type: thruster t600 (n) & (t) 390kg · 2016. 12. 12. · type: thruster t600 (n) & (t)...

CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP

MICROLIGHT TYPE APPROVAL DATA SHEET (TADS)

NO: BM 52 ISSUE: 7

TADS BM 52 Issue 7 of 11

TYPE: Thruster T600 (N) & (T) 390kg (1) MANUFACTURER Thruster Aircraft (UK)

Continued Support: Thruster Aircraft LLP North Hanger Wickenby Airfield Langworth, Lincs LN3 5AX

(2) UK IMPORTER: N/A

(3) CERTIFICATION:

BCAR Section S Issue 1 (4 April 1995) with Working Papers S861 and S901 for the T600 with Rotax 582. JAR 22 paras 1935 and 1939 have been employed to satisfy Section S Subpart J for the composit propeller.

(4) DEFINITION OF BASIC STANDARD:

Mod TAS 001 Issue 1 dated 18 April 1995 Master drawings list F10 (T600N) Issue 1 dated 2 Jan 1997 Master Drawings List F20 (T600T) Issue 1 dated 2 Jan 1997

(5) COMPLIANCE WITH THE MICROLIGHT DEFINITION

(a) MTOW 390 kg

(b) No. Seats 2

(c) Maximum Wing Loading 25 kg/m²

(d) Vso 32 kn CAS

(e) Permitted range of seat loading* 55-86 kg per seat

(f) T600N: Typical Empty Weight (ZFW) T600T: Typical Empty Weight (ZFW)

199 189

kg kg

(g) T600N: ZFW + 172 kg crew + 1 hr fuel (21 litres / 15 kg) T600T: ZFW + 172 kg crew + 1 hr fuel (21 litres / 15kg)

386

376

kg kg

(h)

T600N: MaxZFW + 86 kg pilot + full fuel T600T: MaxZFW + 86 kg pilot + full fuel

40lt Tank 318 318

25lt Tank 307 307

kg kg

(i) T600N Max ZFW at initial permit issue T600T Max ZFW at initial permit issue

203 203

kg kg

*Note: It is the Pilot’s responsibility to ensure the aircraft is flown within the MTOW



NO: BM 52 ISSUE: 7


(6) POWER PLANTS Designation T600N T600T T600T

Engine Type Rotax 503 DCDI-2V Rotax 503 DCDI-2V Rotax 582 2v

Reduction Gear B-Type 2.58:1 B-Type 2.58:1 B-Type 2.58:1

Exhaust System Rotax straight. After Muffler Optional

Rotax straight. After Muffler Optional

Rotax straight. After Muffler Optional

Intake System Air Filter Air Filter Air Filter

Propeller Type Brolga 2 Blade Brolga 3 Blade

Brolga 2 Blade Brolga 3 Blade

Brolga 3 Blade

Propeller Dia x Pitch 68" x 13 º 68" x 09 º

68" x 13 º 68" x 09 º

68" x 12 º

Noise Type Cert No. 44M Issue 11 44M Issue 11 44M Issue 15

AAN approving configuration 24970 24970 26145 (7) MANDATORY LIMITATIONS: (a) Max Take-Off Weight 390 kg

(b) CG Limits Aft Limit: FWD Limit:

482 mm Aft of datum 389 mm Aft of datum

(c) CG datum (see annex C)

(d) Cockpit Loadings

Min: Max:

Port 55 86

Starboard Either Seat 86

Total kg kg

(e) Never Exceed Speed 80 KIAS

(f) Manoeuvring Speed 60 KIAS

(g) Permitted Manoeuvres 30° Nose up / 30° nose down Non Aerobatic Normal acceleration limits, +4 / -2g

(h) Fuel Contents (Max Useable) 25lt or 38.7lt depending on tank fitted

(i) Power Plant (see table below)



NO: BM 52 ISSUE: 7


Engine T600N Rotax 503 DCDI-2V

T600T Rotax 503 DCDI-2V

T600T Rotax 582 DCDI-2V

Max RPM 6500 6500 6500

MAX CHT 250°C(480°F) 250°C(480°F) -na- water cooled

MAX EGT 650°C (1200°F)

650°C (1200°F)

650°C (1200°F)

Fuel Spec Mogas min RON 91 (mon83) leaded or non leaded or Argas fuel 100LL (blue) mixed 50:1 with 2 stroke oil

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- -na- 80°C

Oil Pressure -na- -na- -na-

Oil Temperature -na- -na- -na-

Fuel Pressure -na- -na- -na- (8) INSTRUMENTS REQUIRED:

ASI

Altimeter RPM CHT / EGT

Compass Coolant temp

Fuel Pressure

VSI Slip ball

Required 0 to 100 Kts min.)

