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TYPE-CERTIFICATE DATA SHEET...TCDS No.: EASA.A.010 TBM700 Issue: 15 Date: 28 July 2020...

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TCDS No.: EASA.A.010 TBM700 Issue: 15 Date: 28 July 2020 TE.CERT.00048-002 © European Union Aviation Safety Agency, 2019. All rights reserved. ISO9001 Certified.Page 1 of 114 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union TYPE-CERTIFICATE DATA SHEET NO. EASA.A.010 for TBM700 Type Certificate Holder DAHER AEROSPACE 23 route de TOURS 41400 SAINT JULIEN DE CHEDON FRANCE For Variants: TBM700 A TBM700 B TBM700 C1 TBM700 C2 TBM700 N
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  • TCDS No.: EASA.A.010 TBM700 Issue: 15

    Date: 28 July 2020

    TE.CERT.00048-002 © European Union Aviation Safety Agency, 2019. All rights reserved. ISO9001 Certified.Page 1 of 114 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.

    An agency of the European Union

    TYPE-CERTIFICATE

    DATA SHEET

    NO. EASA.A.010

    for

    TBM700

    Type Certificate Holder

    DAHER AEROSPACE

    23 route de TOURS 41400 SAINT JULIEN DE CHEDON

    FRANCE

    For Variants: TBM700 A

    TBM700 B

    TBM700 C1

    TBM700 C2

    TBM700 N

  • TCDS No.: EASA.A.010 TBM700 Issue: 15 Date: 28 July 2020

    TE.CERT.00048-002 © European Union Aviation Safety Agency, 2019. All rights reserved. ISO9001 Certified. Page 2 of 114 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.

    An agency of the European Union

    Intentionally left blank

  • TCDS No.: EASA.A.010 TBM700 Issue: 15 Date: 28 July 2020

    TE.CERT.00048-002 © European Union Aviation Safety Agency, 2019. All rights reserved. ISO9001 Certified. Page 3 of 114 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.

    An agency of the European Union

    SECTION A. TBM700 A, Basic TBM700 Type Design .................................................................................................. 15

    A.I. General .................................................................................................................................................................. 15 1. Type/ Model/ Variant ............................................................................................................................................ 15 2. Airworthiness Category ......................................................................................................................................... 15 3. Manufacturer ........................................................................................................................................................ 15 4. DGAC Type Certification Application Date ............................................................................................................ 15 5. State of Design Authority ...................................................................................................................................... 15 6. State of Design Authority Type Certificate Date ................................................................................................... 15 7. EASA Type Certification Date ................................................................................................................................ 15 8. Other informations ................................................................................................................................................ 15

    A.II. EASA Certification Basis ......................................................................................................................................... 15 1. Reference Date for determining the applicable requirements ............................................................................. 15 2. Airworthiness Requirements ................................................................................................................................. 15 3. Special Conditions ................................................................................................................................................. 15 4. Exemptions ............................................................................................................................................................ 15 5. (Reserved) Deviations ........................................................................................................................................... 15 6. Equivalent Safety Findings .................................................................................................................................... 15 7. Requirements elected to comply .......................................................................................................................... 15 8. Environmental Protection ..................................................................................................................................... 16 9. Operational Suitability Data (OSD) ........................................................................................................................ 16

    A.III. Technical Characteristics and Operational Limitations ......................................................................................... 16 1. Type Design Definition .......................................................................................................................................... 16 2. Description ............................................................................................................................................................ 16 3. Equipment ............................................................................................................................................................. 16 4. Operational Suitability Data (OSD) ........................................................................................................................ 16 5. Dimensions ............................................................................................................................................................ 16 6. Engine .................................................................................................................................................................... 16 7. Load factors ........................................................................................................................................................... 17 8. Propeller ................................................................................................................................................................ 17 9. Fluids ..................................................................................................................................................................... 17 10. Fluid capacities .................................................................................................................................................. 18 11. Air Speeds ......................................................................................................................................................... 18 12. Flight Envelope .................................................................................................................................................. 18 13. Approved Operational Capability ..................................................................................................................... 18 14. Maximum Masses ............................................................................................................................................. 18 15. Centre of Gravity Range .................................................................................................................................... 19 16. Datum ............................................................................................................................................................... 19 17. Control surface deflections ............................................................................................................................... 19 18. Levelling Means ................................................................................................................................................ 19 19. Minimum Flight Crew ....................................................................................................................................... 19 20. Maximum Passenger Seating Capacity ............................................................................................................. 20 21. Baggage / Cargo Compartments ....................................................................................................................... 20 22. Wheels and Tyres .............................................................................................................................................. 20 23. (Reserved) ......................................................................................................................................................... 20

