ACCORDANCE WITH INSTRUCTION SHEETS PROVIDED BY COMPONENT MANUFACTURER.

COMPONENT MANUFACTURER DETAILS ARE: TERRY JANTZI, PO BOX 20052, PIONEER PARK POSTAL OUTLET, KITCHENER, ON CADAN, N2P 2B4. VANS RV-7 12276 INSTALLATION OF 'BELL' TAILWHEEL INSTALLATION OF 'BELL' TAILWHEEL FORK TO INCREASE GROUND CLEARANCE OF FUSELAGE REAR LYCOMING AEIO-320-D1B CDYZ FORK IN ACCORDANCE WITH DRAWINGS STATED BELOW. VANS RV-7 12369 TIP TANKS CL GF4 RV FUEL TIP-TANKS MANUFACTURED BY FLYMORE PTY, AUSTRALIA, INSTALLED IN ACCORDANCE WITH LYCOMING AEIO-360-A1B6 IIXF COMPONENT MANUFACTURER'S INSTRUCTIONS. VANS RV-7 12370 RUDDER CABLE AND HORN FAIRING CARBON FIBRE FAIRINGS FOR RUDDER CABLE (1 EACH SIDE) WHERE IT EXITS FUSELAGE TO RUDDER LYCOMING AEIO-360-A1B6 IIXF HORN. ATTACHED TO FUSELAGE USING SIKAFLEX ADHESIVE. VANS RV-7 12371 HARTZELL HC-C2YR-1BFP/F7497-2 HARTZELL HC-C2YR-1BFP/F7497-2 PROPELLER FITTED. LYCOMING AEIO-360-A1B6 IIXF PROPELLER VANS RV-7 12372 ORIGINAL DESIGN RUDDER ORIGINAL DESIGN OF RV-7 RUDDER INCORPORATED, RATHER THAN LATER, LARGER AREA RV-9 LYCOMING AEIO-360-A1B6 IIXF TYPE. VANS RV-7 12373 CARBON FIBRE ENGINE COVER MOULDED CARBON FIBRE ENGINE COOLING PLENUM FITTED. LYCOMING AEIO-360-A1B6 IIXF VANS RV-7 12374 ENGINE COWL FRONT FIXING MOULDED FRONT COWL CUFFS FITTED TO RETAIN COWL RETAINING PINS. CUFFS RETAINED BY LYCOMING AEIO-360-A1B6 IIXF SCREWS INTO ANCHOR NUTS. VANS RV-7 12375 TAIL WHEEL STEERING LINKAGE SILVER BULLET DIRECT TAILWHEEL STEERING LINK. LYCOMING AEIO-360-A1B6 IIXF

Prototype mods that have been approved since 1/1/2008 Page 114 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-7 12426 BLUE MOUNTAIN AVIONICS AUTOPILOT BLUE MOUNTAIN AUTOPILOT SYSTEM (PITCH AND ROLL CONTROL) LYCOMING AEIO-360-A1B6 IIXF SYSTEM VANS RV-7 12506 LONG RANGE FUEL SYSTEM AS PER G- LONG RANGE FUEL TANK INSTALLED IN PASSENGER SEAT, WITH ASSOCIATED SYSTEMS. INCREASE LYCOMING AEIO-360-A1B6 IIXF GDRV IN MAXIMUM TAKE-OFF WEIGHT TO 2000 LBS (MAXIMUM LANDING WEIGHT REMAINS 1800 LBS).

VANS RV-7 12774 INSTALLATION OF G900X EFIS GARMIN G900X EFIS INSTALLED. INSTRUMENT PANEL SUB-STRUCTURE MODIFIED TO LYCOMING AEIO-360-A1B6 IIXF ACCOMMODATE UNIT. VANS RV-7 12045 DIGIFLIGHT II AUTOPILOT INSTALLATION OF TRUTRAK DIGIFLIGHT II DUAL AXIS AUTO PILOT ACCORDING TO VANS APPROVED LYCOMING AEIO-360-A1B6 IIXF INSTRUCTIONS PROVIDED BY TRUTRAK VANS RV-7 14774 HARTZELL HC-G2YR-1WX/N7605W-2X INSTALLATION OF HARTZELL HC-G2YR-1WX/N7605W-2X 74 INCH DIAMETER CONSTANT SPEED LYCOMING AEIO-360-A1B6 IIXF 74" DIAMETER PROPELLER INSTALLATION PROPELLER

VANS RV-7 12737 THROTTLE QUADRANT ANDAIR TQ1 THROTTLE QUADRANT INSTALLED. LYCOMING AEIO-360-A1B6 RVTT VANS RV-7 12738 SAM JAMES COWLING SAM JAMES ENGINE COWLING INSTALLED, INCLUDING INTERNAL PLENUM. LYCOMING AEIO-360-A1B6 RVTT VANS RV-7 13983 DYNON HEATED AOA/PITOT HEAD ON INSTALLATION OF DYNON HEATED AOA/PITOT PROBE MOUNTED ON GRETZ MAST. LYCOMING AEIO-360-A1B6 RVTT GRETZ MAST INSTALLATION VANS RV-7 13999 B&C SD-8 STANDBY ALTERNATOR INSTALLATION OF A B&C SD-8 ALTERNATOR FITTED TO VACUUM PUMP PAD WITH PMR1C LYCOMING AEIO-360-A1B6 RVTT INSTALLATION VOLTAGE REGULATOR VANS RV-7 14292 ANDAIR FS20 TYPE 5 FUEL VALVE INSTALLATION OF AN ANDAIR FS20 TYPE 5, 4-WAY FUEL SELECTOR VALVE TO ALLOW SELECTION OF LYCOMING AEIO-360-A1B6 RVTT INSTALLATION LEFT, RIGHT AND AUXILIARY FUEL TANKS AND OFF. BLANKING CAP TO BE FITTED WHEN AUXILIARY TANK IS REMOVED. VANS RV-7 14293 AUXILIARY FUEL TANK AUXILIARY FUEL TANK DESIGNED BY FRAZER NASH CONSULTANCY LIMITED INSTALLED IN LYCOMING AEIO-360-A1B6 RVTT PASSENGER SEAT FOR LONG-DISTANCE FLYING. VANS RV-7 14501 TRUTRAK AUTOMATIC PITCH TRIM TRUTRAK AUTOMATIC TRIM MODULE INSTALLED UNDER AND CONNECTED TO AUTO-PILOT PITCH LYCOMING AEIO-360-A1B6 RVTT INSTALLATION SERVO AND IN ACCORDANCE WITH TRUTRAK INSTALLATION MANUAL 8300-013 REV G. VANS RV-7 14070 AFS AF-PILOT DUAL AXIS AUTO-PILOT INSTALLATION OF TRUTRAK AFS AF-PILOT DUAL AXIS AUTO-PILOT, INSTALLED IN ACCORDANCE LYCOMING AEIO-360-A1B6 RVTT INSTALLATION WITH TRUTRAK DRG NO. RV-7, 10 ROLL SERVO, RV-7, 10 RIGHT WING AND DRG NO RV-6 PITCH, RV- 6,7,9 PITCH SERVO INSTALLATION. VANS RV-7 12494 CROTCH STRAP KIT INSTALLATION OF VANS CROTCH STRAP 5TH ATTACHMENT POINT IN ACCORDANCE WITH THE LYCOMING AEIO-360-A1B6 RVAB VANS INSTRUCTIONS 'OP24 RV-7,9 CROTCH STRAP INSTALL.DOC 8/8/01'. VANS RV-7 12495 TRUTRAK DIGIFLIGHT II VS AUTOPILOT AUTOPILOT INSTALLED AS PER MANUFACTURER'S INSTRUCTIONS. LYCOMING AEIO-360-A1B6 RVAB VANS RV-7 12877 BELL TAILWHEEL FORK AND VANS INSTALL BELL TAILWHEEL FORK AND VANS 'U TAIL LYNX' DELUXE TAILWHEEL SPRING SET, IN LYCOMING AEIO-360-A1B6 RVAB DELUXE TAILWHEEL ACCORDANCE WITH THE MANUFACTURER'S INSTRUCTIONS. VANS RV-7 12283 TIP-UP INSTRUMENT PANEL SUPPORT INSTRUMENT PANEL ALTERED PER APPLICANT'S APPLICATION TO ENABLE EFIS PANELS TO BE LYCOMING AEIO-360-A1B6 MRVL WITH EFIS SCREENS FITTED. EXISTING RIBS F745 L/R SHORETENED AND REPLACED WITH FOUR RIBS PLACED SYMETRICALLY EITHER SIDE OF SCREENS VANS RV-7 12893 DELRIN (ACETAL) AILERON STOP PLASTIC STOPS FITTED TO AVOID METAL TO METAL CONTACT, PER APLICANT'S DRAWINGS AND LYCOMING AEIO-360-A1B6 MRVL TESTS. VANS RV-7 14070 AFS AF-PILOT DUAL AXIS AUTO-PILOT INSTALLATION OF TRUTRAK AFS AF-PILOT DUAL AXIS AUTO-PILOT, INSTALLED IN ACCORDANCE LYCOMING AEIO-360-A1B6 MRVL INSTALLATION WITH TRUTRAK DRG NO. RV-7, 10 ROLL SERVO, RV-7, 10 RIGHT WING AND DRG NO RV-6 PITCH, RV- 6,7,9 PITCH SERVO INSTALLATION. VANS RV-7 13489 COWLING FASTENERS REMOVAL OF TOP ENGINE COWLING FACILITATED BY REPLACING STANDARD VANS PIANO HINGE LYCOMING AEIO-360-B2F DVMI JOINTS BETWEEN UPPER AND LOWER COWLINGS AND BETWEEN UPPER COWLING AND FUSELAGE WITH ALUMINIUM ALLOY STRIPS AND ANCHOR NUTS. VANS RV-7 12540 DYNON PITOT PROBE MOUNTED WITH INSTALLATION OF DYNON PITOT/STATIC/AOA PROBE USING GRETZ MOUNTING BRACKET KIT. LYCOMING AEIO-360-B2F DVMI GRETZ MAST VANS RV-7 12884 RAVEN INVERTED OIL SYSTEM INSTALLATION OF INVERTED OIL SYSTEM FROM RAVEN AIRCRAFT CORPORATION, USA. LYCOMING AEIO-360-B2F DVMI

ISSUE 2, 14/3/16: OPTIONALLY, A 'HALF' RAVEN OIL SYSTEM MAY BE FITTED, WHICH USES JUST THE OIL SEPARATOR AND NOT THE OIL VALVE.

Prototype mods that have been approved since 1/1/2008 Page 115 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-7 13996 CRANK IN LEFT AND RIGHT CONTROL INSTALLATION OF CRANKED CONTROL COLUMNS TO PROVIDE CLEARANCE WITH OCCUPANTS' LYCOMING IO-360-A1B6 GERT STICK INBOARD THIGH FOLLOWING INSTALLATION OF CENTRE CONSOLE. ORIGINAL CONTROL COLUMNS EACH CUT IN TWO PLACES AND WELDED TO FORM 1" OUTBOARD OFFSET TO UPPER PORTION. P2 COLUMN WELDED INTO LOWER FITTING. VANS RV-7 15286 AUTOPILOT INSTALLATION INSTALLATION OF DYNON DUAL AXIS AUTO-PILOT WITH SV32 ROLL SERVO MOUNTED IN LYCOMING IO-360-A1D ISMA STARBOARD WING DRIVING AILERON BELLCRANK. SV32 PITCH SERVO IN REAR FUSELAGE DRIVING PITCH IDLER BELLCRANK. SERVOS DRIVEN BY A DYNON D180 EFIS AND A DYNON AP74 CONTROLLER. VANS RV-7 13263 LIGHTSPEED PLASMA II PLUS IGNITION REPLACEMENT OF RH MAGNETO WITH LIGHTSPEED PLASMA II PLUS IGNITION. LYCOMING IO-360-B1B FOZY VANS RV-7 13268 ANGLE OF ATTACK INDICATOR ADVANCED FLIGHT SYSTEMS INC ANGLE OF ATTACK SYSTEM COUPLED TO MGL VOYAGER EFIS LYCOMING IO-360-B1B FOZY UNIT. PRESSURE PORTS INSTALLED IN UPPER AND LOWER PORT WING SKINS. VANS RV-7 12304 TRU TRAK WING LEVELLER ADDED USING TRUTRAK WING LEVELLER INSTALLED USING STANDARD TRU-TRAK DESIGN OF INSTALLATION, LYCOMING IO-360-B1B IVII STANDARD INSTALLATION LOCATING THE SERVO AT THE AILERON BELLCRANK IN THE STARBOARD WING AND MOUNTING IT WITH A TRU-TRAK SUPPLIED RPLACEMENT AILERON BELLCRANK MOUNTING BRACKET. PLACARD IN ACCORDANCE WITH LAA REQUIREMENT TO LIMIT OPERATION TO HEIGHTS ABOVE 1000 ' AGL

VANS RV-7 12853 DYNON D180 WING LEVELLER & AP74 DYNON D180 WING LEVELLER AND AP74 ALTITUDE HOLD INSTALLED AS PER MANUFACTURER'S LYCOMING IO-360-B1B CGJN ALTITUDE HOLD INSTRUCTIONS. PTICH: SERVO MOUNTING INSTRUCTIONS 101046-005 REV E. ROLL: SERVO MOUNTING INSTRUCTIONS 101046.003 REV D. VANS RV-7 11587 WING ROOT FAIRINGS WING ROOT FAIRINGS MANUFACTURED IN CARBON/EPOXY. LYCOMING IO-360-B1B CGJN VANS RV-7 13073 LANDING LIGHTS, NAV LIGHTS, STROBE VANS LNSYS6 (WHELEN POSITION LIGHTS, WING TIP STROBES, TAIL LIGHT AND STROBE, LYCOMING IO-360-M1B STIX LIGHTS INCLUDING WHELEN STROBE POWER PACK), LL7/8 MR-16 (2X 75W LANDING LIGHTS IN EACH WING TIP) AND W-715-1 (WING TIPS WITH PROVISION FOR THESE FITTINGS) INSTALLED. FUSES AND INSTRUMENT PANEL SWITCHES PROVIDED. VANS RV-7 13074 TRUTRAK ADI PILOT II INSTALLATION OF TRUTRAK ADI PILOT II AUTOPILOT SYSTEM. PITCH SERVO ATTACHED TO LYCOMING IO-360-M1B STIX ELEVATOR IDLER ARM IN REAR FUSELAGE AND ROLL SERVO ATTACHED TO STARBOARD AILERON BELL CRANK, BOTH AS PER MANUFACTURER'S DRAWINGS. VANS RV-7 13115 3 LEVER QUADRANT AIRCRAFT SPRUCE CMCT3L 3 LEVER QUADRANT INSTALLED BELOW CENTRE OF PANEL USING ALLOY LYCOMING IO-360-M1B STIX ANGLE AND AN-3 FASTENERS. VANS RV-7 13116 FT-60 FUEL TRANSDUCER FT-60 'RED CUBE' FUEL TRANSDUCER (P/N 42160) INSTALLED ON THE FIREWALL IN FUEL LINE LYCOMING IO-360-M1B STIX BETWEEN FUEL PUMP AND INJECTOR. VANS RV-7 11065 AOA SPORT STALL WARNER ADVANCED FLIGHT SYSTEMS INC. AOA SPORT STALL WARNER INSTALLED IN ACCORDANCE WITH LYCOMING IO-360-M1B STIX MANUFACTURERS INSTRUCTIONS AND APPLICANT'S SUBMISSION VANS RV-7 12276 INSTALLATION OF 'BELL' TAILWHEEL INSTALLATION OF 'BELL' TAILWHEEL FORK TO INCREASE GROUND CLEARANCE OF FUSELAGE REAR LYCOMING IO-360-M1B STIX FORK IN ACCORDANCE WITH DRAWINGS STATED BELOW. VANS RV-7 13205 SKYBOLT CLOC COWL FASTENING INSTALLATION OF SKYBOLT CLOC COWLING FASTENER KIT FOR RV AIRCRAFT. INSTALLATION LYCOMING IO-360-M1B OGRL INCORPORATES ALUMINIUM ALLOY STRIPS RIVETED TO FIREWALL AND COWLS, IN ACCORDANCE WITH SKYBOLT INSTRUCTIONS "2007 VANS RV AND OTHER KIT PLANE INSTRUCTIONS".

VANS RV-7 13431 DYNON SKYVIEW AUTO PILOT INSTALLATION OF TWO DYNON SV32 SERVOS IN ACCORDANCE WITH MANUFACTURER'S LYCOMING IO-360-M1B OGRL INSTRUCTIONS TO CONTROL PITCH AND ROLL. SERVOS CONTROLLED BY DYNON SKYVIEW UNIT. TO AVOID ECESSIVE PITCH RATES, ALTITUDE HOLD RATE OF CLIMB AND DESCENT LIMITS TO BE SET TO 500 FPM AS PROVEN IN FLIGHT TESTS ON THIS AND SIMILAR INSTALLATIONS

VANS RV-7 12540 DYNON PITOT PROBE MOUNTED WITH INSTALLATION OF DYNON PITOT/STATIC/AOA PROBE USING GRETZ MOUNTING BRACKET KIT. LYCOMING IO-360-M1B OGRL GRETZ MAST VANS RV-7 15082 NIGHT/IFR CLEARANCE . LYCOMING IO-360-M1B OGRL

Prototype mods that have been approved since 1/1/2008 Page 116 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-7 11217 BONDING OF PLEXIGLASS CANOPY (TIP- SIKAFLEX 295 UV ADHESIVE COMPOUND USED TO ATTACH CANOPY BUBBLE IN LIEU OF MULTIPLE LYCOMING O-320-D2B RVII UP OR SLIDER) FOR RV-7/7A & RV-9/9A AN507-6R8 SCREWS.

ISSUE 2: MODIFICATION APPLICABILITY EXTENDED TO INCLUDE RV9/9A AIRCRAFT SERIES. ISSUE 3: NOW INCLUDES BOTH TIP-UP AND SLIDING CANOPY AND WINDSCREEN. VANS RV-7 14058 TRIO PRO PILOT DUAL AXIS AUTO-PILOT INSTALLATION OF TRIO PRO PILOT DUAL AXIS AUTO-PILOT UTILISING A NAVAID DEVICES ROLL LYCOMING O-320-D2B RVII INSTALLATION SERVO MOUNTED UNDER THE P2 SEAT COUPLED TO THE AILERON CONTROL ROD AT THE BOTTOM OF THE P2 CONTROL COLUMN AND A TRIO PITCH SERVO MOUNTED ON A TRAY IN THE REAR FUSELAGE AND COUPLED TO THE PITCH PUSH-ROD IDLER.

AT ISSUE 2: ROLL SERVO MAY ALSO BE INSTALLED IN THE RIGHT WING AT THE AILERON BELLCRANK POSITION USING THE TRIO RV 7/8/9/10 INSTALLATION KIT. VANS RV-7 15036 FITTING FLY LED NAV AND STROBE FLY LED NAV AND STROBE LIGHTS FITTED TO EXISTING WING TIP LIGHTING POSITIONS AND TAIL LYCOMING O-320-E2D CMON LIGHTS POSITION IN ACCORDANCE WITH THE LIGHT MANUFACTURER'S INSTRUCTIONS. INCLUDES ASSOCIATED CIRCUIT PROTECTION, WIRING AND SWITCHING. STROBE RATE IS SET TO 45 PER MINUTE. VANS RV-7 14375 TRUTRAK VIZION 385 DUAL AXIS AUTO- INSTALLATION OF TRUTRAK VIZION 385 DUAL AXIS AUTO-PILOT WITH AUTO-TRIM. LYCOMING O-320-E2D CMON PILOT INSTALLATION VANS RV-7 12678 ENGINE MOUNT TUBE BETWEEN UPPER ENGINE MOUNTING POINTS REPLACED WITH ONE OF SMALLER RADIUS TO LYCOMING O-320-H2AD CIWV ENABLE CLEARANCE OF ENGINE ACCESSORY GEARBOX. MATERIAL AND DIMENSIONS AS PER VANS DRAWING. VANS RV-7 14028 FALCON HEATED PITOT ON FALCON INSTALLATION OF FALCON HEATED PITOT TUBE ON FALCON MOUNTING. PITOT TUBE POSITIONED LYCOMING O-360-A1A SEVN MOUNT ON OPPOSITE (OUTBOARD) SIDE OF AILERON BELLCRANK ACCESS HOLE TO ORIGINAL VANS PITOT. ADDITION OF EDGE STIFFENED TRAY BETWEEN RIBS TO REINFORCE LOWER SKIN FOR PITOT.

VANS RV-7 14058 TRIO PRO PILOT DUAL AXIS AUTO-PILOT INSTALLATION OF TRIO PRO PILOT DUAL AXIS AUTO-PILOT UTILISING A NAVAID DEVICES ROLL LYCOMING O-360-A1A SEVN INSTALLATION SERVO MOUNTED UNDER THE P2 SEAT COUPLED TO THE AILERON CONTROL ROD AT THE BOTTOM OF THE P2 CONTROL COLUMN AND A TRIO PITCH SERVO MOUNTED ON A TRAY IN THE REAR FUSELAGE AND COUPLED TO THE PITCH PUSH-ROD IDLER.

AT ISSUE 2: ROLL SERVO MAY ALSO BE INSTALLED IN THE RIGHT WING AT THE AILERON BELLCRANK POSITION USING THE TRIO RV 7/8/9/10 INSTALLATION KIT. VANS RV-7 12402 THICK WALL UNDERCARRIAGE LEG UNDERCARRIAGE LEG SOCKETS REPLACED WITH THICKER WALL COMPONENTS OF 1.875" OD, LYCOMING O-360-A1A XIII SOCKETS WELDED IN PLACE BY SUITABLY APPROVED AIRCRAFT WELDER. UNDRCARRIAGE LEG STIFFENERS REMOVED.PREVIOUS MOD 11649 REFERS. VANS RV-7 14724 CONVERSION FROM RV-7A TRI-GEAR TO REMOVAL OF TRI-GEAR UNDERCARRIAGE AND INSTALLATION OF STANDARD VANS TAILDRAGGER LYCOMING O-360-A1A CCVM RV-7 TAILDRAGGER UNDERCARRIAGE, INCLUDING BLANKING COVERS OVER HOLES IN FUSELAGE FOR MAIN UNDERCARRIAGE LEGS. VANS RV-7 13119 NAVAID WING LEVELLER NAVAID DEVICES WING LEVELLER INSTALLED, SIMILAR TO THE INSTALLATION ON RV-6 G-ESTR. THE LYCOMING O-360-A1A OKER SERVO IS MOUNTED ON A TRAY BENEATH THE PILOT'S SEAT WITH A PUSH ROD CONNECTING THE SERVO TO THE LOWER END OF THE PILOT'S CONTROL COLUMN. THE LIGHTENING HOLE IN THE F716 OUTBOARD SEAT RIB IS EXTENDED SLIGHTLY TO ACCOMMODATE THE PUSH ROD THROW. THE UPPER FLANGE OF THE RIB IS REINFORCED WITH A SHORT LENGTH OF 3/4"x3/4"x0.064" ALLOY ANGLE-SECTION RIVETED TO THE OPPOSITE SIDE OF THE RIB TO THE FLANGE. THE UPPER FLANGE OF THE F716 RIGHT SEAT RIB IS ALSO REINFORCED USING A LONGER PIECE OF THE SAME MATERIAL, RIVETTED IN PLACE.

Prototype mods that have been approved since 1/1/2008 Page 117 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-7 13120 WINDSCREEN DEMIST SYSTEM WINDSCREEN DEMIST SYSTEM AS PREVIOUSLY APPROVED ON RV-6 G-ESTR. SYSTEM CONSISTS OF LYCOMING O-360-A1A OKER SCAT HOSES DIRECTING AIR FROM COOLING PLENUM TO A HEAT EXCHANGER ON ONE EXHAUST PIPE. HOT AIR IS SELECTABLE VIA A SELECTOR BOX ON FORWARD FACE OF FIREWALL. AIR IS THEN DIRECTED TO TWO 4"x3"x1" PLENUM CHAMBERS CONSTRUCTED OF LIGHT ALLOY MOUNTED UNDER THE FORWARD SKIN F6107 WITH SLOTS TO ALLOW AIR TO IMPINGE ON LOWER EDGE OF WINDSCREEN. VANS RV-7 13121 START SWITCH PROTECTION REED SWITCHES ADDED TO FUEL SELECTOR VALVE LEVER TO PREVENT STARTER BEING OPERATED LYCOMING O-360-A1A OKER WITH THE FUEL SELECTOR IN THE OFF POSITION. INDICATOR LAMPS SHOW WHICH TANK HAS BEEN SELECTED. AN OVERRIDE BUTTON IS INCLUDED TO ALLOW THE STARTER TO OPERATE SHOULD THE REED SWITCH SYSTEM FAIL. THE SYSTEM IS AS FITTED TO G-ESTR.

VANS RV-7 13935 INSTRUMENT PANEL SUPPORT TO FACILITATE INSTALLATION OF EFIS UNIT AND RADIO UNIT, INSTRUMENT PANEL SUPPORT LYCOMING O-360-A4A RIDG BRACKET REDUCED IN LENGTH AND SUPPLEMENTED BY AN ANGLE CONNECTING THE REMAINING (MODIFIED) PORTION OF THE SUPPORT BRACKET AND THE INSTRUMENT PANEL, ALSO ANGLES TO SUPPORT REAR OF RADIO TRAY. VANS RV-7 13936 BONDING OF PLEXIGLASS BUBBLE TO TIP CANOPY BONDED IN PLACE USING SIKAFLEX 295 ADHESIVE IN PLACE OF SCREWS ON BOTH LYCOMING O-360-A4A RIDG UP CANOPY FRAME FORWARD AND REAR SECTIONS. CARBON FIBRE SHROUD ON EDGE OF FORWARD SECTION, LAID (MODIFIED) UP FROM THREE LAYERS OF 3" 400G CARBON TAPE AND EPOXY RESIN. VANS RV-7 13937 ADVANCED FLIGHT SYSTEMS ANGLE OF ADVANCED FLIGHT SYSTEMS ANGLE OF ATTACK MEASURING AND WARNING SYSTEM INSTALLED. LYCOMING O-360-A4A RIDG ATTACK PRESSURE PORTS INSTALLED IN WING AS PER MANUFACTURER'S INSTRUCTIONS. SYSTEM (MODIFIED) CONNECTED TO ADVANCED FLIGHT SYSTEMS 5500 EFIS WHICH PROVIDES VISUAL AND AURAL INDICATIONS AND WARNINGS OF AOA. SYSTEM INCORPORATES A RAY ALLEN 'POS 12' FLAP POSITION SENSOR WHICH IS MOUNTED BEHIND THE SEATS AND IS CONNECTED TO THE FLAP ACTUATING ARM VIA PIANO WIRE AND A P-CLIP. VANS RV-7 14078 LIGHTSPEED PLASMA II+ IGNITION LIGHTSPEED PLASMA II+ ELECTRONIC IGNITION FITTED IN PLACE OF RIGHT-HAND MAGNETO, LYCOMING O-360-A4A RIDG SYSTEM FITTED TO AN O-360-A4A MODIFIED WITH FUEL INJECTION. (MODIFIED) VANS RV-7 13178 PROPELLER CHANGE TO CATTO THREE CATTO THREE BLADED 68" x 74" PROPELLER FITTED LYCOMING O-360-A4K JKEL BLADED VANS RV-7 13552 AOA STALL WARNING SENSOR SINGLE-PORT AOA PRESSURE PORT ADDED TO PITOT HEAD, FEEDING AN AOA GAUGE ON AN MGL LYCOMING O-360-A4M IBEN ODYSSEY EFIS UNIT. VANS RV-7 14079 MGL AUTO-PILOT (ROLL) INSTALLATION INSTALLATION OF MGL AUTO-PILOT (ROLL) USING TRIO GOLD STANDARD SERVO IN RIGHT WING LYCOMING O-360-A4M IBEN FITTED WITH TRIO INSTALLATION KIT WITH ACCEPTABLE POST-AUGUST 2009 BRACKET. VANS RV-7 15421 VETTERMAN TWIN MUFFLED TAILPIPES EXISTING TWIN TAILPIPES REPLACED WITH TWIN VETTERMAN MUFFLED EXHAUST TAILPIPES. LYCOMING O-360-A4M IBEN EXISTING 4 INTO 2 'CROSSOVER' PRIMARY EXHAUST SYSTEM REMAINS IN PLACE. TAILPIPES SECURED TO EACH OTHER AND ENGINE SUMP USING FLEXIBLE STEADY BRACKETS OF VETTERMAN DESIGN. HEAT EXCHANGER ON STARBOARD MUFFLER USED FOR CABIN HEAT. VANS RV-7 12686 SMOKE SYSTEM INSTALLATION CUSTOM SMOKE SYSTEM INSTALLED LYCOMING YIO-360-B1B DAME YIO-360-B1B VANS RV-7 13478 SAM JAMES COWL, PLENUM AND AIR INSTALLATION OF SAM JAMES COWL, PLENUM AND AIR FILTER HOUSING IN ACCORDANCE WITH LYCOMING YIO-360-M1B WOWI FILTER HOUSING JAMES AIRCRAFT INSTRUCTIONS, USING CAMLOC FASTENERS AROUND FIREWALL AND PIANO HINGES ALONG SIDES. VANS RV-7 13479 FUEL SYSTEM MODS FITMENT OF ANDAIR GASCOLATOR GAS375 IN EACH WING ROOT SPACE. MOVE ANDAIR FUEL LYCOMING YIO-360-M1B WOWI SELECTOR FS20X3 TO A CENTRE PANEL FOR GREATER VISIBILITY. AN FITTINGS USED TO CONNECT COMPONENTS.

Prototype mods that have been approved since 1/1/2008 Page 118 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-7 13480 JD AIRPARTS TAILWHEEL FORK & PART 1: JD AIRPARTS TAILWHEEL FORK (P/N 'TWFORK') FOR RV AIRCRAFT REPLACES STANDARD LYCOMING YIO-360-M1B WOWI LIGHTWEIGHT TAILWHEEL VANS TAILWHEEL FORK. PART 2: LIGHTWEIGHT TAILWHEEL (P/N 'U TAILWHEEL LW 6"') REPLACES STANDARD TAILWHEEL.

BOTH ARE DIRECT REPLACEMENTS FOR ORIGINAL ITEMS.

ISSUE 2: PARTS 1 AND/OR 2 OF THIS MODIFICATION MAY BE INSTALLED.

