CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP
MICROLIGHT TYPE APPROVAL DATA SHEET (TADS)
NO: BM 34 ISSUE: 9
TYPE: Thruster T300
(1) MANUFACTURER Tempest Aviation (UK) Continued Support: Thruster Aircraft LLP North Hanger Wickenby Airfield Langworth, Lincolnshire LN3 5AX (2) UK IMPORTER: N/A
(3) CERTIFICATION: BCAR Section S Advance Issue March1983 plus paper D37/112/1 dated 11th October, 1988
(4) DEFINITION OF BASIC Thruster T300 Mk 1 Master G/A Drawing 05-005 STANDARD: 1.2,Issue 1 dated 6.9.1988 and Drawings list Form F33A latest issue 26.2.1991
(5) COMPLIANCE WITH THE MICROLIGHT DEFINITION
40l Basic 40l Basic 25l Basic 25l Basic Aerofoil Aerofoil Aerofoil Strut Strut Strut Wide Ailerons (a) MTOW 361 380 380 390 (b) No. Seats 2 2 2 2 (c) Maximum Wing Loading 25 25 25 25 kg/m² (d) Vso 32 32 32 32 kn CAS (e) Permitted range of seat loading* 55-86 55-86 55-86 55-86 kg per seat (f) Typical Empty Weight (ZFW) 174 182 190 200 kg (g) Max ZFW + 172 kg crew + 1 hr fuel 361 369 370 370 (18litres / 13kg) (h) Max ZFW + 86 kg pilot + full fuel 288 308 297 307 (18litres /13 kg) (i) Max ZFW at initial permit issue 176 195 195 203 * Note It is the Pilot’s responsibility that the aircraft is not flown outside the permitted MTOW
TADS BM 34 Issue 9 Page 1 of 11 CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP
MICROLIGHT TYPE APPROVAL DATA SHEET (TADS)
NO: BM 34 ISSUE: 9
(6) POWER PLANTS
T300 MK T300 MK T300 MK T300 MK T300 MK T300 MK T300 MK T300 MK Designatio 1 1 1 1 1 1 1 1 n Rotax 503 Rotax 532 Rotax 582 Rotax 503 Rotax 503 Rotax 532 Rotax 582 Rotax 503 Engine 2v FA SS 2v 2v 2v FA SS 2v DCDI 2v 2v DCDI 2v FA SS Type or DCDI- or DCDI- 2V 2V Reduction B-Type B-Type B-Type B-Type B-Type B-Type B-Type B-Type Gear 2.58:1 2.58:1 2.58:1 2.58:1 2.58:1 2.58:1 2.58:1 2.58:1 Exhaust Rotax Rotax Rotax Rotax Rotax Rotax Rotax Rotax System straight. straight. straight. straight. straight. straight. straight. straight. No After No After After After After After After After Muffler Muffler Muffler Muffler Muffler Muffler Muffler Muffler Optional Optional Optional Optional Optional Optional Intake Air Filter Air Filter Air Filter Air Filter Air Filter Air Filter Air Filter Air Filter System Propeller Catto 2 Catto 2 Catto 2 Brolga 3 Brolga 3 Brolga 3 Brolga 3 Brolga 2 Type Blade Blade Blade Blade Blade Blade Blade Blade Catto or Catto or Catto or GSC 3 GSC 3 GSC 3 Blade Blade Blade Propeller 64" x 37" 64" x 42" 64" x 42" 68" x 09 º 60" x 16 º 68" x 12 º 68" x 12 º 68" x 13 º Dia x Pitch 64" x 30" 64" x 36" 64" x 36" Noise 44M 44M 44M 44M 44M 44M 44M 44M Type Cert No. AAN 21883 21883 21883 21883 21883 21883 21883 21883 approving 21885 21885 25244 25244 21885 23586 25244 configurati on 23586 23586 23586 25244 25244 26863
TADS BM 34 Issue 9 Page 2 of 11 CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP
MICROLIGHT TYPE APPROVAL DATA SHEET (TADS)
NO: BM 34 ISSUE: 9
(7) MANDATORY LIMITATIONS:
