TCDS No.: EASA.A.379 MS 890 and Issue: 05 RALLYE 235 series Date: 06 January 2021 TYPE-CERTIFICATE DATA SHEET NO. EASA.A.379 for MS 890 and RALLYE 235 Series Type Certificate Holder DAHER AEROSPACE 23 route de TOURS 41400 SAINT JULIEN DE CHEDON FRANCE For models: MS 890 A, MS 890 B MS 892 A.150, MS 892 B.150, MS 892 E.150, MS 892 E-D.150 MS 893 A, MS 893 B, MS 893 E, MS 893 E-D MS 894 A, MS 894 C, MS 894 E RALLYE 235 E, RALLYE 235 E-D, RALLYE 235 A, RALLYE 235 C, RALLYE 235 F TE.CERT.00048-002 © European Union Aviation Safety Agency, 2019. All rights reserved. ISO9001 Certified. Page 1 of 50 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union TCDS No.: EASA.A.379 MS 890 and Issue: 05 RALLYE 235 series Date: 06 January 2021 Intentionally left blank TE.CERT.00048-002 © European Union Aviation Safety Agency, 2019. All rights reserved. ISO9001 Certified. Page 2 of 50 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union TCDS No.: EASA.A.379 MS 890 and Issue: 05 RALLYE 235 series Date: 06 January 2021 TABLE OF CONTENTS SECTION A: MODEL MS 890 ......................................................................................... 9 A.I. GENERAL .................................................................................................................................................. 9 1. Type/ Model/ Variant ............................................................................................................................ 9 2. Airworthiness Category ......................................................................................................................... 9 3. Manufacturer ......................................................................................................................................... 9 4. EASA Type Certification Application Date .............................................................................................. 9 5. State of Design Authority ....................................................................................................................... 9 6. State of Design Authority Type Certificate Date .................................................................................... 9 7. EASA Type Certification Date ................................................................................................................. 9 8. Other information .................................................................................................................................. 9 A.II. EASA CERTIFICATION BASIS ......................................................................................................................... 9 1. Reference Date for determining the applicable requirements .............................................................. 9 2. Airworthiness Requirements .................................................................................................................. 9 3. Special Conditions .................................................................................................................................. 9 4. Exemptions ............................................................................................................................................ 9 5. Deviations .............................................................................................................................................. 9 6. Equivalent Safety Findings ..................................................................................................................... 9 7. Environmental Protection ...................................................................................................................... 9 A.III. TECHNICAL CHARACTERISTICS AND OPERATIONAL LIMITATIONS ........................................................................... 9 1. Type Design Definition ........................................................................................................................... 9 2. Description ............................................................................................................................................. 9 3. Equipment ............................................................................................................................................ 10 4. Dimensions .......................................................................................................................................... 10 5. Engine .................................................................................................................................................. 10 6. Load factors ......................................................................................................................................... 10 7. Propeller .............................................................................................................................................. 10 8. Fluids .................................................................................................................................................... 11 9. Fluid capacities .................................................................................................................................... 11 10. Air Speeds ........................................................................................................................................ 11 11. Flight Envelope ................................................................................................................................ 12 12. Approved Operations Capability ..................................................................................................... 12 13. Maximum Masses (see Note 3) ....................................................................................................... 12 14. Centre of Gravity Range .................................................................................................................. 12 15. Datum .............................................................................................................................................. 12 16. Control surface deflections .............................................................................................................. 12 17. Levelling Means ............................................................................................................................... 13 18. Minimum Flight Crew ...................................................................................................................... 13 19. Maximum Passenger Seating Capacity ........................................................................................... 13 20. Baggage/ Cargo Compartments...................................................................................................... 13 21. Wheels and Tyres ............................................................................................................................ 13 22. Special equipment ........................................................................................................................... 13 A.IV. OPERATING AND SERVICE INSTRUCTIONS ....................................................................................................... 14 1. Flight Manuals (one per model) ........................................................................................................... 14 2. Technical Manual................................................................................................................................. 14 3. Repair Manual ..................................................................................................................................... 14 4. Weight and Balance Manual ............................................................................................................... 14 5. Illustrated Parts Catalogue .................................................................................................................. 14 6. Service Information and Service Bulletins ............................................................................................ 14 A.V. NOTES .................................................................................................................................................... 14 TE.CERT.00048-002 © European Union Aviation Safety Agency, 2019. All rights reserved. ISO9001 Certified. Page 3 of 50 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union TCDS No.: EASA.A.379 MS 890 and Issue: 05 RALLYE 235 series Date: 06 January 2021 TABLE OF CONTENTS SECTION B: MODEL MS 892 ....................................................................................... 15 B.I. GENERAL ................................................................................................................................................ 15 1. Type/ Model/ Variant .......................................................................................................................... 15 2. Airworthiness Category ....................................................................................................................... 15 3. Manufacturer ......................................................................................................................................