VANS RV-7 13517 CANOPY EJECT STANDARD CANOPY EJECT MECHANISM MODIFIED. QUICK RELEASE PIN AND MECHANISM LYCOMING YIO-360-M1B WOWI RETAINED BUT HANDLE REPLACED BY A SHORT ALLOY BAR TO ENABLE RELEASE OF CANOPY FOR MAINTENANCE. VANS RV-7 13539 ADVANCED FLIGHT SYSTEMS AOA ADVANCED FLIGHT SYSTEMS ANGLE OF ATTACK INDICATOR FITTED IN ACCORDANCE WITH LYCOMING YIO-360-M1B WOWI MANUFACTURER'S INSTRUCTIONS REVISION 4. INCLUDES FLAP POSITION SWITCH. VANS RV-7 12495 TRUTRAK DIGIFLIGHT II VS AUTOPILOT AUTOPILOT INSTALLED AS PER MANUFACTURER'S INSTRUCTIONS. LYCOMING YIO-360-M1B WOWI VANS RV-7 11575 RV/ROCKET TAILWHEEL STEERING LINK RV/ROCKET TAILWHEEL STEERING LINK FITTED BETWEEN STEERING ARMS ON RUDDER AND LYCOMING YIO-360-M1B WOWI TAILWHEEL.

INSTALLATION CARRIED OUT IN ACCORDANCE WITH INSTRUCTION SHEETS PROVIDED BY COMPONENT MANUFACTURER.

COMPONENT MANUFACTURER DETAILS ARE: TERRY JANTZI, PO BOX 20052, PIONEER PARK POSTAL OUTLET, KITCHENER, ON CADAN, N2P 2B4. VANS RV-7 13431 DYNON SKYVIEW AUTO PILOT INSTALLATION OF TWO DYNON SV32 SERVOS IN ACCORDANCE WITH MANUFACTURER'S LYCOMING YIO-360-M1B MACI INSTRUCTIONS TO CONTROL PITCH AND ROLL. SERVOS CONTROLLED BY DYNON SKYVIEW UNIT. TO AVOID ECESSIVE PITCH RATES, ALTITUDE HOLD RATE OF CLIMB AND DESCENT LIMITS TO BE SET TO 500 FPM AS PROVEN IN FLIGHT TESTS ON THIS AND SIMILAR INSTALLATIONS

VANS RV-7 14034 DYNON HEATED PITOT AND SAFEAIR1 INSTALLATION OF DYNON HEATED PITOT PROBE (POST OCTOBER 2014 MODEL) MOUNTED ON LYCOMING YIO-360-M1B MACI PITOT MAST SAFEAIR1 MAST TO PORT WING UNDERSIDE IN ACCORDANCE WITH DYNON AND SAFEAIR1 INSTRUCTIONS. VANS RV-7 14458 ALTERATION TO INSTRUMENT PANEL INSTRUMENT PANEL SUPPORTING BRACKETS MODIFIED TO ENABLE FITMENT OF DYNON SKYVIEW LYCOMING YIO-360-M1B MACI UNITS. AFT SECTION OF BRACKETS REMOVED AND ADDITIONAL ANGLES AND DOUBLERS ADDED TO MAKE GOOD THE STRUCTURE. VANS RV-7 14186 MODIFICATION OF INSTRUMENT PANEL PORT SIDE INSTRUMENT PANEL SUPPORT RIB F-745-L MODIFIED TO REMOVE AFT SECTION TO LYCOMING YIO-360-M1B ELVN SUPPORT ALLOW FITMENT OF EFIS. VANS RV-7 13361 INSTALLATION OF ELECTRONICS ELECTRONICS INTERNATIONAL FT-60 FLOW TRANSDUCER FITTED DOWNSTREAM OF ELECTRIC FUEL LYCOMING YIO-360-M1B ELVN INTERNATIONAL FT-60 FUEL FLOW PUMP AND FILTER. TRANSDUCER VANS RV-7 14268 GRETZ PITOT MOUNT & DYNON PITOT DYNON UNHEATED PITOT/ANGLE OF ATTACK HEAD P/N 100141-000 MOUNTED ON GRETZ AERO LYCOMING YIO-360-M1B ELVN HEAD WITH AOA PORT CBK-12 PITOT MOUNT. THIS IS LOCATED ON THE UNDERSIDE OF THE PORT WING OUTBOARD OF THE INSPECTION HATCH, IN ACCORDANCE WITH THE MANUFACTURER'S INSTRUCTIONS. ANGLE OF ATTACK PORT CONNECTED TO DYNON D180 EFIS.

AT ISSUE 2, DYNON SKYVIEW UNIT ADDED AS ACCEPTABLE ALTERNATIVE ANGLE OF ATTACK DISPLAY/WARNING DEVICE.

VANS RV-7 15224 UNDER CARRIAGE CONFIGURATION CHANGE TO RV7 UNDERCARRIAGE LYCOMING YIO-360-M1B ELVN CHANGE VANS RV-7 13740 TAILWHEEL LINK REPLACING SPRINGS JD AIR PARTS TAILWHEEL STEERING LINK, IN SUBSTITUTION FOR CONVENTIONAL SPRINGS, LYCOMING YIO-360-M1B OJLD INSTALLED IN ACCORDANCE WITH JDAIR PARTS INSTRUCTIONS V 1.2.

Prototype mods that have been approved since 1/1/2008 Page 119 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-7 13480 JD AIRPARTS TAILWHEEL FORK & PART 1: JD AIRPARTS TAILWHEEL FORK (P/N 'TWFORK') FOR RV AIRCRAFT REPLACES STANDARD LYCOMING YIO-360-M1B OJLD LIGHTWEIGHT TAILWHEEL VANS TAILWHEEL FORK. PART 2: LIGHTWEIGHT TAILWHEEL (P/N 'U TAILWHEEL LW 6"') REPLACES STANDARD TAILWHEEL.

BOTH ARE DIRECT REPLACEMENTS FOR ORIGINAL ITEMS.

ISSUE 2: PARTS 1 AND/OR 2 OF THIS MODIFICATION MAY BE INSTALLED.

VANS RV-7 11217 BONDING OF PLEXIGLASS CANOPY (TIP- SIKAFLEX 295 UV ADHESIVE COMPOUND USED TO ATTACH CANOPY BUBBLE IN LIEU OF MULTIPLE LYCOMING YIO-360-M1B OJLD UP OR SLIDER) FOR RV-7/7A & RV-9/9A AN507-6R8 SCREWS.

ISSUE 2: MODIFICATION APPLICABILITY EXTENDED TO INCLUDE RV9/9A AIRCRAFT SERIES. ISSUE 3: NOW INCLUDES BOTH TIP-UP AND SLIDING CANOPY AND WINDSCREEN. VANS RV-7 12884 RAVEN INVERTED OIL SYSTEM INSTALLATION OF INVERTED OIL SYSTEM FROM RAVEN AIRCRAFT CORPORATION, USA. LYCOMING YIO-360-M1B OJLD

ISSUE 2, 14/3/16: OPTIONALLY, A 'HALF' RAVEN OIL SYSTEM MAY BE FITTED, WHICH USES JUST THE OIL SEPARATOR AND NOT THE OIL VALVE. VANS RV-7 13431 DYNON SKYVIEW AUTO PILOT INSTALLATION OF TWO DYNON SV32 SERVOS IN ACCORDANCE WITH MANUFACTURER'S LYCOMING YIO-360-M1B OJLD INSTRUCTIONS TO CONTROL PITCH AND ROLL. SERVOS CONTROLLED BY DYNON SKYVIEW UNIT. TO AVOID ECESSIVE PITCH RATES, ALTITUDE HOLD RATE OF CLIMB AND DESCENT LIMITS TO BE SET TO 500 FPM AS PROVEN IN FLIGHT TESTS ON THIS AND SIMILAR INSTALLATIONS

VANS RV-7 14099 RELOCATION OF FUSELAGE RIBS TO INSTRUMENT PANEL SUPPORT RIBS F-745-L AND F 745-R CUT AND AFT PORTIONS MOVED LYCOMING YIO-360-M1B OJLD ACCOMMODATE DUAL EFIS SCREENS INBOARD BY 3". SUPPORTED BY VERTICAL ANGLES AT THE FORWARD END AND STIFFENED WITH HORIZONTAL ANGLES ON THEIR TOP EDGES. ALSO ATTACHED TO ADJACENT RADIO/TRANSPONDER TRAYS. CONNECTED TO THE INSTRUMENT PANEL AS PER ORIGINAL DESIGN.

VANS RV-7 13446 JD AIR PARTS TAIL LINK JD AIR PARTS TAIL LINK INSTALLED IN ACCORDANCE WITH MANUFACTURER'S INSTRUCTIONS, LYCOMING YIO-360-M1B RVAH REPLACING STANDARD VANS TAIL SPRINGS. VANS RV-7 13447 DYNON AUTO PILOT (PITCH) DYNON SV32 PITCH SERVO INSTALLED IN REAR FUSELAGE AND CONNECTED TO ELEVATOR IDLER LYCOMING YIO-360-M1B RVAH INSTALLATION BELLCRANK IN ACCORDANCE WITH MANUFACTURER'S INSTRUCTIONS. SERVO CONTROLLED BY DYNON SKYVIEW SV-D1000. VANS RV-7 13448 DYNON AUTO PILOT (ROLL) DYNON SV32 ROLL SERVO INSTALLED IN WING AND CONNECTED TO AILERON BELLCRANK IN LYCOMING YIO-360-M1B RVAH INSTALLATION ACCORDANCE WITH MANUFACTURER'S INSTRUCTIONS. SERVO CONTROLLED BY DYNON SKYVIEW SV-D1000. VANS RV-7 15325 SINGLE P-MAG P114-L4 ELECTRONIC INSTALLATION OF P-MAG P114-L4 SERIES REPLACING RIGHT HAND MAGNETO. LYCOMING YIO-360-M1B CKMX IGNITION UNIT INSTALLATION VANS RV-7 14488 ELECTRONIC STANDBY INSTRUMENTS GARMIN G5 EFIS UNIT INSTALLED AS BACKUP FLIGHT INSTRUMENTS IN ACCORDANCE WITH THE LYCOMING YIO-360-M1B ICRV GARMIN G5 MANUFACTURER'S INSTRUCTIONS. INCORPORATES STANDBY BATTERY. HSI PAGE DISABLED.

VANS RV-7 14507 GARMIN DUAL AXIS AUTO-PILOT INSTALLATION OF GARMIN DUAL AXIS AUTO-PILOT WITH GARMIN G3X TOUCH AND GNC 307 LYCOMING YIO-360-M1B ICRV INSTALLATION INTERFACE VANS RV-7 11217 BONDING OF PLEXIGLASS CANOPY (TIP- SIKAFLEX 295 UV ADHESIVE COMPOUND USED TO ATTACH CANOPY BUBBLE IN LIEU OF MULTIPLE LYCOMING YIO-360-M1B ICRV UP OR SLIDER) FOR RV-7/7A & RV-9/9A AN507-6R8 SCREWS.

ISSUE 2: MODIFICATION APPLICABILITY EXTENDED TO INCLUDE RV9/9A AIRCRAFT SERIES. ISSUE 3: NOW INCLUDES BOTH TIP-UP AND SLIDING CANOPY AND WINDSCREEN. VANS RV-7 11587 WING ROOT FAIRINGS WING ROOT FAIRINGS MANUFACTURED IN CARBON/EPOXY. LYCOMING YIO-360-M1B OMPH VANS RV-7 12738 SAM JAMES COWLING SAM JAMES ENGINE COWLING INSTALLED, INCLUDING INTERNAL PLENUM. LYCOMING YIO-360-M1B OMPH

Prototype mods that have been approved since 1/1/2008 Page 120 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-7 12283 TIP-UP INSTRUMENT PANEL SUPPORT INSTRUMENT PANEL ALTERED PER APPLICANT'S APPLICATION TO ENABLE EFIS PANELS TO BE LYCOMING YIO-360-M1B RVHD WITH EFIS SCREENS FITTED. EXISTING RIBS F745 L/R SHORETENED AND REPLACED WITH FOUR RIBS PLACED SYMETRICALLY EITHER SIDE OF SCREENS VANS RV-7 15425 GARMIN G3X AUTOPILOT WITH GMC507 GARMIN AUTOPILOT SYSTEM INSTALLED, CONSISTING OF G3X EFIS, GMC 507 CONTROL PANEL AND LYCOMING YIO-360-M1B OVEY CONTROLLER 2 OFF GSA 28 SERVOS. PITCH SERVO INSTALLED IN AFT FUSELAGE USING GARMIN BRACKET 011- 09252-14; ROLL SERVO INSTALLED IN WING USING GARMIN BRACKET 011-02952-12. INSTALLATION IN ACCORDANCE WITH GARMIN INSTRUCTIONS. VANS RV-7 15426 BERINGER BRAKE AND WHEEL KIT BERINGER WHEELS AND BRAKES INSTALLED IN ACCORDANCE WITH THE MANUFACTURER'S LYCOMING YIO-360-M1B OVEY INSTRUCTIONS USING THE FOLLOWING PARTS: RF-022(A) MAIN WHEELS MP-OO2N(A) MASTER CYLINDER FP-001N(A) PARKING BRAKE VALVE EA-002N(A) BRAKE ASSEMBLIES 070-310-0 MICHELIN TYRES RE-001N(B) BRAKE REGULATOR VANS RV-7 15036 FITTING FLY LED NAV AND STROBE FLY LED NAV AND STROBE LIGHTS FITTED TO EXISTING WING TIP LIGHTING POSITIONS AND TAIL LYCOMING YIO-360-M1B OVEY LIGHTS POSITION IN ACCORDANCE WITH THE LIGHT MANUFACTURER'S INSTRUCTIONS. INCLUDES ASSOCIATED CIRCUIT PROTECTION, WIRING AND SWITCHING. STROBE RATE IS SET TO 45 PER MINUTE. VANS RV-7 12373 CARBON FIBRE ENGINE COVER MOULDED CARBON FIBRE ENGINE COOLING PLENUM FITTED. LYCOMING YIO-360-M1B OVEY VANS RV-7 13361 INSTALLATION OF ELECTRONICS ELECTRONICS INTERNATIONAL FT-60 FLOW TRANSDUCER FITTED DOWNSTREAM OF ELECTRIC FUEL LYCOMING YIO-360-M1B OVEY INTERNATIONAL FT-60 FUEL FLOW PUMP AND FILTER. TRANSDUCER VANS RV-7 15431 FUEL SYSTEM MODS ANDAIR FX375-M IN-LINE FILTERS FITTED IN EACH WING ROOT BETWEEN TANK OUTLET AND LYCOMING YIO-360-M1B OVEY ANDAIR FS20X7-T FUEL SELECTOR LOCATED ON CENTRE PANEL. ANDAIR PX375-TC ELECTRIC FUEL PUMP LOCATED BETWEEN FUEL SELECTOR AND MECHANICAL FUEL PUMP. INCORPORATES AN FITTINGS TO CONNECT COMPONENTS. VANS RV-7 12760 REPLACEMENT OF NAVAID WING INSTALLATION OF TRIO PRO PILOT DUAL AXIS AUTO-PILOT INCORPORATING EXISTING NAVAID SUPERIOR XP-IO-360-A1A2 CDME LEVELLER WITH TRIO PRO PILOT WING LEVELLER SERVO INSTALLATION. PITCH CONTROL SERVO INSTALLED ON PLATFORM ATTACHED TO SUPPORT STRUCTURE FOR PITCH SYSTEM IDLER BELLCRANK. VANS RV-7 13147 DYNON FUEL FLOW TRANSDUCER & INSTALLATION OF FLOSCAN 201B BETWEEN FUEL PUMP AND GASCOLATOR TO PROVIDE FUEL SUPERIOR XP-IO-360-B1A2 KAOS CAPACITANCE TO VOLT CONVERTER FLOW OUTPUT TO DYNON D120 ENGINE MANAGEMENT SYSTEM. INSTALLATION OF VANS CAPACITANCE CONVERTER UNDER INSTRUMENT PANEL TO CONVERT CAPACITANCE FROM FUEL LEVEL SENDER TO VOLTAGE FOR DYNON D120 SYSTEM. VANS RV-7 13181 DYNON D100/AP74 DUAL AXIS AUTO- INSTALLATION OF DYNON DUAL AXIS AUTO-PILOT COMMANDED BY A DYNON D100 EFIS THROUGH SUPERIOR XP-IO-360-B1A2 KAOS PILOT A DYNON AP74 INTERFACE UNIT. NOTE THAT IT IS A REQUIREMENT OF THIS APPROVAL TO SET THE MAXIMUM AUTOMATIC ASCENT/DESCENT RATE TO NO MORE THAN 500 FEET PER MINUTE.

VANS RV-7 13246 DUAL THROTTLE CONTROLS THROTTLE CONTROL ADDED TO PORT SIDE OF INSTRUMENT PANEL. FRICTION DEVICE REMOVED SUPERIOR XP-IO-360-B1A2 KAOS FROM THROTTLE CONTROL. ADDITIONAL FIREWALL FITTING AND MODIFIED THROTTLE LEVER ARM TO ACCOMMODATE EXTRA THROTTLE CABLE. VANS RV-7 12574 TRIO EZ-PILOT WING LEVELLER INSTALLATION OF TRIO EZ-PILOT WING LEVELLER IN WING TIP USING SAFEAIR1 INSTALLATION KIT SUPERIOR XP-IO-360-B1AA2 OVII INSTALLED WITH SAFEAIR1 WITH THE ADDITION OF A BOLT AT EACH LOWER CORNER OF THE MOUNTING PLATE. INSTALLATION KIT. VANS RV-7 13499 INSTALLATION OF SAFEAIR 1 PITOT MAST SAFEAIR 1 PITOT MAST INSTALLED ON PORT WING OUTBOARD OF AILERON BELLCRANK SUPERIOR XP-IO-360-B1AD2 RVRP & DYNON HEATED PITOT INSPECTION PANEL, WITH DYNON AOA/PITOT HEATED PROBE P/N 100667-000, INCLUDING ASSOCIATED CONTROLLER, WIRING AND SWITCHING. INSTALLED IN ACCORDANCE WITH THE MANUFACTURERS' INSTRUCTIONS. VANS RV-7 13740 TAILWHEEL LINK REPLACING SPRINGS JD AIR PARTS TAILWHEEL STEERING LINK, IN SUBSTITUTION FOR CONVENTIONAL SPRINGS, SUPERIOR XP-IO-360-B1AD2 RVRP INSTALLED IN ACCORDANCE WITH JDAIR PARTS INSTRUCTIONS V 1.2.

Prototype mods that have been approved since 1/1/2008 Page 121 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-7 13431 DYNON SKYVIEW AUTO PILOT INSTALLATION OF TWO DYNON SV32 SERVOS IN ACCORDANCE WITH MANUFACTURER'S SUPERIOR XP-IO-360-B1AD2 RVRP INSTRUCTIONS TO CONTROL PITCH AND ROLL. SERVOS CONTROLLED BY DYNON SKYVIEW UNIT. TO AVOID ECESSIVE PITCH RATES, ALTITUDE HOLD RATE OF CLIMB AND DESCENT LIMITS TO BE SET TO 500 FPM AS PROVEN IN FLIGHT TESTS ON THIS AND SIMILAR INSTALLATIONS

VANS RV-7 12276 INSTALLATION OF 'BELL' TAILWHEEL INSTALLATION OF 'BELL' TAILWHEEL FORK TO INCREASE GROUND CLEARANCE OF FUSELAGE REAR SUPERIOR XP-IO-360-B1AD2 PBEC FORK IN ACCORDANCE WITH DRAWINGS STATED BELOW. VANS RV-7 15392 GARMIN GAP26 HEATED PITOT SAFEAIR INSTALLATION OF SAFEAIR PITOT MAST TO ACCOMMODATE GARMIN GAP26 PITOT HEAD. SUPERIOR XP-IO-360-B1AD2 CFET MAST VANS RV-7 14375 TRUTRAK VIZION 385 DUAL AXIS AUTO- INSTALLATION OF TRUTRAK VIZION 385 DUAL AXIS AUTO-PILOT WITH AUTO-TRIM. SUPERIOR XP-IO-360-B1AD2 CIOO PILOT INSTALLATION VANS RV-7 14199 TRUTRAK ADI PILOT II AUTOPILOT INSTALLATION OF TRUTRAK ADI PILOT II DUAL AXIS AUTO PILOT ACCORDING TO VANS-APPROVED SUPERIOR XP-IO-360-B1AD3 FIXX INSTRUCTIONS PROVIDED BY TRUTRAK. AUTOPILOT CONTROL UNIT PARAMETERS AND SETTINGS AS DOCUMENTED IN THE FLIGHT TEST REPORT DATED 7/9/15. VANS RV-7 12414 SEGA TAILWHEEL YOKE SUBSTITUTION OF SEGA TYPE TAILWHEEL YOKE IN ACCORDANCE WITH SEGA INSTRUCTIONS. SUPERIOR XP-IO-360-B1B2 CETS TAILWHEEL YOKE INTERCHANGEABLE WITH VANS DESIGN BUT OFFERS INCREASED GROUND CLEARANCE. VANS RV-7 12304 TRU TRAK WING LEVELLER ADDED USING TRUTRAK WING LEVELLER INSTALLED USING STANDARD TRU-TRAK DESIGN OF INSTALLATION, SUPERIOR XP-IO-360-B1C2 RISY STANDARD INSTALLATION LOCATING THE SERVO AT THE AILERON BELLCRANK IN THE STARBOARD WING AND MOUNTING IT WITH A TRU-TRAK SUPPLIED RPLACEMENT AILERON BELLCRANK MOUNTING BRACKET. PLACARD IN ACCORDANCE WITH LAA REQUIREMENT TO LIMIT OPERATION TO HEIGHTS ABOVE 1000 ' AGL

VANS RV-7 12424 STROBE AND INSTALLATION OF VANS SUPPLIED STROBE/NAVIGATION LIGHTS KIT LN SYS6 COMPRISING SUPERIOR XP-IO-360-B1C2 RISY INSTALLATION WHELAN A650PG/PR COMBINED NAVIGATION AND STROBE LIGHT UNITS MOUNTED IN WING TIP LEADING EDGES WITH TRANSPARENT COVERS AND AN A500A COMBINATION STROBE/TAIL NAVIGATION LIGHT MOUNTED TO LOWER REAR OF RUDDER. WHELAN A413A-HDACF COMET FLASH POWER SUPPLY MOUNTED TO FLOOR PAN IMMEDIATELY AFT OF STARBOARD SEAT. VANS RV-7 14477 DUAL P-MAGS INSTALLATION INSTALLATION OF DUAL E-MAGS P114 MODEL P-MAGS SUPERIOR XP-IO-360-B1C2 RISY VANS RV-7 13634 FITMENT OF DUAL P-MAGS FITMENT OF DUAL EMAG PMAG P114L4 ELECTRONIC IGNITION MODULES AND ASSOCIATED SUPERIOR XP-IO-360-B1CA2 XTAZ SWITCHES/WIRING. VANS RV-7 13795 DYNON FLIGHTDEK D180 DUAL AXIS INSTALLATION OF DYNON FLIGHTDEK D180 DUAL AXIS AUTO-PILOT. ROLL SERVO FITTED IN SUPERIOR XP-IO-360-B1CA2 XTAZ AUTO-PILOT INSTALLATION ACCORDANCE WITH DYNON INSTRUCTIONS RV-7/8/10 ROLL KIT 101046-003 REV F AND PITCH SERVO WITH DYNON INSTRUCTIONS RV6/7/9 PITCH KIT 101046-005 REV F. VANS RV-7 14787 FT-60 FUEL FLOW TRANSDUCER 'RED FT-60 FUEL FLOW TRANSDUCER INSTALLED BETWEEN FUEL SERVO AND FLOW DIVIDER, MOUNTED SUPERIOR XP-IO-360-B1CA2 XTAZ CUBE' INSTALLATION ON ENGINE MOUNT. VANS RV-7 11217 BONDING OF PLEXIGLASS CANOPY (TIP- SIKAFLEX 295 UV ADHESIVE COMPOUND USED TO ATTACH CANOPY BUBBLE IN LIEU OF MULTIPLE SUPERIOR XP-IO-360-B1HD2 DMBO UP OR SLIDER) FOR RV-7/7A & RV-9/9A AN507-6R8 SCREWS.

ISSUE 2: MODIFICATION APPLICABILITY EXTENDED TO INCLUDE RV9/9A AIRCRAFT SERIES. ISSUE 3: NOW INCLUDES BOTH TIP-UP AND SLIDING CANOPY AND WINDSCREEN. VANS RV-7 13634 FITMENT OF DUAL P-MAGS FITMENT OF DUAL EMAG PMAG P114L4 ELECTRONIC IGNITION MODULES AND ASSOCIATED SUPERIOR XP-IO-360-B1HD2 DMBO SWITCHES/WIRING. VANS RV-7 13795 DYNON FLIGHTDEK D180 DUAL AXIS INSTALLATION OF DYNON FLIGHTDEK D180 DUAL AXIS AUTO-PILOT. ROLL SERVO FITTED IN SUPERIOR XP-IO-360-B1HD2 DMBO AUTO-PILOT INSTALLATION ACCORDANCE WITH DYNON INSTRUCTIONS RV-7/8/10 ROLL KIT 101046-003 REV F AND PITCH SERVO WITH DYNON INSTRUCTIONS RV6/7/9 PITCH KIT 101046-005 REV F.

Prototype mods that have been approved since 1/1/2008 Page 122 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-7 13431 DYNON SKYVIEW AUTO PILOT INSTALLATION OF TWO DYNON SV32 SERVOS IN ACCORDANCE WITH MANUFACTURER'S SUPERIOR XP-IO-360-B1HD2 DANP INSTRUCTIONS TO CONTROL PITCH AND ROLL. SERVOS CONTROLLED BY DYNON SKYVIEW UNIT. TO AVOID ECESSIVE PITCH RATES, ALTITUDE HOLD RATE OF CLIMB AND DESCENT LIMITS TO BE SET TO 500 FPM AS PROVEN IN FLIGHT TESTS ON THIS AND SIMILAR INSTALLATIONS

VANS RV-7 12884 RAVEN INVERTED OIL SYSTEM INSTALLATION OF INVERTED OIL SYSTEM FROM RAVEN AIRCRAFT CORPORATION, USA. SUPERIOR XP-IO-360-B1HD2 DANP

ISSUE 2, 14/3/16: OPTIONALLY, A 'HALF' RAVEN OIL SYSTEM MAY BE FITTED, WHICH USES JUST THE OIL SEPARATOR AND NOT THE OIL VALVE. VANS RV-7 13474 DUAL P MAGS INSTALLATION OF E-MAGS ELECTRONIC IGNITION DUAL P114 P-MAG UNITS. SUPERIOR XP-IO-360-B1HD2 DANP VANS RV-7 12540 DYNON PITOT PROBE MOUNTED WITH INSTALLATION OF DYNON PITOT/STATIC/AOA PROBE USING GRETZ MOUNTING BRACKET KIT. SUPERIOR XP-IO-360-B1HD2 DANP GRETZ MAST VANS RV-7 13473 DYNON PITOT HEAD INSTALLATION OF DYNON UNHEATED AOA/PITOT HEAD P/N 100141-000 TO PORT WING. SUPERIOR XP-IO-360-B1HD2 CHHI MOUNTING BRACKET FABRICATED FROM 4130 22 GAUGE ALLOY, INCLUDING WING DOUBLER. ANGLE OF ATTACK INDICATION PROVIDED BY DYNON SKYVIEW UNIT. VANS RV-7 13474 DUAL P MAGS INSTALLATION OF E-MAGS ELECTRONIC IGNITION DUAL P114 P-MAG UNITS. SUPERIOR XP-IO-360-B1HD2 CHHI VANS RV-7 13497 EPL NAV LIGHTS FITMENT OF EPL NAVIGATION LIGHTS P/N 11-05120 IN WING TIPS, WITH ASSOCIATED WIRING, SUPERIOR XP-IO-360-B1HD2 CHHI SWITCH AND FUSE, IN ACCORDANCE WITH THE MANUFACTURER'S INSTRUCTIONS. VANS RV-7 11587 WING ROOT FAIRINGS WING ROOT FAIRINGS MANUFACTURED IN CARBON/EPOXY. SUPERIOR XP-IO-360-B1HD2 CHHI VANS RV-7 13431 DYNON SKYVIEW AUTO PILOT INSTALLATION OF TWO DYNON SV32 SERVOS IN ACCORDANCE WITH MANUFACTURER'S SUPERIOR XP-IO-360-B1HD2 CHHI INSTRUCTIONS TO CONTROL PITCH AND ROLL. SERVOS CONTROLLED BY DYNON SKYVIEW UNIT. TO AVOID ECESSIVE PITCH RATES, ALTITUDE HOLD RATE OF CLIMB AND DESCENT LIMITS TO BE SET TO 500 FPM AS PROVEN IN FLIGHT TESTS ON THIS AND SIMILAR INSTALLATIONS

VANS RV-7 12752 INSTALLATION OF TRIO EZ PILOT WING INSTALLATION OF TRIO EZ PILOT WING LEVELLER USING TRIO BRACKET MOUNT (POST AUG 2009) SUPERIOR XP-O-360-B1A2 RINZ LEVELLER FOR SERVO ATTACHMENT IN STARBOARD WING. VANS RV-7 11200 FLAP POSITION SWITCHES A BRACKET IS MANUFACTURED AND INSTALLED AGAINST THE FLAP TORQUE TUBE TO MOUNT A SUPERIOR XP-O-360-B1A2 RINZ MICROSWITCH WHICH DETECTS THE FLAP POSITION. VANS RV-7 11217 BONDING OF PLEXIGLASS CANOPY (TIP- SIKAFLEX 295 UV ADHESIVE COMPOUND USED TO ATTACH CANOPY BUBBLE IN LIEU OF MULTIPLE SUPERIOR XP-O-360-B1A2 RINZ UP OR SLIDER) FOR RV-7/7A & RV-9/9A AN507-6R8 SCREWS.

