AAIB Bulletin 10/2014
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Alone Across the Atlantic
® 8 - DECEMBER 2013 www.kitplanes.com RV Atlantic Across in an in Swage Fittings Swage Secure? Cables Your Are the Adventure FT A Alone T REVIEW H ’S GUIDE SHOP R E H Easy Fiberglass Prep Aerodynamic Bookworm Tire Changing 101 T Soaring on Homemade Wings 2014 BUYER’S GUIDE2014 ISSUE! N • • • I HP-24 FLIG HP-24 BUYE Over 350 Planes Listed! Planes 350 Over 2014 KIT AIRCR KITPLANES DECEMBER 2013 Kit Buyer’s Guide • Transatlantic RV-8 • HP-24 Sailplane • Design to Fit • Swagelocks • Dawn Patrol • Testing to DO-160 • Home Shop Machines BELVOIR PUBLICATIONS Enjoy the Freedom of Homebuilt Aircraft Weather the Storm with SkyView’s IFR Capabilities Redundant flight instruments that automatically cross-check each other • ADS-B traffic and weather in-flight • SkyView network modules that detect wiring faults without losing capability • Li-Ion backup batteries that keep your SkyView system up when the power goes down • Autopilot with fully coupled ILS and GPS WAAS/LPV approaches. SkyView should already be your IFR platform of choice. But if that’s not enough, SkyView 7.0 introduces geo-referenced instrument approach charts, airport diagrams, and the best mapping software we’ve ever built. Go Fly! www.DynonAvionics.com 425-402-0433 [email protected] Seattle,Washington December 2013 | Volume 30, Number 12 Annual Buyer’s Guide, Part 1 26 2014 KIT AIRCRAFT BUYER’S GUIDE: The state of the kit world is sound. By Paul Dye and Mark Schrimmer. 38 KIT AIRCRAFT QUICK REFERENCE: A brief overview of available kit aircraft for 2014. Compiled by Richard VanderMeulen and Omar Filipovic. -
Civil Aviation Authority – Safety Regulation Group
CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO: BM3 ISSUE: 6 TYPE: Tri-Flyer Sprint (1) MANUFACTURER: Mainair Sports Ltd. Now supported by P & M Aviation Ltd. Unit B, Crawford Street Rochdale, Lancashire, OL16 5NU. (2) UK IMPORTER: N/A (3) CERTIFICATION: BCAR Section S, Advance Issue March 1983 (4) DEFINITION OF 440 Dual Master List of Drawings, Issue 2 BASIC STANDARD: (5) COMPLIANCE WITH THE MICROLIGHT DEFINITION (a) MTOW 338 kg (b) No. Seats 2 (c) Maximum Wing Loading 20.2 kg/m² (d) Vso 26 kts (30 mph) (e) Permitted range of pilot weights 55 – 90 kg per seat. (f) Typical Empty Weight (ZFW) 134 kg (g) ZFW + 172 kg crew + 1 hr fuel 326 kg (litres / kg) (h) ZFW + 86 kg pilot + full fuel 235kg ( litres / kg) (i) Max ZFW at initial permit issue 146 kg TADS BM3 Issue 6 Page 1 of 9 CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO: BM3 ISSUE: 6 (6) POWER PLANTS Tri-Flyer 440 Designation Engine Type Fuji Robin EC44PM Reduction Gear 2.67:1 Exhaust System Rota Flow Underslung Intake System Unique Foam Muffler Propeller Type Mainair Sports Round Tip Propeller Dia x Pitch 62” x 27½” Noise Type Cert No. M2 AAN approving 28478 configuration (7) MANDATORY LIMITATIONS: (A) Max Take-Off Weight 338 Kg (B) CG Limits N/A (C) CG datum N/A (D) Cockpit Loadings Front Rear Total Min 55kg 15 kg 70 kg Max 90kg 90 kg 180 kg (E) Never Exceed Speed 51 knots (59 mph) (F) Manoeuvring Speed 38 knots (44 mph) (G) Permitted Manoeuvres 30° Nose up / 30° nose down 60deg Max Bank Angle Non Aerobatic Normal acceleration limits, +4 / -0g (H) Fuel Contents (Max Useable) 22 litres TADS BM3 Issue 6 Page 2 of 9 CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO: BM3 ISSUE: 6 (I) Power Plant See Table Engine Fuji 440 Max RPM 6900 MAX CHT 218 degC MAX EGT 815 degC Fuel Spec 83 MON or 90 RON minimum unleaded to BS(EN)228 or 97+ octane 4-star /MOGAS leaded fuel to BS 4040, or AVGAS 100LL. -
