Piper Aircraft, Inc. PA-46R-350T: certification basis

Basis entries as written on the TCDS

1. REG

   For those portions of the aeroplane that are unchanged from the basic PA-46-350P the applicable certification basis is FAR Part 23, effective 1 February 1965, as amended by Amendment 23-25, effective 6 March 1980; FAR 25.783(e) as amended by Amendment 25-54, effective 14 October 1980; FAR 25.831(c) and (d) as amended by Amendment 25-41, effective 1 September 1977.

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

2. REG

   No equivalent safety findings.

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

3. ◆ SPECIAL

   Special Conditions No. 23-ACE-53, Docket No. 082CE.

4. REG

   a) For changed areas (Avidyne Entegra and PA-46R-350T specific areas) the certification basis is CS-23 as defined in CRI-A01, issue 5, or later revision (for details on applicable paragraphs see D.V., note 6 and 7).

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

5. REG

   b) For PA-46R-350T aeroplanes equipped with the factory installed G1000 integrated avionics and GFC700 AFCS option the additional certification basis for installation specific items only is CS-23 as defined in CRI-A01, issue 5, or later revision (for details on applicable paragraphs see D.V., note 9).

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

6. REG

   c) For PA-46R-350T aeroplanes equipped with the factory installed HC-I3Y1R-1N/N7605+2, N7605C+2, N7605K+2 or N7605CK+2 propeller the additional certification basis for installation specific items only is CS-23 as defined in CRI-A01, issue 5, or later (for details on applicable paragraphs see D.V., note 10)

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

7. REG

   a) FAR 23 and CS-23 for PA-46R-350T aeroplanes (for applicable amendments see D.II.4.a))

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

8. REG

   b) FAR 23 and CS-23 for PA-46R-350T aeroplanes equipped with the factory installed G1000 integrated avionics and GFC700 AFCS option (for applicable amendments see D.II.4.b))

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

9. REG

   c) FAR 23 and CS-23 for PA-46R-350T aeroplanes equipped with the factory installed HC-I3Y1R-1N/N7605K+2, N7605C+2, N7605K+2 or N7605CK+2 propeller (for applicable amendments see D.II.4.c and D.V.10))

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

10. ◆ SPECIAL

    CRI F-01, Protection from the Effects of HIRF

11. ◆ SPECIAL

    CRI F-02, Protection from the Effects of Lightning Strike; Indirect Effects, CRI F-05, Human Factors in Integrated Avionic Systems,

12. ◆ SPECIAL

    CRI-F01, issue 3 or later revision, Protection from the Effects of HIRF

13. ◆ SPECIAL

    CRI-F02, issue 3 or later revision, Protection from the Effects of Lightning Strike; Indirect Effects, CRI-F05, issue 3 or later revision, Human Factors in Integrated Avionic Systems, for PA-46R-350T aeroplanes equipped with the factory installed G1000 integrated avionics and GFC700 AFCS option.

14. ELOS

    CRI F-03, Powerplant Instruments

15. ELOS

    CRI-F03, issue 2 or later revision, Powerplant Instruments, for PA-46R-350T aeroplanes equipped with the factory installed G1000 integrated avionics and GFC700 AFCS option.

16. OTHER

    ICAO Annex 16, Volume 1, Chapter 10

17. OTHER

    ICAO Annex 16, Volume 1, Chapter 10, Amendment 9, if equipped with HC-I3Y1R-1N/N7605+2, N7605C+2, N7605K+2 or N7605CK+2 propeller (3-bladed)

18. Exemptions: none recorded.