ISSUE 2: MODIFICATION APPLICABILITY EXTENDED TO INCLUDE RV9/9A AIRCRAFT SERIES. ISSUE 3: NOW INCLUDES BOTH TIP-UP AND SLIDING CANOPY AND WINDSCREEN. VANS RV-7 11317 FITMENT OF EXTRA PITOT TUBE FOR AOA ADDITIONAL PITOT TUBE ADDED SOLELY TO OPERATE AOA INDICATOR, IN ADDITION TO SUPERIOR XP-O-360-B1A2 RINZ INDICATION STANDARD PITOT STATIC SYSTEM AND STALL WARNER SWITCH VANS RV-7 11318 FITMENT OF STROBE POWER SUPPLY THREE SHEET METAL PARTS ARE INSTALLED UNDER THE BAGGAGE BAY TO SUPPORT THE WHELEN SUPERIOR XP-O-360-B1A2 RINZ LN.A415-HDA-CF STROBE POWER SUPPLY UNIT. VANS RV-7 11319 FITMENT OF REMOTE COMPASS HEAD A COMPASS SENDER UNIT WEIGHING LESS THAN 4 OZ IS MOUNTED ON A FABRICATED SUPERIOR XP-O-360-B1A2 RINZ ALUMINIUM BRACKET MOUNTED TO A FUSELAGE FRAME IN THE TAILCONE. VANS RV-7 11376 COWL FASTENING (CAM LOCKS) THE EXISTING "PIANO HINGE" ARRANGEMENT TO FASTEN THE UPPER AND LOWER COWLINGS IS SUPERIOR XP-O-360-B1A2 RINZ REPLACED BY STANDARD AIRCRAFT CAMLOCS. EDGES OF COWLS ARE REINFORCED WITH ADDITIONAL LAYERS OF GFRP. VANS RV-7 11600 ALTERED CANOPY RELEASE CANOPY RELEASE HANDLE IS ALTERED TO PROVIDE INCREASED SPACE ON INSTRUMENT PANEL. SUPERIOR XP-O-360-B1A2 RINZ

VANS RV-7 11645 TRIO EZ-1 ALTITUDE HOLD SYSTEM TRIO EZ-1 ALTITUDE HOLD SYSTEM FITTED PER APPLICANT'S DRAWING, INCLUDING ALTITUDE SUPERIOR XP-O-360-B1A2 RINZ HOLD ACTIVE WARNING LIGHT AND DUPLICATED DISENGAGE SWITCHES. VANS RV-7 13185 INSTALLATION OF RAY ALLEN STICK RAY ALLEN G301 AND G307 STICK GRIPS IN ACCORDANCE WITH THE MANUFACTURER'S SUPERIOR XP-O-360-B1A2 CGWF GRIPS INSTRUCTIONS.

Prototype mods that have been approved since 1/1/2008 Page 123 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-7 13186 VANS LN SYS6 STROBE LIGHT KIT INSTALLATION OF VANS LN SYS6 STROBE LIGHT KIT, CONSISTING OF A POWER SUPPLY UNIT LN SUPERIOR XP-O-360-B1A2 CGWF A413A-HAD-CF-14, TAIL NAV/STROBE LIGHT LN A500-14, WING TIP STROBES LN A650 (2 OFF) AND INSTALLATION KIT LN HD-60-1. INSTALLED IN ACCORDANCE WITH THE MANUFACTURER'S INSTRUCTIONS. VANS RV-7 13215 TRUTRACK ADI PILOT II AUTO-PILOT INSTALLATION OF TRUTRACK ADI PILOT II AUTOPILOT (PITCH & ROLL), IN ACCORDANCE WITH VANS SUPERIOR XP-O-360-B1A2 CGWF AND TRUTRACK INSTALLATION INSTRUCTIONS. VANS RV-7 13634 FITMENT OF DUAL P-MAGS FITMENT OF DUAL EMAG PMAG P114L4 ELECTRONIC IGNITION MODULES AND ASSOCIATED SUPERIOR XP-IO-360-B1HC2 DSRV SWITCHES/WIRING. VANS RV-7 12540 DYNON PITOT PROBE MOUNTED WITH INSTALLATION OF DYNON PITOT/STATIC/AOA PROBE USING GRETZ MOUNTING BRACKET KIT. SUPERIOR XP-IO-360-B1HC2 DSRV GRETZ MAST VANS RV-7 14101 SHORTENING OF HANDLE FOR TIP-UP EXISTING CANOPY JETTISON HANDLE WD-620 SHORTENED AND SECURED IN THE 'LATCHED' SUPERIOR XP-IO-360-B1HC2 RVDB CANOPY FORWARD HINGE RELEASE POSITION TO SUB-PANEL F-768 USING P-CLIPS, AN BOLTS AND ANCHOR NUTS. HANDLE NO MECHANISM LONGER AVAILABLE FOR IN-FLIGHT OPERATION BUT FACILITATES REMOVAL OF CANOPY FOR MAINTENANCE. VANS RV-7 14102 DYNON HEATED PITOT/AOA HEAD ON INSTALLATION OF DYNON HEATED PITOT/AOA HEAD ON SAFEAIR1 MAST IN ACCORDANCE WITH SUPERIOR XP-IO-360-B1HC2 RVDB SAFEAIR1 MAST INSTALLATION SAFEAIR1 INSTRUCTIONS. HEATER CONTROLLER MOUNTED TO AILERON BELLCRANK ACCESS COVER. VANS RV-7 14103 DUAL AXIS AUTO-PILOT INSTALLATION INSTALLATION OF DUAL AXIS AUTO-PILOT. ROLL CONTROL PROVIDED BY TRIO EZ PILOT AND PITCH SUPERIOR XP-IO-360-B1HC2 RVDB CONTROL PROVIDED BY GRAND RAPIDS GRT SPORT EFIS.

ROLL SERVO - TRIO GOLD STANDARD SERVO MOUNTED TO TRIO MOUNTING BRACKET (POST AUGUST 2009 VERSION) IN STARBOARD WING IN ACCORDANCE WITH TRIO DOCUMENT RV 7, 8, 9 & 10 INSTALLATION KIT. SERVO ARM SAFETY WASHER INSTALLED IN ACCORDANCE WITH LAA AIRWORTHINESS INFORMATION LEAFLET MOD/EQUIP/002 ISSUE 1.

PITCH SERVO - GRAND RAPIDS (GRT) AP-SERVO-PITCH-B MOUNTED IN REAR FUSELAGE ON PITCH IDLER BELLCRANK RIB F-729A USING TRUTRAK MOUNTING BRACKET IN ACCORDANCE WITH GRT INSTALLATION INSTRUCTIONS. ADDITIONAL SUPPORT TO F-729A RIB PROVIDED BY TRANSVERSE PARTIAL BULKHEAD INSTALLED AS PART OF CUSTOM MADE AVIONICS MOUNTING TRAY.

VANS RV-7 14843 RV7 INSTRUMENT PANEL SUPPORT INSTRUMENT PANEL SUPPORT STRUCTURE MODIFIED TO ENABLE INSTALLATION OF EFIS AND NAV SUPERIOR XP-IO-360-B1HC2 RVDB MODIFICATION RECEIVER, CONSISTING OF MODIFIED PORT PANEL SUPPORT BRACKET AND NEW APERTURE IN SUB- PANEL, REINFORCED WITH ANGLES. VANS RV-7 14845 FUEL SYSTEM IMPLEMENTATION ANDAIR GASCOLATOR GAS375-M INSTALLED BETWEEN EACH FUEL TANK AND SELECTOR VALVE SUPERIOR XP-IO-360-B1HC2 RVDB FS20X7-T, LOCATED IN WING ROOT ON ALLOY BRACKETS. ANDAIR HIGH PRESSURE FUEL PUMP PX375-TC INSTALLED DOWNSTREAM OF SELECTOR VALVE. FLOSCAN 201B FUEL FLOW SENSOR INSTALLED DOWNSTREAM OF ELECTRIC FUEL PUMP. FINE FILTER INSTALLED DOWNSTREAM OF MECHANICAL FUEL PUMP. VANS RV-7 14897 FITTING OF AIRWORLD UK TWIN HEAD AIRWORLD SKYFLASH STROBE SYSTEM INSTALLED, CONSISTING OF A POWER UNIT MOUNTED SUPERIOR XP-IO-360-B1HC2 RVDB SKYFLASH STROBE SYSTEM UNDER CHANNEL F-732A, A STROBE HEAD MOUNTED AT THE TOP OF THE FIN, AND A STROBE HEAD MOUNTED BENEATH THE COCKPIT. VANS RV-7 13205 SKYBOLT CLOC COWL FASTENING INSTALLATION OF SKYBOLT CLOC COWLING FASTENER KIT FOR RV AIRCRAFT. INSTALLATION SUPERIOR XP-IO-360-A1AC2 RVTB INCORPORATES ALUMINIUM ALLOY STRIPS RIVETED TO FIREWALL AND COWLS, IN ACCORDANCE WITH SKYBOLT INSTRUCTIONS "2007 VANS RV AND OTHER KIT PLANE INSTRUCTIONS".

VANS RV-7 14471 NAV LIGHTS/STROBES INSTALLATION OF WHELEN LED MICROBURST II WING TIP NAV/STROBE LIGHTS AND TAIL SUPERIOR XP-IO-360-A1AC2 RVTB NAV/STROBE LIGHT (MB2G & MB1WT), FITTED IN ACCORDANCE WITH MANUFACTURER'S INSTRUCTIONS.

AT ISSUE 2, WHELEN A555 TAIL LIGHT UNIT ADDED AS ALTERNATIVE TO MB1WT.

Prototype mods that have been approved since 1/1/2008 Page 124 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-7 13847 SLIDING CANOPY FITMENT WITH VANS SLIDING CANOPY TRANSPARENCY BONDED IN PLACE USING SIKAFLEX 295 ADHESIVE IN SUPERIOR XP-IO-360-A1AC2 RVTB ADHESIVE PLACE OF SCREWS. ALUMINIUM ALLOY 'SKIRTS' RETAINED FOR ADDITIONAL SECURITY. VANS RV-7 14769 GARMIN GAP26 PITOT PROBE ON GRETZ GRETZ PITOT MAST FITTED TO UNDERSIDE OF WING OUTBOARD OF INSPECTION HATCH COVER IN SUPERIOR XP-IO-360-A1AC2 RVTB MOUNT ACCORDANCE WITH MANUFACTURER'S INSTRUCTIONS. MAST FITTED WITH A GARMIN GAP26 PITOT HEAD. AOA PORT AND HEATING FUNCTION NOT CONNECTED. VANS RV-7 14185 MGL AVIONICS DUAL AXIS AUTO-PILOT ISSUE 1. INSTALLATION OF MGL DUAL AXIS AUTO-PILOT USING STRATOMASTER ODYSSEY EFIS SUPERIOR XP-IO-360-A1AC2 RVTB INSTALLATION CONTROL UNIT.

ISSUE 2. INSTALLATION OF MGL DUAL AXIS AUTO-PILOT USING iEFIS LITE EXPLORER CONTROL UNIT.

MGL ROLL SERVO MOUNTED IN STARBOARD WING USING DYNON MOUNTING HARDWARE AND IN ACCORDANCE WITH DYNON AUTOPILOT SERVO INSTALLATION GUIDE 101046-003 REV G OR LATER. MGL PITCH SERVO MOUNTED IN REAR FUSELAGE USING DYNON MOUNTING HARDWARE AND IN ACCORDANCE WITH DYNON AUTOPILOT SERVO INSTALLATION GUIDE 101046-005 REV F OR LATER. AUTO-PILOT SETTINGS ARE AS RECORDED IN LAA/FT-AP DATED 25/10/2015.

VANS RV-7 15203 GT3/G37-SAE2-RTWS-180, 180CM INSTALLATION OF GT3/G37-SAE2-RTWS-180, 180CM DIAMETER GROUND ADJUSTABLE PROPELLER. SUPERIOR XP-IO-360-A1AC2 RVTB DIAMETER PROPELLER INSTALLATION VANS RV-7A 14568 IFR CLEARANCE IFR CLEARANCE SOUGHT USING LAA ESTABLISHED PROCESS LYCOMING IO-360-A1B6 PROS VANS RV-7A 11217 BONDING OF PLEXIGLASS CANOPY (TIP- SIKAFLEX 295 UV ADHESIVE COMPOUND USED TO ATTACH CANOPY BUBBLE IN LIEU OF MULTIPLE LYCOMING IO-360-M1B CILG UP OR SLIDER) FOR RV-7/7A & RV-9/9A AN507-6R8 SCREWS.

ISSUE 2: MODIFICATION APPLICABILITY EXTENDED TO INCLUDE RV9/9A AIRCRAFT SERIES. ISSUE 3: NOW INCLUDES BOTH TIP-UP AND SLIDING CANOPY AND WINDSCREEN. VANS RV-7A 14034 DYNON HEATED PITOT AND SAFEAIR1 INSTALLATION OF DYNON HEATED PITOT PROBE (POST OCTOBER 2014 MODEL) MOUNTED ON LYCOMING IO-360-M1B CILG PITOT MAST SAFEAIR1 MAST TO PORT WING UNDERSIDE IN ACCORDANCE WITH DYNON AND SAFEAIR1 INSTRUCTIONS. VANS RV-7A 14177 FITMENT OF SINGLE P114 P MAG UNITS E-MAG IGNITION P-114 P-MAG ELECTRONIC IGNITION UNIT INSTALLED IN PLACE OF STARBOARD LYCOMING IO-360-M1B CILG MAGNETO IN ACCORDANCE WITH THE MANUFACTURER'S INSTRUCTIONS, INCLUDING BLAST COOLING AND TEMPERATURE-SENSITIVE LABELS. VANS RV-7A 14216 INSTALLATION OF DYNON SKYVIEW DYNON SKYVIEW DUAL AXIS AUTOPILOT INSTALLATION. LYCOMING IO-360-M1B CILG DUAL AXIS AUTOPILOT ROLL SERVO INSTALLED IN ACCORDANCE WITH DYNON SERVO MOUNTING INSTRUCTIONS - RV- 7/8/10 ROLL KIT 101046-003 REV H. PITCH SERVO INSTALLED IN ACCORDANCE WITH DYNON SERVO MOUNTING INSTRUCTIONS - RV- 6/7/9 PITCH KIT 101046-005 REV F. VANS RV-7A 14821 GARMIN G3X TOUCH DUAL AXIS AUTO- INSTALLATION OF GARMIN G3X TOUCH DUAL AXIS AUTO-PILOT WITH GMC 307 CONTROLLER. GSA LYCOMING O-320-D1A JFRV PILOT INSTALLATION 28 SERVOS INSTALLED IN ACCORDANCE WITH GARMIN DOCUMENT 190-01115-01 REV. V.

VANS RV-7A 14822 GARMIN GAP 26 HEATED PITOT/AOA INSTALLATION ON PORT WING UNDERSIDE OF GARMIN GAP 26 HEATED (NOT REGULATED) LYCOMING O-320-D1A JFRV HEAD ON GRETZ MAST INSTALLATION PITOT/AOA HEAD ON GRETZ MAST. VANS RV-7A 14640 G3X TOUCH, G5 & GNC255A SYSTEM AVIONICS UPGRADE, INCLUDING VP-X SPORT POWER DISTRIBUTION SYSTEM, INSTALLED IN NEW LYCOMING O-360-A1A PPLL INSTALLATION INSTRUMENT PANEL. PANEL MOUNTING STRUCTURE MODIFIED TO ACCOMMODATE EFIS DISPLAYS. INCLUDES MOUNTING OF SENSORS, WIRING, CIRCUIT PROTECTION AND SWITCHING.

VANS RV-7A 15473 BERINGER WHEELS BERINGER WHEELS, BRAKES AND ANTI-SKID REGULATOR SUBSTITUTED, IN ACCORDANCE WITH LYCOMING O-360-A1A PPLL BERINGER INSTALLATION MANUAL

Prototype mods that have been approved since 1/1/2008 Page 125 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-7A 14185 MGL AVIONICS DUAL AXIS AUTO-PILOT ISSUE 1. INSTALLATION OF MGL DUAL AXIS AUTO-PILOT USING STRATOMASTER ODYSSEY EFIS LYCOMING YIO-360-M1B EGSR INSTALLATION CONTROL UNIT.

ISSUE 2. INSTALLATION OF MGL DUAL AXIS AUTO-PILOT USING iEFIS LITE EXPLORER CONTROL UNIT.

MGL ROLL SERVO MOUNTED IN STARBOARD WING USING DYNON MOUNTING HARDWARE AND IN ACCORDANCE WITH DYNON AUTOPILOT SERVO INSTALLATION GUIDE 101046-003 REV G OR LATER. MGL PITCH SERVO MOUNTED IN REAR FUSELAGE USING DYNON MOUNTING HARDWARE AND IN ACCORDANCE WITH DYNON AUTOPILOT SERVO INSTALLATION GUIDE 101046-005 REV F OR LATER. AUTO-PILOT SETTINGS ARE AS RECORDED IN LAA/FT-AP DATED 25/10/2015.

VANS RV-7A 14200 FALCON PITOT TUBE INSTALLATION FALCON 12-AN 5812 HEATED PITOT HEAD MOUNTED ON UNDERSIDE OF PORT WING USING A LYCOMING YIO-360-M1B EGSR FALCON 30-PT2000 MOUNT AND CUSTOM-MADE WING SKIN DOUBLER AND REINFORCING ANGLES. INCLUDES ASSOCIATED WIRING AND SWITCHABLE 15A CIRCUIT BREAKER. VANS RV-7A 15022 FLYBOYS SUPERTRACKS CANOPY TRACK FLYBOYS SUPERTRACKS CANOPY TRACK EXTENSION, CONSISTING OF A PORT AND STARBOARD LYCOMING YIO-360-M1B EGSR EXTENSION MACHINED EXTENSION TRACKS, A SPINE RAIL EXTENSION INSTALLED AND ASSOCIATED FITTINGS AND FASTENERS. INSTALLED AS PER MANUFACTURER'S INSTRUCTIONS. VANS RV-7A 13431 DYNON SKYVIEW AUTO PILOT INSTALLATION OF TWO DYNON SV32 SERVOS IN ACCORDANCE WITH MANUFACTURER'S LYCOMING YIO-360-M1B UKRV INSTRUCTIONS TO CONTROL PITCH AND ROLL. SERVOS CONTROLLED BY DYNON SKYVIEW UNIT. TO AVOID ECESSIVE PITCH RATES, ALTITUDE HOLD RATE OF CLIMB AND DESCENT LIMITS TO BE SET TO 500 FPM AS PROVEN IN FLIGHT TESTS ON THIS AND SIMILAR INSTALLATIONS

VANS RV-7A 13431 DYNON SKYVIEW AUTO PILOT INSTALLATION OF TWO DYNON SV32 SERVOS IN ACCORDANCE WITH MANUFACTURER'S LYCOMING YIO-360-M1B IIRV INSTRUCTIONS TO CONTROL PITCH AND ROLL. SERVOS CONTROLLED BY DYNON SKYVIEW UNIT. (MODIFIED) TO AVOID ECESSIVE PITCH RATES, ALTITUDE HOLD RATE OF CLIMB AND DESCENT LIMITS TO BE SET TO 500 FPM AS PROVEN IN FLIGHT TESTS ON THIS AND SIMILAR INSTALLATIONS

VANS RV-7A 13432 USE OF CLICK BOND NUTPLATES CLICK BOND WING TIP KIT KA100E2CN614CR06P (6/32 STAINLESS STEEL TWO LUG MINATURE LYCOMING YIO-360-M1B IIRV NUTPLATES) USED TO FASTEN WING TIPS. 7 OFF CN614CR06P ADDITIONALLY USED TO FASTEN (MODIFIED) TAILPLANE FAIRING. VANS RV-7A 11217 BONDING OF PLEXIGLASS CANOPY (TIP- SIKAFLEX 295 UV ADHESIVE COMPOUND USED TO ATTACH CANOPY BUBBLE IN LIEU OF MULTIPLE LYCOMING YIO-360-M1B IIRV UP OR SLIDER) FOR RV-7/7A & RV-9/9A AN507-6R8 SCREWS. (MODIFIED)

ISSUE 2: MODIFICATION APPLICABILITY EXTENDED TO INCLUDE RV9/9A AIRCRAFT SERIES. ISSUE 3: NOW INCLUDES BOTH TIP-UP AND SLIDING CANOPY AND WINDSCREEN. VANS RV-7A 13205 SKYBOLT CLOC COWL FASTENING INSTALLATION OF SKYBOLT CLOC COWLING FASTENER KIT FOR RV AIRCRAFT. INSTALLATION LYCOMING YIO-360-M1B IIRV INCORPORATES ALUMINIUM ALLOY STRIPS RIVETED TO FIREWALL AND COWLS, IN ACCORDANCE (MODIFIED) WITH SKYBOLT INSTRUCTIONS "2007 VANS RV AND OTHER KIT PLANE INSTRUCTIONS".

VANS RV-7A 14155 CUSTOM MADE PITOT MAST INSTALLATION OF DYNON PITOT/AOA P/N 100141-000 HEAD USING CUSTOM MADE MAST. MAST LYCOMING YO-320-D1A DMPL IS FABRICATED FROM STEEL SHEETING INTO AN AEROFOIL SHAPE WITH TIG WELDED BASE PLATE AND 0.032"ALUMINIUM ALLOY SKIN REINFORCING PLATE, SIMILAR IN DESIGN TO THE SAFEAIR1 MAST. MAST IS MOUNTED TO UNDERSIDE OF PORT WING AFT OF MAIN SPAR AND OUTBOARD OF INSPECTION HATCH. DEVICE CONNECTS TO DYNON SKYVIEW UNIT WHICH PROVIDES ANGLE OF ATTACK INDICATION AND WARNINGS.

Prototype mods that have been approved since 1/1/2008 Page 126 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-7A 14158 DYNON SKYVIEW DUAL AXIS AUTO PILOT INSTALLATION OF DYNON SKYVIEW DUAL AXIS AUTO-PILOT WITH ROLL SERVO MOUNTED IN LYCOMING YO-320-D1A DMPL INSTALLATION STARBOARD WING ADJACENT TO AILERON BELLCRANK IN ACCORDANCE WITH DYNON INSTALLATION INSTRUCTIONS DOCUMENT 101046-003, REV G AND PITCH SERVO MOUNTED IN REAR FUSELAGE ADJACENT TO PITCH IDLER IN ACCORDANCE WITH DYNON INSTALLATION INSTRUCTIONS DOCUMENT 101046-005, REV F. SERVOS ARE DYNON SV32 UNITS CONTROLLED BY A SKYVIEW D1000. VANS RV-7A 15000 GARMIN G5 DUAL AXIS AUTOPILOT INSTALLATION OF GARMIN G5 DUAL AXIS AUTO-PILOT WITH GARMIN GMC 507 CONTROLLER LYCOMING YO-360-A1A RVEM INSTALLATION USING GARMIN G3X INSTALLATION MANUAL 190-01115-01 REV AF. ROLL SERVO INSTALLED USING GARMIN 011-02952-12 RV-7/8/10 ROLL INSTALLATION KIT. PITCH SERVO INSTALLED USING GARMIN 011-02952-014 RV-6/7/9 PITCH INSTALLATION KIT. VANS RV-7A 15035 FT-60 FUEL FLOW TRANSDUCER INSTALLATION OF ELECTRONICS INTERNATIONAL FT-60 FUEL FLOW TRANSDUCER BETWEEN LYCOMING YO-360-A1A RVEM INSTALLATION MECHANICAL FUEL PUMP AND CARBURETTOR. VANS RV-7A 12540 DYNON PITOT PROBE MOUNTED WITH INSTALLATION OF DYNON PITOT/STATIC/AOA PROBE USING GRETZ MOUNTING BRACKET KIT. LYCOMING YO-360-A1A JCIH GRETZ MAST VANS RV-7A 13103 STALL WARNER STANDARD VANS VANE TYPE STALL WARNER FITTED, WITH ADDITIONAL AUDIO BUZZER IN LYCOMING YO-360-A1A CTED COCKPIT. VANS RV-7A 13104 DYNON DUAL AXIS AUTO-PILOT INSTALLATION OF DYNON DUAL AXIS AUTO-PILOT WITH ROLL SERVO MOUNTED IN STARBOARD LYCOMING YO-360-A1A CTED INSTALLATION WING DRIVING AILERON BELLCRANK VIA SHORT PUSH-ROD AND 0.875 INCH LONG PILLAR AND PITCH SERVO IN REAR FUSELAGE DRIVING PITCH IDLER BELLCRANK VIA SHORT PUSHROD.

SERVOS DRIVEN BY A DYNON D100 EFIS AND A DYNON AP74 CONTROLLER.

VANS RV-7A 13428 GRETZ PITOT TUBE BRACKET KIT GRETZ AERO PITOT TUBE BRACKET KIT CBK-12 FITTED IN ACCORDANCE WITH THE LYCOMING YO-360-A1A CTED MANUFACTURER'S INSTRUCTIONS ON PORT WING, OUTBOARD OF LOWER INSPECTION ACCESS COVER PLATE. INSTALLATION OF PITOT TUBE IN THIS POSITION ABANDONED BUT GRETZ BRACKET LEFT INSTALLED WITH 0.125" ALLOY PLATE TO COVER OPENING USING SAME FASTENERS.

VANS RV-7A 14237 DYNON SKYVIEW DUAL AXIS AUTO-PILOT INSTALLATION OF DYNON SKYVIEW DUAL AXIS AUTO-PILOT WITH ROLL SERVO INSTALLED IN LYCOMING O-360-A1G6 COLS INSTALLATION ACCORDANCE WITH DYNON SERVO INSTALLATION GUIDE 101046-003 REVISION F AND THE PITCH (MODIFIED) SERVO INSTALLED IN ACCORDANCE WITH DYNON SERVO INSTALLATION GUIDE 101046-005 REVISION F.

PITCH SERVO PROVIDES ALTITUDE HOLD CAPABILITY ONLY DUE TO LACK OF LINKED NAVIGATION EQUIPMENT THAT IS REQUIRED TO ENABLE AUTOMATIC CLIMB, DESCENT AND ALTITUDE CAPTURE CAPABILITY. CLIMB AND DESCENT TESTING REQUIRED SHOULD LINKED NAVIGATION EQUIPMENT BE INSTALLED. VANS RV-7A 14034 DYNON HEATED PITOT AND SAFEAIR1 INSTALLATION OF DYNON HEATED PITOT PROBE (POST OCTOBER 2014 MODEL) MOUNTED ON SUPERIOR XP-IO-360-B2CA2 RMRV PITOT MAST SAFEAIR1 MAST TO PORT WING UNDERSIDE IN ACCORDANCE WITH DYNON AND SAFEAIR1 INSTRUCTIONS. VANS RV-7A 14035 TRIO PRO PILOT DUAL AXIS AUTO-PILOT INSTALLATION OF TRIO PRO PILOT DUAL AXIS AUTO-PILOT AND PITCH CONTROL SERVO TO SUPERIOR XP-IO-360-B2CA2 RMRV INSTALLATION UPGRADE ROLL ONLY FACILITY OF PREVIOUSLY FITTED TRIO EZ PILOT. PITCH SERVO MOUNTED IN REAR FUSELAGE ON TRAY SUPPORTED BY TWO TRIANGULAR GUSSETS WITH PUSH-ROD CONNECTED TO PITCH SYSTEM IDLER BELLCRANK. LAA-MOD/EQUIP/002 ISS 1 INCORPORATED ON BOTH SERVOS. VANS RV-7A 14355 REPLACE LIGHTSPEED IGNITION WITH REPLACE SINGLE LIGHTSPEED IGNITION WITH SINGLE EMAG, OTHER IGNITION BY STANDARD SUPERIOR XP-IO-360-B2CA2 RMRV MODEL 114 E MAG MAGNETO

Prototype mods that have been approved since 1/1/2008 Page 127 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-7A 14058 TRIO PRO PILOT DUAL AXIS AUTO-PILOT INSTALLATION OF TRIO PRO PILOT DUAL AXIS AUTO-PILOT UTILISING A NAVAID DEVICES ROLL TITAN OX-340-A4B2T8 DPRV INSTALLATION SERVO MOUNTED UNDER THE P2 SEAT COUPLED TO THE AILERON CONTROL ROD AT THE BOTTOM OF THE P2 CONTROL COLUMN AND A TRIO PITCH SERVO MOUNTED ON A TRAY IN THE REAR FUSELAGE AND COUPLED TO THE PITCH PUSH-ROD IDLER.