Airfoil + Wide Basic + Airfoil Ailerons (A) Max Take-Off Weight 361 380 390 Kg (B) CG Limits Aft Limit: 500 mm Aft of datum FWD Limit: 390mm Aft of datum (C) CG datum Front of wing leading edge tube (see annex C). (D) Cockpit Loadings Port Starboard Total Min 55 - 0 kg Max 90 - 90 kg (E) Never Exceed Speed 80 KIAS (F) Manoeuvring Speed 70 KIAS (G) Permitted Manoeuvres 30° Nose up / 30° nose down Non Aerobatic Normal acceleration limits, +4 / -2g (H) Fuel Contents (Max Useable) 25 lt or 39.8lt Depending on tank fitted (I) Power Plant See Table
Engine Rotax 503 2v Rotax 532 2v Rotax 582 2v DCDI FA SS and DCDI-2V Max RPM 6800/6500* 6800/6500* 6800/6500* MAX CHT 250°C(480°F) -na- -na- MAX EGT 650°C (1200°F) 650°C (1200°F) 650°C (1200°F) 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. Engine Oil Spec Two stroke Two stroke Two stroke Gearbox oil spec SAE 140-API-GL5 SAE 140-API-GL5 SAE 140-API-GL5 Fuel/Oil Mix 50:1 50:1 50:1 Coolant Temperature -na- 80°C(175°F) 80°C(175°F) Oil Pressure -na- -na- -na- Oil Temperature -na- -na- -na- Fuel Pressure -na- -na- -na- * Brolga Propeller Limitation
TADS BM 34 Issue 9 Page 3 of 11 CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP
MICROLIGHT TYPE APPROVAL DATA SHEET (TADS)
NO: BM 34 ISSUE: 9
(8) INSTRUMENTS REQUIRED:
ASI Altimeter RPM CHT / Compass Coolant Fuel VSI Slip ball EGT temp Pressure Required Required Required Required Optional Water -na- Optional Optional 0 to 100 cooled kts only
(9) CONTROL DEFLECTIONS: (3- AXIS SYSTEMS )
Elevator UP: 30°+/- 2° Tailplane trim UP: -na- Elevator DOWN: 30°+/- 2° Tailplane trim DOWN -na- Ailerons UP: 40°+/- 2° Rudder LEFT: 25°+/- 2° AileronsDOWN: 30°+/- 2° Rudder RIGHT: 25°+/- 2°
(10) PILOT'S NOTES, MAINTENANCE MANUALS REFERENCES:
10.1 Manuals approved for use with this aircraft.
Thruster T300 Pilots and Operators Handbook Part No. 210-051 (a) * Change Sheet 2 is required with Brolga propellers. (b) * Change Sheet 4 is required for Ultralam Coverings
10.2 The following placards are to be fitted:-
(a) Flight Limitations Placard (to be visible to pilot) See Annex D.
(b) Engine Limitations Placard (to be located near to engine instruments) See Annex D.
(c) Fuel Limitations Placard (to be located near to filler cap)
A placard is to be fitted showing fuel capacity ( litres), fuel type(s), fuel:oil ratio (if relevant) and if MTOW can be exceeded with full fuel and maximum cockpit weight, the fuel loads at MTOW for cockpit weights of 180kg / 170kg / 160kg etc. at 10kg intervals down to the maximum fuel load. An example is shown at Annex D.
(d) Switches See Annex D.
TADS BM 34 Issue 9 Page 4 of 11 CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP
MICROLIGHT TYPE APPROVAL DATA SHEET (TADS)
NO: BM 34 ISSUE: 9
(11) MANDATORY MODIFICATIONS / SERVICE BULLETINS / AIRWORTHINESS DIRECTIVES ETC:
See Annex A for required modifications.
Annual Bettsometer test is to be carried out to 1320 grammes with wing sails fitted and tensioned to flight. Test must be to both upper and lower surfaces.
