TCDS No.: EASA.IM.A.665 SD3 Series Issue: 01 Date: 28 June 2019 TYPE-CERTIFICATE DATA SHEET NO. EASA.IM.A.665 for SD3 Series Type Certificate Holder Viking Air Limited 1959 de Havilland Way Sidney, B.C. V8L 5V5 Canada For models: SD3-30 SD3-60 SD3-SHERPA SD3-60-SHERPA TE.CERT.00048-002©European Union Aviation Safety Agency. All rights reserved. ISO9001 Certified. Page 1 of 54 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union TCDS No.: EASA.IM.A.665 SD3 Issue: 01 Date: dd month yyyy Intentionally left blank TE.CERT.00048-002©European Union Aviation Safety Agency. All rights reserved. ISO9001 Certified. Page 2 of 54 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union SECTION A: SD3-30 ................................................................................................................... 7 A.I. General ......................................................................................................................... 7 1. Type/ Model/ Approved Variants ............................................................................................... 7 2. Airworthiness Category .............................................................................................................. 7 3. Manufacturer .............................................................................................................................. 7 4. EASA Type Certification Application Date .................................................................................. 7 5. State of Design Authority ............................................................................................................ 7 6. State of Design Authority Type Certificate Date ......................................................................... 7 7. EASA Type Certification Date ...................................................................................................... 7 A.II. EASA Certification Basis ................................................................................................. 7 1. Reference Date for determining the applicable requirements .................................................. 7 2. Airworthiness Requirements ...................................................................................................... 7 3. Special Conditions ....................................................................................................................... 8 4. Exemptions ................................................................................................................................. 8 5. (Reserved) Deviations ................................................................................................................. 8 6. Equivalent Safety Findings .......................................................................................................... 8 7. Environmental Protection ........................................................................................................... 8 A.III. Technical Characteristics and Operational Limitations ................................................. 9 1. Type Design Definition ................................................................................................................ 9 2. Description .................................................................................................................................. 9 3. Equipment................................................................................................................................... 9 4. Dimensions ................................................................................................................................. 9 5. Engine ......................................................................................................................................... 9 6. Load factors .............................................................................................................................. 10 7. Propeller ................................................................................................................................... 10 8. Fluids ......................................................................................................................................... 10 9. Fluid capacities.......................................................................................................................... 11 10. Air Speeds ............................................................................................................................... 11 11. Flight Envelope - Maximum Operating Altitude ..................................................................... 12 12. Approved Operations Capability ............................................................................................. 12 13. Maximum Masses ................................................................................................................... 12 14. Centre of Gravity Range .......................................................................................................... 12 15. Datum ..................................................................................................................................... 13 16. Control surface deflections ..................................................................................................... 13 17. Levelling Means ...................................................................................................................... 13 19. Maximum Passenger Seating Capacity ................................................................................... 14 20. Baggage/ Cargo Compartments .............................................................................................. 14 21. Wheels and Tyres .................................................................................................................... 14 22. (Reserved) ............................................................................................................................... 14 A.IV. Operating and Service Instructions ........................................................................... 15 1. Flight Manual ............................................................................................................................ 15 2. Maintenance Manual ................................................................................................................ 15 3. Structural Repair Manual .......................................................................................................... 15 5. Illustrated Parts Catalogue ....................................................................................................... 16 A.V. Notes .......................................................................................................................... 17 SECTION B: SD3-60 ................................................................................................................. 20 B.I. General ....................................................................................................................... 20 1. Type/ Model/ Approved Variants ............................................................................................. 20 2. Airworthiness Category ............................................................................................................ 20 3. Manufacturer ............................................................................................................................ 20 TE.CERT.00048-002©European Union Aviation Safety Agency. All rights reserved. ISO9001 Certified. Page 3 of 54 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union 4. EASA Type Certification Application Date ................................................................................ 20 5. State of Design Authority .......................................................................................................... 20 6. State of Design Authority Type Certificate Date ....................................................................... 20 7. EASA Type Certification Date .................................................................................................... 20 B.II. EASA Certification Basis ............................................................................................... 21 1. Reference Date for determining the applicable requirements ................................................ 21 2. Airworthiness Requirements .................................................................................................... 21 3. Special Conditions ..................................................................................................................... 22 4. Exemptions ............................................................................................................................... 22 5. (Reserved) Deviations ............................................................................................................... 22 6. Equivalent Safety Findings ........................................................................................................ 22 7. Environmental Protection ........................................................................................................