    A.IV. Operating and Service Instructions ....................................................................................................................... 20 1. Flight Manual ........................................................................................................................................................ 20 2. Maintenance manual ............................................................................................................................................ 21

    A.V. Notes ..................................................................................................................................................................... 21

    SECTION B. TBM 700 B ............................................................................................................................................. 22

    B.I. General .................................................................................................................................................................. 22

  • TCDS No.: EASA.A.010 TBM700 Issue: 15 Date: 28 July 2020

    TE.CERT.00048-002 © European Union Aviation Safety Agency, 2019. All rights reserved. ISO9001 Certified. Page 4 of 114 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.

    An agency of the European Union

    1. Type/ Model/ Variant ............................................................................................................................................ 22 2. Airworthiness Category ......................................................................................................................................... 22 3. Manufacturer ........................................................................................................................................................ 22 4. DGAC Type Certification Application Date ............................................................................................................ 22 5. State of Design Authority ...................................................................................................................................... 22 6. State of Design Authority Type Certificate Date ................................................................................................... 22 7. EASA Type Certification Date ................................................................................................................................ 22 8. Other informations ................................................................................................................................................ 22

    B.II. EASA Certification Basis ......................................................................................................................................... 22 1. Reference Date for determining the applicable requirements ............................................................................. 22 2. Airworthiness Requirements ................................................................................................................................. 22 3. Special Conditions ................................................................................................................................................. 22 4. Exemptions ............................................................................................................................................................ 22 5. (Reserved) Deviations ........................................................................................................................................... 22 6. Equivalent Safety Findings .................................................................................................................................... 22 7. Requirements elected to comply .......................................................................................................................... 22 8. Environmental Protection ..................................................................................................................................... 23 9. Operational Suitability Data (OSD) ........................................................................................................................ 23

    B.III. Technical Characteristics and Operational Limitations ......................................................................................... 23 1. Type Design Definition .......................................................................................................................................... 23 2. Description ............................................................................................................................................................ 23 3. Equipment ............................................................................................................................................................. 23 4. Operational Suitability Data (OSD) ........................................................................................................................ 23 5. Dimensions ............................................................................................................................................................ 23 6. Engine .................................................................................................................................................................... 23 7. Load factors: .......................................................................................................................................................... 24 8. Propeller ................................................................................................................................................................ 24 9. Fluids ..................................................................................................................................................................... 24 10. Fluid capacities .................................................................................................................................................. 25 11. Air Speeds ......................................................................................................................................................... 25 12. Flight Envelope .................................................................................................................................................. 25 13. Approved Operational Capability ..................................................................................................................... 25 14. Maximum Masses ............................................................................................................................................. 25 15. Centre of Gravity Range .................................................................................................................................... 25 16. Datum ............................................................................................................................................................... 26 17. Control surface deflections ............................................................................................................................... 26 18. Levelling Means ................................................................................................................................................ 26 19. Minimum Flight Crew ....................................................................................................................................... 26 20. Maximum Passenger Seating Capacity ............................................................................................................. 26 21. Baggage / Cargo Compartments ....................................................................................................................... 26 22. Wheels and Tyres .............................................................................................................................................. 27 23. (Reserved) ......................................................................................................................................................... 27

    B.IV. Operating and Service Instructions ....................................................................................................................... 27 1. Flight Manual ........................................................................................................................................................ 27 2. Maintenance manual ............................................................................................................................................ 27

    B.V. Notes ..................................................................................................................................................................... 28

    SECTION C. TBM700 C1 ............................................................................................................................................ 29

    C.I. General .................................................................................................................................................................. 29 1. Type/ Model/ Variant ............................................................................................................................................ 29 2. Airworthiness Category ......................................................................................................................................... 29 3. Manufacturer ........................................................................................................................................................ 29

  • TCDS No.: EASA.A.010 TBM700 Issue: 15 Date: 28 July 2020

    TE.CERT.00048-002 © European Union Aviation Safety Agency, 2019. All rights reserved. ISO9001 Certified. Page 5 of 114 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.

