TYPE-CERTIFICATE DATA SHEET EASA.IM.A.629

TCDS No.: EASA.IM.A.629 Issue: 5 DA 62 15-Nov-2017 TE.CERT.00048-001 © European Aviation Safety Agency, 2017. All rights reserved. ISO9001 Certified. Page 1 of 11 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union TYPE-CERTIFICATE DATA SHEET EASA.IM.A.629 DA 62 Type Certificate Holder Diamond Aircraft Industries Inc. 1560 Crumlin Sideroad London, ON, N5V1S2 Canada For models: DA 62 TCDS No.: EASA.IM.A.629 Issue: 5 DA 62 15-Nov-2017 TE.CERT.00048-001 © European Aviation Safety Agency, 2017. All rights reserved. ISO9001 Certified. Page 2 of 11 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union SECTION A: DA 62 ........................................................................................................................................ 3 A.I. GENERAL ................................................................................................................................................... 3 A.III. TECHNICAL CHARACTERISTICS AND OPERATIONAL LIMITATIONS ........................................................... 4 A.IV. OPERATING AND SERVICE INSTRUCTIONS ................................................................................................ 8 A.V. OPERATIONAL SUITABILITY DATA (OSD) ................................................................................................ 9 A.VI. NOTES ........................................................................................................................................................ 9 ADMINISTRATIVE SECTION...........................................................................................................................11 I. ACRONYMS & ABBREVIATIONS.................................................................................................................... 11 II. TYPE CERTIFICATE HOLDER RECORD ......................................................................................................... 11 III. CHANGE RECORD......................................................................................................................................... 11 TCDS No.: EASA.IM.A.629 Issue: 5 DA 62 15-Nov-2017 TE.CERT.00048-001 © European Aviation Safety Agency, 2017. All rights reserved. ISO9001 Certified. Page 3 of 11 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union SECTION A: DA 62 A.I. General 1. a) Type: b) Model: c) Variant: DA 62 DA 62 -- 2. Airworthiness Category: CS-23 Normal Category 3. Type Certificate Holder: Diamond Aircraft Industries Inc. 1560 Crumlin Sideroad London, ON, N5V1S2 Canada 4. Manufacturer: Diamond Aircraft Industries Inc. 1560 Crumlin Sideroad, London Ontario N5V 1S2 Canada Diamond Aircraft Industries GmbH Nikolaus-August-Otto-Strasse 5 2700 Wiener Neustadt Austria 5. Certification Application Date: 02-Oct-2015 6. (Reserved) N/A 7. (Reserved) N/A A.II. EASA Certification Basis 1. Reference Date for determining the applicable requirements: 02-Oct-2015 2. Airworthiness Requirements: CS-23, Amendment 4, issued 15-Jul-2015 3. Special Conditions: CRI E-02 Use of Jet Fuel for Reciprocating Engines CRI E-04 Liquid Cooling – Coolant Tank CRI E-05 Electronically-controlled Reciprocating Diesel Engine TCDS No.: EASA.IM.A.629 Issue: 5 DA 62 15-Nov-2017 TE.CERT.00048-001 © European Aviation Safety Agency, 2017. All rights reserved. ISO9001 Certified. Page 4 of 11 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union CRI E-06 Engine Vibration Level CRI E-07 Engine Torque CRI F-04 Power plant Instruments CRI F-07 Human Factors