AT ISSUE 2: ROLL SERVO MAY ALSO BE INSTALLED IN THE RIGHT WING AT THE AILERON BELLCRANK POSITION USING THE TRIO RV 7/8/9/10 INSTALLATION KIT. VANS RV-8 12663 SA-101H SMOKE SYSTEM INSTALLATION SMOKE SYSTEM INSTALLED IN ACCORDANCE WITH APPLICANT DETAILS LYCOMING AEIO-360-A1A WIKD TO RV-8 FORWARD BAGGAGE BAY

VANS RV-8 13220 LIGHTSPEED PLASMA III IGNITION INSTALLATION OF A LIGHTSPEED ENGINEERING PLASMA III IGNITION SYSTEM IN PLACE OF THE LYCOMING AEIO-360-A1A WIKD SYSTEM STARBOARD MAGNETO. VANS RV-8 13733 REAR SEAT EFIS SCREEN FRONT SEAT BACK EXTENDED TO MOUNT EFIS SCREEN VISIBLE IN FRONT OF REAR OCCUPANT, LYCOMING AEIO-360-A1B6 LSPH WITH SHAPED GLASS FIBRE COVER VANS RV-8 13547 SINGLE E-MAG P-114 ELECTRONIC SUBSTITUTION OF RIGHT HAND MAGNETO WITH E-MAG P-114 ELECTRONIC IGNITION UNIT. LYCOMING AEIO-360-A1B6 RVPL IGNITION UNIT INSTALLATION VANS RV-8 12276 INSTALLATION OF 'BELL' TAILWHEEL INSTALLATION OF 'BELL' TAILWHEEL FORK TO INCREASE GROUND CLEARANCE OF FUSELAGE REAR LYCOMING AEIO-360-A1B6 RVPL FORK IN ACCORDANCE WITH DRAWINGS STATED BELOW. VANS RV-8 12999 SMOKE SYSTEM INSTALLATION OF SMOKING AIRPLANES LLC SA-101H VCAS SMOKE SYSTEM IN ACCORDANCE WITH LYCOMING AEIO-360-A1B6 RVPL THE MANUFACTURER'S INSTRUCTIONS, WITH THE ADDITION OF AN ANDAIR NON-RETURN VALVE AT THE BULKHEAD. TANK INSTALLED IN REAR BAGGAGE BAY. VANS RV-8 13858 PROPELLER CHANGE TO MTV-12B/183- INSTALLATION OF MTV-12-B/183-59b PROPELLER WITH MT P-420-3 GOVERNOR. LYCOMING AEIO-360-A1B6 RVPL 59b VANS RV-8 14947 SUPERIOR AIR PARTS LIGHTWEIGHT INSTALLATION OF SUPERIOR AIR PARTS CAST ALUMINIUM LIGHTWEIGHT COLD AIR SUMP. LYCOMING AEIO-360-A1B6 RVPL COLD AIR SUMP INSTALLATION VANS RV-8 15216 INSTALLATION OF AIRFLOW AIRFLOW PERFORMANCE FM-200A FUEL INJECTION UNIT INSTALLED. LOWER ENGINE COWLING LYCOMING AEIO-360-A1B6 RVPL PERFORMANCE FM-200A FUEL MODIFIED TO ACCEPT A RAM-AIR INLET DIRECT TO A CONICAL AIR FILTER MOUNTED TO THE FUEL INJECTION UNIT INJECTION UNIT. VANS RV-8 13662 EFIS, AVIONICS & AUTOPILOT UPGRADE GARMIN G3X WITH GMC 305 CONTROLLER INTERFACE DUAL AXIS AUTO-PILOT USING GSA 28 LYCOMING AEIO-360-A1B6 GRVY SERVOS INSTALLED IN ACCORDANCE WITH GARMIN G3X INSTALLATION MANUAL 190-01115-01 REV J. PITCH SERVO INSTALLED ADJACENT TO PITCH PUSH-RODS IDLER IN FUSELAGE REAR USING GARMIN MOUNTING KIT. ROLL SERVO INSTALLED IN STARBOARD WING ADJACENT TO AILERON BELLCRANK USING GARMIN MOUNTING KIT. USER-ACCESSIBLE PARAMETERS SET UP AS RECORDED ON ATTACHED SHEET TITLED 'G-GRVY AUTOPILOT SETUP'. VANS RV-8 12999 SMOKE SYSTEM INSTALLATION OF SMOKING AIRPLANES LLC SA-101H VCAS SMOKE SYSTEM IN ACCORDANCE WITH LYCOMING AEIO-360-A1B6 LEXY THE MANUFACTURER'S INSTRUCTIONS, WITH THE ADDITION OF AN ANDAIR NON-RETURN VALVE AT THE BULKHEAD. TANK INSTALLED IN REAR BAGGAGE BAY. VANS RV-8 12355 TRUTRAK DIGIFLIGHT II VS AUTO PILOT INSTALLATION OF TRUTRAK DIGIFLIGHT II VS AUTOPILOT IN ACCORDANCE WITH TRUTRAK FLIGHT LYCOMING HO-360-B1B NFON SYSTEMS INSTALLATION INSTRUCTIONS SPECIFIED FOR THE VANS RV-8. VANS RV-8 12276 INSTALLATION OF 'BELL' TAILWHEEL INSTALLATION OF 'BELL' TAILWHEEL FORK TO INCREASE GROUND CLEARANCE OF FUSELAGE REAR LYCOMING IO-320-B1A CEGI FORK IN ACCORDANCE WITH DRAWINGS STATED BELOW. VANS RV-8 12247 PROPELLER CHANGE CHANGE OF PROPELLER TO SENSENICH W71T5HM8-85 LYCOMING IO-360-A1B CDDY VANS RV-8 14758 CATTO 3 BLADED 68" X 77" PROPELLER INSTALLATION OF CATTO 3 BLADED 68" X 77" PROPELLER. LYCOMING IO-360-A1B CDDY INSTALLATION VANS RV-8 14022 INSTALLATION OF DUAL P-MAGS INSTALLATION OF TWO E-MAG P-MAGS, MODEL P114-L4, ELECTRONIC IGNITION SYSTEMS. LYCOMING IO-360-A1B6 ZAAZ VANS RV-8 13220 LIGHTSPEED PLASMA III IGNITION INSTALLATION OF A LIGHTSPEED ENGINEERING PLASMA III IGNITION SYSTEM IN PLACE OF THE LYCOMING IO-360-A1B6 LEXX SYSTEM STARBOARD MAGNETO. VANS RV-8 12355 TRUTRAK DIGIFLIGHT II VS AUTO PILOT INSTALLATION OF TRUTRAK DIGIFLIGHT II VS AUTOPILOT IN ACCORDANCE WITH TRUTRAK FLIGHT LYCOMING IO-360-A1B6 LEXX SYSTEMS INSTALLATION INSTRUCTIONS SPECIFIED FOR THE VANS RV-8. Prototype mods that have been approved since 1/1/2008 Page 128 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-8 12999 SMOKE SYSTEM INSTALLATION OF SMOKING AIRPLANES LLC SA-101H VCAS SMOKE SYSTEM IN ACCORDANCE WITH LYCOMING IO-360-A1B6 OCTO THE MANUFACTURER'S INSTRUCTIONS, WITH THE ADDITION OF AN ANDAIR NON-RETURN VALVE AT THE BULKHEAD. TANK INSTALLED IN REAR BAGGAGE BAY. VANS RV-8 13220 LIGHTSPEED PLASMA III IGNITION INSTALLATION OF A LIGHTSPEED ENGINEERING PLASMA III IGNITION SYSTEM IN PLACE OF THE LYCOMING IO-360-A1B6 OCTO SYSTEM STARBOARD MAGNETO. VANS RV-8 14898 REPLACE VANS WINGTIPS WITH ZIPTIPS REPLACE VANS WINGTIPS WITH ZIPTIPS PREMIER WINGTIPS LYCOMING IO-360-A1B6 OGZZ PREMIER WINGTIPS VANS RV-8 14911 REPLACE MATCO 5" WHEELS WITH REPLACE MATCO 5" WHEELS WITH GROVE 6" WHEELS LYCOMING IO-360-A1B6 OGZZ GROVE 6" WHEELS VANS RV-8 13662 EFIS, AVIONICS & AUTOPILOT UPGRADE GARMIN G3X WITH GMC 305 CONTROLLER INTERFACE DUAL AXIS AUTO-PILOT USING GSA 28 LYCOMING IO-360-A1B6 OGZZ SERVOS INSTALLED IN ACCORDANCE WITH GARMIN G3X INSTALLATION MANUAL 190-01115-01 REV J. PITCH SERVO INSTALLED ADJACENT TO PITCH PUSH-RODS IDLER IN FUSELAGE REAR USING GARMIN MOUNTING KIT. ROLL SERVO INSTALLED IN STARBOARD WING ADJACENT TO AILERON BELLCRANK USING GARMIN MOUNTING KIT. USER-ACCESSIBLE PARAMETERS SET UP AS RECORDED ON ATTACHED SHEET TITLED 'G-GRVY AUTOPILOT SETUP'. VANS RV-8 12944 SHOW PLANES FASTBACK CONVERSION INSTALLATION OF SHOW PLANES FASTBACK CONVERSION KIT IN ACCORDANCE WITH THE SHOW LYCOMING IO-360-A1B6 OGZZ PLANES MANUAL, EXCEPT ADDITION OF ROLL BAR IS REQUIRED. VANS RV-8 12884 RAVEN INVERTED OIL SYSTEM INSTALLATION OF INVERTED OIL SYSTEM FROM RAVEN AIRCRAFT CORPORATION, USA. LYCOMING IO-360-A1B6 OGZZ

ISSUE 2, 14/3/16: OPTIONALLY, A 'HALF' RAVEN OIL SYSTEM MAY BE FITTED, WHICH USES JUST THE OIL SEPARATOR AND NOT THE OIL VALVE. VANS RV-8 14926 INSTALL CONDOR TAILWHEEL WITH 8 INSTALL CONDOR TAILWHEEL WITH 8 PNEUMATIC TYRE LYCOMING IO-360-A1B6 OGZZ PNEUMATIC TYRE VANS RV-8 15070 BRAKE MASTER CYLINDER LUG BRAKE MASTER CYLINDER ATTACHMENT REINFORCED TO PREVENT DISTORTION UNDER LOAD LYCOMING IO-360-A1B6 OGZZ REINFORCEMENT VANS RV-8 15074 AVIONICS SHELF INSTALLATION IN AVIONICS SHELF INSTALLATION IN REAR/MID FUSELAGE & ACCESS PANEL TO BATTERY LYCOMING IO-360-A1B6 OGZZ REAR/MID FUSELAGE & ACCESS PANEL TO BATTERY VANS RV-8 15085 SHORTENED STEP FROM RV-8A AIRCRAFT INSTALLATION OF A SHORTENED AND REINFORCED RV-8A STEP IN ACCORDANCE WITH VANS LYCOMING IO-360-A1B6 OGZZ INSTALLATION INSTRUCTIONS. VANS RV-8 15096 AEROLAB GASCOLATOR INSTALLATION IN AEROLAB GASCOLATOR INSTALLATION IN EACH WING ROOT LYCOMING IO-360-A1B6 OGZZ EACH WING ROOT VANS RV-8 15181 AUTOMATIC ALTERNATE-AIR DOOR INSTALLATION OF AUTOMATICALLY OPERATED ALTERNATE-AIR DOOR FROM ROBINSON R22 LYCOMING IO-360-A1B6 OGZZ INSTALLATION HELICOPTER, WITH ADDITION OF MICROSWITCH OPERATED 'DOOR OPEN' LAMP IN COCKPIT. VANS RV-8 15333 REPLACE STANDARD RUDDER PEDALS STANDARD VANS RUDDER PEDALS REPLACED WITH 'CONTROL APPROACH' RUDDER PEDALS. LYCOMING IO-360-A1B6 OGZZ WITH CONTROL APPROACH RUDDER PEDALS VANS RV-8 13664 INDIVIDUAL BRAKE PEDAL FLUID SINGLE VANS BRAKE FLUID RESERVOIR REMOVED WITH ASSOCIATED TUBING TO EACH MASTER LYCOMING IO-360-A1B6 OGZZ RESERVOIR CYLINDER. ACS RESERVOIR A-600 SCREWED DIRECTLY INTO EACH MASTER CYLINDER. AN EXTRA 1" LONG STEEL SLEEVE (VANS P/N F-8107) IS REQUIRED IN EACH RUDDER PEDAL ASSEMBLY TO ENSURE CLEARANCE OF RESERVOIRS WITH FIREWALL. VANS RV-8 14658 VINYL WRAPPING VINYL WRAPPING OF FUSELAGE, WING AND CONTROL SURFACES USING 3M1080 FILM. LYCOMING IO-360-A1B6 OGZZ VANS RV-8 13661 HEATED SEATS CLASSIC AERO DESIGNS HEATED SEATS SUBSTITUTED. MINOR CHANGE TO SEAT FRAME GEOMETRY LYCOMING IO-360-A1B6 OGZZ TO ACCOMMODATE HEATED SEAT CUSHIONS. VANS RV-8 13397 FLAP ACTUATOR COVER ALUMINIUM ALLOY COVER ADDED OVER FLAP ACTUATOR TO PREVENT UNINTENTIONAL LYCOMING IO-360-A1B6D NISH INTERFERNCE BY CREW OR FOD INGESTION VANS RV-8 13398 WHELEN NAV/STROBE LIGHT SYSTEM, NAV/STROBE SYSTEM FITTED, POWER UNIT IN REAR FUSELAGE ON CUSTOM BRACKET LYCOMING IO-360-A1B6D NISH SYS 1 OPTION 1

Prototype mods that have been approved since 1/1/2008 Page 129 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-8 11090 COVER PLATE AND GAITER COVER PLATE AND GAITER AROUND REAR COCKPIT CONTROL COLUMN TO PREVENT OBJECTS LYCOMING IO-360-A1B6D NISH FALLING INTO CONTROL WELL. VANS RV-8 12679 FUEL FLOW MONITORING SYSTEM INSTALLATION OF A DTS INSTRUMENTS P1094-B DISPLAY UNIT AND #74318 FUEL FLOW SENSOR, LYCOMING IO-360-B1E IIRW WITH ASSOCIATED WIRING. VANS RV-8 12962 TRIO EZ PILOT AUTO-PILOT (ROLL) ISSUE 1 DESCRIBED INSTALLATION INITIALLY OF NAVAID DEVICES AP-1 WING LEVELLER SYSTEM. LYCOMING IO-360-C1E6 HPWA WITH S-2 SERVO INSTALLED IN BENEATH THE FRONT SEAT, CONNECTED TO ROLL CONTROL SYSTEM VIA A PUSHROD. CONTROL UNIT MOUNTED IN INSTRUMENT PANEL. AT ISSUE 2, TRIO EZ-PILOT SYSTEM SUBSTITUTED BUT KEEPING EXISTING SERVO AND SERVO INSTALLATION

VANS RV-8 12963 TRUTRAK ALTRAK ALTITUDE HOLD TRUTRAK ALTRAK SYSTEM INSTALLED AS PER MANUFACTURER'S INSTRUCTIONS, EXCEPT SERVO LYCOMING IO-360-C1E6 HPWA UNIT INSTALLED ON OPPOSITE SIDE OF MOUNTING BRACKET FROM ILLUSTRATED. SYSTEMS CONSISTS OF ELECTRONIC CONTROL UNIT MOUNTED ON REAR COCKPIT BULKHEAD, A SERVO MOUNTED ON THE ELEVATOR PITCH ROD HORN IN THE REAR FUSELAGE, AND ASSOCIATED POWER AND SWITCHING. VANS RV-8 12964 AFA AV-10 ENGINE AND FUEL AUDIO FLIGHT AVIONICS AV-10 ALERTING ENGINE MONITOR AND ASSOCIATED SENSORS AND LYCOMING IO-360-C1E6 HPWA MONITORING SYSTEM SENSOR INTERFACE BOX INSTALLED AS PER INSTALLATION MANUAL. FUEL FLOW SENSOR IS A FLOSCAN 201-A MOUNTED IN THE ENGINE BAY BETWEEN THE FUEL PUMP AND INJECTOR MANIFOLD. VANS RV-8 14534 NIGHT/IFR CLEARANCE .(No FEE AS FOR RV8 AND PAID FOR FLIGHT TEST LYCOMING IO-360-C1E6 HPWA VANS RV-8 12572 SMOKE TANK, FILL DOOR AND SMOKE SMOKE SYSTEM FITTED PER APPLICATION DETAILS LYCOMING IO-360-M1B WEEV SYSTEM INSTALLATION VANS RV-8 12593 DELRIN (ACETAL) AILERON STOP PLASTIC STOP FITTED INSTEAD OF RELYING ON METAL TO METAL CONTACT, PER APPLICANT'S LYCOMING IO-360-M1B WEEV DRAWING VANS RV-8 12594 MGL 2 AXIS AUTOPILOT INSTALLATION MGL AVIONICS ODYSSEY/VOYAGER EFIS 2 AXIS AUTOPILOT WITH TRIO SERVOS. ROLL SERVO LYCOMING IO-360-M1B WEEV WITH TRIO SERVOS. INSTALLED IN TRIO VERTICAL BRACKET IN STARBOARD WING ADJACENT TO AILERON BELLCRANK. PITCH SERVO INSTALLED AFT OF ELEVATOR CONTROL IDLER BELLCRANK. VANS RV-8 12801 BONDING THE RV8/8A CANOPY AND ATTACHMENT OF CANOPY TO FRAME AND WINDSCREEN TO FUSELAGE BY BONDING USING LYCOMING IO-360-M1B WEEV WINDSHIELD SIKAFLEX-295 UV (BLACK) INSTEAD OF SCREWS AND RIVETS.

ISSUE 2: THIS MODIFICATION UPDATED TO ALLOW THE BONDING OF THE FRONT SECTION AND/OR REAR SECTION. VANS RV-8 13383 DUAL P-MAGS INSTALLATION OF E-MAGS ELECTRONIC IGNITION DUAL P114 P-MAG UNITS. LYCOMING IO-360-M1B WEEV VANS RV-8 12276 INSTALLATION OF 'BELL' TAILWHEEL INSTALLATION OF 'BELL' TAILWHEEL FORK TO INCREASE GROUND CLEARANCE OF FUSELAGE REAR LYCOMING IO-360-M1B WEEV FORK IN ACCORDANCE WITH DRAWINGS STATED BELOW. VANS RV-8 13848 PROPELLER CHANGE TO CATTO 68" X 75" INSTALLATION OF CATTO 3 BLADED 68 INCH DIAMETER X 75 INCH PITCH PROPELLER LYCOMING IO-360-M1B WEEV INCORPORATING BONDED NICKEL LEADING EDGE PROTECTION. VANS RV-8 14083 RV WING TIP/TIE DOWN GO-PRO INSTALLATION OF GO-PRO HERO 3 OR 4 CAMERA ON PURPOSE MADE MOUNTING, SUPPLIED BY LYCOMING IO-360-M1B WEEV CAMERA MOUNT PLANE AROUND LLC, USA ATTACHED TO EITHER WING TIP - UPPER SURFACE OR EITHER TIE-DOWN ATTACHMENT POINT - LOWER SURFACE IN ANY ORIENTATION. VANS RV-8 15066 REPLACEMENT WHEEL AND BRAKE BERINGER WHEELS AND BRAKE SYSTEM FITTED. BRAKE MASTER CYLINDER ATTACHMENTS LYCOMING IO-360-M1B WEEV SYSTEM (BERINGER) REINFORCED TO PREVENT FLEXURE. VANS RV-8 13677 TRUTRAK PICTORIAL PILOT AUTOPILOT TRUTRAK PICTORIAL PILOT (ROLL) AND ALTRAK (PITCH) AUTOPILOT SYSTEMS INSTALLED USING LYCOMING IO-360-M1B RRVV WITH ALTRAK ALTITUDE HOLD TRUTRAK HARDWARE AND INSTRUCTIONS. ROLL SERVO IS MOUNTED ON THE AILERON TORQUE TUBE BETWEEN THE TWO CONTROL COLUMNS AND INCORPORATES TWO ADDITIONAL RIVETS TO SECURE THE CLAMPING SADDLE TO THE TORQUE TUBE. PITCH CONTROL SERVO MOUNTED IN REAR FUSELAGE, CONNECTED TO PITCH IDLER ARM. VANS RV-8 13678 FLOSCAN 201B FUEL FLOW SENSOR FLOSCAN 201B FUEL FLOW SENSOR INSTALLED ON FIREWALL UPSTREAM OF THE FUEL PUMP. LYCOMING IO-360-M1B RRVV VANS RV-8 12999 SMOKE SYSTEM INSTALLATION OF SMOKING AIRPLANES LLC SA-101H VCAS SMOKE SYSTEM IN ACCORDANCE WITH LYCOMING IO-360-M1B RRVV THE MANUFACTURER'S INSTRUCTIONS, WITH THE ADDITION OF AN ANDAIR NON-RETURN VALVE AT THE BULKHEAD. TANK INSTALLED IN REAR BAGGAGE BAY.

Prototype mods that have been approved since 1/1/2008 Page 130 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-8 12817 PROPELLER CHANGE TO MTV-18-C/180- INSTALLATION OF MTV-18-C/180-57 3 BLADED ELECTRIC CONSTANT SPEED PROPELLER. LYCOMING O-320-D2A RVDH 57 VANS RV-8 12668 FITMENT OF 2 HINGED ACCESS DOORS TWO HINGED ACCESS PANELS FITTED FORWARD OF INSTRUMENT PANEL PER APPLICANT'S LYCOMING O-320-D2C RVIS FORWARD OF INSTRUMENT PANEL DRAWINGS VANS RV-8 12849 EXHAUST SILENCER INSTALLATION INSTALLATION OF AIRCRAFT EXHAUST TECHNOLOGIES INC STAINLESS STEEL EXHAUST SYSTEM. LYCOMING O-320-D2C RVIS EXHAUST SYSTEM COMPRISES 4-INTO-1 PIPE LAYOUT, SUPERTRAPP SILENCER AND SUPPORT FITTINGS. VANS RV-8 12276 INSTALLATION OF 'BELL' TAILWHEEL INSTALLATION OF 'BELL' TAILWHEEL FORK TO INCREASE GROUND CLEARANCE OF FUSELAGE REAR LYCOMING O-320-D2C RVIS FORK IN ACCORDANCE WITH DRAWINGS STATED BELOW. VANS RV-8 12355 TRUTRAK DIGIFLIGHT II VS AUTO PILOT INSTALLATION OF TRUTRAK DIGIFLIGHT II VS AUTOPILOT IN ACCORDANCE WITH TRUTRAK FLIGHT LYCOMING O-320-D2C RVIS SYSTEMS INSTALLATION INSTRUCTIONS SPECIFIED FOR THE VANS RV-8. VANS RV-8 15174 FLEXIBLE BRAKE PIPES ALUMINIUM ALLOY BRAKE LINES REPLACED WITH FLEXIBLE STAINLESS STEEL BRAIDED PTFE BRAKE LYCOMING O-320-D2C RVIS LINES IN SECTION OF RUN DOWN UNDERCARRIAGE LEG TO ACCOMMODATE FLEXURE IN LEG WITHOUT RISK OF CRACKING. VANS RV-8 11110 STROBE LIGHTS FOR SAFETY STROBE LIGHTS FITTED USING AIRWORLD POWER SUPPLY UNDER THE FIN LYCOMING O-320-E2A CKBE (MODIFIED) VANS RV-8 13901 FUEL SYSTEM UPGRADE STANDARD VANS FUEL SELECTOR REPLACED WITH ANDAIR FS20X2. STANDARD VANS FUEL FILTER LYCOMING O-320-E2A CKBE REPLACED WITH ANDAIR FX375M. ANDAIR GASCOLATOR GAS375F ADDED ON FORWARD FACE OF (MODIFIED) FIREWALL, INCLUDING MOUNTING BRACKET. VANS RV-8 15235 FUEL FLOW TRANSDUCER FLOSCAN 201 FUEL FLOW TRANSDUCER INSTALLED BETWEEN ENGINE DRIVEN PUMP AND FUEL LYCOMING O-320-E2A CKBE INJECTOR UNIT. (MODIFIED) VANS RV-8 12276 INSTALLATION OF 'BELL' TAILWHEEL INSTALLATION OF 'BELL' TAILWHEEL FORK TO INCREASE GROUND CLEARANCE OF FUSELAGE REAR LYCOMING O-360-A1A DUDE FORK IN ACCORDANCE WITH DRAWINGS STATED BELOW. VANS RV-8 14360 PROPELLER CHANGE TO HERCULES HERCULES 7080522-S PROPELLER SUBSTITUTED LYCOMING O-360-A1A DUDE 7080522-S VANS RV-8 13146 DUAL E MAG (P MODEL) INSTALLATION ISSUE 1: SINGLE P MAG FITTED IN ACCORDANCE WITH E MAG INSTRUCTIONS. SECOND IGNITION LYCOMING O-360-A1A RVMZ SYSTEM PROVIDED BY STANDARD SLICK MAG

ISSUE 2 BOTH IGNITION SYSTEMS REPLACED BY EMAG (P-MAG) AS FOR ISSUE 1 VANS RV-8 12966 DYNON AP47 DUAL AXIS AUTOPILOT INSTALLATION OF DYNON SV32 PITCH AND ROLL AUTO-PILOT SERVOS INTERFACED WITH DYNON LYCOMING O-360-A1A RVMZ AP47 AUTO-PILOT CONTROLLER. ROLL SERVO INSTALLED IN FUSELAGE IN ACCORDANCE WITH THE TRUTRAK METHOD WITH THE ADDITION OF TWO RIVETS TO SECURE THE CLAMPED ROLL DRIVE HORN TO THE AILERON TORQUE TUBE. VANS RV-8 12663 SA-101H SMOKE SYSTEM INSTALLATION SMOKE SYSTEM INSTALLED IN ACCORDANCE WITH APPLICANT DETAILS LYCOMING O-360-A1A RVMZ TO RV-8 FORWARD BAGGAGE BAY

VANS RV-8 13594 PROPELLER CHANGE TO HARTZELL HC- INSTALLATION OF HARTZELL HC-C2YR-1N/N7605 76 INCH DIAMETER 2 COMPOSITE BLADED LYCOMING O-360-A1A RVMZ C2YR-1N/N7605 CONSTANT SPEED PROPELLER. VANS RV-8 13637 FIT AVEOMAXX ATLAS LED WINGTIP AVEOMAXX ATLAS LED HIGH INTENSITY WINGTIP LIGHTS FITTED TO MODIFIED MOUNTINGS LYCOMING O-360-A1A RVMZ LIGHTS VANS RV-8 12739 PROPELLER CHANGE TO HARTZELL HC-C2YR-1BFP/F7497-2 PROPELLER FITTED LYCOMING O-360-A1A RVAL VANS RV-8 12804 BAGGAGE TIE DOWNS BAGGAGE TIE DOWN ANCHOR POINTS ATTACHED TO BAGGAGE BAY FLOOR USING ANCHOR NUTS LYCOMING O-360-A1A RVAL INSTEAD OF ORIGINAL VANS DESIGN USING RIVNUTS. VANS RV-8 13463 TRUTRAK ALTRAK INSTALLATION OF TRUTRAK ALTRAK ALTITUDE HOLD AUTOPILOT SYSTEM IN ACCORDANCE WITH LYCOMING O-360-A1A RVAL THE MANUFACTURER'S INSTRUCTIONS. NOTE THAT ALTHOUGH HEIGHT DEVIATION WITH THE SYSTEM ENGAGED CAN EXCEED 30 FEET, IT FALLS WITHIN THE MANUFACTURER'S EXPECTATIONS OF 50 FEET DEVIATION PROVIDED TURNS ARE KEPT WITHIN 30° BANK ANGLE. VANS RV-8 12276 INSTALLATION OF 'BELL' TAILWHEEL INSTALLATION OF 'BELL' TAILWHEEL FORK TO INCREASE GROUND CLEARANCE OF FUSELAGE REAR LYCOMING O-360-A1A RVAL FORK IN ACCORDANCE WITH DRAWINGS STATED BELOW. Prototype mods that have been approved since 1/1/2008 Page 131 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-8 14223 RUDDER PEDAL EXTENSION EXTENSIONS ADDED TO BOTTOM OF P1 RUDDER PEDALS TO ALLOW RUDDER TO BE USED LYCOMING O-360-A1A RVAL WITHOUT APPLYING INVOLUNTARY BRAKE PRESSURE VANS RV-8 12801 BONDING THE RV8/8A CANOPY AND ATTACHMENT OF CANOPY TO FRAME AND WINDSCREEN TO FUSELAGE BY BONDING USING LYCOMING O-360-A1A RVBI WINDSHIELD SIKAFLEX-295 UV (BLACK) INSTEAD OF SCREWS AND RIVETS.

ISSUE 2: THIS MODIFICATION UPDATED TO ALLOW THE BONDING OF THE FRONT SECTION AND/OR REAR SECTION. VANS RV-8 12801 BONDING THE RV8/8A CANOPY AND ATTACHMENT OF CANOPY TO FRAME AND WINDSCREEN TO FUSELAGE BY BONDING USING LYCOMING O-360-A3A TDJP WINDSHIELD SIKAFLEX-295 UV (BLACK) INSTEAD OF SCREWS AND RIVETS. (MODIFIED)

ISSUE 2: THIS MODIFICATION UPDATED TO ALLOW THE BONDING OF THE FRONT SECTION AND/OR REAR SECTION. VANS RV-8 12593 DELRIN (ACETAL) AILERON STOP PLASTIC STOP FITTED INSTEAD OF RELYING ON METAL TO METAL CONTACT, PER APPLICANT'S LYCOMING O-360-A3A TDJP DRAWING (MODIFIED) VANS RV-8 13078 DUAL P-MAGS INSTALLATION. DUAL P-MAGS REPLACING STANDARD MAGNETOS INSTALLED IN ACCORDANCE WITH LYCOMING O-360-A4A CCIR MANUFACTURER'S INSTRUCTIONS. VANS RV-8 13279 DYNON AP74 DUAL AXIS AUTOPILOT INSTALLATION OF DUAL AXIS AUTO-PILOT DRIVEN BY A DYNON D10A EFIS AND CONTROLLED VIA A LYCOMING O-360-A4A CCIR INSTALLATION DYNON AP74 USING SV32 SERVOS INSTALLED IN ACCORDANCE WITH DYNON INSTRUCTIONS AS SPECIFIED BELOW. VANS RV-8 13968 IMPROVED COWLING FASTENING MILSPEC PRODUCTS INC CAMLOC FASTENER KIT INSTALLED IN PLACE OF STANDARD VANS PIANO LYCOMING YIO-360-M1B JRVB HINGE ARRANGEMENT TO ATTACH ENGINE COWLING TO FUSELAGE, IN ACCORDANCE WITH MILSPEC INSTALLATION INSTRUCTIONS. VANS RV-8 14658 VINYL WRAPPING VINYL WRAPPING OF FUSELAGE, WING AND CONTROL SURFACES USING 3M1080 FILM. LYCOMING YIO-360-M1B JRVB VANS RV-8 13279 DYNON AP74 DUAL AXIS AUTOPILOT INSTALLATION OF DUAL AXIS AUTO-PILOT DRIVEN BY A DYNON D10A EFIS AND CONTROLLED VIA A LYCOMING YIO-360-M1B NRFK INSTALLATION DYNON AP74 USING SV32 SERVOS INSTALLED IN ACCORDANCE WITH DYNON INSTRUCTIONS AS SPECIFIED BELOW. VANS RV-8 12540 DYNON PITOT PROBE MOUNTED WITH INSTALLATION OF DYNON PITOT/STATIC/AOA PROBE USING GRETZ MOUNTING BRACKET KIT. LYCOMING YIO-360-M1B NRFK GRETZ MAST VANS RV-8 12540 DYNON PITOT PROBE MOUNTED WITH INSTALLATION OF DYNON PITOT/STATIC/AOA PROBE USING GRETZ MOUNTING BRACKET KIT. LYCOMING YIO-360-M1B CHPK GRETZ MAST VANS RV-8 13279 DYNON AP74 DUAL AXIS AUTOPILOT INSTALLATION OF DUAL AXIS AUTO-PILOT DRIVEN BY A DYNON D10A EFIS AND CONTROLLED VIA A LYCOMING YIO-360-M1B CHPK INSTALLATION DYNON AP74 USING SV32 SERVOS INSTALLED IN ACCORDANCE WITH DYNON INSTRUCTIONS AS SPECIFIED BELOW. VANS RV-8 12539 INSTRUMENT PANEL ACCESS SEE APPLICANTS DRAWINGS FOR DETAILS LYCOMING YIO-360-M1B PHVM VANS RV-8 12540 DYNON PITOT PROBE MOUNTED WITH INSTALLATION OF DYNON PITOT/STATIC/AOA PROBE USING GRETZ MOUNTING BRACKET KIT. LYCOMING YIO-360-M1B PHVM GRETZ MAST VANS RV-8 12828 DYNON D-100 DUAL AXIS AUTO-PILOT INSTALLATION OF DYNON D-100 DUAL AXIS AUTO-PILOT WITH AP-74 CONTROLLER. LYCOMING YIO-360-M1B RUVE INSTALLATION SV-32 ROLL SERVO FITTED IN ACCORDANCE WITH DYNON DOCUMENT 101046-003 REV H, AUTOPILOT SERVO INSTALLATION GUIDE RV7, RV8, RV10 ROLL. SV-32 PITCH SERVO FITTED IN ACCORDANCE WITH DYNON DOCUMENT 101046-002 REV F, AUTOPILOT SERVO INSTALLATION GUIDE RV4, RV8 PITCH WITH ADDITIONAL BRACKET TO SUPPORT SERVO ANGLE BRACKETS WHICH OVERHANG AFT OF BULKHEAD F808-1. VANS RV-8 13553 IMPROVED FUEL SYSTEM LAYOUT USING ANDAIR GAS375 GASCOLATOR INSTALLED IN LEFT WING ROOT. LYCOMING YIO-360-M1B RUVE ANDAIR COMPONENTS VANS RV-8 12276 INSTALLATION OF 'BELL' TAILWHEEL INSTALLATION OF 'BELL' TAILWHEEL FORK TO INCREASE GROUND CLEARANCE OF FUSELAGE REAR LYCOMING YIO-360-M1B RUVE FORK IN ACCORDANCE WITH DRAWINGS STATED BELOW. VANS RV-8 12539 INSTRUMENT PANEL ACCESS SEE APPLICANTS DRAWINGS FOR DETAILS LYCOMING YIO-360-M1B RUVE

Prototype mods that have been approved since 1/1/2008 Page 132 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-8 12801 BONDING THE RV8/8A CANOPY AND ATTACHMENT OF CANOPY TO FRAME AND WINDSCREEN TO FUSELAGE BY BONDING USING LYCOMING YIO-360-M1B RUVE WINDSHIELD SIKAFLEX-295 UV (BLACK) INSTEAD OF SCREWS AND RIVETS.