(12) MINIMUM PERFORMANCE AT MAX TAKE-OFF WEIGHT
Rate of Climb: 450 fpm at 45 KIAS on Rotax 503. 600 fpm at 45 KIAS on Rotax 532. 600 fpm at 45 KIAS on Rotax 582.
Stall or Minimum Flying Speed: 32 KIAS at MTOW / idle.
TADS BM 34 Issue 9 Page 5 of 11 CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP
MICROLIGHT TYPE APPROVAL DATA SHEET (TADS)
NO: BM 34 ISSUE: 9
Issue History
Issue No. Reason and signatory 1 22/08/03 Initial Issue F J TUCKER 2 28/11/90 F J TUCKER 3 22/08/95 Alternative engine added. Alternative propeller added. Service Bulletin TAS/SB02 for return to compliance with BCAR Section S added, together with alternative fuel tanks, modified area accounting with wing aerofoil lift struts, and wide chord ailerons together with permission to use 86 kg per occupant allowed increase in MTWA. A C LOVE 4 13/06/97 Propeller options (with 6500 rpm limit) added to Modification TAS 004 (AAN 25244). A C LOVE 5 10/05/99 Propeller option added to modification TAS 009 (AAN 26863). A J MAXWELL 6 15/06/99 Alternative material for wing and empennage skins - modification TAS 010 (AAN 26144) A J MAXWELL 7 03/09/03 Revised to new format A J MAXWELL 8 06/11/07 Editorial Corrections A J MAXWELL 9 05/05/12 Editorial Corrections, Corrections to Cockpit Loading, Control Deflections, AAIB Safety action addition of “Area Of Special Attention” ANNEX E
T LOVE
TADS BM 34 Issue 9 Page 6 of 11 CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP
MICROLIGHT TYPE APPROVAL DATA SHEET (TADS)
NO: BM 34 ISSUE: 9
Illustration of Aircraft - 3 View
Illustration of Aircraft - Photograph
Picture to follow
TADS BM 34 Issue 9 Page 7 of 11 CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP
MICROLIGHT TYPE APPROVAL DATA SHEET (TADS)
NO: BM 34 ISSUE: 9
ANNEX A – MANDATORY MODIFICATIONS
1. TAS/SB02 Issue 1 Return to compliance with BCAR Section S Note: A definitive list of Mandatory actions is to be obtained by reference to CAA published Mandatory Permit Directories. The list on this TADS is not necessarily up-to-date. Also see Thruster website @ www.thruster.co.uk for latest information
ANNEX B - APPROVED OPTIONAL MODIFICATIONS
Below is a list of minor modifications approved by Thruster Air Services. The installation of all optional modifications is to be inspected by a BMAA inspector and an entry made in the appropriate logbook(s). Note that other approved modifications may exist which are not listed here. Also see Thruster website @ www.thruster.co.uk for latest information.
Thruster Mod Date Title TUKM-001 Rear fuselage boom brace tubes TUKM-002 Revised Rudder Pedal assy TUKM-003 Introduces steel tube tail plane assy TUKM-004 Ground Adjustable seat TUKM-005 Angles rear “A” Frame TUKM-006 Change to Control Stick Ali to Steel TUKM-007 Details of Aileron root and tip fittings TUKM-008 Details changes to wing Jury struts TUKM-009 Detail changes to Throttle lever system TUKM-10 Introduction of Ali instrument Panel TUKM-011 Introduce extra stiffening sleeve Wing Bay TUKM-012 Introduce Separate exhaust mounting Brkt TUKM-21-032 Mod to main axle and spring TUKM-21-033 Detail change to rear jury strut TUKM-21-034 Revised Tailwheel steering TUKM-21-035 re-Rout Ruder Cables TUKM-21-036 Improve Throttle Torque Tube TUKM-21-037 Changes to main “A”frame/Fuse Brkt TUKM-21-038 Introduce Ali fuel Tank TUKM-21-041 Overhead Instrument Panel TUKM-21-044 Subframe and seat rail changes TUKM-21-045 Elevator Crank Improvement TUKM-22 Electric Start Facility