in Integrated Avionic System CRI F-18 Cyber security CRI F-21 Battery Endurance 3. Exemptions: None 4. Deviations: None 5. Equivalent Safety Findings: CRI E-10 Electrical Fuel Pump CRI B-03 Stalling Speed in Icing Conditions 6. Requirements elected to comply: None 7. Environmental Standards: ICAO, Annex 16, Volume 1, Part II and as implemented in Decision No. 2003/4/RM amended by Decision 2007/007/R of The Executive Director of the Agency dated 2 April 2007, on certification specifications providing for acceptable means of compliance for aircraft noise CS-36, Amendment 1 see Note 2 8. (Reserved) N/A 9. (Reserved) N/A 10. Operational Suitability Requirements OSD MMEL: CS-GEN-MMEL, Initial Issue dated 31 January 2014 A.III. Technical Characteristics and Operational Limitations 1. Type Design Definition: Doc. No. D62-AW-0004, latest revision 2. Description: Twin engine, up to seven-seated cantilever low wing airplane, composite construction, retractable tricycle landing gear, T-tail 3. Equipment: Equipment list, AFM, Section 6 4. Dimensions: Span Length Height Wing Area 14.57 m (47 ft 10 in) 9.17 m (30 ft 1 in) 2.82 m ( 9 ft 3 in) 17.10 m² (184.1 sqft) TCDS No.: EASA.IM.A.629 Issue: 5 DA 62 15-Nov-2017 TE.CERT.00048-001 © European Aviation Safety Agency, 2017. All rights reserved. ISO9001 Certified. Page 5 of 11 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union 5. Engine: 5.1.1 Model: 2 Austro Engine E4P see Note 4 5.1.2 Type Certificate: EASA Engine Type Certificate E.200 5.1.3 Limitations: Max take-off rotational speed (5 min.) 2300 r.p.m. Max continuous rotational speed 2200 r.p.m Max T/O Power (5min) 100% (132 kW) Max. continuous Power 95% (126 kW) For power-plants limits refer to AFM, Section 2 5.1.4 Firmware: see DAI MSB 62-002 See Note 4 5.1.5 Mapping: see DAI MSB 62-002 See Note 4 6. Load factors: at vA at vNE with flaps in T/O or LDG position Positive: 3.8 3.8 2.0 Negative -1.52 0 0 7. Propeller: 7.1 Model: 2 MT-Propeller MTV-6-R-C-F/CF194-80 7.2 Type Certificate: EASA Prop. Type Certificate P.094 See note 5 7.3 Number of blades: 3 7.4 Diameter: 1940 mm 7.5 Sense of Rotation: CW 7.6 Settings: Low pitch setting 11 ° Feather position: 80 ° Start Lock: 15° 8. Fluids: 8.1 Fuel: Jet A-1 (ASTM 1655), see note 6 8.2 Oil: Engine: Gearbox: Shell Helix Ultra 5W30 or 5W40 or see AFM, Section 2 Shell SPIRAX GSX 75W-80 or Shell SPIRAX S6 GXME 75W-80 or see AFM, Section 2 8.3 Coolant: Water / Cooler Protection for more details see AFM, Section 2 8.4 Ice Protection Fluids: Fluids according DTD 406B TCDS No.: EASA.IM.A.629 Issue: 5 DA 62 15-Nov-2017 TE.CERT.00048-001 © European Aviation Safety Agency, 2017. All rights reserved. ISO9001 Certified. Page 6 of 11 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union 9. Fluid capacities: 9.1 Fuel: Standard Fuel Tank Total: 196.8 liters 52 US Gallons Usable: 189.2 liters 50 US Gallons Auxiliary Fuel Tank Total: 140 liters 37 US Gallons Usable: 137.8 liters 36,4 US Gallons 9.2 Oil: each engine Maximum: 7 liters Minimum: 5 liters 9.3 Coolant system capacity: Approx. 