ISSUE 2: THIS MODIFICATION UPDATED TO ALLOW THE BONDING OF THE FRONT SECTION AND/OR REAR SECTION. VANS RV-8 14091 RV-8 IPAD GPS ATTACHMENTS 'IPAD MINI' MOUNTS INSTALLED ON FRONT INSTRUMENT PANEL AND ON A CUSTOM BRACKET IN LYCOMING YIO-360-M1B RUVE REAR COCKPIT. VANS RV-8 12539 INSTRUMENT PANEL ACCESS SEE APPLICANTS DRAWINGS FOR DETAILS LYCOMING YIO-360-M1B GAST VANS RV-8 12540 DYNON PITOT PROBE MOUNTED WITH INSTALLATION OF DYNON PITOT/STATIC/AOA PROBE USING GRETZ MOUNTING BRACKET KIT. LYCOMING YIO-360-M1B GAST GRETZ MAST VANS RV-8 12540 DYNON PITOT PROBE MOUNTED WITH INSTALLATION OF DYNON PITOT/STATIC/AOA PROBE USING GRETZ MOUNTING BRACKET KIT. LYCOMING YIO-360-M1B GORV GRETZ MAST VANS RV-8 13664 INDIVIDUAL BRAKE PEDAL FLUID SINGLE VANS BRAKE FLUID RESERVOIR REMOVED WITH ASSOCIATED TUBING TO EACH MASTER LYCOMING YIO-360-M1B GORV RESERVOIR CYLINDER. ACS RESERVOIR A-600 SCREWED DIRECTLY INTO EACH MASTER CYLINDER. AN EXTRA 1" LONG STEEL SLEEVE (VANS P/N F-8107) IS REQUIRED IN EACH RUDDER PEDAL ASSEMBLY TO ENSURE CLEARANCE OF RESERVOIRS WITH FIREWALL. VANS RV-8 11108 STALL WARNER REDDISH TYPE STALL WARNING INSTALLED IN ACCORDANCE WITH MANUFACTURER'S LYCOMING YIO-360-M1B GORV INSTRUCTIONS. VANS RV-8 13673 VANS WHELAN LN SYS 6 LIGHTING INSTALLATION OF WHELAN LN SYS 6 LIGHTING SYSTEM INCORPORATING WHELAN STROBE UNITS LYCOMING YIO-360-M1B GORV IN FLUSH-MOUNTED WING TIP FAIRINGS AND LOWER RUDDER FAIRING, POWER SUPPLY UNIT MOUNTED ON STARBOARD FUSELAGE BETWEEN MID LONGERON F-888-R-1 AND LOWER LONGERON F-889-R-1, AND ASSOCIATED ELECTRICAL CONNECTIONS. VANS RV-8 13674 RV-8 TIE DOWN RINGS FOR AFT 4 BAGGAGE TIE-DOWN POINTS ADDED TO BAGGAGE COMPARTMENT AT EACH CORNER. EACH LYCOMING YIO-360-M1B GORV BAGGAGE FLOOR CONSISTS OF A VANS 'CA BAGGAGE TIE DOWN KIT' WITH A 5" X 5" 0.063" THICK 2024-T3 DOUBLER PLATE BELOW THE COMPARTMENT FLOOR. DOUBLER IS FASTENED BY A GRID OF 20 OFF LP4-3 RIVETS. VANS RV-8 13966 DYNON DUAL AXIS AUTO-PILOT INSTALLATION OF DYNON SKYVIEW DUAL AXIS AUTO-PILOT. LYCOMING YIO-360-M1B GORV INSTALLATION ROLL SERVO MOUNTED IN STARBOARD WING BESIDE AILERON BELLCRANK, WITH PUSH-ROD DRIVING A MODIFIED AILERON BELLCRANK, IN ACCORDANCE WITH DYNON AVIONICS AUTOPILOT SERVO INSTALLATION GUIDE DOCUMENT 101046-003 REV. G.

PITCH SERVO MOUNTED IN REAR FUSELAGE, WITH PUSH-ROD DRIVING PITCH PUSH-ROD IDLER, IN ACCORDANCE WITH DYNON AVIONICS AUTOPILOT SERVO INSTALLATION GUIDE, DOCUMENT 101046-002 REV. F.

ADDITIONAL SUPPORT BRACKET INSTALLED TO BRACE DYNON SUPPLIED ANGLES WHERE THEY OVERHANG A FUSELAGE FRAME.

PITCH TRIM SERVO OPERATING SPEED REDUCED TO 50% STANDARD SPEED VIA THE PREVIOUSLY INSTALLED VERTICAL POWER VP-100. VANS RV-8 12276 INSTALLATION OF 'BELL' TAILWHEEL INSTALLATION OF 'BELL' TAILWHEEL FORK TO INCREASE GROUND CLEARANCE OF FUSELAGE REAR LYCOMING YIO-360-M1B RVOM FORK IN ACCORDANCE WITH DRAWINGS STATED BELOW. VANS RV-8 12355 TRUTRAK DIGIFLIGHT II VS AUTO PILOT INSTALLATION OF TRUTRAK DIGIFLIGHT II VS AUTOPILOT IN ACCORDANCE WITH TRUTRAK FLIGHT LYCOMING YIO-360-M1B RVOM SYSTEMS INSTALLATION INSTRUCTIONS SPECIFIED FOR THE VANS RV-8. VANS RV-8 12593 DELRIN (ACETAL) AILERON STOP PLASTIC STOP FITTED INSTEAD OF RELYING ON METAL TO METAL CONTACT, PER APPLICANT'S LYCOMING YIO-360-M1B RVOM DRAWING

Prototype mods that have been approved since 1/1/2008 Page 133 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-8 12801 BONDING THE RV8/8A CANOPY AND ATTACHMENT OF CANOPY TO FRAME AND WINDSCREEN TO FUSELAGE BY BONDING USING LYCOMING YIO-360-M1B RVOM WINDSHIELD SIKAFLEX-295 UV (BLACK) INSTEAD OF SCREWS AND RIVETS.

ISSUE 2: THIS MODIFICATION UPDATED TO ALLOW THE BONDING OF THE FRONT SECTION AND/OR REAR SECTION. VANS RV-8 12943 GROVE STREAMLINED GEAR LEGS INSTALLATION OF GROVE RV-8 AEROFOIL GEAR LEGS. LYCOMING YIO-360-M1B RVEI VANS RV-8 12944 SHOW PLANES FASTBACK CONVERSION INSTALLATION OF SHOW PLANES FASTBACK CONVERSION KIT IN ACCORDANCE WITH THE SHOW LYCOMING YIO-360-M1B RVEI PLANES MANUAL, EXCEPT ADDITION OF ROLL BAR IS REQUIRED. VANS RV-8 12998 DYNON SKYVIEW AUTOPILOT DYNON SKYVIEW 2-AXIS AUTOPILOT INSTALLED AS PER MANUFACTURER'S INSTRUCTIONS. LYCOMING YIO-360-M1B RVEI VANS RV-8 12999 SMOKE SYSTEM INSTALLATION OF SMOKING AIRPLANES LLC SA-101H VCAS SMOKE SYSTEM IN ACCORDANCE WITH LYCOMING YIO-360-M1B RVEI THE MANUFACTURER'S INSTRUCTIONS, WITH THE ADDITION OF AN ANDAIR NON-RETURN VALVE AT THE BULKHEAD. TANK INSTALLED IN REAR BAGGAGE BAY. VANS RV-8 13866 INSTALLATION OF DYNON HEATED PITOT INSTALLATION OF DYNON AOA/PITOT PROBE USING SAFEAIR1 MAST. AOA DISPLAYED AND LYCOMING YIO-360-M1B MUKY TUBE AND AOA PROBE USING SAFEAIR1 WARNINGS GENERATED ON A DYNON SKYVIEW UNIT. PLUMBING & MOUNTING SYSTEM

VANS RV-8 13867 VANS RV-8 TIE DOWN RINGS FOR AFT FOUR BAGGAGE TIE-DOWN POINTS ADDED TO BAGGAGE COMPARTMENT, ONE AT EACH CORNER. LYCOMING YIO-360-M1B MUKY BAGGAGE FLOOR EACH CONSISTS OF A 6.5" X 5" 0.063" THICK 2024-T3 TRIANGULAR DOUBLER PLATE RIVETED TO THE TOP OF THE COMPARTMENT FLOOR AND FUSELAGE SIDE VIA A 7/8" DEEP VERTICAL FLANGE. DOUBLER IS FASTENED BY 4 OFF LP4-3 POP RIVETS AND 11 OFF AN470-AD4-4 SOLID RIVETS.

VANS RV-8 12801 BONDING THE RV8/8A CANOPY AND ATTACHMENT OF CANOPY TO FRAME AND WINDSCREEN TO FUSELAGE BY BONDING USING LYCOMING YIO-360-M1B MUKY WINDSHIELD SIKAFLEX-295 UV (BLACK) INSTEAD OF SCREWS AND RIVETS.

ISSUE 2: THIS MODIFICATION UPDATED TO ALLOW THE BONDING OF THE FRONT SECTION AND/OR REAR SECTION. VANS RV-8 12593 DELRIN (ACETAL) AILERON STOP PLASTIC STOP FITTED INSTEAD OF RELYING ON METAL TO METAL CONTACT, PER APPLICANT'S LYCOMING YIO-360-M1B MUKY DRAWING VANS RV-8 12539 INSTRUMENT PANEL ACCESS SEE APPLICANTS DRAWINGS FOR DETAILS LYCOMING YIO-360-M1B MUKY VANS RV-8 13966 DYNON DUAL AXIS AUTO-PILOT INSTALLATION OF DYNON SKYVIEW DUAL AXIS AUTO-PILOT. LYCOMING YIO-360-M1B MUKY INSTALLATION ROLL SERVO MOUNTED IN STARBOARD WING BESIDE AILERON BELLCRANK, WITH PUSH-ROD DRIVING A MODIFIED AILERON BELLCRANK, IN ACCORDANCE WITH DYNON AVIONICS AUTOPILOT SERVO INSTALLATION GUIDE DOCUMENT 101046-003 REV. G.

PITCH SERVO MOUNTED IN REAR FUSELAGE, WITH PUSH-ROD DRIVING PITCH PUSH-ROD IDLER, IN ACCORDANCE WITH DYNON AVIONICS AUTOPILOT SERVO INSTALLATION GUIDE, DOCUMENT 101046-002 REV. F.

ADDITIONAL SUPPORT BRACKET INSTALLED TO BRACE DYNON SUPPLIED ANGLES WHERE THEY OVERHANG A FUSELAGE FRAME.

PITCH TRIM SERVO OPERATING SPEED REDUCED TO 50% STANDARD SPEED VIA THE PREVIOUSLY INSTALLED VERTICAL POWER VP-100. VANS RV-8 13188 SUBSTITUTE CLICK BOND NUTPLATES 'CLICK BOND' FASTENERS SUBSTITUTED FOR NUTPLATES IN SUNDRY LOCATIONS. THESE BONDED- LYCOMING YIO-360-M1B LEMI FOR SUPPLIED NUTPLATES ON NUTS AVOID THE NEED FOR RIVETS TO ATTACH THEM TO STRUCTURE, AVOIDING ASSOCIATED RIVET HOLES AND STRESS RAISERS IN STRUCTURE VANS RV-8 13689 VANS FORWARD BATTERY BOX SPECIALLY DESIGNED HIGH QUALITY BATTERY BOX MADE TO SUIT ODYSSEY BATTERY, MOUNTED LYCOMING YIO-360-M1B LEMI REDESIGN ON FRONT FACE OF FIREWALL

Prototype mods that have been approved since 1/1/2008 Page 134 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-8 13924 LYCOMING THUNDERBOLT ENGINE & LYCOMING-BUILT THUNDERBOLT ENGINE WITH 10:1 COMPRESSION RATIO AND TWIN P MAG LYCOMING YIO-360-M1B LEMI DUAL ELECTRONIC IGNITION IGNITION VANS RV-8 13925 AVIONICS PANEL & POWER SYSTEMS VERTICAL POWER VP-X SYSTEM AND IBBS BACK UP BATTERIES LYCOMING YIO-360-M1B LEMI VANS RV-8 13926 INSTALLATION OF JAMES COWLINGS & ALTERNATIVE JAMES COWLS, PLENUM AND AIR FILTER FITTED LYCOMING YIO-360-M1B LEMI PLENUM CHAMBER & AIR FILTER VANS RV-8 13928 FLAP SWITCH LOCATED ON STICK GRIP FLAP SWITCH MOUNTED ON STICK GRIP, OPERATING VIA VERTICAL POWER VP-X LYCOMING YIO-360-M1B LEMI VANS RV-8 13930 COCKPIT SIDE WALL LIGHTS COCKPIT SIDEWALL LIGHTS FITTED SIMILAR TO SM11170 FOR RV7 LYCOMING YIO-360-M1B LEMI VANS RV-8 12355 TRUTRAK DIGIFLIGHT II VS AUTO PILOT INSTALLATION OF TRUTRAK DIGIFLIGHT II VS AUTOPILOT IN ACCORDANCE WITH TRUTRAK FLIGHT LYCOMING YIO-360-M1B LEMI SYSTEMS INSTALLATION INSTRUCTIONS SPECIFIED FOR THE VANS RV-8. VANS RV-8 13661 HEATED SEATS CLASSIC AERO DESIGNS HEATED SEATS SUBSTITUTED. MINOR CHANGE TO SEAT FRAME GEOMETRY LYCOMING YIO-360-M1B LEMI TO ACCOMMODATE HEATED SEAT CUSHIONS. VANS RV-8 13581 PITOT HEAD MODIFICATION SAFEAIR1 STREAMLINED PITOT MAST FITTED ON PORT WING IN ACCORDANCE WITH SAFEAIR1 LYCOMING YO-320-D1A RVSR INSTRUCTIONS. CUSTOM PITOT TUBE FITTED TO MAST. VANS RV-8 13096 TRUTRAK DIGITRAK ROLL AUTOPILOT INSTALLATION OF TRUTRAK DIGITRAK WING LEVELLING AUTO-PILOT WITH SERVO MOUNTED LYCOMING YO-360-A1A RVAR UNDER THE PORT FORWARD INBOARD SEAT RIB USING TRUTRAK BRACKET. TWO POP RIVETS INSTALLED TO SECURE DRIVE HORN CLAMPED TO AILERON TUBE. VANS RV-8 14913 WHELAN STROBE AND NAV LIGHTS INSTALLATION OF WHELAN WINGTIP STROBES AND NAV LIGHTS INSTALLATION USING VANS LN LYCOMING YO-360-A1A RVAR SYSTEM INSTALLATION SYS 6 SYSTEM. POWER SUPPLY MODEL NO. HDACF ATTACHED TO CUSTOM MADE MOUNTING TRAY THAT ALSO SUPPORTS THE BATTERY IN THE AFT POSITION FORWARD OF THE PITCH IDLER BELLCRANK.

VANS RV-8 14919 ELECTRONICS INTERNATIONAL FT-60 RED INSTALLATION OF AN ELECTRONICS INTERNATIONAL FT-60 RED CUBE FUEL FLOW TRANSDUCER LYCOMING YO-360-A1A RVAR CUBE FUEL FLOW TRANSDUCER DOWNSTREAM OF THE ELECTRICAL FUEL PUMP AND FILTER PER MANUFACTURER'S INSTRUCTIONS INSTALLATION #0506931. VANS RV-8 14223 RUDDER PEDAL EXTENSION EXTENSIONS ADDED TO BOTTOM OF P1 RUDDER PEDALS TO ALLOW RUDDER TO BE USED LYCOMING YO-360-A1A RVDC WITHOUT APPLYING INVOLUNTARY BRAKE PRESSURE VANS RV-8 12540 DYNON PITOT PROBE MOUNTED WITH INSTALLATION OF DYNON PITOT/STATIC/AOA PROBE USING GRETZ MOUNTING BRACKET KIT. LYCOMING IO-360-M1B WTSN GRETZ MAST (MODIFIED) VANS RV-8 13383 DUAL P-MAGS INSTALLATION OF E-MAGS ELECTRONIC IGNITION DUAL P114 P-MAG UNITS. LYCOMING IO-360-M1B WTSN (MODIFIED) VANS RV-8 12877 BELL TAILWHEEL FORK AND VANS INSTALL BELL TAILWHEEL FORK AND VANS 'U TAIL LYNX' DELUXE TAILWHEEL SPRING SET, IN LYCOMING IO-360-M1B WTSN DELUXE TAILWHEEL ACCORDANCE WITH THE MANUFACTURER'S INSTRUCTIONS. (MODIFIED) VANS RV-8 14874 HERCULES 7080522-S 70" x 80" INSTALLATION OF HERCULES 7080522-S 70 INCH DIAMETER X 80 INCH PITCH PROPELLER LYCOMING IO-360-M1B WTSN PROPELLER INSTALLATION (MODIFIED) VANS RV-8 13901 FUEL SYSTEM UPGRADE STANDARD VANS FUEL SELECTOR REPLACED WITH ANDAIR FS20X2. STANDARD VANS FUEL FILTER LYCOMING YIO-360-A1B6 XRVB REPLACED WITH ANDAIR FX375M. ANDAIR GASCOLATOR GAS375F ADDED ON FORWARD FACE OF FIREWALL, INCLUDING MOUNTING BRACKET. VANS RV-8 12540 DYNON PITOT PROBE MOUNTED WITH INSTALLATION OF DYNON PITOT/STATIC/AOA PROBE USING GRETZ MOUNTING BRACKET KIT. LYCOMING YIO-360-A1B6 XRVB GRETZ MAST VANS RV-8 13664 INDIVIDUAL BRAKE PEDAL FLUID SINGLE VANS BRAKE FLUID RESERVOIR REMOVED WITH ASSOCIATED TUBING TO EACH MASTER LYCOMING YIO-360-A1B6 XRVB RESERVOIR CYLINDER. ACS RESERVOIR A-600 SCREWED DIRECTLY INTO EACH MASTER CYLINDER. AN EXTRA 1" LONG STEEL SLEEVE (VANS P/N F-8107) IS REQUIRED IN EACH RUDDER PEDAL ASSEMBLY TO ENSURE CLEARANCE OF RESERVOIRS WITH FIREWALL. VANS RV-8 14412 MODIFICATION OF ENGINE SUMP AND ENGINE SUMP INTAKE BLANKED OFF WITH 1/4" ALLOY PLATE. MANUFACTURER'S PROVISION FOR LYCOMING IO-360-C1C6 DOBS THROTTLE BRACKET INTAKE OPENING ON OPPOSITE SIDE OF SUMP MACHINED OPEN TO ACCEPT FORWARD INTAKE. (MODIFIED) BRACKET MANUFACTURED FROM MILD STEEL SHEET TO PROVIDE MOUNTING FOR THROTTLE CABLE.

Prototype mods that have been approved since 1/1/2008 Page 135 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-8 15482 FUEL SYSTEM CHANGES PORT AND STARBOARD FUEL TANK OUTLETS CONNECT TO AN ANDAIR FS20 TYPE 2 SELECTOR LYCOMING AEIO-360-H1B YELA VALVE ON THE PORT SIDE OF THE COCKPIT, THEN TO AN ANDAIR GAS375 GASOCLATOR MOUNTED IN THE PORT WING ROOT, THEN TO AN ANDAIR PX375-TC FUEL PUMP IN THE FORWARD FUSELAGE AND THEN TO AN EI FT-60 FUEL FLOW TRANSDUCER MOUNTED ON THE FORWARD FACE OF THE FIREWALL. VANS RV-8 15483 WINGTIP LIGHTING FLYLEDS 'ORIGINAL' AND 'SKINNY BOARD' FITTED TO STANDARD VANS WINGTIP LIGHTING LYCOMING AEIO-360-H1B YELA ENCLOSURE IN ACCORDANCE WITH MANUFACTURER'S INSTRUCTIONS. INCLUDES ASSOCIATED CABLING, CIRCUIT PROTECTION AND SWITCHING. VANS RV-8 15484 DYNON AUTOPILOT DYNON AUTOPILOT INSTALLED, CONSISTING OF DYNON D180 EFIS, AP74 CONTROLLER AND 2 OFF LYCOMING AEIO-360-H1B YELA SV42 SERVOS. SERVOS ARE INSTALLED IN THE STARBOARD WING FOR ROLL AND AFT FUSELAGE FOR PITCH USING INSTALLATION KITS SUPPLIED BY DYNON FOR USE IN RV-8 AIRCRAFT.

VANS RV-8 14470 COWL FASTENERS ENGINE COWL ATTACHED USING MILSPEC PRODUCTS 'KIT RV8-CP-F' CAMLOC FASTENERS. LYCOMING O-360-A2A IDRS (MODIFIED) VANS RV-8 14471 NAV LIGHTS/STROBES INSTALLATION OF WHELEN LED MICROBURST II WING TIP NAV/STROBE LIGHTS AND TAIL LYCOMING O-360-A2A IDRS NAV/STROBE LIGHT (MB2G & MB1WT), FITTED IN ACCORDANCE WITH MANUFACTURER'S (MODIFIED) INSTRUCTIONS.

AT ISSUE 2, WHELEN A555 TAIL LIGHT UNIT ADDED AS ALTERNATIVE TO MB1WT. VANS RV-8 14472 AOA/PITOT PROBE STANDARD VANS PITOT TUBE AUGMENTED BY A SECOND ALLOY TUBE POSITIONED AFT OF PITOT LYCOMING O-360-A2A IDRS TUBE AND WELDED TO IT TO PROVIDE ANGLE OF ATTACK PRESSURE INFORMATION TO DYNON (MODIFIED) D100 UNIT. ANGLE OF ATTACK TUBE ATTACHED TO WING USING SAME FITTINGS AS PITOT TUBE, ATTACHED TO INSPECTION PANEL FLANGE. VANS RV-8 12663 SA-101H SMOKE SYSTEM INSTALLATION SMOKE SYSTEM INSTALLED IN ACCORDANCE WITH APPLICANT DETAILS LYCOMING O-360-A2A IDRS TO RV-8 FORWARD BAGGAGE BAY (MODIFIED)

VANS RV-8 15402 AIRFLOW PERFORMANCE FUEL AIRFLOW PERFORMANCE FM-150 FUEL INJECTION SYSTEM FITTED (INCLUDES REPLACEMENT LYCOMING O-360-A2A IDRS INJECTION ENGINE DRIVEN PUMP) (MODIFIED)

ELECTRIC PUMP REPLACED WITH ANDAIR PUMP AND FILTER

ELECTRONICS INTERNATIONAL FT-60 FUEL FLOW TRANSDUCER FITTED BETWEEN FUEL INJECTION SERVO AND FLOW DIVIDER VANS RV-8 15237 COVER PLATES ON GEAR TOWER LOWER TWO INSPECTION HOLES IN GEAR TOWERS AMALGAMATED INTO ONE LARGER ACCESS MATTITUCK TMX-IO-360 RVFT HOLE COVER/REINFORCEMENT PLATE ATTACHED WITH SCREWS INTO ANCHOR NUTS VANS RV-8 12442 EXTERNAL POWER SOCKET INSTALLATION OF EXTERNAL POWER SOCKET IN REAR FUSELAGE FLOOR ADJACENT TO BATTERY. MATTITUCK TMX-IO-360 RVFT INSTALLATION VANS RV-8 12539 INSTRUMENT PANEL ACCESS SEE APPLICANTS DRAWINGS FOR DETAILS MATTITUCK TMX-IO-360 RVFT VANS RV-8 12663 SA-101H SMOKE SYSTEM INSTALLATION SMOKE SYSTEM INSTALLED IN ACCORDANCE WITH APPLICANT DETAILS MATTITUCK TMX-IO-360 RVFT TO RV-8 FORWARD BAGGAGE BAY

VANS RV-8 15295 DYNON SKYVIEW AUTOPILOT DYNON SKYVIEW 2-AXIS AUTOPILOT MATTITUCK TMX-IO-360 RVFT PITCH SERVO INSTALLED AS PER DYNON INSTRUCTIONS (POST SEPTEMBER 2006 DESIGN; SECURED WITH ADDITIONAL CHERRYMAX RIVETS) TRU-TRAK ROLL SERVO INSTALLATION VANS RV-8 12884 RAVEN INVERTED OIL SYSTEM INSTALLATION OF INVERTED OIL SYSTEM FROM RAVEN AIRCRAFT CORPORATION, USA. SUPERIOR XP-IO-360-B1A2 EGRV

ISSUE 2, 14/3/16: OPTIONALLY, A 'HALF' RAVEN OIL SYSTEM MAY BE FITTED, WHICH USES JUST THE OIL SEPARATOR AND NOT THE OIL VALVE.

Prototype mods that have been approved since 1/1/2008 Page 136 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-8 13129 PROPELLER CHANGE TO MTV-12-B/183- INSTALLATION OF MTV-12-B/183-59b HYDRAULIC CONSTANT SPEED PROPELLER USING MT SUPERIOR XP-IO-360-B1A2 EGRV 59b PROPELLER HYDRAULIC GOVERNOR. NOTE: THIS PROPELLER IS NOT SUITABLE FOR UNLIMITED AEROBATIC USE BUT IS CONSIDERED ACCEPTABLE FOR THIS APPLICATION WHICH INVOLVES POSITIVE G MANOEUVRING AND NO INTERUPTIONOF OIL PRESSURE TO PROPELLER. VANS RV-8 12999 SMOKE SYSTEM INSTALLATION OF SMOKING AIRPLANES LLC SA-101H VCAS SMOKE SYSTEM IN ACCORDANCE WITH SUPERIOR XP-IO-360-B1A2 EGRV THE MANUFACTURER'S INSTRUCTIONS, WITH THE ADDITION OF AN ANDAIR NON-RETURN VALVE AT THE BULKHEAD. TANK INSTALLED IN REAR BAGGAGE BAY. VANS RV-8 15089 DISPLAY LAMP INSTALLATION INSTALLATION OF AN LED LAMP IN A CUSTOM MADE GRP MOUNT AND REAR FAIRING WITH SUPERIOR XP-IO-360-B1A2 EGRV TRANSPARENT FRONT FAIRING ATTACHED TO CENTRELINE OF LOWER COWLING TO PROVIDE VISUAL EFFECT DURING DISPLAYS.

ISS 2. IMPROVED AERODYNAMIC SHAPE OF REAR FAIRING AND TRANSPARENT FRONT FAIRING UTILISING EXISTING MOUNTINGS. IMPROVED LAMP MOUNTING WHICH ALLOWS ANGLE ADJUSTMENT. VANS RV-8 13772 DUAL P MAGS DUAL P MAGS FITTED INSTEAD OF CONVENTIONAL MAGNETOS SUPERIOR XP-IO-360-B1A2 CIBM VANS RV-8 12593 DELRIN (ACETAL) AILERON STOP PLASTIC STOP FITTED INSTEAD OF RELYING ON METAL TO METAL CONTACT, PER APPLICANT'S SUPERIOR XP-IO-360-B1A2 CIBM DRAWING VANS RV-8 12999 SMOKE SYSTEM INSTALLATION OF SMOKING AIRPLANES LLC SA-101H VCAS SMOKE SYSTEM IN ACCORDANCE WITH SUPERIOR XP-IO-360-B1A2 CIBM THE MANUFACTURER'S INSTRUCTIONS, WITH THE ADDITION OF AN ANDAIR NON-RETURN VALVE AT THE BULKHEAD. TANK INSTALLED IN REAR BAGGAGE BAY. VANS RV-8 13129 PROPELLER CHANGE TO MTV-12-B/183- INSTALLATION OF MTV-12-B/183-59b HYDRAULIC CONSTANT SPEED PROPELLER USING MT SUPERIOR XP-IO-360-B1A2 CIBM 59b PROPELLER HYDRAULIC GOVERNOR. NOTE: THIS PROPELLER IS NOT SUITABLE FOR UNLIMITED AEROBATIC USE BUT IS CONSIDERED ACCEPTABLE FOR THIS APPLICATION WHICH INVOLVES POSITIVE G MANOEUVRING AND NO INTERUPTIONOF OIL PRESSURE TO PROPELLER. VANS RV-8 15089 DISPLAY LAMP INSTALLATION INSTALLATION OF AN LED LAMP IN A CUSTOM MADE GRP MOUNT AND REAR FAIRING WITH SUPERIOR XP-IO-360-B1A2 CIBM TRANSPARENT FRONT FAIRING ATTACHED TO CENTRELINE OF LOWER COWLING TO PROVIDE VISUAL EFFECT DURING DISPLAYS.