QUANTUM 15 Operator‘S Manual - Issue 10
QUANTUM 15 Operator‘s Manual - Issue 10 SERIAL NO: P&M Aviation Ltd. Unit B Crawford Street Rochdale Lancashire OL16 5NU Tel: +44 (0)1706 655134 Fax: +44 (0)1706 631561 email: flying@ pmaviation.co.uk www.pmaviation.co.uk Pegasus Quantum Manual, Issue 10 Page 1 TABLE OF CONTENTS PAGE 1. Preparation for Safe Microlight/Ultralight Operation 8 1.1. Training 8 1.2. Pre-flight Planning 8 1.3. Modifications 10 1.4. Pre-flight Checks 10 1.5. Safety Harness 10 1.6. Ground Handling 10 1.7. Airstrip Criteria 11 1.8. Special Hazards 11 2. General Description 13 2.1. General Arrangement Drawing 13 2.2. Primary Structures and Systems - The Wing 14 2.3. Primary Structures and Systems - The Trike 15 2.4. Secondary Structures and Systems - Engine Controls 17 2.5. Secondary Structures and Systems - Braking System 18 2.6. Secondary Structures and Systems - Fuel System 18 2.7. Secondary Structures and Systems - Seat Belts 19 2.8. Secondary Structures and Systems - Cockpit and Fairing 19 2.9. Secondary Structures and Systems - Electrical System 19 2.10. Secondary Structures and Systems - Carburettor Heat 19 2.11. Secondary Structures and Systems - Radiator Covers 20 3. General Inform ation 22 3.1. Empty Weight 22 3.2. Fuel Loads 22 3.3. Centre of Gravity 23 3.4. Dimensions 23 3.5. Powerplant Specifications 23 3.6. Running Gear 23 3.7. Placards, Decals and Locations 24 3.8. Performance 24 3.9. Electrical System Specification 26 4. Operating Lim itations 28 4.1. General Limitations 28 4.2. -
CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO: BM54 ISSUE: 4 TADS BM54 Is
CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO: BM54 ISSUE: 4 TYPE: Mainair Rapier (1) MANUFACTURER: P & M Aviation Ltd, Unit B, Crawford Street Rochdale, Lancashire, OL16 5NU. (2) UK IMPORTER: N/A (3) CERTIFICATION: BCAR Section S Issue 1 (4) DEFINITION OF Betawing Drawing Register 27th April 1994 BASIC STANDARD: Gemini 2 Drawing Register Issue 3, 5th November 1996 (as amended) (5) COMPLIANCE WITH THE MICROLIGHT DEFINITION (a) MTOW 370 kg (b) No. Seats 2 (c) Maximum Wing Loading 23.72 kg/m² (d) Vso 30 mph (e) Permitted range of pilot weights 55 – 90 kg per seat. (f) Typical Empty Weight (ZFW) (Rapier 503) 152kg (Rapier 462) 152kg (g) ZFW + 172 kg crew + 1 hr fuel (503) 339kg (litres / kg) (426) 343 kg (h) ZFW + 86 kg pilot + full fuel (503) 270kg [285kg ( litres / kg) with mod 99] (462) 270kg [285kg with mod 99] (i) Max ZFW at initial permit issue (503) 183 Kg (462) 179 kg TADS BM54 Issue 4 Page 1 of 11 CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO: BM54 ISSUE: 4 (6) POWER PLANTS Rapier 503 Rapier 503 Rapier 503 Designation Engine Type Rotax 503-2V Rotax 503-2V Rotax 503-2V Upright Upright Upright Twin Electronic Twin Electronic Twin Electronic Ign. Ign. Ign. Reduction Gear 2.58:1 2.58:1 2.58:1 Exhaust System Rotax Side Rotax Side Rotax Side Mounted with After Mounted with After Mounted with After Muffler Muffler Muffler Intake System Intake Filter or Intake Filter or Intake Filter or Rotax Intake Rotax Intake Rotax Intake Silencer Silencer Silencer Propeller Type Mainair Mainair Grd Mainair WD Grd Adjustable Adj Propeller Dia x Pitch 62” x 40” 3 Blade 62” 3 Blade 62” 110deg at 12” 113deg at 12” Noise Type Cert No. -
