Baykar Piaggio Aerospace S.p.A. Avanti: certification basis

Basis entries as written on the TCDS

1. REG

   RAI Regolamento Tecnico Part 223, including amendments 223-1 through 223-33, correspondent to FAR 23, effective February 1st 1965, including amendments 23-1 through 23-33

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

2. REG

   JAR AWO Subpart 2, Change 2, dated August 1st 1996

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

3. REG

   RVSM specific requirements included in the JAA Leaflet n. 6 rev.1 and in the FAA Interim Guidance Material 91 – RVSM, Ch. 1

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

4. REG

   as above, except CS-23 requirements (first issue) applicable to the areas affected by the change (see Appendix 2 – MTOW Increased Major Change (80-0642) CRI A-01).

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

5. REG

   Special Federal Aviation Regulations n. 27, effective 1st February 1974, including amendments 27-1 through 27-5.

   Requirements elected to comply

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

6. REG

   FAR 23.2, amendment 36.

   Requirements elected to comply

   Includes 14 CFR 23 §23.2 through 23-36 · current is 23-63, 25 revisions later

   Expands to 1 provision link · shown below

7. REG

   FAR 91 Appendix A dated August 18, 1989. Applicable JAR 23 (first issue dated March 11, 1994) requirements for the following modifications 80-0228 “Vertical fin - aluminum alloy instead of composite” 80-0229 “Aluminum canard wing instead of composite” 80-0241 “Aluminum rudder and trim tab”

   Requirements elected to comply

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

8. REG

   and for the relevant Service Bulletins: 80-0106 “Replacement of the Composite Forward Wing Assembly with the new metallic one” 80-0142 “Replacement of the Composite Material Tail- cone/Vertical Fin Assembly, with the Metal Construction Assembly, in the event of not repairable damages”

   Requirements elected to comply

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

9. REG

   14 CFR Part 36, effective 1st Dec. 1969, including amendments 36-1 through 36-16. EASA Certification Specifications CS-23, dated 23/11/2003, paragraph 23.1529.

   Requirements elected to comply

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

10. ◆ SPECIAL

    Issue Paper Special Condition

    Applies to: Special Conditions enclosed to the RAI paper n. 257.240/SCMA dated July 21, 1989 (Docket n. 031 CE, Special Conditions n. 23-ACE-29, and Special Condition FAA n. 23-ACE-52) which include the following Issue Papers

11. ◆ SPECIAL

    C-1 Composite Structures Fatigue/Damage Tolerance 23-ACE-29 No. 4

    Applies to: Special Conditions enclosed to the RAI paper n. 257.240/SCMA dated July 21, 1989 (Docket n. 031 CE, Special Conditions n. 23-ACE-29, and Special Condition FAA n. 23-ACE-52) which include the following Issue Papers

12. ◆ SPECIAL

    C-2 Full Scale Airload Verification 23-ACE-29 No. 5

    Applies to: Special Conditions enclosed to the RAI paper n. 257.240/SCMA dated July 21, 1989 (Docket n. 031 CE, Special Conditions n. 23-ACE-29, and Special Condition FAA n. 23-ACE-52) which include the following Issue Papers

13. ◆ SPECIAL

    C-3 Doors and Exits (Outward Opening) 23-ACE-29 No. 6

    Applies to: Special Conditions enclosed to the RAI paper n. 257.240/SCMA dated July 21, 1989 (Docket n. 031 CE, Special Conditions n. 23-ACE-29, and Special Condition FAA n. 23-ACE-52) which include the following Issue Papers

14. ◆ SPECIAL

    C-4 Lightning Protection of Composite Structure 23-ACE-29 No. 4

    Applies to: Special Conditions enclosed to the RAI paper n. 257.240/SCMA dated July 21, 1989 (Docket n. 031 CE, Special Conditions n. 23-ACE-29, and Special Condition FAA n. 23-ACE-52) which include the following Issue Papers

15. ◆ SPECIAL

    C-6 Forward and Main Wing Flap Interconnection 23-ACE-29 No. 7

    Applies to: Special Conditions enclosed to the RAI paper n. 257.240/SCMA dated July 21, 1989 (Docket n. 031 CE, Special Conditions n. 23-ACE-29, and Special Condition FAA n. 23-ACE-52) which include the following Issue Papers