ISS 2. IMPROVED AERODYNAMIC SHAPE OF REAR FAIRING AND TRANSPARENT FRONT FAIRING UTILISING EXISTING MOUNTINGS. IMPROVED LAMP MOUNTING WHICH ALLOWS ANGLE ADJUSTMENT. VANS RV-8 12355 TRUTRAK DIGIFLIGHT II VS AUTO PILOT INSTALLATION OF TRUTRAK DIGIFLIGHT II VS AUTOPILOT IN ACCORDANCE WITH TRUTRAK FLIGHT SUPERIOR XP-IO-360-B1AA2 XSEA SYSTEMS INSTALLATION INSTRUCTIONS SPECIFIED FOR THE VANS RV-8. VANS RV-8 12442 EXTERNAL POWER SOCKET INSTALLATION OF EXTERNAL POWER SOCKET IN REAR FUSELAGE FLOOR ADJACENT TO BATTERY. SUPERIOR XP-IO-360-B1AA2 XSEA INSTALLATION VANS RV-8 12700 TRUTRAK DIGITRAK WING LEVELLING INSTALLATION OF TRUTRAK DIGITRAK WING LEVELLING AUTO-PILOT WITH SERVO MOUNTED SUPERIOR XP-IO-360-B1AA2 VRVB AUTO-PILOT UNDER THE PORT FORWARD INBOARD SEAT RIB USING TRUTRAK BRACKET. TWO POP RIVETS INSTALLED TO SECURE DRIVE HORN CLAMPED TO AILERON TUBE. VANS RV-8 12355 TRUTRAK DIGIFLIGHT II VS AUTO PILOT INSTALLATION OF TRUTRAK DIGIFLIGHT II VS AUTOPILOT IN ACCORDANCE WITH TRUTRAK FLIGHT SUPERIOR XP-IO-360-B1AA2 VRVB SYSTEMS INSTALLATION INSTRUCTIONS SPECIFIED FOR THE VANS RV-8. VANS RV-8 13166 E MAG (P MODEL) INSTALLATION SINGLE P MAG FITTED IN PLACE OF ONE OF THE EXISTING SLICK MAGNETOS. SUPERIOR XP-IO-360-B1AA2 VRVB ISSUE 2: SECOND E MAG (P MODEL) FITTED IN PLACE OF OTHER MAGNETO ISSUE 4 (SUPERSEDES ISSUE 3): FOR HC-C2YR-1BF/F7496 ON SUPERIOR XP-IO-360-B()()2 ENGINES: DO NOT OPERATE ABOVE 22" MANIFOLD PRESSURE BELOW 2350 RPM. OPERATION ABOVE 2600 RPM IS LIMITED TO TAKE-OFF. AS SOON AS PRACTICAL AFTER TAKE-OFF THE RPM SHOULD BE REDUCED TO 2600 RPM OR LESS. FOR HC-C2YR-1BF/F7497 ON SUPERIOR XP-IO-360-B()()2 ENGINES: NO RESTRICTIONS

Prototype mods that have been approved since 1/1/2008 Page 137 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-8 12663 SA-101H SMOKE SYSTEM INSTALLATION SMOKE SYSTEM INSTALLED IN ACCORDANCE WITH APPLICANT DETAILS SUPERIOR XP-IO-360-B1AA2 HILZ TO RV-8 FORWARD BAGGAGE BAY

VANS RV-8 13166 E MAG (P MODEL) INSTALLATION SINGLE P MAG FITTED IN PLACE OF ONE OF THE EXISTING SLICK MAGNETOS. SUPERIOR XP-IO-360-B1AA2 HILZ ISSUE 2: SECOND E MAG (P MODEL) FITTED IN PLACE OF OTHER MAGNETO ISSUE 4 (SUPERSEDES ISSUE 3): FOR HC-C2YR-1BF/F7496 ON SUPERIOR XP-IO-360-B()()2 ENGINES: DO NOT OPERATE ABOVE 22" MANIFOLD PRESSURE BELOW 2350 RPM. OPERATION ABOVE 2600 RPM IS LIMITED TO TAKE-OFF. AS SOON AS PRACTICAL AFTER TAKE-OFF THE RPM SHOULD BE REDUCED TO 2600 RPM OR LESS. FOR HC-C2YR-1BF/F7497 ON SUPERIOR XP-IO-360-B()()2 ENGINES: NO RESTRICTIONS VANS RV-8 13410 GROVE RV-8 STANDARD LIGHTWEIGHT GROVE LIGHTWEIGHT MAIN UNDERCARRIAGE FITTED SUPERIOR XP-IO-360-B1AA2 HILZ GEAR VANS RV-8 12999 SMOKE SYSTEM INSTALLATION OF SMOKING AIRPLANES LLC SA-101H VCAS SMOKE SYSTEM IN ACCORDANCE WITH SUPERIOR XP-IO-360-B1AA2 HILZ THE MANUFACTURER'S INSTRUCTIONS, WITH THE ADDITION OF AN ANDAIR NON-RETURN VALVE AT THE BULKHEAD. TANK INSTALLED IN REAR BAGGAGE BAY. VANS RV-8 12884 RAVEN INVERTED OIL SYSTEM INSTALLATION OF INVERTED OIL SYSTEM FROM RAVEN AIRCRAFT CORPORATION, USA. SUPERIOR XP-IO-360-B1AA2 HILZ

ISSUE 2, 14/3/16: OPTIONALLY, A 'HALF' RAVEN OIL SYSTEM MAY BE FITTED, WHICH USES JUST THE OIL SEPARATOR AND NOT THE OIL VALVE. VANS RV-8 13637 FIT AVEOMAXX ATLAS LED WINGTIP AVEOMAXX ATLAS LED HIGH INTENSITY WINGTIP LIGHTS FITTED TO MODIFIED MOUNTINGS SUPERIOR XP-IO-360-B1AA2 HILZ LIGHTS VANS RV-8 13594 PROPELLER CHANGE TO HARTZELL HC- INSTALLATION OF HARTZELL HC-C2YR-1N/N7605 76 INCH DIAMETER 2 COMPOSITE BLADED SUPERIOR XP-IO-360-B1AA2 HILZ C2YR-1N/N7605 CONSTANT SPEED PROPELLER. VANS RV-8 12608 FLOSCAN FUEL FLOW TRANSDUCER INSTALLATION OF FLOSCAN 200 SERIES FUEL FLOW TRANSDUCER FOR USE WITH DYNON SUPERIOR XP-IO-360-B1AA2 GUNZ FLIGHTDEK D180 INSTRUMENT. VANS RV-8 12663 SA-101H SMOKE SYSTEM INSTALLATION SMOKE SYSTEM INSTALLED IN ACCORDANCE WITH APPLICANT DETAILS SUPERIOR XP-IO-360-B1AA2 GUNZ TO RV-8 FORWARD BAGGAGE BAY

VANS RV-8 13096 TRUTRAK DIGITRAK ROLL AUTOPILOT INSTALLATION OF TRUTRAK DIGITRAK WING LEVELLING AUTO-PILOT WITH SERVO MOUNTED SUPERIOR XP-IO-360-B1AD2 RATD UNDER THE PORT FORWARD INBOARD SEAT RIB USING TRUTRAK BRACKET. TWO POP RIVETS INSTALLED TO SECURE DRIVE HORN CLAMPED TO AILERON TUBE. VANS RV-8 12276 INSTALLATION OF 'BELL' TAILWHEEL INSTALLATION OF 'BELL' TAILWHEEL FORK TO INCREASE GROUND CLEARANCE OF FUSELAGE REAR SUPERIOR XP-IO-360-B1AD2 RATD FORK IN ACCORDANCE WITH DRAWINGS STATED BELOW. VANS RV-8 12668 FITMENT OF 2 HINGED ACCESS DOORS TWO HINGED ACCESS PANELS FITTED FORWARD OF INSTRUMENT PANEL PER APPLICANT'S SUPERIOR XP-IO-360-B1AD2 RATD FORWARD OF INSTRUMENT PANEL DRAWINGS VANS RV-8 12651 SKYFLASH STROBES SYSTEM SKYFLASH STROBES SYSTEM. LIGHT UNITS FITTED WITHIN WING TIP FAIRINGS AND POWER UNIT SUPERIOR XP-IO-360-B1AD2 GIGZ FITTED TO WING CENTRE SECTION. VANS RV-8 12659 SAFEAIR1 PITOT MAST INSTALLATION OF SAFEAIR1 PITOT MAST TO ACCOMMODATE DYNON PITOT HEAD. SUPERIOR XP-IO-360-B1AD2 GIGZ VANS RV-8 12539 INSTRUMENT PANEL ACCESS SEE APPLICANTS DRAWINGS FOR DETAILS SUPERIOR XP-IO-360-B1AD2 OCXI VANS RV-8 15194 FUEL SYSTEM UPGRADE STANDARD VANS FUEL SELECTOR REPLACED WITH ANDAIR FS20X2. STANDARD VANS FUEL FILTER SUPERIOR XP-IO-360-B1AD2 OCXI REPLACED WITH 2 OFF ANDAIR FX375M FILTERS POSITIONED IN THE WING ROUTES UPSTREAM OF THE FUEL SELECTOR VALVE. VANS RV-8 15195 COWL FASTENERS ENGINE COWL ATTACHED USING MILSPEC PRODUCTS 'KIT RV8-CP-F' CAMLOC FASTENERS. SUPERIOR XP-IO-360-B1AD2 OCXI VANS RV-8 12966 DYNON AP47 DUAL AXIS AUTOPILOT INSTALLATION OF DYNON SV32 PITCH AND ROLL AUTO-PILOT SERVOS INTERFACED WITH DYNON SUPERIOR XP-IO-360-B1BA3 TUCK AP47 AUTO-PILOT CONTROLLER. ROLL SERVO INSTALLED IN FUSELAGE IN ACCORDANCE WITH THE TRUTRAK METHOD WITH THE ADDITION OF TWO RIVETS TO SECURE THE CLAMPED ROLL DRIVE HORN TO THE AILERON TORQUE TUBE.

Prototype mods that have been approved since 1/1/2008 Page 138 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-8 14451 AEROBATICS MODIFICATIONS - HALF PART 1. INSTALLATION OF RAVEN OIL/AIR SEPARATOR, WITHOUT CHECK-VALVE,TO PREVENT LOSS SUPERIOR XP-IO-360-B1HD2 MIRV RAVEN OIL SYSTEM AND RESERVOIR OF OIL DURING BRIEF PERIODS OF NEGATIVE G. DOGS BRAKE FLUID CHECK VALVE PART 2. INSTALLATION OF RESERVOIR DOGS CHECK-VALVE BETWEEN FILLER OF BRAKE RESERVOIR AND BREATHER CAP TO PREVENT LOSS OF BRAKE FLUID DURING PERIODS OF NEGATIVE G.

(PART 1 ONLY IS INSTALLED ON G-MIRV)

VANS RV-8 13664 INDIVIDUAL BRAKE PEDAL FLUID SINGLE VANS BRAKE FLUID RESERVOIR REMOVED WITH ASSOCIATED TUBING TO EACH MASTER SUPERIOR XP-IO-360-B1HD2 MIRV RESERVOIR CYLINDER. ACS RESERVOIR A-600 SCREWED DIRECTLY INTO EACH MASTER CYLINDER. AN EXTRA 1" LONG STEEL SLEEVE (VANS P/N F-8107) IS REQUIRED IN EACH RUDDER PEDAL ASSEMBLY TO ENSURE CLEARANCE OF RESERVOIRS WITH FIREWALL. VANS RV-8 13188 SUBSTITUTE CLICK BOND NUTPLATES 'CLICK BOND' FASTENERS SUBSTITUTED FOR NUTPLATES IN SUNDRY LOCATIONS. THESE BONDED- SUPERIOR XP-IO-360-B1HD2 MIRV FOR SUPPLIED NUTPLATES ON NUTS AVOID THE NEED FOR RIVETS TO ATTACH THEM TO STRUCTURE, AVOIDING ASSOCIATED RIVET HOLES AND STRESS RAISERS IN STRUCTURE VANS RV-8 15135 FALCON HEATED PITOT PROBE FALCON HEATED PITOT PROBE MOUNTED TO GRETZ MAST INSTALLED IN SAME LOCATION AS VANS SUPERIOR XP-IO-360-B1HD2 MIRV MOUNTED TO GRETZ MAST STANDARD PITOT HEAD. INSTALLATION VANS RV-8 13661 HEATED SEATS CLASSIC AERO DESIGNS HEATED SEATS SUBSTITUTED. MINOR CHANGE TO SEAT FRAME GEOMETRY SUPERIOR XP-IO-360-B1HD2 MIRV TO ACCOMMODATE HEATED SEAT CUSHIONS. VANS RV-8 12999 SMOKE SYSTEM INSTALLATION OF SMOKING AIRPLANES LLC SA-101H VCAS SMOKE SYSTEM IN ACCORDANCE WITH SUPERIOR XP-IO-360-B1HD2 IIDD THE MANUFACTURER'S INSTRUCTIONS, WITH THE ADDITION OF AN ANDAIR NON-RETURN VALVE AT THE BULKHEAD. TANK INSTALLED IN REAR BAGGAGE BAY. VANS RV-8 12884 RAVEN INVERTED OIL SYSTEM INSTALLATION OF INVERTED OIL SYSTEM FROM RAVEN AIRCRAFT CORPORATION, USA. SUPERIOR XP-IO-360-B1HD2 IIDD

ISSUE 2, 14/3/16: OPTIONALLY, A 'HALF' RAVEN OIL SYSTEM MAY BE FITTED, WHICH USES JUST THE OIL SEPARATOR AND NOT THE OIL VALVE. VANS RV-8 13383 DUAL P-MAGS INSTALLATION OF E-MAGS ELECTRONIC IGNITION DUAL P114 P-MAG UNITS. SUPERIOR XP-IO-360-B1HD2 IIDD VANS RV-8 12944 SHOW PLANES FASTBACK CONVERSION INSTALLATION OF SHOW PLANES FASTBACK CONVERSION KIT IN ACCORDANCE WITH THE SHOW SUPERIOR XP-IO-360-B1HD2 IIDD PLANES MANUAL, EXCEPT ADDITION OF ROLL BAR IS REQUIRED. VANS RV-8 12540 DYNON PITOT PROBE MOUNTED WITH INSTALLATION OF DYNON PITOT/STATIC/AOA PROBE USING GRETZ MOUNTING BRACKET KIT. SUPERIOR XP-IO-360-B1HD2 IIDD GRETZ MAST VANS RV-8 13966 DYNON DUAL AXIS AUTO-PILOT INSTALLATION OF DYNON SKYVIEW DUAL AXIS AUTO-PILOT. SUPERIOR XP-IO-360-B1HD2 IIDD INSTALLATION ROLL SERVO MOUNTED IN STARBOARD WING BESIDE AILERON BELLCRANK, WITH PUSH-ROD DRIVING A MODIFIED AILERON BELLCRANK, IN ACCORDANCE WITH DYNON AVIONICS AUTOPILOT SERVO INSTALLATION GUIDE DOCUMENT 101046-003 REV. G.

PITCH SERVO MOUNTED IN REAR FUSELAGE, WITH PUSH-ROD DRIVING PITCH PUSH-ROD IDLER, IN ACCORDANCE WITH DYNON AVIONICS AUTOPILOT SERVO INSTALLATION GUIDE, DOCUMENT 101046-002 REV. F.

ADDITIONAL SUPPORT BRACKET INSTALLED TO BRACE DYNON SUPPLIED ANGLES WHERE THEY OVERHANG A FUSELAGE FRAME.

PITCH TRIM SERVO OPERATING SPEED REDUCED TO 50% STANDARD SPEED VIA THE PREVIOUSLY INSTALLED VERTICAL POWER VP-100.

Prototype mods that have been approved since 1/1/2008 Page 139 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-8 13166 E MAG (P MODEL) INSTALLATION SINGLE P MAG FITTED IN PLACE OF ONE OF THE EXISTING SLICK MAGNETOS. SUPERIOR XP-IO-360-B1HD2 CJSM ISSUE 2: SECOND E MAG (P MODEL) FITTED IN PLACE OF OTHER MAGNETO ISSUE 4 (SUPERSEDES ISSUE 3): FOR HC-C2YR-1BF/F7496 ON SUPERIOR XP-IO-360-B()()2 ENGINES: DO NOT OPERATE ABOVE 22" MANIFOLD PRESSURE BELOW 2350 RPM. OPERATION ABOVE 2600 RPM IS LIMITED TO TAKE-OFF. AS SOON AS PRACTICAL AFTER TAKE-OFF THE RPM SHOULD BE REDUCED TO 2600 RPM OR LESS. FOR HC-C2YR-1BF/F7497 ON SUPERIOR XP-IO-360-B()()2 ENGINES: NO RESTRICTIONS VANS RV-8 12884 RAVEN INVERTED OIL SYSTEM INSTALLATION OF INVERTED OIL SYSTEM FROM RAVEN AIRCRAFT CORPORATION, USA. SUPERIOR XP-IO-360-B1HD2 CJSM

ISSUE 2, 14/3/16: OPTIONALLY, A 'HALF' RAVEN OIL SYSTEM MAY BE FITTED, WHICH USES JUST THE OIL SEPARATOR AND NOT THE OIL VALVE. VANS RV-8 12999 SMOKE SYSTEM INSTALLATION OF SMOKING AIRPLANES LLC SA-101H VCAS SMOKE SYSTEM IN ACCORDANCE WITH SUPERIOR XP-IO-360-B1HD2 CJSM THE MANUFACTURER'S INSTRUCTIONS, WITH THE ADDITION OF AN ANDAIR NON-RETURN VALVE AT THE BULKHEAD. TANK INSTALLED IN REAR BAGGAGE BAY. VANS RV-8 15089 DISPLAY LAMP INSTALLATION INSTALLATION OF AN LED LAMP IN A CUSTOM MADE GRP MOUNT AND REAR FAIRING WITH SUPERIOR XP-IO-360-B1HD2 CJSM TRANSPARENT FRONT FAIRING ATTACHED TO CENTRELINE OF LOWER COWLING TO PROVIDE VISUAL EFFECT DURING DISPLAYS.

ISS 2. IMPROVED AERODYNAMIC SHAPE OF REAR FAIRING AND TRANSPARENT FRONT FAIRING UTILISING EXISTING MOUNTINGS. IMPROVED LAMP MOUNTING WHICH ALLOWS ANGLE ADJUSTMENT. VANS RV-8 14451 AEROBATICS MODIFICATIONS - HALF PART 1. INSTALLATION OF RAVEN OIL/AIR SEPARATOR, WITHOUT CHECK-VALVE,TO PREVENT LOSS SUPERIOR XP-IO-360-B1HC2 RVPH RAVEN OIL SYSTEM AND RESERVOIR OF OIL DURING BRIEF PERIODS OF NEGATIVE G. DOGS BRAKE FLUID CHECK VALVE PART 2. INSTALLATION OF RESERVOIR DOGS CHECK-VALVE BETWEEN FILLER OF BRAKE RESERVOIR AND BREATHER CAP TO PREVENT LOSS OF BRAKE FLUID DURING PERIODS OF NEGATIVE G.

(PART 1 ONLY IS INSTALLED ON G-MIRV)

VANS RV-8 12884 RAVEN INVERTED OIL SYSTEM INSTALLATION OF INVERTED OIL SYSTEM FROM RAVEN AIRCRAFT CORPORATION, USA. SUPERIOR XP-IO-360-B1HC2 VFDS

ISSUE 2, 14/3/16: OPTIONALLY, A 'HALF' RAVEN OIL SYSTEM MAY BE FITTED, WHICH USES JUST THE OIL SEPARATOR AND NOT THE OIL VALVE. VANS RV-8 13166 E MAG (P MODEL) INSTALLATION SINGLE P MAG FITTED IN PLACE OF ONE OF THE EXISTING SLICK MAGNETOS. SUPERIOR XP-IO-360-B1HC2 VFDS ISSUE 2: SECOND E MAG (P MODEL) FITTED IN PLACE OF OTHER MAGNETO ISSUE 4 (SUPERSEDES ISSUE 3): FOR HC-C2YR-1BF/F7496 ON SUPERIOR XP-IO-360-B()()2 ENGINES: DO NOT OPERATE ABOVE 22" MANIFOLD PRESSURE BELOW 2350 RPM. OPERATION ABOVE 2600 RPM IS LIMITED TO TAKE-OFF. AS SOON AS PRACTICAL AFTER TAKE-OFF THE RPM SHOULD BE REDUCED TO 2600 RPM OR LESS. FOR HC-C2YR-1BF/F7497 ON SUPERIOR XP-IO-360-B()()2 ENGINES: NO RESTRICTIONS VANS RV-8 12999 SMOKE SYSTEM INSTALLATION OF SMOKING AIRPLANES LLC SA-101H VCAS SMOKE SYSTEM IN ACCORDANCE WITH SUPERIOR XP-IO-360-B1HC2 VFDS THE MANUFACTURER'S INSTRUCTIONS, WITH THE ADDITION OF AN ANDAIR NON-RETURN VALVE AT THE BULKHEAD. TANK INSTALLED IN REAR BAGGAGE BAY. VANS RV-8 15089 DISPLAY LAMP INSTALLATION INSTALLATION OF AN LED LAMP IN A CUSTOM MADE GRP MOUNT AND REAR FAIRING WITH SUPERIOR XP-IO-360-B1HC2 VFDS TRANSPARENT FRONT FAIRING ATTACHED TO CENTRELINE OF LOWER COWLING TO PROVIDE VISUAL EFFECT DURING DISPLAYS.

ISS 2. IMPROVED AERODYNAMIC SHAPE OF REAR FAIRING AND TRANSPARENT FRONT FAIRING UTILISING EXISTING MOUNTINGS. IMPROVED LAMP MOUNTING WHICH ALLOWS ANGLE ADJUSTMENT.

Prototype mods that have been approved since 1/1/2008 Page 140 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-8 15326 PROPELLER CHANGE TO MTV-12-B/183- INSTALLATION OF MTV-12-B/183-59b HYDRAULIC CONSTANT SPEED PROPELLER USING MT SUPERIOR XP-IO-360-B1HC2 VFDS 59b PROPELLER HYDRAULIC GOVERNOR. NOTE: THIS PROPELLER IS NOT SUITABLE FOR UNLIMITED AEROBATIC USE BUT IS CONSIDERED ACCEPTABLE FOR THIS APPLICATION WHICH INVOLVES POSITIVE G MANOEUVRING AND NO INTERUPTIONOF OIL PRESSURE TO PROPELLER. VANS RV-8 13531 GROUND START POWER SOCKET GROUND ELECTRICAL POWER SUPPLY SOCKET AN 2552-3A LOCATED BEHIND DOOR IN PORT SUPERIOR XP-IO-360-B1AC2 RRRZ FUSELAGE. INCLUDES ASSOCIATED RELAYS AND STRUCTURAL REINFORCEMENT. VANS RV-8 12540 DYNON PITOT PROBE MOUNTED WITH INSTALLATION OF DYNON PITOT/STATIC/AOA PROBE USING GRETZ MOUNTING BRACKET KIT. SUPERIOR XP-IO-360-B1AC2 RRRZ GRETZ MAST VANS RV-8 12801 BONDING THE RV8/8A CANOPY AND ATTACHMENT OF CANOPY TO FRAME AND WINDSCREEN TO FUSELAGE BY BONDING USING SUPERIOR XP-IO-360-B1AC2 RRRZ WINDSHIELD SIKAFLEX-295 UV (BLACK) INSTEAD OF SCREWS AND RIVETS.

ISSUE 2: THIS MODIFICATION UPDATED TO ALLOW THE BONDING OF THE FRONT SECTION AND/OR REAR SECTION. VANS RV-8 13166 E MAG (P MODEL) INSTALLATION SINGLE P MAG FITTED IN PLACE OF ONE OF THE EXISTING SLICK MAGNETOS. SUPERIOR XP-IO-360-B1AC2 RRRZ ISSUE 2: SECOND E MAG (P MODEL) FITTED IN PLACE OF OTHER MAGNETO ISSUE 4 (SUPERSEDES ISSUE 3): FOR HC-C2YR-1BF/F7496 ON SUPERIOR XP-IO-360-B()()2 ENGINES: DO NOT OPERATE ABOVE 22" MANIFOLD PRESSURE BELOW 2350 RPM. OPERATION ABOVE 2600 RPM IS LIMITED TO TAKE-OFF. AS SOON AS PRACTICAL AFTER TAKE-OFF THE RPM SHOULD BE REDUCED TO 2600 RPM OR LESS. FOR HC-C2YR-1BF/F7497 ON SUPERIOR XP-IO-360-B()()2 ENGINES: NO RESTRICTIONS VANS RV-8 12999 SMOKE SYSTEM INSTALLATION OF SMOKING AIRPLANES LLC SA-101H VCAS SMOKE SYSTEM IN ACCORDANCE WITH SUPERIOR XP-IO-360-B1AC2 RRRZ THE MANUFACTURER'S INSTRUCTIONS, WITH THE ADDITION OF AN ANDAIR NON-RETURN VALVE AT THE BULKHEAD. TANK INSTALLED IN REAR BAGGAGE BAY. VANS RV-8 12966 DYNON AP47 DUAL AXIS AUTOPILOT INSTALLATION OF DYNON SV32 PITCH AND ROLL AUTO-PILOT SERVOS INTERFACED WITH DYNON SUPERIOR XP-IO-360-B1AC2 RRRZ AP47 AUTO-PILOT CONTROLLER. ROLL SERVO INSTALLED IN FUSELAGE IN ACCORDANCE WITH THE TRUTRAK METHOD WITH THE ADDITION OF TWO RIVETS TO SECURE THE CLAMPED ROLL DRIVE HORN TO THE AILERON TORQUE TUBE. VANS RV-8 12539 INSTRUMENT PANEL ACCESS SEE APPLICANTS DRAWINGS FOR DETAILS SUPERIOR XP-IO-360-B1LD2 VMOZ VANS RV-8 12801 BONDING THE RV8/8A CANOPY AND ATTACHMENT OF CANOPY TO FRAME AND WINDSCREEN TO FUSELAGE BY BONDING USING SUPERIOR XP-IO-360-B1LD2 VMOZ WINDSHIELD SIKAFLEX-295 UV (BLACK) INSTEAD OF SCREWS AND RIVETS.

ISSUE 2: THIS MODIFICATION UPDATED TO ALLOW THE BONDING OF THE FRONT SECTION AND/OR REAR SECTION. VANS RV-8 12999 SMOKE SYSTEM INSTALLATION OF SMOKING AIRPLANES LLC SA-101H VCAS SMOKE SYSTEM IN ACCORDANCE WITH SUPERIOR XP-IO-360-B1HD3 SOUT THE MANUFACTURER'S INSTRUCTIONS, WITH THE ADDITION OF AN ANDAIR NON-RETURN VALVE AT THE BULKHEAD. TANK INSTALLED IN REAR BAGGAGE BAY. VANS RV-8 13410 GROVE RV-8 STANDARD LIGHTWEIGHT GROVE LIGHTWEIGHT MAIN UNDERCARRIAGE FITTED SUPERIOR XP-IO-360-B1HD3 SOUT GEAR VANS RV-8 14816 ACE AX50 CYLINDERS, PISTONS AND INSTALLATION OF ACE-PERFORMANCE (ADVANCED COMPONENTS ENGINEERING) AX50 SUPERIOR XP-IO-360-B1HD3 SOUT CONNECTING RODS INSTALLATION CYLINDERS, PISTONS AND CONNECTING RODS TO LYCOMING IO-360-A1B6 ENGINE. UNDER- PISTON OIL SQUIRT COOLING NOZZLES INSTALLED. CAPACITY INCREASED FROM 360 TO 379 CUBIC INCHES. COMPRESSION RATIO 8.75:1. IGNITION TIMING SET TO 17 DEGREES BTDC. VANS RV-8 14817 SKY DYNAMICS FEATHERWEIGHT INSTALLATION OF SKY DYNAMICS PART NO. 30367 - 149 TOOTH FEATHERWEIGHT FLYWHEEL. SUPERIOR XP-IO-360-B1HD3 SOUT FLYWHEEL INSTALLATION

Prototype mods that have been approved since 1/1/2008 Page 141 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-8 15089 DISPLAY LAMP INSTALLATION INSTALLATION OF AN LED LAMP IN A CUSTOM MADE GRP MOUNT AND REAR FAIRING WITH SUPERIOR XP-IO-360-B1HD3 SOUT TRANSPARENT FRONT FAIRING ATTACHED TO CENTRELINE OF LOWER COWLING TO PROVIDE VISUAL EFFECT DURING DISPLAYS.

ISS 2. IMPROVED AERODYNAMIC SHAPE OF REAR FAIRING AND TRANSPARENT FRONT FAIRING UTILISING EXISTING MOUNTINGS. IMPROVED LAMP MOUNTING WHICH ALLOWS ANGLE ADJUSTMENT. VANS RV-8 15271 SUPERIOR IO-360-B1HD3 ENGINE INSTALLATION OF SUPERIOR IO-360-B1HD3 ENGINE WITH MT-V-12B/183-59b PROPELLER. SUPERIOR XP-IO-360-B1HD3 SOUT INSTALLATION VANS RV-8A 15364 DYNON D100A WITH AP74 CONTROLLER INSTALLATION OF DYNON D100A DUAL AXIS AUTO-PILOT WITH AP74 CONTROLLER. LYCOMING IO-360-A1B6 RVCH DUAL AXIS AUTO-PILOT INSTALLATION ROLL SERVO MOUNTED IN STARBOARD WING BESIDE AILERON BELLCRANK, WITH PUSH-ROD DRIVING A MODIFIED AILERON BELLCRANK, IN ACCORDANCE WITH DYNON AVIONICS AUTOPILOT SERVO INSTALLATION GUIDE DOCUMENT 101046-003 REV. G.

PITCH SERVO MOUNTED IN REAR FUSELAGE, WITH PUSH-ROD DRIVING PITCH PUSH-ROD IDLER, IN ACCORDANCE WITH DYNON AVIONICS AUTOPILOT SERVO INSTALLATION GUIDE, DOCUMENT 101046-002 REV. F.

AUTOPILOT OPITCH AND ROLL ACTUATION POWERED BY SV32 SERVOS. VANS RV-8A 14768 DYNON AP74 DUAL AXIS AUTOPILOT DYNON DUAL AXIS AUTOPILOT DRIVEN BY A DYNON D100 EFIS AND CONTROLLED VIA A DYNON LYCOMING YIO-360-M1B SUTE INSTALLATION AP74. DYNON SV32 SERVOS INSTALLED IN ACCORDANCE WITH MANUFACTURER'S DRAWINGS AND USING MANUFACTURER'S HARDWARE, EXCEPT PITCH SERVO MOUNTED ON CUSTOM TRAY ON LOWER LONGERONS OF REAR FUSELAGE. VANS RV-8A 12355 TRUTRAK DIGIFLIGHT II VS AUTO PILOT INSTALLATION OF TRUTRAK DIGIFLIGHT II VS AUTOPILOT IN ACCORDANCE WITH TRUTRAK FLIGHT LYCOMING YIO-360-A1B6 HCCF SYSTEMS INSTALLATION INSTRUCTIONS SPECIFIED FOR THE VANS RV-8. VANS RV-8A 14051 LASAR SYSTEM REPLACING ONE LASAR ELECTRONIC IGNITION MODULE REPLACES ONE STANDARD MAGNETO, IN ACCORDANCE LYCOMING YIO-360-A1B6 HCCF MAGNETO WITH THE MANUFACTURER'S INSTRUCTIONS.

DUE TO INCOMPATIBILITY WITH THE HARTZELL PROPELLER, THE USE OF THE LASAR SYSTEM IS RESTRICTED TO ENGINE START-UP ONLY - ONCE ENGINE HAS STARTED THE LASAR SYSTEM IS TO BE SWITCHED OFF, GIVING STANDARD IGNITION TIMING ON BOTH MAGNETOS.