Nigel Charles Looks at the Europa's Dramatically Changed, Graceful Performance with Motor-Glider Wings
FLIGHT TEST Europa XS Motorglider Nigel Charles looks at the Europa’s dramatically changed, graceful performance with motor-glider wings Photos Andrea Featherby Europa XS Motorglider t has been 18 years since I first saw the he recognised that the requirement for long, straightforward design idea for the main wheel, Europa prototype at the PFA Rally at tarmac runways (readily available in the USA) was but his idea to use the flaps to retract the Wroughton. I think I knew almost a handicap in Europe. The UK, for example, has outriggers (like the Harrier jump jet) was a stroke immediately that the Europa was going to be over 500 airfields with runways over 400m but of genius. From this concept the design of the Isomething special. Kit aircraft at that stage were in only about 125 of these offer hard surface monowheel Europa was born. their infancy and we were at a point where runways. He quickly came to the conclusion that The Rotax 912 four-stroke engine had been modern technologies such as composite materials there was demand for an aircraft that could handle available for a while and was proving to be a and lightweight engines were encouraging farm strips and at the same time cruise at a rugged and economical source of power. Ivan innovation. With the help of the LAA (PFA as it reasonable speed while avoiding consuming large based the design around this engine and, despite was known then) a number of kitplane volumes of avgas. attempts by some to use other powerplants, the manufacturers brought their ideas to the The problem was that tyres with a large Rotax stands out as the powerplant of choice marketplace. -
Europa Classic Trigear Conversion to an Experimental Amateur Built Light
Europa Classic Trigear Conversion to an Experimental Amateur Built Light Sport Aircraft (EABLSA) by use of Vortex Generators normally used for STOL Modifications Testing Dates 3 January 2010 thru 15 September 2010 Test Aircraft: N12AY Europa Classic Kit Power plant: Rotax 914 Propeller: Warp Drive three blade 64 inch wide chord This test was conducted to determine the feasibility of modifying a Europa Classic or XS kit aircraft to Light Sport Aircraft (LSA) standards. Experience has shown that the Europa kit aircraft is an efficient comfortable cruising aircraft with pleasing lines and superb flight characteristics. Many LSA aircraft are limited in cruise speed, strength, efficiency and comfort, which the Europa is not. The criteria for an aircraft to meet LSA, is in Ref 1 at the end of this document. Aerodynamically, the Europa wing is capable of generating a 1.7 Cl. Simple solution of the lift equation indicates the aircraft should stall at approximately 49 Knots for the XS and 53 for the Classic allowing for the slight differences in wing area. The LSA criteria set for the by the Federal Aviation Authority (FAA) calls for a controllable stall at 45 KIAS. My experience with adding vortex generators (VGs) to the Zenith and Piper Aircraft for STOL operations showed that a full length set of VGs, properly placed can lower the stall speed 5- 8 knots. The application of VGs should bring the stall speed of the Europa down to just meet the criteria listed in Ref 1. Since the maximum continuous power setting of the 914 is 73.5 KW or 95 HP the next problem is achieving a propeller setting that will absorb the power but limit the Europa to 120 Kts IAS cruise at sea level. -