    An agency of the European Union

    4. DGAC Type Certification Application Date ............................................................................................................ 29 5. State of Design Authority ...................................................................................................................................... 29 6. State of Design Authority Type Certificate Date ................................................................................................... 29 7. EASA Type Certification Date ................................................................................................................................ 29 8. Other informations ................................................................................................................................................ 29

    C.II. EASA Certification Basis ......................................................................................................................................... 29 1. Reference Date for determining the applicable requirements ............................................................................. 29 2. Airworthiness Requirements ................................................................................................................................. 29 3. Special Conditions ................................................................................................................................................. 29 4. Exemptions ............................................................................................................................................................ 29 5. (Reserved) Deviations ........................................................................................................................................... 29 6. Equivalent Safety Findings .................................................................................................................................... 29 7. Requirements elected to comply .......................................................................................................................... 29 8. Environmental Protection ..................................................................................................................................... 30 9. Operational Suitability Data (OSD) ........................................................................................................................ 30

    C.III. Technical Characteristics and Operational Limitations ......................................................................................... 30 1. Type Design Definition .......................................................................................................................................... 30 2. Description ............................................................................................................................................................ 30 3. Equipment ............................................................................................................................................................. 30 4. Operational Suitability Data (OSD) ........................................................................................................................ 30 5. Dimensions ............................................................................................................................................................ 30 6. Engine .................................................................................................................................................................... 31 7. Load factors ........................................................................................................................................................... 31 8. Propeller ................................................................................................................................................................ 31 9. Fluids ..................................................................................................................................................................... 32 10. Fluid capacities .................................................................................................................................................. 32 11. Air Speeds ......................................................................................................................................................... 32 12. Flight Envelope .................................................................................................................................................. 32 13. Approved Operational Capability ..................................................................................................................... 32 14. Maximum Masses ............................................................................................................................................. 32 15. Centre of Gravity Range .................................................................................................................................... 33 16. Datum ............................................................................................................................................................... 33 17. Control surface deflections ............................................................................................................................... 33 18. Levelling Means ................................................................................................................................................ 33 19. Minimum Flight Crew ....................................................................................................................................... 33 20. Maximum Passenger Seating Capacity ............................................................................................................. 33 21. Baggage / Cargo Compartments ....................................................................................................................... 34 22. Wheels and Tyres .............................................................................................................................................. 34 23. (Reserved) ......................................................................................................................................................... 34

    C.IV. Operating and Service Instructions ....................................................................................................................... 34 1. Flight Manual ........................................................................................................................................................ 34 2. Maintenance manuals: .......................................................................................................................................... 34

    C.V. Notes ..................................................................................................................................................................... 34

    SECTION D. TBM700 C2 ............................................................................................................................................ 35

    D.I. General .................................................................................................................................................................. 35 1. Type/ Model/ Variant ............................................................................................................................................ 35 2. Airworthiness Category ......................................................................................................................................... 35 3. Manufacturer ........................................................................................................................................................ 35 4. EASA Type Certification Application Date ............................................................................................................. 35 5. EASA Type Certification Date ................................................................................................................................ 35 6. Other informations ................................................................................................................................................ 35

  • TCDS No.: EASA.A.010 TBM700 Issue: 15 Date: 28 July 2020

    TE.CERT.00048-002 © European Union Aviation Safety Agency, 2019. All rights reserved. ISO9001 Certified. Page 6 of 114 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.

    An agency of the European Union

    D.II. EASA Certification Basis ......................................................................................................................................... 35 1. Reference Date for determining the applicable requirements ............................................................................. 35 2. Airworthiness Requirements ................................................................................................................................. 35 3. Special Conditions ................................................................................................................................................. 35 4. Exemptions ............................................................................................................................................................ 35 5. (Reserved) Deviations ........................................................................................................................................... 35 6. Equivalent Safety Findings .................................................................................................................................... 35 7. Requirements elected to comply .......................................................................................................................... 35 8. Environmental Protection ..................................................................................................................................... 36 9. Operational Suitability Data (OSD) ........................................................................................................................ 36

    D.III. Technical Characteristics and Operational Limitations ......................................................................................... 36 1. Type Design Definition .......................................................................................................................................... 36 2. Description ............................................................................................................................................................ 36 3. Equipment ............................................................................................................................................................. 36 4. Operational Suitability Data (OSD) ........................................................................................................................ 36 5. Dimensions ............................................................................................................................................................ 36 6. Engine .................................................................................................................................................................... 37 7. Load factors ........................................................................................................................................................... 37 8. Propeller ................................................................................................................................................................ 37 9. Fluids ..................................................................................................................................................................... 38 10. Fluid capacities .................................................................................................................................................. 38 11. Air Speeds ......................................................................................................................................................... 38 12. Flight Envelope .................................................................................................................................................. 38 13. Approved Operational Capability ..................................................................................................................... 38 14. Maximum Masses ............................................................................................................................................. 38 15. Centre of Gravity Range .................................................................................................................................... 39 16. Datum ............................................................................................................................................................... 39 17. Control surface deflections ............................................................................................................................... 39 18. Levelling Means ................................................................................................................................................ 40 19. Minimum Flight Crew ....................................................................................................................................... 40 20. Maximum Passenger Seating Capacity ............................................................................................................. 40 21. Baggage / Cargo Compartments ....................................................................................................................... 40 22. Wheels and Tyres .............................................................................................................................................. 40 23. (Reserved) ......................................................................................................................................................... 40