PLACARD TO BE INSTALLED STATING "SWITCH LASAR SYSTEM OFF AFTER STARTING". VANS RV-9 12669 INSTALLATION OF DYNON ROLL & PITCH INSTALLATION OF DYNON ROLL & PITCH AUTOPILOT. LYCOMING IO-320-D1A RVDG AUTOPILOT THE ROLL SERVO IS ATTACHED TO THE STARBOARD WING SPAR VIA A NEW DYNON SUPPLIED ELONGATED AILERON BELLCRANK SUPPORT BRACKET AND A STAY. THE PUSH-ROD IS CONNECTED TO THE AILERON BELLCRANK VIA A STAND-OFF TUBE AND ADDITIONAL PLATE. THE PITCH SERVO IS ATTACHED, VIA A DYNON SUPPLIED BRACKET, TO THE SAME STRUCTURE AS THE PITCH CONTROL IDLER BELLCRANK. THE PUSH-ROD IS CONNECTED DIRECTLY TO ONE SIDE OF THE IDLER BELLCRANK. VANS RV-9 12276 INSTALLATION OF 'BELL' TAILWHEEL INSTALLATION OF 'BELL' TAILWHEEL FORK TO INCREASE GROUND CLEARANCE OF FUSELAGE REAR LYCOMING IO-320-D1A RVDG FORK IN ACCORDANCE WITH DRAWINGS STATED BELOW. VANS RV-9 12081 INSTALLATION OF DYNON PITOT TUBE INSTALLATION OF DYNON PITOT TUBE WITH SAFEAIR1 INSTALLATION KIT. LYCOMING IO-320-D1A RVDG ON SAFEAIR1 MAST. VANS RV-9 12762 INSTALLATION OF TRUTRAK ALTRAK VS INSTALLATION OF TRUTRAK ALTRAK VS ALTITUDE HOLD AUTO PILOT USING TRU TRAK LYCOMING O-235-L2C IOSL ALTITUDE HOLD AUTO PILOT INSTALLATION KIT. VANS RV-9 12992 JPI 450P FUEL FLOW UNIT JPI 450P FUEL FLOW UNIT INSTALLED IN ENGINE COMPARTMENT SITUATED BETWEEN ELECTRIC LYCOMING O-235-L2C IOSL PUMP AND MECHANICAL VANS RV-9 12590 WING LEVELLER TRUTRAK DIGITRAK WING LEVELLER INSTALLED, WITH SERVO MOUNTED IN THE WING. LYCOMING O-320-B2C RVNV Prototype mods that have been approved since 1/1/2008 Page 142 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-9 11133 DIGITRAK AUTOPILOT DIGITRAK WING LEVELLER FITTED, SERVO INSTALLED IN WING, CONNECTED BY PUSHROD TO LYCOMING O-320-B3B RVIW EXISTING AILERON BELLCRANK PER TRUTRAK INSTRUCTIONS VANS RV-9 13652 DYNON AOA INDICATOR DYNON UNHEATED PITOT HEAD MOUNTED TO THE PORT WING USING A GRETZ MAST. AOA LYCOMING O-320-B3B RVIW INDICATION PROVIDED BY A DYNON D100 EFIS UNIT AND ENHANCED AURAL WARNING VIA A DYNON HS34. PITOT MAST INSTALLED IN ACCORDANCE WITH GRETZ INSTRUCTIONS AND POSITIONED ON THE UNDER-SURFACE OF THE WING, INBOARD OF THE 7TH LEADING EDGE RIB FROM THE TIP AND AFT OF THE SPAR. VANS RV-9 12545 REDESIGNED ENGINE COOLING PLENUM FIBRE GLASS TOP FITTED TO COOLING PLENUM BAFFLES RATHER THAN RELYING ON INSIDE OF LYCOMING O-320-D1A CFED UPPER COWL ACTING AS UPPER SURFACE OF COOLING PLENUM. FIBRE GLASS PLENUM TOP MANUFACTURED AND FITTED TO EXISTING BAFFLES AS DETAILED IN APPLICATION. VANS RV-9 11217 BONDING OF PLEXIGLASS CANOPY (TIP- SIKAFLEX 295 UV ADHESIVE COMPOUND USED TO ATTACH CANOPY BUBBLE IN LIEU OF MULTIPLE LYCOMING O-320-D1A CFED UP OR SLIDER) FOR RV-7/7A & RV-9/9A AN507-6R8 SCREWS.

ISSUE 2: MODIFICATION APPLICABILITY EXTENDED TO INCLUDE RV9/9A AIRCRAFT SERIES. ISSUE 3: NOW INCLUDES BOTH TIP-UP AND SLIDING CANOPY AND WINDSCREEN. VANS RV-9 12276 INSTALLATION OF 'BELL' TAILWHEEL INSTALLATION OF 'BELL' TAILWHEEL FORK TO INCREASE GROUND CLEARANCE OF FUSELAGE REAR LYCOMING O-320-D2A XXRV FORK IN ACCORDANCE WITH DRAWINGS STATED BELOW. VANS RV-9 14268 GRETZ PITOT MOUNT & DYNON PITOT DYNON UNHEATED PITOT/ANGLE OF ATTACK HEAD P/N 100141-000 MOUNTED ON GRETZ AERO LYCOMING O-320-D3G CIPL HEAD WITH AOA PORT CBK-12 PITOT MOUNT. THIS IS LOCATED ON THE UNDERSIDE OF THE PORT WING OUTBOARD OF THE INSPECTION HATCH, IN ACCORDANCE WITH THE MANUFACTURER'S INSTRUCTIONS. ANGLE OF ATTACK PORT CONNECTED TO DYNON D180 EFIS.

AT ISSUE 2, DYNON SKYVIEW UNIT ADDED AS ACCEPTABLE ALTERNATIVE ANGLE OF ATTACK DISPLAY/WARNING DEVICE.

VANS RV-9 13650 DYNON 2 AXIS AUTOPILOT DYNON 2-AXIS AUTOPILOT INSTALLED. DYNON SV32 SERVOS INSTALLED IN WING AND REAR LYCOMING O-320-D3G CIPL FUSELAGE TO CONTROL ROLL AND PITCH RESPECTIVELY. INSTALLED AS PER MANUFACTURER'S INSTRUCTIONS. SERVOS CONTROLLED BY DYNON D100 EFIS. VANS RV-9 12652 TRUTRAK DIGIFLIGHT II WING LEVELLER INSTALLATION OF TRUTRAK DIGIFLIGHT II WING LEVELLER SERVO IN WING AND CONTROL UNIT IN SUPERIOR XP-IO-320-B1AD2 CFSG COCKPIT IN ACCORDANCE WITH THE MANUFACTURER'S INSTRUCTIONS VANS RV-9 13204 DUAL P-MAGS INSTALLATION OF E-MAG IGNITIONS DUAL P-MAG P-114 UNITS AND ASSOCIATED CIRCUIT SUPERIOR XP-O-320-A1C2 CGMG BREAKERS. VANS RV-9 13205 SKYBOLT CLOC COWL FASTENING INSTALLATION OF SKYBOLT CLOC COWLING FASTENER KIT FOR RV AIRCRAFT. INSTALLATION SUPERIOR XP-O-320-A1C2 CGMG INCORPORATES ALUMINIUM ALLOY STRIPS RIVETED TO FIREWALL AND COWLS, IN ACCORDANCE WITH SKYBOLT INSTRUCTIONS "2007 VANS RV AND OTHER KIT PLANE INSTRUCTIONS".

VANS RV-9 13206 COOLING PLENUM CUSTOM-MADE CARBON & GLASS FIBRE REINFORCED PLASTIC PLENUM AND ASSOCIATED FITTINGS SUPERIOR XP-O-320-A1C2 CGMG MANUFACTURED TO AID ENGINE COOLING. VANS RV-9 13207 SKYFLASH/WHELEN STROBES SKYFLASH SFD3 STROBE UNITS MOUNTED IN WING TIPS. WHELEN A500A STROBE UNIT MOUNTED SUPERIOR XP-O-320-A1C2 CGMG ON RUDDER FAIRING. POWER UNIT MOUNTED ON MODIFIED VANS 'ELT/PWR MOUNT 7/9-R' IN REAR SECTION OF FUSELAGE. 5 AMP CIRCTUIT BREAKER FITTED. VANS RV-9 13208 USE SIKAFLEX TO BOND REAR CANOPY SIKAFLEX 295UV USED TO BOND THE FRONT EDGE OF THE REAR (FIXED) CANOPY TO THE FRAME SUPERIOR XP-O-320-A1C2 CGMG INSTEAD OF THE SCREWS CALLED UP BY THE BUILD MANUAL. VANS RV-9 14479 GARMIN G5 DUAL AXIS AUTO-PILOT INSTALLATION OF GARMIN G5 DUAL AXIS AUTO-PILOT WITH GARMIN GMC 307 CONTROLLER AND SUPERIOR XP-O-320-A1C2 CGMG INSTALLATION USING TWO GARMIN GSA 28 SERVOS INSTALLED USING GARMIN SERVO INSTALLATION BRACKETS IN ACCORDANCE WITH GARMIN INSTALLATION MANUAL 190-01115-01 REV AA. VANS RV-9A 13486 INSTALLATION OF VERTICAL POWER VP-X INSTALLATION OF VERTICAL POWER VP-X SPORT ELECTRICAL POWER CONTROL SYSTEM LYCOMING IO-320-B1A OPVM SPORT ELECTRICAL POWER CONTROL INCORPORATING FLAP POSITIONING AND PITCH AND ROLL TRIM CONTROL. SYSTEM

Prototype mods that have been approved since 1/1/2008 Page 143 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-9A 13487 INSTALLATION OF REPLACEMENT AUTO INSTALLATION OF DUAL AXIS AUTO-PILOT SYSTEM USING MGL iEFIS WITH MGL SERVOS REPLACING LYCOMING IO-320-B1A OPVM PILOT USING THE MGL IEFIS PREVIOUSLY FITTED TRIO ROLL AND TRUTRAK PITCH AUTO-PILOT SYSTEMS. ROLL SERVO MOUNTED IN STARBOARD WING ADJACENT TO AILERON BELLCRANK WITH DYNON ROLL SERVO MOUNTING KIT PARTS AND CUSTOM MADE BASE PLATE AND TOP SUPPORT BRACKET. PITCH SERVO MOUNTED TO EXISTING BRACKET. VANS RV-9A 13488 RE-LOCATION OF FUSELAGE RIBS TO PORTION OF FUSELAGE RIBS F-745-L AND F-745-R AFT OF F-768 PANEL REMOVED FROM FORWARD LYCOMING IO-320-B1A OPVM ACCOMMODATE DUAL EFIS SCREENS SECTION AND RE-POSITIONED OUTBOARD 2" RESPECTIVELY TO ALLOW THE INSTALLATION OF DUAL EFIS UNITS IN INSTRUMENT PANEL. VANS RV-9A 14538 LOWER WING SPAR ATTACH BOLT HOLE LOWER WING SPAR ATTACHMENT BOLT HOLES (4 OFF) REAMED OVERSIZE TO REMOVE DAMAGE. LYCOMING O-320-B2C RPRV DAMAGE NAS2907-50 BOLTS USED. VANS RV-9A 12413 TRU-TRAK DIGITRAK WING LEVELLING TRU-TRAK DIGITRAK WING LEVELLING AUTO-PILOT LYCOMING O-320-D1A RVNH AUTO-PILOT VANS RV-9A 13287 COWLING LOUVRES GLOSTER AIRPARTS MOULDED COWLING LOUVRES RIVETTED TO APERTURE MADE IN COWL TO LYCOMING O-320-D1A RVNH IMPROVE COOLING VANS RV-9A 13494 HEATED PITOT GROETZ AERO AUTOMATIC HEATED PITOT GA-1000 FITTED USING GROETZ AERO PITOT MAST AND LYCOMING O-320-D1A RVNH BRACKET AND ASSOCIATED MULTI-LIGHT COCKPIT DISPLAY. VANS RV-9A 12020 TRUTRAK DIGIFLIGHT II VS ALTITUDE INSTALLATION OF TRUTRAK DIGIFLIGHT II VS AUTOPILOT HEAD AND ALTITUDE HOLD SERVO LYCOMING O-320-D1A RVNH HOLD VANS RV-9A 13604 PORTABLE OXYGEN SYSTEM INSTALLATION OF MOUNTING BRACKETS SUPPLIED BY MOUNTAIN HIGH AVIATION OXYGEN LYCOMING O-320-D1A RVNH INSTALLATION SYSTEMS TO SECURE OXYGEN BOTTLE MH AL-415 TO REAR BULKHEAD OF BAGGAGE BAY. VANS RV-9A 13294 OIL COOLER AIR CONTROL OIL COOLER SHUTTER ADDED TO CONTROL COOLING AIRFLOW USING PILOT CONTOLABLE PUSH- LYCOMING O-320-D1A CCND PULL CONTROL VANS RV-9A 12669 INSTALLATION OF DYNON ROLL & PITCH INSTALLATION OF DYNON ROLL & PITCH AUTOPILOT. LYCOMING O-320-D1A CCZY AUTOPILOT THE ROLL SERVO IS ATTACHED TO THE STARBOARD WING SPAR VIA A NEW DYNON SUPPLIED ELONGATED AILERON BELLCRANK SUPPORT BRACKET AND A STAY. THE PUSH-ROD IS CONNECTED TO THE AILERON BELLCRANK VIA A STAND-OFF TUBE AND ADDITIONAL PLATE. THE PITCH SERVO IS ATTACHED, VIA A DYNON SUPPLIED BRACKET, TO THE SAME STRUCTURE AS THE PITCH CONTROL IDLER BELLCRANK. THE PUSH-ROD IS CONNECTED DIRECTLY TO ONE SIDE OF THE IDLER BELLCRANK. VANS RV-9A 12872 COMBO NAV/LANDING WING LIGHTS INSTALLATION OF CREATIVAIR COMBINED WINGTIP LED-TYPE NAVIGATION LIGHTS AND HALOGEN- LYCOMING O-320-D1A DHOP TYPE LANDING LIGHTS. NAVIGATION LIGHTS CONTROLLED BY A SWITCH VIA A 2A INLINE FUSE. LANDING LIGHTS ARE CONTROLLED BY A SWITCH VIA A 15A INLINE FUSE. VANS RV-9A 12873 TRUTRAK PICTORIAL PILOT AUTO-PILOT INSTALLATION OF TRUTRAK PICTORIAL PILOT AUTO-PILOT ROLL CONTROL (WING LEVELLER) IN LYCOMING O-320-D1A DHOP (ROLL) ACCORDANCE WITH THE MANUFACTURER'S INSTRUCTIONS. SERVO MOUNTED IN RIGHT WING. CONTROL UNIT INSTALLED IN COCKPIT. VANS RV-9A 12081 INSTALLATION OF DYNON PITOT TUBE INSTALLATION OF DYNON PITOT TUBE WITH SAFEAIR1 INSTALLATION KIT. LYCOMING O-320-D1A DHOP ON SAFEAIR1 MAST. VANS RV-9A 14344 PROPELLER CHANGE TO HARTZELL INSTALLATION OF HARTZELL HC-C2YL/F7663-4 PROPELLER ON LYCOMING O-320-D1A. LYCOMING O-320-D1A RVJP VANS RV-9A 12770 TRUTRAK DIGITRAK WING LEVELLER TRUTRAK DIGITRAK WING LEVELLER INSTALLED. ROLL SERVO INSTALLED IN STARBOARD WING IN LYCOMING O-320-D2G CFMC ACCORDANCE WITH MANUFACTURER'S DRAWINGS. VANS RV-9A 11899 FLEXIBLE FUEL PIPE SUBSTITUTED STAINLESS STEEL SHEATHED RUBBER AIRCRAFT FLEXIBLE FUEL TUBING SUBSTITUTED BETWEEN LYCOMING O-320-D2G CFMC WING TANK AND FUEL SELECTOR, IN PLACE OF STANDARD ALUMINIMUM TUBING, FOR EASE OF ROUTING PAST OBSTRUCTIONS. VANS RV-9A 11202 RUDDER CABLE FAIRINGS A SMALL ALUMINUIM FAIRING IS MANUFACTURED AND INSTALLED OVER THE CABLE EXIT TUBE IN LYCOMING O-320-D2J CDRV THE REAR FUSELAGE. VANS RV-9A 12082 MODULAR INSTRUMENT PANEL INSTALLATION OF AFFORDABLE PANELS' MODULAR INSTRUMENT PANEL. LYCOMING O-320-D2J CDRV VANS RV-9A 11197 HEATED PITOT INSTALLATION OF AERO INSTRUMENT CO INC ELECTRICALLY HEATED PITOT HEAD AN5812 AND LYCOMING O-320-D2J CDRV GRETZ MOUNT.

Prototype mods that have been approved since 1/1/2008 Page 144 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-9A 13840 INSTALLATION OF TRUTRAK VIZION 380 INSTALLATION OF TRUTRAK VIZION 380 DUAL AXIS AUTO-PILOT WITH THE ROLL SERVO MOUNTED LYCOMING O-320-D2J CDRV AUTO PILOT IN THE LEFT WING IN ACCORDANCE WITH TRUTRAK DRAWING 'RV-9' AND THE PITCH SERVO INSTALLED IN THE REAR FUSELAGE ADJACENT TO THE PITCH SYSTEM IDLER BELLCRANK IN ACCORDANCE WITH TRUTRAK DRAWING 'RV-6 PITCH'. VANS RV-9A 12299 INSTALL WILKSCH WAM 120 ENGINE WILKSCH WAM 12 ENGINE INSTALLED PER PREVIOUS INSTALLATIONS LYCOMING O-320-D3G EGBS VANS RV-9A 13483 RV 'A' TYPE NOSE LEG STIFFENER 'ANTI- INSTALLATION OF ANTI-SPLAT AERO NOSE LEG STIFFENER WITH ASSOCIATED NOSE LEG FAIRING. LYCOMING O-320-D3G EGBS SPLAT NOSE JOB' VANS RV-9A 14611 ENGINE CHANGE TO LYCOMING O-320- ENGINE IS CHANGED TO A LYCOMING O-320-D3G USING A STANDARD VANS ENGINE MOUNT. LYCOMING O-320-D3G EGBS D3G PROPELLER FITTED IS A NEWTON 50R 70" X 70". VANS RV-9A 15162 PANEL UPGRADE INSTRUMENT PANEL SUPPORT STRUCTURE MODIFIED TO FACILITATE INSTALLATION OF EFIS. LYCOMING O-320-E2D IINI FORWARD FUSELAGE RIBS F745L & R CUT FLUSH AT AFT FACE OF INSTRUMENT PANEL SUB PANEL ASSEMBLY. SUBPANEL ATTACHED TO FORWARD STRUCTURE VIA TRANSPONDER/RADIO MOUNTING TRAYS AND BRACKETS PLUS TUBLULAR ALLOY SUPPORTS. VANS RV-9A 15446 GARMIN G3X AUTOPILOT WITH GMC305 GARMIN DUAL AXIS AUTOPILOT INSTALLED. SYSTEM CONSISTS OF G3X SYSTEM WITH GMC305 LYCOMING O-320-E2D IINI CONTROLLER CONTROLLER AND TWO GSA28 SERVOS. SERVOS ARE MOUNTED IN THE AFT FUSELAGE AND RIGHTHAND WING USING GARMIN INSTALLATION KIT. VANS RV-9A 13558 BONDING CANOPY AND WINDSCREEN BONDING OF CANOPY AND WINDSCREEN USING SIKAFLEX -295 UV ADHESIVE IN ACCORDANCE LYCOMING O-320-E2D CHST INSTEAD OF MECHANICAL FASTENERS WITH CANOPY GLUING PROCEDURE BY ERIC WOLF. VANS RV-9A 14844 INSTALLATION OF GRETZ PITOT MAST & INSTALLATION OF GARMIN GAP26 HEATED PITOT PROBE ON GRETZ MOUNT TO UNDERSIDE OF LYCOMING O-320-E2D CEEP GARMIN PITOT HEAD PORT WING OUTBOARD OF INSPECTION HATCH, IN ACCORDANCE WITH MANUFACTURER'S INSTRUCTIONS. VANS RV-9A 12815 AVEOFLASH NAV/STROBE LIGHTS AVEOFLASHLP LSA E-SERIES NAV/POSITION/STROBE LIGHTS FITTED TO WING TIPS. COMPOSITE LYCOMING O-320-H2AD CGXR FAIRING ADDED TO EACH TIP TO ENABLE CORRECT ALIGNMENT OF LAMPS. VANS RV-9A 12879 ALTERATION TO PANEL MOUNTING INSTRUMENT PANEL ALTERED TO ACCOMMODATE EFIS UNIT. PANEL SUPPORT RIBS CUT WAY AND LYCOMING O-320-H2AD CGXR REINFORCED WITH DOUBLING PLATES. VANS RV-9A 12980 COWLING ATTACHMENT WITH MILSPEC ATTACHMENT OF COWLINGS TO FUSELAGE USING MILSPEC 1/4 TURN FASTENERS INPLACE OF LYCOMING O-320-H2AD CGXR 1/4 TURN FASTENERS VANS STANDARD HINGE METHOD, IN ACCORDANCE WITH MILSPEC INSTALLATION INSTRUCTIONS.

VANS RV-9A 12981 DYNON SKYVIEW EFIS, AOA PITOT HEAD DYNON SKYVIEW EFIS WITH DYNON AOA PITOT HEAD ON SAFEAIR MOUNTING, SAFEAIR PITOT- LYCOMING O-320-H2AD CGXR AND DUAL AXIS AUTO-PILOT STATIC AIR SYSTEM AND DYNON DUAL AXIS AUTOPILOT, INSTALLED AS PER MANUFACTURERS' INSTRUCTIONS. VANS RV-9A 13039 SAFE JUMP FACILITY SBX175 GROUND POWER SOCKET INSTALLED BELOW INSTRUMENT PANEL. INCLUDES ISOLATING LYCOMING O-320-H2AD CGXR RELAY, ASSOCIATED WIRING AND MOUNTING BRACKET. VANS RV-9A 13040 SHORTEN CONTROL STICK CONTROL COLUMN SHORTENED BY 2.0" FOR INCREASED PILOT COMFORT LYCOMING O-320-H2AD CGXR VANS RV-9A 13165 INSPECTION PANELS IN FORWARD TOP TWO INSPECTION PANELS ADDED TO FORWARD TOP SKIN TO ALLOW ACCESS TO AVIONICS BAY. LYCOMING O-320-H2AD CGXR SKIN DOUBLER PLATES ADDED TO SKIN WITH MATCHING COVER PLATES. VANS RV-9A 12283 TIP-UP INSTRUMENT PANEL SUPPORT INSTRUMENT PANEL ALTERED PER APPLICANT'S APPLICATION TO ENABLE EFIS PANELS TO BE LYCOMING YIO-320-D1A CIYV WITH EFIS SCREENS FITTED. EXISTING RIBS F745 L/R SHORETENED AND REPLACED WITH FOUR RIBS PLACED SYMETRICALLY EITHER SIDE OF SCREENS VANS RV-9A 12525 INSTALLATION OF CESSNA -TYPE PITOT CESSNA 152 STYLE PITOT MAST SUBSTITUTED LYCOMING YIO-320-D1A NYNA HEAD VANS RV-9A 12082 MODULAR INSTRUMENT PANEL INSTALLATION OF AFFORDABLE PANELS' MODULAR INSTRUMENT PANEL. LYCOMING YIO-320-D1A NYNA VANS RV-9A 12283 TIP-UP INSTRUMENT PANEL SUPPORT INSTRUMENT PANEL ALTERED PER APPLICANT'S APPLICATION TO ENABLE EFIS PANELS TO BE LYCOMING YIO-320-D1A RVWJ WITH EFIS SCREENS FITTED. EXISTING RIBS F745 L/R SHORETENED AND REPLACED WITH FOUR RIBS PLACED SYMETRICALLY EITHER SIDE OF SCREENS VANS RV-9A 13558 BONDING CANOPY AND WINDSCREEN BONDING OF CANOPY AND WINDSCREEN USING SIKAFLEX -295 UV ADHESIVE IN ACCORDANCE LYCOMING YO-320-D1A RTRV INSTEAD OF MECHANICAL FASTENERS WITH CANOPY GLUING PROCEDURE BY ERIC WOLF. VANS RV-9A 13559 INSTALLATION OF DYNON HEATED INSTALLATION OF DYNON HEATED AOA/PITOT TUBE WITH GRETZ MOUNT AND MAST. LYCOMING YO-320-D1A RTRV AOA/PITOT TUBE WITH GRETZ MOUNT AND MAST

Prototype mods that have been approved since 1/1/2008 Page 145 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-9A 13560 SKYFLASH STROBE/NAV LIGHT SKYFLASH STROBE DRIVER MOUNTED BELOW FLAP ACTUATOR MOTOR IN AREA BETWEEN SEATS. LYCOMING YO-320-D1A RTRV INSTALLATION STREAMLINED 'COMBO' STROBE/NAV LIGHT HEADS MOUNTED IN WING TIP RECESSES AS PROVIDED IN KIT. VANS RV-9A 13732 DYNON SKYVIEW AUTO-PILOT DYNON SKYVIEW CONTROLLED DUAL AXIS AUTO-PILOT INSTALLED IN ACCORDANCE WITH DYNON LYCOMING YO-320-D1A RTRV INSTALLATION INSTRUCTIONS. VANS RV-9A 14956 INSPECTION PANELS 2 OFF INSPECTION HATCHES INSTALLED IN UPPER FORWARD FUSELAGE SKIN TO PROVIDE ACCESS LYCOMING O-320-D2A DTPC TO AVIONICS BAY AND CANOPY HINGE MECHANISM. (MODIFIED) VANS RV-9A 15071 AVMAP STANDBY INSTRUMENT AVMAP ULTRA EFIS BACKUP INSTRUMENT INSTALLED TO PROVIDE BACKUP ASI AND ALTIMETER LYCOMING O-320-D2A DTPC INFORMATION. SOFTWARE VERSION 5.21.6C1 OR LATER TO BE USED, WHICH INCORPORATES (MODIFIED) CLEARER INDICATIONS OF ASI AND ALTITUDE WHEN USED IN THE HSI MODE. VANS RV-9A 13482 RV 'A' TYPE NOSE LEG STIFFENER 'ANTI- INSTALLATION OF ANTI-SPLAT AERO NOSE LEG STIFFENER WITH ASSOCIATED NOSE LEG FAIRING. SUPERIOR XP-IO-320-A1A2 RVJO SPLAT NOSE JOB' VANS RV-9A 13559 INSTALLATION OF DYNON HEATED INSTALLATION OF DYNON HEATED AOA/PITOT TUBE WITH GRETZ MOUNT AND MAST. SUPERIOR XP-IO-320-B1AC2 PTEK AOA/PITOT TUBE WITH GRETZ MOUNT AND MAST VANS RV-9A 13732 DYNON SKYVIEW AUTO-PILOT DYNON SKYVIEW CONTROLLED DUAL AXIS AUTO-PILOT INSTALLED IN ACCORDANCE WITH DYNON SUPERIOR XP-IO-320-B1AC2 PTEK INSTALLATION INSTRUCTIONS. VANS RV-9A 13029 FIT LANDING LIGHTS IN WING TIPS VANS LL10 MR-16 RV-10 LANDING LIGHT SYSTEM INSTALLED, MODIFIED TO FIT THIS TYPE. SUPERIOR XP-IO-320-B1AC2 XCRJ VANS RV-9A 13030 TO FIT TRIO EZ PILOT AUTOPILOT TRIO EZ PILOT WING LEVELLER SYSTEM FITTED IN ACCORDANCE WITH THE MANUFACTURER'S SUPERIOR XP-IO-320-B1AC2 XCRJ INSTRUCTIONS. SERVO MOUNTED USING TRIO-SUPPLIED BRACKET. VANS RV-9A 13031 FIT TRIO EZ SERIES ALTITUDE HOLD INSTALLATION OF TRIO EZ SERIES EZ-3 ALTITUDE HOLD IN ACCORDANCE WITH MANUFACTURER'S SUPERIOR XP-IO-320-B1AC2 XCRJ AUTOPILOT (EZ 3 MODEL) INSTRUCTIONS. TRIO GOLD SERVO MOUNTED ON ALLOY BRACKET. VANS RV-9A 13032 STROBE LIGHT FITMENT INSTALLATION OF AIRWORLD SKYFLASH 3SFD3 STROBE SYSTEM INCLUDING CUSTOM MOUNTING SUPERIOR XP-IO-320-B1AC2 XCRJ BRACKET FOR POWER UNIT IN FUSELAGE AND ASSOCIATED WIRING. LAMPS FITTED TO EACH WING TIP AND TO LOWER RUDDER FAIRING. VANS RV-9A 11781 SHORTEN CONTROL STICKS CONTROL STICKS SHORTENED AT TOP BY 3 INCHES IN SIMILAR MANNER AS ACCEPTED ON G-RVIX SUPERIOR XP-IO-320-B1AC2 XCRJ

VANS RV-9A 13131 WHELAN STROBE & POSITION LIGHT INSTALLATION OF WHELAN STROBE AND POSITION LIGHT SYSTEM AS PER VANS OPTION LNSYS6, SUPERIOR XP-O-320-B1A2 RVSG SYSTEM CONSISTING OF A POWER SUPPLY, STARBOARD WINGTIP POSITION LIGHT AND STROBE, PORT WINGTIP POSITION LIGHT AND STROBE AND TAIL POSITION LIGHT AND STROBE.

VANS RV-9A 13132 TRIO EZ PILOT WING LEVELLER TRIO EZ PILOT WING LEVELLER AUTOPILOT INCORPORATING A CONTROL/DISPLAY UNIT, A ROLL SUPERIOR XP-O-320-B1A2 RVSG AUTOPILOT CONTROL SERVO ATTACHED TO THE AILERON BELLCRANK IN THE STARBOARD WING, AND ASSOCIATED ELECTRICAL CONNECTIONS AND SWITCHGEAR. INSTALLED IN ACCORDANCE WITH TRIO OPERATION AND INSTALLATION MANUAL REV 2.3.

ISSUE 2 CORRECTS SOME TYPOGRAPHICAL ERRORS IN ISSUE 1. VANS RV-9A 13133 TRIO EZ-3 ALTITUDE CONTROL INSTALLATION OF TRIO EZ-3 ALTITUDE CONTROL AUTOPILOT CONTROL/DISPLAY HEAD, SERVO AND SUPERIOR XP-O-320-B1A2 RVSG AUTOPILOT ELECTRICAL CONNECTORS AND SWITCH GEAR. EXCEPT FOR THE PROVISION OF AN ADDITIONAL SUPPORT BRACKET AT THE AFT END OF THE SERVO, THE INSTALLATION IS AS PER THE MANUFACTURER'S INSTALLATION INSTRUCTIONS. VANS RV-9A 13650 DYNON 2 AXIS AUTOPILOT DYNON 2-AXIS AUTOPILOT INSTALLED. DYNON SV32 SERVOS INSTALLED IN WING AND REAR SUPERIOR XP-O-320-A1AHD2 PLAR FUSELAGE TO CONTROL ROLL AND PITCH RESPECTIVELY. INSTALLED AS PER MANUFACTURER'S INSTRUCTIONS. SERVOS CONTROLLED BY DYNON D100 EFIS. VANS RV-9A 13651 DUAL P-MAG INSTALLATION ON DUAL E-MAG P-MAG P114L4 UNITS INSTALLED TO REPLACE STANDARD MAGNETOS. INSTALLATION SUPERIOR XP-O-320-A1AHD2 PLAR SUPERIOR O-320 IN ACCORDANCE WITH MANUFACTURER'S INSTRUCTIONS, INCLUDING 3A CIRCUIT BREAKER AND COOLING BLAST TUBES.