Bmaa Technical Information Leaflet (Til) Til 069 Issue 2
BMAA TECHNICAL INFORMATION LEAFLET (TIL) TIL 069 ISSUE 2 SERIES MAJOR MODIFCATIONS 1. Introduction BMAA major modifications that have been both well defined by the original applicant and for which quality control procedures have been put in place are defined as ‘series’ modifications. Subsequent applicants apply for these in the same way as for ‘one-off’ BMAA modifications (using form BMAA/AW/002a), but do not need to provide a technical justification. Notes: o Series modifications must be identical to the first approval; if there is any change or non-compliance with respect to the original MAAN then a new approval is required. o Note that BMAA ‘series’ major modifications may not be applied for with a Permit revalidation application. This is because a Flight Release Certificate has to be issued and then signed by a BMAA Inspector. o BMAA 'series' major modifications are now charged at a reduced rate (compared to ‘one-off’ modifications). A list of existing BMAA 'series' modifications can be found below. 2. Existing BMAA Series Major Modifications The table below contains a list of issued BMAA ‘Series’ Major Modifications (up to January 2021 / MAAN 2864). The ‘Type(s)’ and ‘Brief description’ are indicative only; the BMAA Technical Office should be consulted prior to applying for the modification to confirm the details of the modification. MAAN Issue Type(s) Brief description 1001 1 Pathfinder Intro of 2.3:1 and 2.86:1 reduction drive ratios 1002 2 130SX/Halfpint E Rotax 337 and Newton 2-blade, 54" x 42.5" prop 1061 2 Hornet Duel Trainer Raven 45 litre plastic fuel tank 1066 1 Goldwing Intro Nicklow 2.86:1 reduction and Romain 2-blade 58" x 34" prop 1069 2 Goldwing Installation of Konig SC430 radial engine with Catto 56"X 28" prop 1076 1 Raven-X 3-blade Ivoprop, 62"x 9deg to Rotax 447. -
November 2014 23.60
THE MAGAZINE OF THE LIGHT AIRCRAFT ASSOCIATION www.laauk.com NOVEMBER 2014 23.60 • • • • •••• • • •• MA • • •• • • •• " • • • •• • Light Aircraft Association New catalogue now in production - call to reserve your copy today! LA 1::"•411,1 INSTRUMENTS & HARDWARE IOW jk Jaa IS SOS i"U 11FaltM° \Irri "Au iprown CIF c7la 4,fr s'`VALVES SEALANTS & BATTERIES COMPOUNDS *1-3Ea RAW MATERIALS LUBRICANTS PAINTS , DOPES & FABRICS -4i 4`• ' s WINDOWS & TOOLSQ3/41"1"'s411.111411'1, WINDSHIELDS LIGHTS, LAMPS & FILAMENTS INHCF I C pcRRAKFC CONTROL CABLES TYRES ALLtSSLIKIt 41k HOSE & BOOKS .„,--3\ firDUCTING \Pi 414; cel` 117 FILTERS root. a - I a EDITOR'S DESK azahlos Aid Acieg zed ••• •- msYOURASSOCIATION Tell us how you think the AGM should be run — your input really is valued sympathy for those who have forked opt sometimes quite considerable (1 November) and I hope we will have had a reasonable sums ot money fo ensure teat have the right lief/foe. raring or business B attendance.y the time you It read has thisnever we been will have much had of aour 'must AGM do at event Sywell for the arrangement (for schools and instructors/ only to find that the outlay majority of members but it is important because it reiterates that this is wasn't absotutely necessary . an association. our association, and we do have a say in how it is run. Tge feature article this month is Roy Taylor's lovely Bowers Fly Baby. I can say already that there will have been more members' input this an early plans built 'vintage type that unfortunately wasn't popular here year because the response to the drive to get the proxy voting system in the UK but was widely embraced in its native US Roy had previously better understood and used has resulted in around 60 responses as of a built, and still Hes. -