    D.IV. Operating and Service Instructions ....................................................................................................................... 40 1. Flight Manual ........................................................................................................................................................ 40 2. Maintenance manuals ........................................................................................................................................... 40

    D.V. Notes ..................................................................................................................................................................... 40

    SECTION E. TBM700 N .............................................................................................................................................. 41

    E.I. General .................................................................................................................................................................. 41 1. Type/ Model/ Variant ............................................................................................................................................ 41 2. Airworthiness Category ......................................................................................................................................... 41 3. Manufacturer ........................................................................................................................................................ 41 4. EASA Type Certification Application Date ............................................................................................................. 41 5. EASA Type Certification Date ................................................................................................................................ 41 6. Other informations ................................................................................................................................................ 41

    E.II. EASA Certification Basis ......................................................................................................................................... 41 1. Reference Date for determining the applicable requirements ............................................................................. 41 2. Airworthiness Requirements ................................................................................................................................. 41 3. Special Conditions ................................................................................................................................................. 41 4. Exemptions ............................................................................................................................................................ 41

  • TCDS No.: EASA.A.010 TBM700 Issue: 15 Date: 28 July 2020

    TE.CERT.00048-002 © European Union Aviation Safety Agency, 2019. All rights reserved. ISO9001 Certified. Page 7 of 114 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.

    An agency of the European Union

    5. (Reserved) Deviations ........................................................................................................................................... 41 6. Equivalent Safety Findings .................................................................................................................................... 41 7. Requirements elected to comply .......................................................................................................................... 41 8. Environmental Protection ..................................................................................................................................... 42 9. Operational Suitability Data (OSD) ........................................................................................................................ 42

    E.III. Technical Characteristics and Operational Limitations ......................................................................................... 42 1. Type Design Definition .......................................................................................................................................... 42 2. Description ............................................................................................................................................................ 42 3. Equipment ............................................................................................................................................................. 42 4. Operational Suitability Data (OSD) ........................................................................................................................ 42 5. Dimension ............................................................................................................................................................. 42 6. Engine .................................................................................................................................................................... 43 7. Load factors ........................................................................................................................................................... 43 8. Propeller ................................................................................................................................................................ 43 9. Fluids ..................................................................................................................................................................... 44 10. Fluid capacities .................................................................................................................................................. 44 11. Air Speeds ......................................................................................................................................................... 44 12. Flight Envelope .................................................................................................................................................. 44 13. Approved Operational Capability ..................................................................................................................... 44 14. Maximum Masses ............................................................................................................................................. 44 15. Centre of Gravity Range .................................................................................................................................... 45 16. Datum ............................................................................................................................................................... 45 17. Control surface deflections ............................................................................................................................... 45 18. Levelling Means ................................................................................................................................................ 46 19. Minimum Flight Crew ....................................................................................................................................... 46 20. Maximum Passenger Seating Capacity ............................................................................................................. 46 21. Baggage / Cargo Compartments ....................................................................................................................... 46 22. Wheels and Tyres .............................................................................................................................................. 46 23. (Reserved) ......................................................................................................................................................... 46

    E.IV. Operating and Service Instructions ....................................................................................................................... 46 1. Flight Manual ........................................................................................................................................................ 46 2. Maintenance manuals ........................................................................................................................................... 46

    E.V. Notes ..................................................................................................................................................................... 46

    SECTION F. TBM700 N equipped with MOD70-0176-00 and MOD70-0211-57.......................................................... 47

    F.I. General .................................................................................................................................................................. 47 1. Type/ Model/ Variant ............................................................................................................................................ 47 2. Airworthiness Category ......................................................................................................................................... 47 3. Manufacturer ........................................................................................................................................................ 47 4. EASA Type Certification Application Date ............................................................................................................. 47 5. EASA Type Certification Date ................................................................................................................................ 47 6. Other informations ................................................................................................................................................ 47