Prototype mods that have been approved since 1/1/2008 Page 146 30/11/20 LAA Technical Leaflet TL 3.17 VANS RV-9A 13652 DYNON AOA INDICATOR DYNON UNHEATED PITOT HEAD MOUNTED TO THE PORT WING USING A GRETZ MAST. AOA SUPERIOR XP-O-320-A1AHD2 PLAR INDICATION PROVIDED BY A DYNON D100 EFIS UNIT AND ENHANCED AURAL WARNING VIA A DYNON HS34. PITOT MAST INSTALLED IN ACCORDANCE WITH GRETZ INSTRUCTIONS AND POSITIONED ON THE UNDER-SURFACE OF THE WING, INBOARD OF THE 7TH LEADING EDGE RIB FROM THE TIP AND AFT OF THE SPAR. VANS RV-9A 13816 INSTALLATION OF RED CUBE FUEL FLOW INSTALLATION OF ELECTRONICS INTERNATIONAL FT-60 'RED CUBE' FUEL FLOW TRANSDUCER. SUPERIOR XP-O-320-A1AHD2 PLAR TRANSDUCER VANS RV-9A 13732 DYNON SKYVIEW AUTO-PILOT DYNON SKYVIEW CONTROLLED DUAL AXIS AUTO-PILOT INSTALLED IN ACCORDANCE WITH DYNON WILKSCH WAM-120 XSAM INSTALLATION INSTRUCTIONS. VANS RV-9A 12556 ENGINE WAM 120 WILKSCH WAM 120 DIESEL AND MTV-21 PROPELLER FITTED WILKSCH WAM-120 CETP VANS RV-9A 12557 VANS 9A NOSEWHEEL MODIFICATION BILL KNOTT MODIFICATION PER MOD 12185 BUT APLPIED TO RV9A AIRFRAME WILKSCH WAM-120 CETP VANS RV-9A 12634 INSTALLATION OF STROBE & LANDING FITMENT OF SKYFLASH STROBE HEAD UNITS TO WING TIPS, STROBE DRIVER UNIT BELOW P1 SEAT, WILKSCH WAM-120 CETP LIGHTS RV-10 TYPE LANDING LIGHTS WITH LOWER RATED LAMPS TO WING TIPS, AND LAMP ON RUDDER.

VANS RV-9A 14135 PROPELLER CHANGE TO MT-V-6-D/175- INSTALLATION OF MT-V-6-D/175-112 PROPELLER WILKSCH WAM-120 CETP 112 VM-1 ESQUAL-C 13832 RETURN 3300 #1460 TO SOLID LIFTER CAMIT SOLID VALVE LIFTERS, (HONDA TYPE) CAMIT ROCKERS AND CAMIT 7/16" CRANKCASE JABIRU 3300A PHCJ CONFIGURATION THROUGH BOLTS RETRO-FITTED. CAMIT DOCUMENT ARWW14.12 OPTION 3 REFERS, HONDA LIFTERS WITH FLOOD FEED, KIT AMPTEC14M0-8 VM-1 ESQUAL-C 14197 CAMIT 40A BELT DRIVEN ALTERNATOR INSTALLATION OF CAMIT 40A BELT DRIVEN ALTERNATOR MOUNTED TO REAR OF ENGINE WITH JABIRU 3300A PHCJ INSTALLATION MOUNTING KIT DESIGNED AND SUPPLIED BY CAMIT - MANUFACTURER OF JABIRU ENGINES - IN ACCORDANCE WITH CAMIT INSTRUCTIONS. VM-1 ESQUAL-C 14202 EVO2 (12 CELL) LiFePO4 BATTERY INSTALLATION OF BALLISTIC PERFORMANCE COMPONENTS EVO2, 12 CELL, LiFePO4 LITHIUM ION JABIRU 3300A PHCJ INSTALLATION PHOSPHATE BATTERY (P/N 100-012) MOUNTED TO FORWARD FACE OF FIREWALL IN CUSTOM MADE BRACKET. OVER-VOLTAGE WARNING SYSTEM INCORPORATED IN AIRCRAFT'S EFIS AND SEPARATE BATTERY AND ALTERNATOR ISOLATION SWITCHES INSTALLED. VM-1 ESQUAL-C 14203 RED CUBE FT-60 FUEL FLOW SENDER INSTALLATION OF AN ELECTRONIC COMPONENTS INC. FT-60 'RED CUBE' FUEL FLOW TRANSDUCER JABIRU 3300A PHCJ MOUNTED BEHIND THE FIREWALL AND PLUMBED BETWEEN FUEL SELECTOR AND MECHANICAL FUEL PUMP. VPM M14 SCOUT 12320 ENGINE CHANGE ROTAX 914-F3 ENGINE SUBSTITUTED USING SAVAGE MOD FOR M16 ROTAX 914-F3 BUEN VPM M16 (MODIFIED) 12870 REPLACE VPM FRAME WITH MAGNI M16- MAGNI M16-C FRAME, NACELLE, WHEELS, NOSEWHEEL FORK, FRONT RUDDER PEDALS AND ROTAX 912-ULS ODPJ C FRAME ELECTRIM TRIM FITTED INSTEAD OF VPM ORIGINAL PARTS, FOLLOWING CRACK FOUND IN ORIGINAL MAST. VPM M16 TANDEM TRAINER 13921 REMOTE SPIN-ON OIL FILTER ADAPTER INSTALLATION OF 'HY-LUBE SYSTEMS' OIL FILTER TAKE-OFF ADAPTER TO OIL PUMP AND 'TORQUES SUBARU EA81 IBFP INSTALLATION FITTINGS' REMOTE SPIN-ON OIL FILTER ADAPTER THAT IS BOLTED TO REDUNDANT BATTERY TRAY BESIDE EXISTING BATTERY WITH K&N HP-1002 OIL FILTER. VPM M16 TANDEM TRAINER 12328 FITMENT OF SUBARU ENGINE SUBARU EA81 ENGINE AND ASSOCIATED ANCILIARIES INSTALLED IN PLACE OF EXISTING ARROW SUBARU EA81 BZJM ENGINE. THE VPM COMPOSITE 3 BLADED 68" DIAMETER PROPELLER IS RETAINED. WAG-AERO SPORT TRAINER 12468 PROPELLER CHANGE TO EVRA PROPELLER CHANGE TO EVRA D.11.28.4.C 70" DIAMETER X 43.3" PITCH. CONTINENTAL O-200-A BZHU D.11.28.4.C 70" X 43.3" WAG-AERO SPORT TRAINER 14985 HERCULES 7045261-S 70" X 45" INSTALLATION OF HERCULES 7045261-S 70 INCH DIAMETER X 45 INCH PITCH PROPELLER CONTINENTAL O-200-A BZHU PROPELLER INSTALLATION WAG-AERO SUPER SPORT 13144 ENGINE CHANGE TO LYCOMING O-360 LYCOMING 0-360-A4A ENGINE FITTED WITH SENSENICH W80CM84S WOOD PROPELLER , LYCOMING O-360-A4A DTUG LIGHTWEIGHT STARTER AND ALTERNATOR TO PRESERVE LOW INSTALLED ENGINE WEIGHT WAG-AERO SUPER SPORT 13385 GLIDER TOW HOOK INSTALLATION . LYCOMING O-360-A4A DTUG WAG-AERO WAGABOND 14744 NEWTON 07R 69" X 47" PROPELLER INSTALLATION OF NEWTON 07R 69" X 47" PROPELLER CONTINENTAL O-200-A WAGA INSTALLATION WICKO GM1 14710 HERCULES LA604-HP PROPELLER INSTALLATION OF HERCULES REPLICA OF A LANG LA604 PROPELLER DESIGNATED LA604-HP. DE HAVILLAND GIPSY MAJOR 1 AFJB INSTALLATION

Prototype mods that have been approved since 1/1/2008 Page 147 30/11/20 LAA Technical Leaflet TL 3.17 WITTMAN W10 TAILWIND 13400 HERCULES 6772345-C 67" X 72" INSTALLATION OF HERCULES 6772345-C 67 INCH DIAMETER X 72 INCH PITCH PROPELLER. CONTINENTAL O-300-D BOIB PROPELLER INSTALLATION WITTMAN W10 TAILWIND 12517 PROPELLER CHANGE TO CATTO 68" X 60" PROPELLER CHANGE TO CATTO 68 INCH DIAMETER X 60 INCH PITCH. LYCOMING O-290-G BJWT

WITTMAN W8 TAILWIND 12912 MCCAULEY 1A105/SCM7053 70" X 53" INSTALLATION OF MCCAULEY 1A105/SCM7053 70 INCH DIAMETER X 53 INCH PITCH PROPELLER. CONTINENTAL O-200-A BCBR PROPELLER WITTMAN W8 TAILWIND 12880 MODIFICATION OF W8 WING TIP TO W10 WING TIP REWORKED TO W10 DRAWINGS. CONTINENTAL O-200-A BOHV WING TIP WITTMAN W8 TAILWIND 13917 SPIN-ON OIL FILTER ADAPTER FOR INSTALLATION OF CUSTOM MADE SPIN-ON OIL FILTER ADAPTER P/N 79001003 WITH CHAMPION CONTINENTAL PC60 BPYJ CONTINENTAL PC60 (O-200) CH48108 OR C138 OR BLUE PRINT ADT32109 OIL FILTER.

AT ISSUE 4: APPLICABILITY EXTENDED TO CONTINENTAL C90-12 ENGINE. AT ISSUE 6: APPLICABILITY EXTENDED TO CONTINENTAL C85-12F ENGINE. AT ISSUE 7: APPLICABILITY EXTENDED TO CONTINENTAL C90-14F ENGINE. WITTMAN W8 TAILWIND 13837 INCREASE MTOW AND OTHER Max gross weight increased to 1400 Lbs, Vne increased to 181 mph, 150 mph VNO introduced. LYCOMING O-235-K2B ZIPY LIMITATIONS CHANGES WOLF WII BOREDOM FIGHTER 12619 PROPELLER CHANGE TO LODGE TYPE 100 FITMENT OF LODGE TYPE 100 PROPELLER, 70 INCHES DIAMETER BY 47 INCHES PITCH, TO A CONTINENTAL A65-8F BMZX CONTINENTAL A65-8F ENGINE. WOLF WII BOREDOM FIGHTER 12665 PROPELLER CHANGE TO SENSENICH PROPELLER CHANGE TO SENSENICH W72CK44, 72 INCH DIAMETER X 44 INCH PITCH PROPELLER. CONTINENTAL A65-8F BMZX W72CK44 X'AIR HAWK 14651 ENGINE & PROPELLER CHANGE TO D STANDARD OPTIONAL DMOTOR INSTALLATION RETRO-FITTED D-MOTOR LF26 CEON MOTOR LF26 & NEWTON WOODEN 2 BLADED 58 X 47 X'AIR HAWK 13623 ENGINE AND PROPELLER CHANGE D-MOTOR LF26 TRIAL INSTALLATION D-MOTOR LF26 CGHV X'AIR HAWK 13632 CHANGE WINGS FOR NEW AS SUPPLIED LATER MOULDED WING TIPS STYLE HAWK WINGS RETRO-FITTED. JABIRU 2200A IWIN IN NEW KIT X'AIR HAWK 13017 THERMOSTATIC OIL COOLER ADAPTOR SELF-DESIGNED THERMOSTAT UNIT FITTED IN OIL CIRCUIT PER APLICANT'S SUBMISSION JABIRU 2200A CFKE (TOCA) FOR JABIRU ENGINES X'AIR HAWK 14273 KIEV 273/1700 PROPELLER INSTALLATION INSTALLATION OF KIEV 273/1700 170CM DIAMETER X 24 DEGREES AT 35CM RADIUS PITCH ROTAX 912-UL CGCV PROPELLER X'AIR HAWK 14733 STROBE LIGHTS INSTALLATION OF SKYFLASH STROBES/NAV LIGHTS TO WINGTIPS, ALONG WITH ASSOCIATED ROTAX 912-UL CGVE CONTROL UNIT MOUNTED TO FUSELAGE FLOOR. X'AIR HAWK 13906 WATER RADIATOR CUSTOM COOLANT RADIATOR FABRICATED FOR ROTAX 912 ENGINE ROTAX 912-UL CICU X'AIR HAWK 14969 BRAKES INSTALLATION OF MAGURA 42-A18-03D SOLID BRAKE DISC IN PLACE OF ORIGINAL MAGURA ROTAX 912-UL CICU 2.701.446 VENTED BRAKE DISC. XTREME AIR SBACH 300 14073 PROPELLER CHANGE TO MT-V-14-B-C/C INSTALLATION OF MT-V-14-B-C/C 190-130, 4 BLADED HYDRAULIC CONSTANT SPEED PROPELLER. LYCOMING AEIO-580-EXP IIRI 190-130 ZENAIR CH 250 14284 SENSENICH 72CK-0-56, 70" DIAMETER INSTALLATION OF SENSENICH 72CK-0-56 PROPELLER, CROPPED TO BE 70 INCHES DIAMETER. LYCOMING O-235-C2A GFKY PROPELLER INSTALLATION ZENAIR CH 601HD 12756 PROPELLER CHANGE TO JAMES JAMES AJ6652/LC/RR 66" x 52" PROPELLER FITTED CONTINENTAL O-200-A CBDG AJ6652/LC/RR 66" x 52" ZENAIR CH 601HD 13202 HERCULES 6753277-S 67" x 53" INSTALLATION OF HERCULES 6753277-S 67 INCH DIAMETER X 53 INCH PITCH PROPELLER. CONTINENTAL O-200-A CBDG PROPELLER. ZENAIR CH 601HD 13771 PROPELLER CHANGE TO WOODCOMP SR INSTALLATION OF WOODCOMP SR3000/3 1700MM DIAMETER PROPELLER WITH SMART AVIONICS ROTAX 912-UL BVAC 3000/3 CSC-1/G CONTROLLER. ZENAIR CH 601HD 14068 WOODCOMP SR3000/3N 1720MM INSTALLATION OF WOODCOMP SR3000/3N 1720MM DIAMETER PROPELLER. ROTAX 912-UL BVAC DIAMETER PROPELLER INSTALLATION ZENAIR CH 601HD 13158 PROVISION FOR FITTING OF TOWBAR ON STEEL PLATE INSERTED BETWEEN NOSEWHEEL LEG AND NOSEWHEEL FORK TO ENABLE A TOWBAR ROTAX 912-UL EZUB NOSEWHEEL TO BE ATTACHED FOR THE PURPOSES OF GROUND HANDLING.

Prototype mods that have been approved since 1/1/2008 Page 148 30/11/20 LAA Technical Leaflet TL 3.17 ZENAIR CH 601HD 12448 TYPE DESIGNATION CHANGE FROM HDS INSTALLATION OF HD WINGS. ROTAX 912-UL OANN TO HD ZENAIR CH 601HD 12639 WOODCOMP PROPELLER WOODCOMP KLASSIC 170/3/R PROPELLER FITTED. ROTAX 912-UL OANN ZENAIR CH 601HD 11361 TWIN CONTROL STICKS STANDARD CENTRAL CONTROL STICK REPLACED WITH TWIN CONTROL STICKS. UL POWER 260i ZENY ZENAIR CH 601HD 11782 BRAKE PEDALS BRAKE PEDALS REVISED TO IMPROVE BRAKE OPERATION. UL POWER 260i ZENY ZENAIR CH 601HD 11783 UNDERCARRIAGE BEARING PLATES TUFNOL BEARING PLATES ADDED TO EXISTING ALLOY UNDERCARRIAGE BEARINGS. UL POWER 260i ZENY ZENAIR CH 601HD 11784 IMPROVED RUDDER CENTRING ADDITION OF CENTRING CAM AND SHOCK CORD ROLLERS TO IMPROVE CENTRING EFFECT. UL POWER 260i ZENY ZENAIR CH 601HD 11785 REPLACE FAIRLEADS WITH PULLEYS FAIRLEADS ON TWO RUDDER CABLES AND ONE ELEVATOR CABLE REPLACED WITH PULLEYS TO UL POWER 260i ZENY REDUCE FRICTION AND IMPROVE MAINTENANCE ACCESS. ZENAIR CH 601HD 12213 CHANGES TO CANOPY AND LATCH CANOPY HINGES MODIFIED FROM SIDE-OPENING TO TIP-UP WITH INTERNAL ARMS MOUNTED ON UL POWER 260i ZENY A FORWARD PIVOT POINT. LATCH CHANGED TO MULTI-POSITION HOOK AND OVERCENTRE LATCH.

ZENAIR CH 601HD 12472 ENGINE MOUNT ENGINE MOUNT TO CARRY ULPOWER 260I ENGINE, CONSTRUCTED FROM WELDED TUBULAR UL POWER 260i ZENY STEEL. ZENAIR CH 601HD 12473 DUAL THROTTLE LEVERS REPLACEMENT OF STANDARD T-BARS AT EACH SIDE OF COCKPIT WITH PORT AND CENTRAL LEVERS UL POWER 260i ZENY LINKED BY A ROD BEHIND THE INSTRUMENT PANEL. INCORPORATES FRICTION NUT. ZENAIR CH 601HD 13364 ENGINE & PROPELLER CHANGE INSTALLATION OF ULPOWER 260I ENGINE AND DUC SWIRL 3-BLADED 1520 MM DIA PROPELLER. UL POWER 260i ZENY (NOTE THAT ENGINE MOUNT IS APPROVED IN MOD 12472.) ZENAIR CH 601HDS 10589 IMPROVEMENT TO WHEEL BRAKING MODIFIED BRAKE SYSTEM GEOMETRY FOR IMPROVED BRAKING AUTHORITY. ROTAX 912-UL BVAB SYSTEM. ZENAIR CH 601HDS 12298 ELECTRICAL CARBURETTOR HEAT SYSTEM ELECTRIC CARB HEAT SYSTEM FITTED TO BING CARBURETTORS BASED ON DESIGN BY RON ROTAX 912-ULS BYJT BARNARD (SEE MOD 11465). ZENAIR CH 601HDS 12497 REPLACEMENT OF ENGINE COWLING REPLACEMENT OF ENGINE COWLING WITH ZENAIR CH601XL COWLING ROTAX 912-ULS BYJT WITH ZENAIR CH601XL COWLING ZENAIR CH 601HDS 12732 FIT ELEVATOR TRIM TAB CH601 XL TYPE WIDE SPAN SERVO DRIVEN TRIM TAB FITTED, WITH SUITABLY MODIFIED TAB ROTAX 912-ULS BYJT OPERATING HORN (DRAWING V 2.0 DATED 4/12/09). EXISTING ELEVATOR DOWN SPRING REMAINS INSTALLED TO PROVIDE IMPROVED LONGITUDINAL STATIC STABILITY ENHANCEMENT.

ZENAIR CH 601HDS 13194 FITTING OF POSITION LIGHTS POSITION LIGHTS FITTED TO WING TIPS AND RUDDER TRAILING EDGE PER STANDARD AVIATION ROTAX 912-ULS BYJT PRACTISE. LIGHTS NOT CHECKED FOR COMPLIANCE WITH LIGHTING REQUIREMENTS HENCE ONLY SUITABLE FOR DAY FLIGHT. ZENAIR CH 601HDS 13980 HELICES E-PROPS DURANDEL 100-L INSTALLATION OF HELICES E-PROPS DURANDEL 100-L 175CM DIAMETER 3 BLADED GROUND ROTAX 912-ULS BYJT 175CM DIA 3 BLADED PROPELLER ADJUSTABLE PROPELLER. INSTALLATION ZENAIR CH 601HDS 12603 PROPELLER CHANGE TO WOODCOMP WOODCOMP VARIA 170/2/R MODIFIED AND RE-DESIGNATED WOODCOMP 160/2/R 1600MM ROTAX 912-ULS OMEZ VARIA 160/2/R DIAMETER. ZENAIR CH 601HDS 13273 FITMENT OF MATCO BRAKE INTENSIFIER STANDARD RETRO FIT BRAKE INTENSIFIER FITTED IN ACCORDANCE WITH MATCO INSTRUCTIONS ROTAX 912-ULS OMEZ KIT ZENAIR CH 601HDS 13461 CUSTOM BUILT LED LIGHTING INSTALLATION OF CUSTOM MADE WINGTIP MOUNTED LED NAVIGATION AND STROBE LIGHTS ROTAX 912-ULS OMEZ REPLACING CONVENTIONAL BULB TYPE WHELAN NAV/STROBE LIGHTS AND A WING LEADING EDGE MOUNTED CONSPICUITY LIGHT REPLACING A CONVENTIONAL BULB TYPE LANDING LIGHT. FOR DAYTIME VFR USE ONLY.

ZENAIR CH 601UL 13824 AILERON HINGE MECHANISM FLEXIBLE SKIN AILERON HINGES REPLACED RETROSPECTIVELY WITH PIANO HINGES SIMILAR TO ROTAX 912 S CBUR ZENAIR'S STANDARD OPTION ZENAIR CH 601UL 13654 INSTALLATION OF LOW-VOLTAGE AVEO LOW VOLTAGE AVEO STROBE AND LANDING LIGHT FITTED ROTAX 912 S OOSH STROBE AND LANDING LIGHTS ZENAIR CH 601UL 13503 STROBES AIRWORLD SKYFLASH STROBE SYSTEM FITTED ROTAX 912-UL PATO ZENAIR CH 601UL 12791 DUAL STICK MODIFICATION DUAL STICK OPTION AS DESIGNED BY ALAN COZENS AND APPROVED ON G-BVAC ROTAX 912-UL FAOH

Prototype mods that have been approved since 1/1/2008 Page 149 30/11/20 LAA Technical Leaflet TL 3.17 ZENAIR CH 601ULA 13738 CATEGORY CHANGE TO GROUP A AS FLAPS LOCKED IN RAISED POSITION USING MODIFIED GATE, TO PREVENT LOWERING FLAP. MAX ROTAX 912-ULS CBAP CH601-ULA VARIANT GROSS WEIGHT INCREASED TO 473 Kg TAKING AIRCRAFT OUTSIDE OF MICROLIGHT CATEGORY

ZENAIR CH 601XL 14484 ZENAIR 'UPGRADE' KIT INSTALLATION OF ZENAIR WING REINFORCEMENTS AS PER DRAWINGS 6-ZU-1 (FEB 2010) AND 6-ZU-LYCOMING O-235-L2C CFKH 2 TO -4 (JAN 2010), WITH THE FOLLOWING CHANGES: - PART 6-ZU-4-2 FITTED HIGHER THAN DRAWING TO PROVIDE CLEARANCE. - ACCESS PANELS ADDED TO SKINS ADJACENT TO REAR WING ATTACHMENT PLATES TO PROVIDE ACCESS. - CENTRE SPAR FITTED TO FLOOR WITH ADDITIONAL ROW OF RIVETS DUE TO ELONGATION OF ORIGINAL HOLES DUE TO ALIGNMENT OF NEW AND OLD PARTS. ZENAIR CH 601XL 12451 DUAL STICK OPTION CZAW DUAL STICK OPTION ROTAX 912-ULS XLNT ZENAIR CH 601XL 12711 AILERON MASS BALANCE, WING ATTACH AILERON MASS BALANCES ADDED, WING ATTACHMENT AND CARRY-THROUGH REINFORCEMENTS, ROTAX 912-ULS EXLL REINFORCEMENT AND OTHER MISC CHANGE TO ELEVATOR TRIM RANGE, CHANGE TO CG AFT LIMIT, INTRODUCTION OF MAX ZERO CHANGES FUEL WEIGHT, ELIMINATION OF ELEVATOR TRIM BIAS SPRING, ADDITIONAL COCKPIT PLACARDS PER LAA MOD/162B/004 ZENAIR CH 601XL 13989 WOODCOMP SR3000/3N 1720MM INSTALLATION OF WOODCOMP SR3000/3N 1720MM DIAMETER PROPELLER. ROTAX 912-ULS EXLL DIAMETER PROPELLER INSTALLATION ZENAIR CH 601XL 13261 WOODCOMP PROPULS AES 170 INSTALLATION OF WOODCOMP PROPULS AES 170CM DIAMETER 3 BLADED COMPOSITE PROPELLER ROTAX 912-ULS CGPX PROPELLER WITH 6.5 KG SPACER. ZENAIR CH 601XL 15270 VERNIER THROTTLE VERNIER THROTTLE CONTROL TO REPLACE FRICTION LOCK THROTTLE CONTROL. ROTAX 912-ULS CEUW ZENAIR CH 601XL 13406 ACCESS DOOR OPTION ACCESS DOOR ADDED TO REAR FUSELAGE BOTTOM SKIN PANEL PER LIGHT SPORT VERSION OF ROTAX 912-ULS CHZL 601XL ZENAIR CH 601XL 13523 RELOCATE RIGHT HAND THROTTLE TO RIGHT HAND THROTTLE IN COCKPIT RELOCATED TO CENTRE OF INSTRUMENT PANEL. LEFT HAND ROTAX 912-ULS CHZL CENTRAL POSITION THROTTLE INSTALLED AS STANDARD. BALANCING SPRING FITTED. ZENAIR CH 601XL 13128 ADDITION OF ANTI OIL CANNING STRINGERS RIVETED TO WING SKINS TO REDUCE 'OIL CANNING' EFFECT: ONE STRINGER ON ROTAX 912-ULS CGVZ STRINGERS BOTTOM SKIN; TWO STRINGERS ON UPPER SKIN. ZENAIR CH 601XL 13485 THROTTLE LINKAGE RE-DESIGN THROTTLE LINKAGE ON ENGINE CHANGED TO INCLUDE TORQUE ROD LINKING BOTH ROTAX 912-ULS CGVZ CARBURETTOR THROTTLES, ALLOWING A MUCH WEAKER BIAS -OPEN SPRING ARRANGEMENT TO BE USED. ZENAIR CH 601XL 13744 WOODCOMP SR3000/3N 1720MM WOODCOMP SR3000/3N 1700 3 BLADED 1720MM DIAMETER VARIABLE PITCH PROPELLER ROTAX 912-ULS CGVZ DIAMETER VARIABLE PITCH PROPELLER INSTALLATION. INSTALLATION ZENAIR CH 701 STOL 14341 Category change from Group A to CATEGORY CHANGE TO MICROLIGHT BY REDUCING MAX GROSS WEIGHT TO 450 Kg. NON- ROTAX 912-UL BXIG Microlight AEROBATIC LIMITATIONS CHANGED ACCORDINGLY. NOISE CERTIFICATE OBTAINED. ZENAIR CH 701 STOL 14637 CATEGORY CHANGE TO GROUP A CATEGORY CHANGE TO GROUP A WITH 460 KG MAX GROSS WEIGHT ROTAX 912-UL CBZW ZENAIR CH 701SP 15111 WOODCOMP SR3000/3N 1720MM INSTALLATION OF WOODCOMP SR3000/3N 1720MM DIAMETER PROPELLER WITH PILOT ROTAX 912-UL CIXS DIAMETER PROPELLER INSTALLATION OPERATED SWITCHES FOR VARIABLE PITCH OPERATION. ZENAIR CH 701SP 14960 DOOR LATCH EACH DOOR MODIFIED BY THE ADDITION OF TWO LATCHES, INTERCONNECTED WITH STEEL RODS. ROTAX 912-ULS CHTH MECHANISM RETAINS THE ORIGINAL LATCH AND THE ABILITY TO BE OPENED FROM INSIDE AND OUTSIDE THE AIRCRAFT. ZENAIR CH 701UL 14071 INSTALL ROTEC E-IGNITION UPGRADE ROTEC E-IGNITION UNIT INSTALLED IN PLACE OF STARBOARD MAGNETO IN ACCORDANCE WITH JABIRU 2200A RAYH 'ROTEC AEROSPORT - JABIRU ELECTRIC UPGRADE KITS - INSTALLATION GUIDE 21/11/2014 REV 1.10'. AIRCRAFT ELECTRICAL SYSTEM AS PER FIGURE 5.1 OF THAT MANUAL. ZENAIR CH 701UL 13340 ENGINE & PROPELLER CHANGE STANDARD ROTAX 912-UL AND WOODCOMP KLASSIC 170/3/R PROPELLER SUBSTITUTED ROTAX 912-UL EOIN ZENAIR CH 701UL 14260 BUBBLE WINDOWED DOORS INSTALLATION OF ZENAIR BUBBLE WINDOWED DOORS WITH TUBULAR METAL FRAME. DOOR ROTAX 912-UL CDYU INSTALLATION WITH REVISED LATCHING LATCH MODIFIED TO INCORPORATE ADDITIONAL LATCH AT FORWARD FRAME. SYSTEM ZENAIR CH 750 15184 ZENAIR 7 SERIES WINDSHEILD FAIRING RUBBER SEALING STRIP AROUND BOTTOM EDGE OF WINDSCREEN REPALCED WITH MOULDED ROTAX 912-iS WXYZ FIBREGLASS STRIP MOULDED IN SITU TO PROVIDE IMPROVED MECHANICAL SUPPORT AND AIR SEAL TO PREVENT VIBRATION AND DRAFTS. ZENAIR CH 750 15185 HEADER TANK SYSTEM CUSTOM FUEL HEADER TANK LOCATED TO REAR OF SEATS ON PORT SIDE OF CABIN. ROTAX 912-iS WXYZ Prototype mods that have been approved since 1/1/2008 Page 150 30/11/20 LAA Technical Leaflet TL 3.17 ZENAIR CH 750 15186 PITOT SYSTEM PITOT TUBE ASSEMBLY ATTACHED TO WING UNDERSURFACE USING CUSTOM CLAMP, TUBE FED ROTAX 912-iS WXYZ VIA WING STRUT RATHER THAN THROUGH WING ZENAIR CH 750 15192 ALTERNATIVE COWL SOLUTION CUSTOM ENGINE COWL MANUFACTURED TO SUIT ROTAX 912IS ENGINE INSTALLATION ROTAX 912-iS WXYZ ZENAIR CH701 UL 14789 FLAP SELECT MECHANISM ZENAIR OPTIONAL FLAP GATE FITTED ROTAX 912-UL MULE ZENAIR CH701 UL 15422 GSC SYSTEMS TECH III 68 INCH DIAMETER INSTALLATION OF GSC TECH III 68 INCH DIAMETER GROUND ADJUSTABLE PROPELLER. ROTAX 912-UL MULE PROPELLER INSTALLATION

Prototype mods that have been approved since 1/1/2008 Page 151 30/11/20