7 liters 10. Air Speeds: Operating Manoeuvring Speed vo up to 1700 kg 117 KEAS 1800 to 1900 kg 126 KEAS 1901 kg to 1999 kg 130 KEAS 2000 kg to 2100 kg 133 KEAS 2101 kg to 2200 kg 136 KEAS Above 2201 kg 140 KEAS Flap Extended Speed vFE Approach 135 KEAS Landing 118 KEAS Maximum Landing Gear Operation Speed vLO 160 KEAS Maximum Landing Gear Extended Speed vLE 201 KEAS Minimum Control Speed Airborne vMCA 75 KEAS Maximum structural cruising speed vNO (= Maximum structural design speed vC) 160 KEAS Never exceed speed vNE 201 KEAS 11. Maximum Operating Altitude: 6096 m (20 000 ft) 12. Allweather Operations Capability: Day/Night-VFR, IFR Flights into known or forecast icing conditions, see Note 8 TCDS No.: EASA.IM.A.629 Issue: 5 DA 62 15-Nov-2017 TE.CERT.00048-001 © European Aviation Safety Agency, 2017. All rights reserved. ISO9001 Certified. Page 7 of 11 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union 13. Maximum Weights: Take-off Zero Fuel Landing 1999 kg (4407 lb) With MÄM 62-001 2300 kg (5071 lb) 2036 kg (4489 lb) With MÄM 62-063 2200 kg (4850 lb) 2300 kg (5071 lb) 14. Centre of Gravity Range: Forward limit From 1600 kg to 1800 kg 2.340 m behind Datum At 2300 kg 2.460 m behind Datum Varying linearly with mass in between Rear limit At 1600 kg 2.460 m behind Datum At 1900 kg to 1999 kg 2.510 m behind Datum At 2300 kg 2.530 m behind Datum Varying linearly with mass in between 15. Datum: 2.196 m in front of leading edge of stub-wing at the wing joint 16. Control surface deflections: Aileron Elevator Elevator Trim Tab Rudder Rudder Trim Tab Flaps trailing edge up 25º ± 2º trailing edge down 15º +2/-0º trailing edge up 18° ± 0.5º trailing edge down 15º ± 1º nose up at elevator 10° up + 17º ± 5º nose down at elevator 10° up -35º ± 5º left 30º ± 1º right 30º ± 1º trim RH at rudder 20° LH + 45º ± 5º trim LH at rudder 20° LH + 28º ± 3º Cruise flap setting 0° + 2°- 0° Approach flap setting 20º + 4º - 2° Landing flap setting 42º +3º - 1º 17. Levelling Means: floor of front baggage compartment levelled 18. Minimum Flight Crew: 1 (Pilot) 19. Maximum Passenger Seating Capacity: 4, with OÄM 62-019: 6 20. Baggage/Cargo Compartments: Location max. allowable Load LH Nose Baggage Compartment 30 kg (66 lb) TCDS No.: EASA.IM.A.629 Issue: 5 DA 62 15-Nov-2017 TE.CERT.00048-001 © European Aviation Safety Agency, 2017. All rights reserved. ISO9001 Certified. Page 8 of 11 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union RH Nose Baggage Compartment 30 kg (66 lb) Rear Baggage Compartment 120 kg (265 lb) With OÄM 62-019 46 kg (101 lb) For detail see AFM Section 2.7 21. Wheels and Tyres: Nose Wheel Tyre Size 6.00–6 see Note 7 Main Wheel Tyre Size 6.00–6 see Note 7 A.IV. Operating and Service Instructions 1. Flight Manual: Document No. 7.01.25-E 2. Technical Manual: Airplane Maintenance Manual (AMM) Document No. 7.02.25 (incl. Airworthiness Limitations) Service Information and Service Bulletins 3. Spare Parts Catalogue (IPC): Document No. 7.03.25 4. Instruments and aggregates: refer to AMM Doc. No. 7.02.25 Chapter 1 TCDS No.: EASA.IM.A.629 Issue: 5 DA 62 15-Nov-2017 TE.CERT.00048-001 © European Aviation Safety Agency, 2017. All rights reserved. ISO9001 Certified. Page 9 of 11 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union A.V. Operational Suitability Data (OSD) The Operational Suitability Data elements listed below are approved by the European Aviation Safety Agency under the EASA Type Certificate EASA.A.005 as per Commission Regulation (EU) 748/2012 as amended by Commission Regulation (EU) No 69/2014. 