    F.II. EASA Certification Basis ......................................................................................................................................... 47 1. Reference Date for determining the applicable requirements ............................................................................. 47 2. Airworthiness Requirements ................................................................................................................................. 47 3. Special Conditions ................................................................................................................................................. 47 4. Exemptions ............................................................................................................................................................ 47 5. (Reserved) Deviations ........................................................................................................................................... 48 6. Equivalent Safety Findings .................................................................................................................................... 48 7. Requirements elected to comply .......................................................................................................................... 48 8. Environmental Protection ..................................................................................................................................... 48 9. Operational Suitability Data (OSD) ........................................................................................................................ 48

  • TCDS No.: EASA.A.010 TBM700 Issue: 15 Date: 28 July 2020

    TE.CERT.00048-002 © European Union Aviation Safety Agency, 2019. All rights reserved. ISO9001 Certified. Page 8 of 114 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.

    An agency of the European Union

    F.III. Technical Characteristics and Operational Limitations ......................................................................................... 48 1. Type Design Definition .......................................................................................................................................... 48 2. Description ............................................................................................................................................................ 48 3. Equipment ............................................................................................................................................................. 48 4. Operational Suitability Data (OSD) ........................................................................................................................ 48 5. Dimensions ............................................................................................................................................................ 48 6. Engine .................................................................................................................................................................... 49 7. Load factors ........................................................................................................................................................... 49 8. Propeller ................................................................................................................................................................ 49 9. Fluids ..................................................................................................................................................................... 50 10. Fluid capacities .................................................................................................................................................. 50 11. Air Speeds ......................................................................................................................................................... 50 12. Flight Envelope .................................................................................................................................................. 50 13. Approved Operational Capability ..................................................................................................................... 50 14. Maximum Masses ............................................................................................................................................. 51 15. Centre of Gravity Range .................................................................................................................................... 51 16. Datum ............................................................................................................................................................... 51 17. Control surface deflections ............................................................................................................................... 51 18. Levelling Means ................................................................................................................................................ 52 19. Minimum Flight Crew ....................................................................................................................................... 52 20. Maximum Passenger Seating Capacity ............................................................................................................. 52 21. Baggage / Cargo Compartments ....................................................................................................................... 52 22. Wheels and Tyres .............................................................................................................................................. 52 23. (Reserved) ......................................................................................................................................................... 52

    F.IV. Operating and Service Instructions ....................................................................................................................... 52 1. Flight Manual ........................................................................................................................................................ 52 2. Maintenance manual ............................................................................................................................................ 53

    F.V. Notes ..................................................................................................................................................................... 53

    SECTION G. TBM700 N equipped with MOD70-0176-00, -0211-57, -0234-24, -0322-00, -0323-71, -0324-00, -0325-21 and -0357-71 .............................................................................................................................................................. 54

    G.I. General .................................................................................................................................................................. 54 1. Type/ Model/ Variant ............................................................................................................................................ 54 2. Airworthiness Category ......................................................................................................................................... 54 3. Manufacturer ........................................................................................................................................................ 54 4. EASA Type Certification Application Date ............................................................................................................. 54 5. EASA Type Certification Date ................................................................................................................................ 54 6. Other informations ................................................................................................................................................ 54

    G.II. EASA Certification Basis ......................................................................................................................................... 54 1. Reference Date for determining the applicable requirements ............................................................................. 54 2. Airworthiness Requirements ................................................................................................................................. 54 3. Special Conditions ................................................................................................................................................. 54 4. Exemptions ............................................................................................................................................................ 55 5. (Reserved) Deviations ........................................................................................................................................... 55 6. Equivalent Safety Findings .................................................................................................................................... 55 7. Requirements elected to comply .......................................................................................................................... 55 8. Environmental Protection ..................................................................................................................................... 55 9. Operational Suitability Data (OSD) ........................................................................................................................ 55

    G.III. Technical Characteristics and Operational Limitations ......................................................................................... 56 1. Type Design Definition .......................................................................................................................................... 56 2. Description ............................................................................................................................................................ 56 3. Equipment ............................................................................................................................................................. 56

  • TCDS No.: EASA.A.010 TBM700 Issue: 15 Date: 28 July 2020

    TE.CERT.00048-002 © European Union Aviation Safety Agency, 2019. All rights reserved. ISO9001 Certified. Page 9 of 114 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.

