TYPE APPROVAL DATA SHEET

(a) C42C Owner’s Manual OHB/C42/002 Issue 2, or later approved version (b) Maintain to Pilot Operators Handbook. (c) Engine, propeller, parachute system and other fitted equipment manufacturer’s Operating and Maintenance Manuals as appropriate to fitted powerplant and equipment, at their current issues. BRITISH MICROLIGHT AIRCRAFT ASSOCIATION (BMAA) MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO: BM-92 ISSUE: 2 Issued on behalf of the UK CAA by the BMAA, UK CAA organisation approval ref. DAI/8909/84 TADS BM92 Issue 2 Page 6 of 11 10.2 The following placards are to be fitted: (a) Flight Limitations Placard (to be visible to the pilot) Contains airspeed, manoeuvring and loading limitations. See Pilot Operators Handbook. (b) Engine Limitations Placard (to be located near to the engine instruments) A placard showing the limitations for all indicated engine parameters is to be mounted close to the engine instruments. Also, main limitations are to be shown as coloured markers (red for danger, amber for caution) on the instrument displays. See Pilot Operators Handbook. (c) Occupant Warning Placard (to be visible to both occupants) See Pilot Operators Handbook. (d) Fuel Filler Placard (to be located adjacent to the fuel filler cap) A placard is to be fitted showing fuel capacity, fuel type(s), and if MTOW can be exceeded with full fuel and 180kg cockpit weight, the fuel loads at MTOW for cockpit weights of 180kg / 170kg / 160kg etc. at 10kg intervals down to the maximum fuel load. See Pilot Operators Handbook. (e) Parachute Warning Placards (to be located on the exterior of the aircraft) If an Airframe Mounted Total Recovery Parachute System (AMTPRS) is fitted, placards complying with BCAR Section S Issue 7 must be fitted. See Pilot Operators Handbook. (f) Secondary Control Markings Choke, cabin heat, trim, flaps, fuel shut-off: see Pilot Operators Handbook. Other secondary controls are to be placarded as per the associated Pilot Operators Handbook supplement or normal aviation practice (if no associated Pilot Operators Handbook supplement). (g) ASI Markings See Pilot Operators Handbook. (h) Switches All switches are to be marked with function and sense (up=on, down=off). (i) Fuses and Circuit Breakers All fuses and circuit breakers are to be marked with function and rating. (j) Fireproof Metal Plate Showing the aircraft nationality and registration marks (e.g. G-ABCD) to be mounted in a prominent position on the fuselage. BRITISH MICROLIGHT AIRCRAFT ASSOCIATION (BMAA) MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO: BM-92 ISSUE: 2 Issued on behalf of the UK CAA by the BMAA, UK CAA organisation approval ref. DAI/8909/84 TADS BM92 Issue 2 Page 7 of 11 (11) MANDATORY MODIFICATIONS / SERVICE BULLETINS / AIRWORTHINESS DIRECTIVES ETC: See Annex A for required modifications. Annual Bettsometer Test Stitching only: 1000 grammes using a 1.2mm diameter hook, pull at 90degs to surface of tensioned sail. (12) MINIMUM PERFORMANCE AT MAX TAKE-OFF WEIGHT (450 kg – ISA – Sea Level) Rate of Climb: C42 FB80 C42 FB100 700 fpm at 69 mph (60 kt) IAS. 1000 fpm at 69 mph (60 kt) IAS. Stall or Minimum Flying Speed: 36 mph (31 kt) IAS at MTOW / idle / full flap. Sink rate 700 fpm TODR (on short dry grass) 205m (includes 1.3 safety factor) LDR (on short dry grass) 205m (no safety factor) Issue History Issue Reason and Signatory 1 18/12/2020 Initial issue. Approved for issue by R. Pattrick BMAA Chief Technical Officer 2 29/11/2021 Modification TMC42-15 Operation at 472.5kg without BPRS added. POH / MM Issue 2 added. SBs added. Approved for issue by R. Pattrick BMAA Chief Technical Officer Issued on behalf of the UK CAA by the BMAA, UK CAA organisation approval ref. DAI/8909/84 BRITISH MICROLIGHT AIRCRAFT ASSOCIATION (BMAA) MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO: BM-92 ISSUE: 2 Issued on behalf of the UK CAA by the BMAA, UK CAA organisation approval ref. DAI/8909/84 TADS BM92 Issue 2 Page 8 of 11 Illustration of Aircraft - 3 View BRITISH MICROLIGHT AIRCRAFT ASSOCIATION (BMAA) MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO: BM-92 ISSUE: 2 Issued on behalf of the UK CAA by the BMAA, UK CAA organisation approval ref. DAI/8909/84 TADS BM92 Issue 2 Page 9 of 11 ANNEX A – MANDATORY MODIFICATIONS / SERVICE BULLETINS CAA Mandatory Permit Directives (AIRFRAME ONLY) 2004-005 R1 Elevator Horn Cracking 2004-013 Stub Axle Shock Absorber Attachment Cracking 2007-007 Fouling of Rear Fuselage Composite Fairing on Rudder Horn Bolts 2007-008 Cracking in Weld on Wing Root Rib 2016-004-E Inspection of Main Fuselage Tube for Cracking 2016-006-E Inspection of Neuform Prop Hub for Cracking 2019-005 3 Placarding Requirements for Aircraft fitted with a BPRS 4 (for more info see TIL063) Manufacturer Essential Service Bulletins Flybuy Ultralights OSB 16 Elevator Horn Cracking Flybuy Ultralights OSB 18 Stub Axle Cracking Aerosport Ltd OSB 24 Rudder Horn Bolt Clearance Aerosport Ltd OSB 25 Wing Root Rib Weld Cracking Red Aviation OSB 29 Main Fuselage Tube Cracking Red Aviation OSB 30 Neuform Prop Hub Cracking Red Aviation OSB 31 Inspection of inside of A-strut for cracking TLAC OSB 32 Inspection of nosewheel steering pushrods TLAC OSB 33 Inspection of control surface hinge and horn attachments for corrosion or cracking Latest Bulletins - https://www.g-tlac.com/login/ (User Name: G-WOLV Password: BMAA) ANNEX B - APPROVED OPTIONAL MODIFICATIONS The installation of all optional modifications is to be inspected by an inspector from an Organisation approved by the CAA for the purpose and an entry made in the appropriate logbook(s). Note that other approved modifications may exist which are not listed here. Flybuy/Aerosport Optional Modifications 1. Landing Light 42UKA11.10.00 2. Strobe 42D03.05.00 3. Falcon Artificial Horizon C42/003 4. Samsonite Luggage Case C42/004 5. Additional 50 Litre Fuel Tank C42/005 3 with approved Airframe Mounted Total Recovery Parachute System (AMTPRS) BRITISH MICROLIGHT AIRCRAFT ASSOCIATION (BMAA) MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO: BM-92 ISSUE: 2 Issued on behalf of the UK CAA by the BMAA, UK CAA organisation approval ref. DAI/8909/84 TADS BM92 Issue 2 Page 10 of 11 6. Vertical Card Compass C42/012 7. Flying Without Doors C42/019 Performance Aviation Optional Modifications 8. BRS Reserve Parachute C42PAUK/003 9. Beringer Brakes C42PAUK/004 Red-Air / Red Aviation Optional Modifications 10. FUNKE ATR833 Radio C42RAUK/02 11. FUNKE TRT800H Transponder C42RAUK/03 12. Sailplane Tow Kit C42RAUK/12 13. Electric Flaps C42RAUK/19 14. Dual 65 Litre Fuel Tank (Max limit 100 Litres) C42RAUK/22 TLAC Optional Modifications 15. Rudder Pedal Extensions TMC42-3 16. BRS-5-1050 Parachute TMC42-11 17. Strut Mount Repair TMC42 12 18. Radio Equipment (Radio, Transponder, ADS-B, PilotAware) TMC42-13 19. Operation at 472.5kg without a BPRS TMC42-15 ANNEX C - WEIGHING INFORMATION 1. CG Datum: Wing Leading Edge 2. Weighing attitude: Stabiliser horizontal 3. Mainwheel moment arm: 770 mm aft of datum (or factory measurement) 4. Nosewheel moment arm: 770 mm forward of datum (or factory measurement) 5. Fuel moment arm: 950 mm aft of datum 6. Crew moment arm: 400 mm aft of datum 7. Baggage moment arm: 950 mm aft of datum 8. Crew weights: Minimum 55 kg / maximum 220 kg 9. Aft CG Limit: 540 mm aft of datum 10. Fwd CG Limit: 350 mm aft of datum ANNEX D – EXAMPLE PLACARDS See Pilot Operating Handbook (POH) BRITISH MICROLIGHT AIRCRAFT ASSOCIATION (BMAA) MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO: BM-92 ISSUE: 2 Issued on behalf of the UK CAA by the BMAA, UK CAA organisation approval ref. DAI/8909/84 TADS BM92 Issue 2 Page 11 of 11 ANNEX E – POINTS FOR SPECIAL ATTENTION Tyre Pressures Main wheels 1.8 - 2.5 bar 26 to 36 psi. Front wheel 1.5 - 1.8 bar 22 to 26 psi. Shock absorbers – DO NOT attempt to adjust, contact TLAC for help as special equipment is required! Annual Bettsometer Test Stitching only: 1000 grammes using a 1.2mm diameter hook, pull at 90degs to surface of tensioned sail. Baggage Allowance 10kg using approved modification (Samsonite Case or TLAC Basket), weight report and CG to be checked before use.