Leonardo S.p.A. – Divisione Velivoli C-27J: certification basis

Basis entries as written on the TCDS

1. REG

   JAR 25, Large Aeroplanes, Change 14, Amendment 25/96/1 dated 19 April 1996

   Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.

2. REG

   JAR 1, Definitions, Change 5 dated 15 July 1996 JAR AWO Change 2, effective 01 August 1996

   Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.

3. REG

   Reversions to FAR 25 amdt 35 paragraphs are applicable to C-27J: 25.783 Doors 25.805 Flight crew emergency exits 25.809 Emergency exit arrangement 25.811 Emergency exit marking 25.812 Emergency lighting 25.813 Emergency exit access.

   Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.

4. ◆ SPECIAL

   SC C27J/C-01 Interaction of Systems and Structures CRI C-01 (NPA 25C-199)

5. ◆ SPECIAL

   SC C27J/D-01 Class E Cargo Compartments CRI D-01

6. ◆ SPECIAL

   SC C27J/E-01 Propeller Reversing System CRI E-01

7. ◆ SPECIAL

   SC C27J/F-05 Electronic Hardware Design Assurance CRI F-05

8. ◆ SPECIAL

   SC C27J/F-01 Protection from Effects of HIRF CRI F-01 (INT/POL/25/2 Iss 2)

9. ◆ SPECIAL

   SC C27J/F-08 Flight in Icing Conditions CRI F-08 (NPA 25F-219)

10. ◆ SPECIAL

    SC C27J/F-10 Severe Icing Conditions CRI F-10 (INT/POL/25/11)

11. ◆ SPECIAL

    SC C-27J/H-01 Enhanced Airworthiness Programme for CRI H-01 Aeroplane System – ICA on EWIS

12. EXEMPT

    JAR 25.841 (a) Max cabin altitude 8000 ft CRI D-02

13. EXEMPT

    JAR 25.841 (b)(6) Max cabin altitude warning at 10000 ft CRI D-02

14. ELOS

    JAR 25.779 (b)(2) Motion and effect of emergency landing gear control CRI D-03

15. ELOS

    JAR 25.791(b) Passenger information signs CRI D-04

16. ELOS

    JAR 25.1093 (b) Air intake system Ice Protection CRI E-02

17. ELOS

    JAR 25A.1193(e)(3) Cowling and nacelle skin CRI J-02

18. ELOS

    JAR 25.1305 (e)(1) Torque indicator CRI F-12

19. ELOS

    JAR 25A1549 APU Instruments–Marking and Placards CRI J-03

20. REG

    The following paragraphs of FAR 25 are elected to comply: FAR 25.307 (a) Proof of structure amdt 25-87 FAR 25.631 Bird Strike Damage amdt 25-87 FAR 25.562 Emergency landing dynamic conditions amdt 25-87 FAR 25.671 (c)(1) Control Systems amdt 25-87 FAR 25.831 (g) Ventilation amdt 25-87 FAR 25.856 (a) Thermal Acoustic amdt 25-111 FAR 25.981 (b)(d) Fuel Tank Ignition Prevention amdt 25-125

    Elect to Comply

    Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.

21. OTHER

    Noise: ICAO Annex 16, Volume I, Chapter 3 See EASA Type Certificate Data Sheet for Noise (TCDSN) EASA.A.407

22. OTHER

    Fuel venting and emissions: ICAO Annex 16, Volume II