    An agency of the European Union

    4. Operational Suitability Data (OSD) ........................................................................................................................ 56 5. Dimensions ............................................................................................................................................................ 56 6. Engine .................................................................................................................................................................... 57 7. Load factors ........................................................................................................................................................... 57 8. Propeller ................................................................................................................................................................ 57 9. Fluids ..................................................................................................................................................................... 58 10. Fluid capacities .................................................................................................................................................. 58 11. Air Speeds ......................................................................................................................................................... 58 12. Flight Envelope .................................................................................................................................................. 58 13. Approved Operational Capability ..................................................................................................................... 59 14. Maximum Masses ............................................................................................................................................. 59 15. Centre of Gravity Range .................................................................................................................................... 59 16. Datum ............................................................................................................................................................... 59 17. Control surface deflections ............................................................................................................................... 59 18. Levelling Means ................................................................................................................................................ 60 19. Minimum Flight Crew ....................................................................................................................................... 60 20. Maximum Passenger Seating Capacity ............................................................................................................. 60 21. Baggage / Cargo Compartments ....................................................................................................................... 60 22. Wheels and Tyres .............................................................................................................................................. 60 23. (Reserved) ......................................................................................................................................................... 60

    G.IV. Operating and Service Instructions ....................................................................................................................... 60 1. Flight Manual ........................................................................................................................................................ 60 2. Maintenance manuals ........................................................................................................................................... 61

    G.V. Notes ..................................................................................................................................................................... 61

    SECTION H. TBM700 N equipped with MOD70-0476-00, -0211-57, -0234-24, -0322-00, -0323-71, -0324-00, -0325-21, -0357-71, -0439-79, -0423-34 and -0462-34 ............................................................................................................... 63

    H.I. General .................................................................................................................................................................. 63 1. Type/ Model/ Variant ............................................................................................................................................ 63 2. Airworthiness Category ......................................................................................................................................... 63 3. Manufacturer ........................................................................................................................................................ 63 4. EASA Type Certification Application Date ............................................................................................................. 63 5. EASA Type Certification Date ................................................................................................................................ 63 6. Other informations ................................................................................................................................................ 63

    H.II. EASA Certification Basis ......................................................................................................................................... 63 1. Reference Date for determining the applicable requirements ............................................................................. 63 2. Airworthiness Requirements ................................................................................................................................. 63 3. Special Conditions ................................................................................................................................................. 64 4. Exemptions ............................................................................................................................................................ 64 5. (Reserved) Deviations ........................................................................................................................................... 64 6. Equivalent Safety Findings .................................................................................................................................... 64 7. Requirements elected to comply .......................................................................................................................... 64 8. Environmental Protection ..................................................................................................................................... 65 9. Operational Suitability Data (OSD) ........................................................................................................................ 65

    H.III. Technical Characteristics and Operational Limitations ......................................................................................... 65 1. Type Design Definition .......................................................................................................................................... 65 2. Description ............................................................................................................................................................ 65 3. Equipment ............................................................................................................................................................. 66 4. Operational Suitability Data (OSD) ........................................................................................................................ 66 5. Dimensions ............................................................................................................................................................ 66 6. Engine .................................................................................................................................................................... 66 7. Load factors ........................................................................................................................................................... 66

  • TCDS No.: EASA.A.010 TBM700 Issue: 15 Date: 28 July 2020

    TE.CERT.00048-002 © European Union Aviation Safety Agency, 2019. All rights reserved. ISO9001 Certified. Page 10 of 114 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.

    An agency of the European Union

    8. Propeller ................................................................................................................................................................ 67 9. Fluids ..................................................................................................................................................................... 67 10. Fluid capacities .................................................................................................................................................. 68 11. Air Speeds ......................................................................................................................................................... 68 12. Flight Envelope .................................................................................................................................................. 68 13. Approved Operational Capability ..................................................................................................................... 68 14. Maximum Masses ............................................................................................................................................. 68 15. Centre of Gravity Range .................................................................................................................................... 68 16. Datum ............................................................................................................................................................... 69 17. Control surface deflections ............................................................................................................................... 69 18. Levelling Means ................................................................................................................................................ 69 19. Minimum Flight Crew ....................................................................................................................................... 69 20. Maximum Passenger Seating Capacity ............................................................................................................. 69 21. Baggage / Cargo Compartments ....................................................................................................................... 69 22. Wheels and Tyres .............................................................................................................................................. 70

    H.IV. Operating and Service Instructions ....................................................................................................................... 70 1. Flight Manual ........................................................................................................................................................ 70 2. Maintenance Manual ............................................................................................................................................ 70

    H.V. Notes ..................................................................................................................................................................... 70

    SECTION I. TBM700 N equipped with MOD70-0176-00, -0211-57, -0234-24, -0322-00, -0323-71, -0324-00, -0325-21, -0357-71, -0407-00, -0423-34, -0439-79, -0462-34 and -0539-00 Versions A & B .............................................................. 72

