TYPE-CERTIFICATE DATA SHEET Diamond DA20-A1 and DA20-C1

A.IV. Operating and Service Instructions 1. Airplane Flight Manual (AFM) Model with engine Rotax 912 A3 or 912 F3 Document No. DA202-VLA Model with engine Rotax 912 S3 Document No. DA202-100-VLA (English) or Document No. DA2002D-100-VLA (German) 2. Airplane Maintenance Manual (AMM) Document No. DA201 (incl. Airworthiness Limitations) 3. Service Informations, Service Bulletins and Services Letters 4. Life Limited Parts as listed in AMM Document No. DA201, chapter 4 A.V. Notes 1. S/N 10002 through 10092 originally equipped with Rotax 912 A3 engine may be retrofitted with a Rotax 912 F3 engine accordance with Service bulletin DA20-73-01. S/N 10093 through 10331 inclusive is originally equipped with Rotax 912 F3 engine. S/N 10002 through 10332 inclusive originally equipped with Rotax 912 A3 or F3 engine may be modified to a Rotax 912 S3 by Diamond Aircraft or its Agents in accordance with Diamond Drawing No. 20-0100-00-00. 2. Night VFR, IFR, Acrobatic flights including intentional spins are prohibited. Flight in known or expected icing condition is also prohibited. TCDS IM.A.223 Diamond DA20-A1, DA20-C1 Page 7 of 12 Issue 02 - 02. July 2009 3. The minimum oil pressure limit for Rotax 912 A3 and 912 F3 powered Da20-A1airplanes, as delivered, is 1.5 bar (22psi). Rotax has retroactively revised the minimum oil pressure limit for Rotax 912 A3 and 912 F3 engines to be 0,8 bar (12 psi) below 3500 RPM and 2.0 bar (29 psi) above 3500 RPM. The original oil pressure limits are valid for aircraft equipped with an oil pressure gauge marked accordingly. The revised limit is valid for any aircraft retrofit with an oil prossure gauge marked with the revised limits. (see also AFM) TCDS IM.A.223 Diamond DA20-A1, DA20-C1 Page 8 of 12 Issue 02 - 02. July 2009 SECTION 2 DA20-C1 B.I. General 1. a) Type: DA20-A1 b) Variant: DA20-C1 2. Airworthiness Category: CS-VLA 3. Type Certificate Holder: Diamond Aircraft Industries Inc. 1560 Crumlin Sideroad, London Ontario, N5V 1S2 CANADA 4. Manufacturer: Diamond Aircraft Industries Inc. 1560 Crumlin Sideroad, London Ontario, N5V 1S2 CANADA 5. EASA Certification Application Date: None (Prior to 28. September 2003, accepted under EU Regulation EC 1702/2003) 6. TCCA Type Certification Date: 19. December 1997 7. EU Member States reference Type Certificates Germany: LBA 1099 Italia: A 410 United Kingdom: Approval Note No. 27046 8. EASA Type Certificate Issue Date: 07. November 2008 B.II. Certification Basis 1. Reference Date for determining the applicable requirements: Accepted under EU Regulation EC 1702/2003 2. (Reserved) 3. (Reserved) 4. Certification Basis: The EASA Aircraft Type Certification standard includes that of TCCA TCDS A-191, based on individual EU member state acceptance or certification of this standard prior to 28. September 2003 using JAR-VLA as the applicable airworthiness requirement. Other standards conforming to TC/TCDS standards certificated by individual EU member states prior to 28. September 2003 are also acceptable. (See note 4.) 5. Airworthiness Requirements: JAR-VLA including Amendment VLA/92/1 6. Requirements elected to comply: None TCDS IM.A.223 Diamond DA20-A1, DA20-C1 Page 9 of 12 Issue 02 - 02. July 2009 7. Special Conditions: None 8. (Reserved): 9. Equivalent Safety Findings: None 10. Environmental Standards: ICAO, Annex 16, Volume I, see EASA Type Certificate Data Sheet Noise TCDSN IM.A.223 B.III. Technical Characteristics and Operational Limitations 1. Type Design Definition: Configuration Document No. DA20-C1 2. Description: Single engine, two-seated cantilever low wing airplane, composite construction, fixed tricycle landing gear, T-tail 3. Equipment: see Equipment List, AFM. In addition a fire extinguisher and a fuel dipstic acc. AFM must be installed. 