16. ◆ SPECIAL

    C-7 Loads for P180 Configuration 23-ACE-29 No. 5

    Applies to: Special Conditions enclosed to the RAI paper n. 257.240/SCMA dated July 21, 1989 (Docket n. 031 CE, Special Conditions n. 23-ACE-29, and Special Condition FAA n. 23-ACE-52) which include the following Issue Papers

17. ◆ SPECIAL

    F-1 Buffet Onset Envelope 23-ACE-29 No. 1

    Applies to: Special Conditions enclosed to the RAI paper n. 257.240/SCMA dated July 21, 1989 (Docket n. 031 CE, Special Conditions n. 23-ACE-29, and Special Condition FAA n. 23-ACE-52) which include the following Issue Papers

18. ◆ SPECIAL

    F-2 Effect of Rain or Contamination on Laminar Flow Airfoils 23-ACE-29 No. 3

    Applies to: Special Conditions enclosed to the RAI paper n. 257.240/SCMA dated July 21, 1989 (Docket n. 031 CE, Special Conditions n. 23-ACE-29, and Special Condition FAA n. 23-ACE-52) which include the following Issue Papers

19. ◆ SPECIAL

    F-5 Inadvertent Excursion Beyond Maximum Operating Speed 23-ACE-29 No. 2

    Applies to: Special Conditions enclosed to the RAI paper n. 257.240/SCMA dated July 21, 1989 (Docket n. 031 CE, Special Conditions n. 23-ACE-29, and Special Condition FAA n. 23-ACE-52) which include the following Issue Papers

20. ◆ SPECIAL

    P-6 Propeller Ground Clearance 23-ACE-29 No. 8

    Applies to: Special Conditions enclosed to the RAI paper n. 257.240/SCMA dated July 21, 1989 (Docket n. 031 CE, Special Conditions n. 23-ACE-29, and Special Condition FAA n. 23-ACE-52) which include the following Issue Papers

21. ◆ SPECIAL

    P-7 Propeller marking 23-ACE-29 No. 9

    Applies to: Special Conditions enclosed to the RAI paper n. 257.240/SCMA dated July 21, 1989 (Docket n. 031 CE, Special Conditions n. 23-ACE-29, and Special Condition FAA n. 23-ACE-52) which include the following Issue Papers

22. ◆ SPECIAL

    P-8 Propeller Ice Protection and Exhaust Gas Impingement 23-ACE-29 No. 10

    Applies to: Special Conditions enclosed to the RAI paper n. 257.240/SCMA dated July 21, 1989 (Docket n. 031 CE, Special Conditions n. 23-ACE-29, and Special Condition FAA n. 23-ACE-52) which include the following Issue Papers

23. ◆ SPECIAL

    SE-4 Cockpit Smoke Evacuation 23-ACE-29 No. 11

    Applies to: Special Conditions enclosed to the RAI paper n. 257.240/SCMA dated July 21, 1989 (Docket n. 031 CE, Special Conditions n. 23-ACE-29, and Special Condition FAA n. 23-ACE-52) which include the following Issue Papers

24. ◆ SPECIAL

    SE-5 Protection for Systems from Lightning and High Energy Radio Frequency (HERF) 23-ACE-52 No. 2

    Applies to: Special Conditions enclosed to the RAI paper n. 257.240/SCMA dated July 21, 1989 (Docket n. 031 CE, Special Conditions n. 23-ACE-29, and Special Condition FAA n. 23-ACE-52) which include the following Issue Papers

25. ELOS

    23.1305(g) Fuel pressure indication

26. ELOS

    23.1545(b)(5) Marking of Air Speed

27. ELOS

    Indicator for VYSE

28. OTHER

    Noise: ICAO Annex 16,Ed. 1988, Vol. I, Chapter 10. [Airplanes incorporating the optional Mod. n. 80-0642 or SB 80-0215: ICAO Annex 16, Ed. 1993, Amdt. 7, Vol. I, Chapter 10/EASA-CS 36 (see Appendix 2 – MTOW Increased Major Change (80- 0642) CRI A-01)] Emissions: ICAO Annex 16, Ed. 1993, Vol. II, Part II, Chapter 2 (fuel venting).

29. Exemptions: none recorded.