Required Required Required Optional Water cooled engines

only

-na- Optional Optional

(9) CONTROL DEFLECTIONS: Elevator UP: 30°+/- 2° Tailplane trim UP: -na- Elevator DOWN: 30° +/- 2° Tailplane trim DOWN: -na- Ailerons UP: 40°+/- 2° Rudder LEFT: 25°+/- 2° Ailerons Down: 30°+/- 2° Rudder RIGHT: 25°+/- 2°



NO: BM 52 ISSUE: 7


(10) PILOT'S NOTES, MAINTENANCE MANUALS REFERENCES:

10.1 Manuals approved for use with this aircraft.

(a) Pilot Operating Handbook POH Part Number 210-055 POH Supplement Rotax 582 Pt No. 210-057 Change Sheet N0. 2 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.

(11) MANDATORY MODIFICATIONS / SERVICE BULLETINS / AIRWORTHINESS

DIRECTIVES ETC: See Annex A for required modifications. Also see Thruster website @ www.thruster.co.uk for

latest information.

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: Rotax 503 400 fpm at 50 KIAS Rotax 582 600 fpm at 50 KIAS

Stall or Minimum Flying Speed: 32 KIAS at MTOW / idle



NO: BM 52 ISSUE: 7


(13) APPROVED OPTIONAL MODIFICATIONS See Annex B. Also see Thruster website @ www.thruster.co.uk for latest information



NO: BM 52 ISSUE: 7


Issue History

Issue No. Reason and signatory 1 02/04/97 Initial Issue

A C LOVE 2 10/05/99 Propeller option added to modification TAS 009 (AAN 26863)

Rotax 582 engine option for T600T added to modification TAS 006 (AAN 26145) A J MAXWELL

3 06/07/99 Alternative material for wing and empennage skins - Modifications TAS 010 (AAN 26144) A J MAXWELL

4 07/09/99 Rotax 582 engine options for T600N with increased MTOW to 450 kg - Modification TAS 020 (AAN 27119) A J MAXWELL

5 23/05/03 BM52 Issue 5 removes reference to T600N (450 kg) Rotax are now being transferred to BM63 Issue 1. A J MAXWELL

6 06/11/07 Editorial Corrections A J MAXWELL

7 05/05/12 Editorial Corrections, Corrections to Cockpit Loading, Control Deflections, AAIB Safety action addition of “Area Of Special Attention” ANNEX E T LOVE



NO: BM 52 ISSUE: 7


Illustration of Aircraft - 3 View T600N

T600T



NO: BM 52 ISSUE: 7


Illustration of Aircraft - Photograph T600N

T600T



NO: BM 52 ISSUE: 7


ANNEX A – MANDATORY MODIFICATIONS

1. None

ANNEX B - APPROVED OPTIONAL MODIFICATIONS 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.

Thruster Mod Date Title TAL 03-3 12/02/1992 Rotax Exhaust After Muffler TAL 03-9 12/02/1992 GRP Wheel Spats TAS 010 10/07/1997 Ultralam Wing Skins

TAS 013 02/12/1997 Ivo Prop Installation

TAS 018 29/09/1997 Disabled Person Mod “Crip Kit”

TAS 026 01/03/2004 Lever for existing Bungee Trim System

TAS 030 01/03/2004 Carburettor Inlet Heater

TAS 031 01/03/2004 Wing Strobe Lights

TAS 033 01/03/2004 Roll Trim Bias

TAS 034 01/03/2004 Battery Isolator Switch

TAS 035 01/03/2004 Extended Control Colum Stick (Training Aid)

TAS 037 01/03/2004 Wider Nose Wheel



NO: BM 52 ISSUE: 7


ANNEX C WEIGHING INFORMATION

1. CG Datum: Aft of Wing Leading Edge Tube 2. Weighing attitude: Wings and Fusetube Level 3. Mainwheel moment arm: T600N: 767.5 mm AOD

T600T: 31.5mm AOD 4. Nosewheel moment arm:

Tailwheel moment arm: 750 (mm) (Forward) of datum 4075 (mm) (Aft) of datum

5. Fuel moment arm: 1030 (mm) (Aft) of datum 6. Crew moment arm: 423 (mm) (Aft) of datum (Front Seat position)

448 (mm) (Aft) of datum (Mid Seat Position) 473 (mm) (Aft) of datum (Rear Seat Position)

7. Crew weights: Minimum 55 kg / maximum 86 kg 8. Aft CG Limit: 482 (mm) (Aft) of datum 9. Fwd CG Limit: 389 (mm) (Aft) of datum

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: 199 kg * Max Take-Off Weight: 390 kg 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.



NO: BM 52 ISSUE: 7


(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

* dependant on Fuel Tank Fitted

(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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type: thruster t600 (n) & (t) 390kg · 2016. 12. 12. · type: thruster t600 (n) & (t)...

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