4. Dimensions: Span 10.87 m (35 ft. 8 in) Length 7.17 m (23 ft. 6 in) Height 2.19 m ( 7 ft. 2 in) Wing Area 11.6 m² (125 sqft) 5. Engines: Teledyne Condinental Motors IO-240-B EASA Engine TCDS No. IM.E.169 Engine Limits: Max take-off rotational speed 2800 r.p.m. Max continuous rotational speed 2800 r.p.m For power-plants limits, refer to AFM. 6. (Reserved) 7. Propellers: Hoffmann HO-14HM-175-157 or Sensenich W69EK7-63 or Sensenich W69EK7-63G or Sensenich W69EK-63 (up to Aircraft S/N C0149) Propeller limits (Diameter): HO-14HM-175-157 : 1.750 m (68.9 in.) W69EK7-63 : 1.752 m (69.0 in.) W69EK7-63G : 1.752 m (69.0 in.) W69EK-63 : 1.752 m (69.0 in.) 8. Fluids: Fuel: AVGAS 100 or 100LL TCDS IM.A.223 Diamond DA20-A1, DA20-C1 Page 10 of 12 Issue 02 - 02. July 2009 See AFM for approved possible fuel types. Oil: See AFM for approved possible oil types. 9. Fluid capacities: Fuel: S/N C0001 to C0013 Usable: 80.5 litres 21.3 US Gall. Unusable: 14.5 litres 3.8 US Gall. Total: 95.0 litres 25.0 US Gall. S/N C0014 and subsequent, and S/N C0001 to C0013 if Service bulletin DA C1-28-01 incorporated Usable: 91 litres 24.0 US Gall. Unusable: 2 litres 0.5 US Gall. Total: 93 litres 24.5 US Gall. All S/N if 20 U.S. Gal. fuel tank (Dwg. No. 22- 2813-00-00 is installed) Usable: 76 litres 20.0 US Gall. Unusable: 2 litres 0.5 US Gall. Total: 78 litres 20.5 US Gall. Oil: Minimum: 3.79 litres 4 US Qt. Maximum: 5.68 litres 6 US Qt. 10. Air Speeds: Design Manoeuvring Speed vA: 106 KIAS Flap Extended Speed vFE: 100 KIAS with flaps in T/O position (15°) 78 KIAS with flaps in Landing position (45°) Maximum structural cruising speed vNO: 118 KIAS Never exceed speed vNE: 164 KIAS 11. All-weather Capability: Day-VFR (see note 4.) 12. Maximum Masses: Take-Off 750 kg (1653 lbs) Landing 750 kg (1653 lbs) 13. Centre of Gravity Range: Forward limit (for all masses): 202 mm ( 7.96 in.) behind Datum Rear limit (for all masses): 317 mm (12.49 in.) behind Datum 14. Datum: tangent to the leading edge of the wing at the root rib 15. (reserved) 16. Levelling Means: Wedge 55.84:1000, 2000mm (78.7 in.) behind the canopy. 17. Minimum Flight Crew: 1 (Pilot) 18. Maximum Passenger Seating Capacity: 1 TCDS IM.A.223 Diamond DA20-A1, DA20-C1 Page 11 of 12 Issue 02 - 02. July 2009 19. (Reserved) 20. Baggage / Cargo Compartments: Max. allowable load 20 kg (44 lbs) only permissible with baggage harness 21. Wheels and Tyres Nose Wheel Tyre Size 5.00 – 5, 6 ply Main Wheel Tyre Size 5.00 – 5, 6 ply For approved types and rating, refer to AFM. B.IV. Operating and Service Instructions 1. Airplane Flight Manual (AFM) Document No. DA202-C1 (English) Document No. DA202-C1-D (German) 2. Airplane Maintenance Manual (AMM) Document No. DA201-C1 (incl. Airworthiness Limitations) 3. Service Informations, Service Bulletins and Services Letters 4. Life Limited Parts as listed in AMM Document No. DA201-C1, Ch. 4 B.V. Notes 1. Night VFR, IFR or Acrobatic flights including intentional spins are prohibited. Flight in known or expected icing condition is also prohibited. TCDS IM.A.223 Diamond DA20-A1, DA20-C1 Page 12 of 12 Issue 02 - 02. July 2009 Change Record Issue Date Changes Issue 1 07. Nov 2008 Initial Issue Issue 2 02.July 2009 Editorial Changes Clarification of the 912 A3 engine capability according to the TCCA TC A.III.5. Note 1 A.V.1 rewording Typographical Error B.III.2 and 5