TADS BM 34 Issue 9 Page 8 of 11 CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP
MICROLIGHT TYPE APPROVAL DATA SHEET (TADS)
NO: BM 34 ISSUE: 9
Thruster Mod Date Title 91/01 17/07/1991 Aluminium Fuel Tank 91-02 Cockpit Pod new style 91-03 Cockpit Sub assy 91-04 Aileron Torque Tube TAL-01 Catto 3 blade Propeller TAL 03-3 12/02/1992 Rotax Exhaust After Muffler TAL 03-9 12/02/1992 GRP Wheel Spats TAL 03-20 12/02/1992 GRP Wing Tip Cap TAS 010 10/07/1997 Ultralam Wing Skins TAS 013 02/12/1997 Ivo Prop Installation TAS 015 29/09/1997 Disabled Person Mod “Crip Kit” TAS 017 10/09/1998 Fitting Back and Doors TST TAS 030 01/03/2004 Carburettor Inlet Heater TAS 031 01/03/2004 Wing Strobe Lights TAS 034 01/03/2004 Battery Isolator Switch TAS 037 01/03/2004 Wider Nose Wheel
ANNEX C WEIGHING INFORMATION
1. CG Datum: Front of Wing Leading Edge Tube 2. Weighing attitude: Wings and Fusetube Level 3. Mainwheel moment arm: 31.5mm Aft of Datum 4. Tailwheel moment arm: 4075 (mm) (Aft) of datum 5. Fuel moment arm: 1030 (mm) (Aft) of datum 6. Crew moment arm: 410 (mm) (Aft) of datum (Front Seat position) 448 (mm) (Aft) of datum (Mid Seat Position) 486 (mm) (Aft) of datum (Rear Seat Position) 7. Crew weights: Minimum 55 kg / maximum 86 kg (maximum reducible, not below 86 kg, if required) 8. Aft CG Limit: 500 (mm) (Aft) of datum 9. Fwd CG Limit: 390 (mm) (Aft) of datum
TADS BM 34 Issue 9 Page 9 of 11 CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP
MICROLIGHT TYPE APPROVAL DATA SHEET (TADS)
NO: BM 34 ISSUE: 9
ANNEX D EXAMPLE PLACARDS
(a) Flight Limitations Placard (to be visible to pilot)
[Type] [Engine] [Registration] Never Exceed Speed: 80 KIAS Manoeuvring Speed : 70 KIAS Stall Speed: 32 KIAS Best climb speed: 50 KIAS Best glide speed: 45 KIAS Pitch Limits: 30° nose down, 30° nose up. Bank angle limits: +/- 60° Maximum Stall entry rate: 1 kn/s Normal Acceleration Limits: +4 / -2g Empty Weight: 164 kg * Max Take-Off Weight: 361, 380 or 390kg Minimum Cockpit Weight: 55 kg Maximum Cockpit Weight: 86 kg in each seat.* Aerobatics and deliberate spinning prohibited. * This must match the most recent W&CG report for the aircraft.
(b) Engine Limitations Placard (to be located near to engine instruments))
A placard showing the limitations for all indicated engine parameters is to be mounted close to the engine instruments. This requirement need not be complied with for limitations shown as coloured markers (red for danger, amber for caution) on the instrument displays.
(c) Fuel Limitations Placard (to be located near to filler cap)
FUEL Capacity * Litres 50:1 2 Stroke oil Cockpit Weight (kg) Max. Fuel Load (litres) 180 170 …. …. Or below Full fuel 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
* Depending on Fuel Tank Fitted
TADS BM 34 Issue 9 Page 10 of 11 CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP
MICROLIGHT TYPE APPROVAL DATA SHEET (TADS)
NO: BM 34 ISSUE: 9
(d) Switches
All switches are to be marked with function and sense (up=on, down=off).
ANNEX E
Areas for Special Attention During Inspections
1. Carburettor Heating System to minimise risk of Carburettor Icing. An accident caused by Carburettor Icing has been reported which was due in part to the Electric Carburettor Heating system being fitted on the inlet of the Carburettor rather than the outlet in the vicinity of the butterfly valve. Check that the installation is correct and operational.
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