NO:BM 5 ISSUE: 6 TADS BM5 Is
CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO:BM 5 ISSUE: 6 TYPE: Panther XL-S (1) MANUFACTURER: Solar Wings Ltd, Now supported by P & M Aviation Ltd, Unit B, Crawford St, Rochdale, Lancashire OL16 5NU (2) UK IMPORTER: N/A (3) CERTIFICATION: BCAR SECTION S - Advance Issue March 1983 List of Section S Blue Papers and Additional CAA Requirements: N/A. (4) DEFINITION OF Panther XL-S Drawing Schedule issue 1 BASIC STANDARD: Dated: 16.4.85 (5) COMPLIANCE WITH THE MICROLIGHT DEFINITION (a) MTOW 350 kg (b) No. Seats 2 (c) Maximum Wing Loading 20 kg/sq m (d) Vso 31mph CAS (e) Permitted range of pilot weights 55 – 95 kg per seat. (f) Typical Empty Weight (ZFW) 155 kg (g) ZFW + 172 kg crew + 1 hr fuel 339 kg (17litres /12 kg) (h) ZFW + 86 kg pilot + full fuel 257 kg ( 22.5 litres / 16kg) (i) Max ZFW at initial permit issue 159kg TADS BM5 issue 6 Page 1 of 11 CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO:BM 5 ISSUE: 6 (6) POWER PLANTS Panther XL-S Panther XL-S Designation Engine Type Fuji Robin EC44PM Inverted Fuji Robin EC44-2PM Inverted Reduction Gear 2.63:1 2.63:1 Exhaust System Nicklow Nicklow Intake System Filters only Filters only Propeller Type Newton Newton Propeller Dia x 60" x 32" 60" x 32" Pitch Noise Type 7M 7M Cert No. AAN approving 18479P 18479P configuration (7) MANDATORY LIMITATIONS: (A) Max Take-Off Weight 350kg (B) CG Limits N/A (C) CG datum N/A (D) Cockpit Loadings Front Rear Total Min 55Kg - 55kg Max 95kg 95kg 190kg (E) Never -
Ref SB144 Split Rings
ref SB144 Splliit Riings SERVICE BULLETIN NUMBER 144, issue 2. TITLE Split Rings CLASSIFICATION P&M Aviation have classified this service bulletin essential. COMPLIANCE Inspection before further flight. APPLICABILITY All Pegasus, Mainair and P&M types including BM2 Gemini Sprint BM3 Tri-Flyer Sprint BM4 Gemini Flash BM5 Panther XL-S BM9 Pegasus XL-R BM10 Pegasus Flash BM17 Pegasus Flash 2 BM14 Gemini Flash 2 BM16 Scorcher BM17 Pegasus Flash 2 BM23 Gemini Flash 2 Alpha BM25 Pegasus XL-Q BM27 Chaser S BM28 Pegasus Photon BM31 Chaser S 1000 BM33 Chaser S 508 BM37 Chaser S 447 BM38 Pegasus Quasar BM42 Pegasus Quasar - TC BM43 Mainair Mercury BM44 Pegasus Quasar 2 TC BM45 Cyclone AX3/503 BM46 Pegasus Quantum 15 (Rotax 2-stroke engines) BM47 Mainair Blade BM50 Pegasus Quantum 15-912 BM51 Mainair Blade 912 BM53 Cyclone AX2000 BM54 Mainair Rapier BM56 Pegasus Quantum 15-HKS BM60 Mainair Blade 912S BM65 Flight Design CT2K ( rudder control ) BM66 Pegasus Quik BM70 Quik GT450 BM72 Flight Design CTSW (rudder control) BM77 QuikR BM80 Quik GTR BM81 PulsR BM83 Flight Design CTSL (Rudder control) 1) INTRODUCTION Following maintenance, a clevis pin came out of the RP-4 roll trim system pulley on a QuikR causing a left turn. The split ring securing the clevis pin had come out. It is not known if the ring was disturbed during the maintenance. 1 ref SB144 Splliit Riings The split ring which came out was the same “spiral start” pattern as that which has caused trouble before (see Service Bulletin 139). This pattern of ring has no positive stop, so that simple rotation of the ring (e.g. -