    I.I. General ...................................................................................................................................................................... 72 1. Type/ Model/ Variant ............................................................................................................................................ 72 2. Airworthiness Category ......................................................................................................................................... 72 3. Manufacturer ........................................................................................................................................................ 72 4. EASA Type Certification Application Date ............................................................................................................. 72 5. EASA Type Certification Date ................................................................................................................................ 72 6. Other informations ................................................................................................................................................ 72

    I.II. EASA Certification Basis ......................................................................................................................................... 72 1. Reference Date for determining the applicable requirements ............................................................................. 72 2. Airworthiness Requirements ................................................................................................................................. 72 3. Special Conditions ................................................................................................................................................. 73 4. Exemptions ............................................................................................................................................................ 73 5. (Reserved) Deviations ........................................................................................................................................... 73 6. Equivalent Safety Findings .................................................................................................................................... 73 7. Requirements elected to comply .......................................................................................................................... 73 8. Environmental Protection ..................................................................................................................................... 74 9. Operational Suitability Data (OSD) ........................................................................................................................ 74

    I.III. Technical Characteristics and Operational Limitations ......................................................................................... 74 1. Type Design Definition .......................................................................................................................................... 74 2. Description ............................................................................................................................................................ 74 3. Equipment ............................................................................................................................................................. 75 4. Operational Suitability Data (OSD) ........................................................................................................................ 75 5. Dimensions ............................................................................................................................................................ 75 6. Engine .................................................................................................................................................................... 75 7. Load factors ........................................................................................................................................................... 75 8. Propeller ................................................................................................................................................................ 75 9. Fluids ..................................................................................................................................................................... 76 10. Fluid capacities .................................................................................................................................................. 76 11. Air Speeds ......................................................................................................................................................... 77 12. Flight Envelope .................................................................................................................................................. 77

  • TCDS No.: EASA.A.010 TBM700 Issue: 15 Date: 28 July 2020

    TE.CERT.00048-002 © European Union Aviation Safety Agency, 2019. All rights reserved. ISO9001 Certified. Page 11 of 114 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.

    An agency of the European Union

    13. Approved Operational Capability ..................................................................................................................... 77 14. Maximum Masses ............................................................................................................................................. 77 15. Centre of Gravity Range .................................................................................................................................... 77 16. Datum ............................................................................................................................................................... 77 17. Control surface deflections ............................................................................................................................... 78 18. Levelling Means ................................................................................................................................................ 78 19. Minimum Flight Crew ....................................................................................................................................... 78 20. Maximum Passenger Seating Capacity ............................................................................................................. 78 21. Baggage / Cargo Compartments ....................................................................................................................... 78 22. Wheels and Tyres .............................................................................................................................................. 78 23. (Reserved) ......................................................................................................................................................... 79

    I.IV. Operating and Service Instructions ....................................................................................................................... 79 1. Flight Manual ........................................................................................................................................................ 79 2. Maintenance Manual ............................................................................................................................................ 79

    I.V. Notes ..................................................................................................................................................................... 79

    SECTION J. TBM700 N equipped with MOD70-0476-00, -0211-57, -0234-24, -0322-00, -0323-71, -0324-00, -0325-21, -0357-71, -0439-79, -0423-34, -0462-34 and with -0549-00 Versions A & B ............................................................... 81

    J.I. General ...................................................................................................................................................................... 81 1. Type/ Model/ Variant ............................................................................................................................................ 81 2. Airworthiness Category ......................................................................................................................................... 81 3. Manufacturer ........................................................................................................................................................ 81 4. EASA Type Certification Application Date ............................................................................................................. 81 5. EASA Type Certification Date ................................................................................................................................ 81 6. Other informations ................................................................................................................................................ 81

    J.II. EASA Certification Basis ......................................................................................................................................... 81 1. Reference Date for determining the applicable requirements ............................................................................. 81 2. Airworthiness Requirements ................................................................................................................................. 81 3. Special Conditions ................................................................................................................................................. 82 4. Exemptions ............................................................................................................................................................ 82 5. (Reserved) Deviations ........................................................................................................................................... 82 6. Equivalent Safety Findings .................................................................................................................................... 82 7. Requirements elected to comply .......................................................................................................................... 82 8. Environmental Protection ..................................................................................................................................... 83 9. Operational Suitability Data (OSD) ........................................................................................................................ 83