1. Master Minimum Equipment List (MMEL) The MMEL is defined in the Document No: 11.11.01, Revision Original or later approved revisions. A.VI. Notes 1. (a) Serial Numbers Eligible: 62.007 and 62.009 and subsequent 62.C001 and subsequent (b) Type Certificate Holder Record: Effective 15-Nov-2017 design responsibility for the Model DA 62 certified under TC EASA.A.629 was transferred from Diamond Aircraft Industries GmbH and EASA to Diamond Aircraft Industries Inc. and Transport Canada. The Model DA 62 was originally certified by EASA as a derivative of the DA 42 and was approved on TC EASA.A.005. The Model was later certified on TC EASA.A.629. Aircraft manufactured against TC EASA.A.005 were eligible to be transferred to TC EASA.A.629 in accordance with DAI Factory Campaign FC 62- 010. Serial numbers originally produced under TC EASA.A.005 and still associated with that TC at the date of design responsibility transfer remain under the responsibility of Diamond Aircraft Industries GmbH and EASA until they are transferred to TCCA TC A-273 under an agreed design transfer plan. The serial numbers still associated with TC EASA.A.005 as of 15-Nov-2017 were: 62.007, 62.010, 62.012, 62.013, 62.014, 62.015, 62.020, 62.021, 62.025, 62.026, 62.030, 62.031, 62.032, 62.034, 62.037, 62.038, 62.041, 62.048, 62.053, 62.056, 62.060, 62.062, 62.C001 TCDS No.: EASA.IM.A.629 Issue: 5 DA 62 15-Nov-2017 TE.CERT.00048-001 © European Aviation Safety Agency, 2017. All rights reserved. ISO9001 Certified. Page 10 of 11 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union (c) Manufacturer Record: Serial numbers 62.007 and 62.009 through 62.077 were produced by Diamond Aircraft Industries GmbH against EASA TC A.005. Serial number 62.C001 was manufactured by Diamond Aircraft Industries Inc. against EASA TC A.005 under license from Diamond Aircraft Industries GmbH. Additional serial numbers up to and including 62.C020, may be produced against EASA TC A.005 during the transition period for the transfer of all DA 62 serial numbers to TCCA TC A-273. 2. Approved Noise Levels in accordance to the EASA data sheet for noise TCDSN IM.A.629. 3. For approved software versions of Gamin G1000 Integrated Avionic System see, until further notice, DAI MSB 62-003, at latest issue. 4. Approved engine model for installation in the DA 62: E4P-C The approved firmware and mapping is, until further notice, according to DAI MSB 62-002 at latest issue. 5. Propeller Equipment: Governor P-877-16 6. For additional approved Jet Fuel specifications see AFM Section 2. 7. Only specific brand names and types of tires are allowed for installation, see AMM and IPC 8. Flights into known or forecast icing conditions is approved if the liquid fluid ice protection system in accordance to Major Design Change OÄM 62-003 is installed. TCDS No.: EASA.IM.A.629 Issue: 5 DA 62 15-Nov-2017 TE.CERT.00048-001 © European Aviation Safety Agency, 2017. All rights reserved. ISO9001 Certified. Page 11 of 11 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union ADMINISTRATIVE SECTION I. Acronyms & Abbreviations AFM Airplane Flight Manual Amdt. Amendment AMM Airplane Maintenance Manual CG Centre of Gravity DWN down EASA European Aviation Safety Agency IAS Indicated Airspeed ICAO International Civil Aviation Organization kg kilograms km/h kilometres per hour MAC Mean Aerodynamic Chord N.A. Not applicable SC Special Condition TCDSN Type Certificate Datasheet Noise VFR Visual Flight Rules II. Type Certificate Holder Record Until 15-Nov-2017 Diamond Aircraft Industries GmbH Nicolaus-August-Otto-Straße 5 2700 Wiener Neustadt Austria Since 15-Nov-2017 Diamond Aircraft Industries Inc. 1560 Crumlin Sideroad London, ON, N5V1S2 Canada III. Change Record Issue Date Changes TC Issue No & Date 1 to 4 15-Nov-2017 Revisions as done prior transfer of TC. Kept for record only - 5 15-Nov-2017 First published issue for TCDS EASA.IM.A.629, after TC- Transfer of the original EASA TC A.629 at TCDS EASA.A.629, Issue 4 to Diamond Aircraft Industries Inc., Canada, with TCCA TC A-273. 15-Nov-2017