Microlight Accident and Incident Summary 0 /201
Microlight Accident and Incident Summary 03/2011 This accident report summary is collated by the BMAA from information gathered. The information sources used are the Air Accident Investigation Branch of the Department for Transport (AAIB), the Civil Aviation Authority Mandatory Occurrence Reports (CAA MOR) and reports made directly to the BMAA by members and operators. The individual reports within the accident summary are taken from the information available to the BMAA and where the BMAA has made comment this is clearly shown. The BMAA does not investigate accidents and incidents, this role being the responsibility of the AAIB and the CAA who have the expertise, experience and funding for investigation. All pilots reading the reports should try to make their own assessment of underlying causes and use the experience of others to enhance their own knowledge to help them become safer pilots. AAIB Bulletin: 1/2011 EW/G2010/09/22 ACCIDENT Aircraft Type and Registration: Ikarus C42 FB80 No & Type of Engines: 1 Rotax 912-UL piston engine Year of Manufacture: 2005 Date & Time (UTC): 21 September 2010 at 1400 hrs Location: Type of Flight: Training Persons on Board: Crew - 1 Passengers - None Injuries: Crew - None Passengers - N/A Nature of Damage: Significant damage to forward fuselage and right wing Commander’s Licence: Student pilot Commander’s Age: 53 years Commander’s Flying Experience: 40 hours (of which 40 were on type) Last 90 days - 6 hours Last 28 days - 6 hours Information Source: Aircraft Accident Report Form submitted by the pilot The student pilot was undertaking a solo flight from edge marker and applied full power. -
Contents Contents
AAIB Bulletin: 1/2013 CONTENTS SPECIAL BULLETINS / INTERIM REPORTS S7/2012 EC225 LP Super Puma G-CHCN 22-Oct-12 3 SUMMARIES OF AIRCRAFT ACCIDENT (‘FORMAL’) REPORTS None AAIB FIELD INVESTIGATIONS COMMERCIAL AIR TRANSPORT FIXED WING Airbus A300B4-622R(F) D-AEAP 14-Apr-12 13 Airbus A319-111 G-EZFV 14-Feb-12 19 ROTORCRAFT None GENERAL AVIATION FIXED WING None ROTORCRAFT Agusta Bell 206B Jet Ranger II G-SUEZ 20-Feb-12 27 SPORT AVIATION / BALLOONS Pegasus Quik G-CWIK 12-May-12 31 AAIB CORRESPONDENCE INVESTIGATIONS COMMERCIAL AIR TRANSPORT DH89A Rapide Dragon G-AIYR 08-Sep-12 41 Piper PA-23-250 Aztec G-BKJW 28-Sep-12 42 GENERAL AVIATION Aero AT-3 R100 G-SACY 05-Sep-12 43 Beech A23 Musketeer II G-ATBI 05-Sep-12 44 Beechcraft 33 Debonair N35SN 22-Sep-12 45 Cessna 152 G-BSZI 22-Sep-12 46 Cessna FR172J Reims Rocket G-BDOE 20-Aug-12 49 Corben Junior Ace G-BSDI 09-Sep-12 50 Europa G-OJHL 24-Jun-12 51 Jodel D117 G-AWWI 14-Oct-12 52 Navion NAV 4 F-BAVZ 01-Jul-12 53 © Crown copyright 2013 i AAIB Bulletin: 1/2013 AAIB CORRESPONDENCE INVESTIGATIONS - Cont GENERAL AVIATION - Cont Pioneer 300 G-CDPA 21-Jul-12 54 Piper PA-28-151 Cherokee Warrior G-BOTF 09-Sep-12 55 Piper PA-28-151 Cherokee Warrior G-BTNT 09-Sep-12 57 Piper PA-28-161 Cherokee Warrior II G-BURT 27-Aug-12 58 Piper PA-38-112 Tomahawk G-BJUR 06-Oct-12 60 Rans S6-116 Coyote II G-BUWK 10-Oct-12 61 Silence Twister G-TWIS 25-Jul-12 63 Slingsby T67M260 Firefly G-BWXD 17-Oct-12 64 Vans RV-8A G-RVCH 08-Sep-12 65 SPORT AVIATION / BALLOONS Mainair Blade G-MYYG 07-Sep-12 66 Pegasus Quantum 15-912 G-MDBC