    J.III. Technical Characteristics and Operational Limitations ......................................................................................... 83 1. Type Design Definition .......................................................................................................................................... 83 2. Description ............................................................................................................................................................ 83 3. Equipment ............................................................................................................................................................. 83 4. Operational Suitability Data (OSD) ........................................................................................................................ 84 5. Dimensions: ........................................................................................................................................................... 84 6. Engine: ................................................................................................................................................................... 84 7. Load factors ........................................................................................................................................................... 84 8. Propeller ................................................................................................................................................................ 84 9. Fluids capacities .................................................................................................................................................... 85 10. Fluid capacities .................................................................................................................................................. 85 11. Air Speeds ......................................................................................................................................................... 86 12. Flight Envelope .................................................................................................................................................. 86 13. Approved Operational Capability ..................................................................................................................... 86 14. Maximum Masses ............................................................................................................................................. 86 15. Centre of Gravity Range .................................................................................................................................... 86 16. Datum ............................................................................................................................................................... 86

  • TCDS No.: EASA.A.010 TBM700 Issue: 15 Date: 28 July 2020

    TE.CERT.00048-002 © European Union Aviation Safety Agency, 2019. All rights reserved. ISO9001 Certified. Page 12 of 114 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.

    An agency of the European Union

    17. Control surface deflections ............................................................................................................................... 87 18. Levelling Means ................................................................................................................................................ 87 19. Minimum Flight Crew ....................................................................................................................................... 87 20. Maximum Passenger Seating Capacity ............................................................................................................. 87 21. Baggage / Cargo Compartments ....................................................................................................................... 87 22. Wheels and Tyres .............................................................................................................................................. 87

    J.IV. Operating and Service Instructions ....................................................................................................................... 88 1. Flight Manual ........................................................................................................................................................ 88 2. Maintenance Manual ............................................................................................................................................ 88

    J.V. Notes ..................................................................................................................................................................... 88

    SECTION K. TBM700 N equipped with MOD70-0176-00, -0211-57, -0234-24, -0322-00, -0323-71, -0324-00, -0325-21, -0357-71, -0407-00, -0423-34, -0439-79, -0462-34, -0539-00 Versions A & B and Version H, -0619-11, -0632-34 and -0570-30 .............................................................................................................................................................. 90

    K.I. General .................................................................................................................................................................. 90 1. Type/ Model/ Variant ............................................................................................................................................ 90 2. Airworthiness Category ......................................................................................................................................... 90 3. Manufacturer ........................................................................................................................................................ 90 4. EASA Type Certification Application Date ............................................................................................................. 90 5. EASA Type Certification Date ................................................................................................................................ 90 6. Other informations ................................................................................................................................................ 90

    K.II. EASA Certification Basis ......................................................................................................................................... 90 1. Reference Date for determining the applicable requirements ............................................................................. 90 2. Airworthiness Requirements ................................................................................................................................. 90 3. Special Conditions ................................................................................................................................................. 91 4. Exemptions ............................................................................................................................................................ 91 5. (Reserved) Deviations ........................................................................................................................................... 91 6. Equivalent Safety Findings .................................................................................................................................... 91 7. Requirements elected to comply .......................................................................................................................... 91 8. Environmental Protection ..................................................................................................................................... 92 9. Operational Suitability Data (OSD) ........................................................................................................................ 92

    K.III. Technical Characteristics and Operational Limitations ......................................................................................... 92 1. Type Design Definition .......................................................................................................................................... 92 2. Description ............................................................................................................................................................ 92 3. Equipment ............................................................................................................................................................. 93 4. Operational Suitability Data (OSD) ........................................................................................................................ 93 5. Dimensions ............................................................................................................................................................ 93 6. Engine .................................................................................................................................................................... 93 7. Load factors ........................................................................................................................................................... 93 8. Propeller ................................................................................................................................................................ 93 9. Fluids ..................................................................................................................................................................... 94 10. Fluid capacities .................................................................................................................................................. 95 11. Air Speeds ......................................................................................................................................................... 95 12. Flight Envelope .................................................................................................................................................. 95 13. Approved Operational Capability ..................................................................................................................... 95 14. Maximum Masses ............................................................................................................................................. 95 15. Centre of Gravity Range .................................................................................................................................... 95 16. Datum ............................................................................................................................................................... 96 17. Control surface deflections ............................................................................................................................... 96 18. Levelling Means ................................................................................................................................................ 96 19. Minimum Flight Crew ....................................................................................................................................... 96 20. Maximum Passenger Seating Capacity ............................................................................................................. 96

  • TCDS No.: EASA.A.010 TBM700 Issue: 15 Date: 28 July 2020

    TE.CERT.00048-002 © European Union Aviation Safety Agency, 2019. All


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