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

Basis entries as written on the TCDS

1. REG

   For the basic PA-46-350P aeroplane 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;

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

2. REG

   FAR 25.831(c) and (d) as amended by Amendment 25- 41, effective 1 September 1977; For PA-46-350P aeroplanes equipped with the factory installed Avidyne Entegra System the additional certification basis for installation specific items only is CS-23 as defined in CRI-A01, issue 1, or later revision (for details on applicable paragraphs see B.V., note 7). For PA-46-350P 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 B.V., note 9). For PA-46-350P aeroplanes equipped with the factory installed HC-I3Y1R-1N/N7605C+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 revision (for details on applicable paragraphs see B.V., note 10).

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

3. REG

   For PA-46-350P aeroplanes equipped with the factory installed G1000 Phase III option the additional certification basis for installation specific items only is CS-23 as defined in CRI-A01 (for details on applicable paragraphs see B.V., note 11). For PA-46-350P aeroplanes equipped with the factory installed G1000 NXI Integrated Avionics, the additional certification basis for installation specific items only is CS-23 as defined in CRI-A01 (for details on applicable paragraphs see B.V., note 12). For PA-46-350P aeroplanes with G1000NXi Integrated Avionics that incorporate Landing Gear Warning Inhibit and GDL 60, the additional certification basis for installation is CS-23 (for applicable amendments see B.V., note 14) For PA-46-350P aeroplanes equipped with hand-held halon free Fire Extinguisher, the additional certification basis for installation is CS-23 (for applicable amendments see B.V., note 15)

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

4. REG

   FAR 23 for the basic PA-46-350P aeroplane (for applicable amendments see B.II.4.a))

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

5. REG

   FAR 23 and CS-23 for PA-46-350P aeroplanes equipped with the factory installed Avidyne Entegra System (for applicable amendments see B.II.4.b))

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

6. REG

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

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

7. REG

   FAR 23 and CS-23 for PA-46-350P aeroplanes equipped with the factory installed HC- -I3Y1R-1N/N7605C+2 or N7605CK+2 propeller (for applicable amendments see B.II.4.d))

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

8. REG

   FAR 23 and CS-23 for PA-46-350P aeroplanes equipped with the factory installed G1000 Phase III option (for applicable amendments see B.II.4.e)

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

9. REG

   FAR 23 and CS-23 for PA-46-350P aeroplanes equipped with the factory installed G1000 NXI Integrated Avionics option (for applicable amendments see B.II.4.f)

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

10. REG

    14 CFR 23 and CS-23 for PA-46-350P aeroplanes with Garmin G1000NXi Integrated Avionics that incorporate Landing Gear Warning Inhibit and GDL 60 (for applicable amendments see B.II.4.g)

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

11. ◆ SPECIAL

    No. 23-ACE-53, Docket No. 082CE, for the basic

12. ◆ SPECIAL

    PA-46-350P aeroplane, CRI-F01, Protection from the Effects of HIRF

13. ◆ SPECIAL

    CRI-F02, Protection from the Effects of Lightning Strike; Indirect Effects, CRI-F05, Human Factors in Integrated Avionic Systems, for PA-46-350P aeroplanes equipped with the factory installed Avidyne Entegra System

14. ◆ SPECIAL

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

15. ◆ 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-46-350P aeroplanes equipped with the factory installed G1000 integrated avionics and GFC700 AFCS option.

16. ◆ SPECIAL

    CRI F-14 Electronic Stability and Protection (ESP), FAR 23.1306, Amdt. 23-61, Protection of the effects of lightning strike, indirect effects (formerly CRI F-54), FAR 23.1308(a)(b)(c), Amdt. 23-61, Protection of the effects of HIRF (formerly CRI F-52), for PA-46-350P aeroplanes equipped with the factory installed Garmin G1000 Phase III option

17. ◆ SPECIAL

    CRI F-14 Electronic Stability and Protection (ESP), CRI-F05, issue 3 or later revision, Human Factors in Integrated Avionic Systems, FAR 23.1306, Amdt. 23-61, Protection of the effects of lightning strike, indirect effects (formerly CRI F-54), FAR 23.1308(a)(b)(c), Amdt. 23-61, Protection of the effects of HIRF (formerly CRI F-52), CRI F-90, Security Protection of Aircraft Systems and Networks For PA-46-350P aeroplanes equipped with the factory installed Garmin G1000 NXI Integrated Avionics

18. ELOS

    None for the basic PA-46-350P aeroplane, CRI-F03, Power Plant Instruments, for PA-46-350P aeroplanes equipped with the factory installed Avidyne Entegra System

19. ELOS

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

20. ELOS

    CRI F-201, Flight Instruments, Stabilized Magnetic Compass, CRI F-203, Power Plant Instruments, Fuel Flow Indication, for PA-46-350P (Malibu Meridian) aeroplanes equipped with the factory installed Garmin G1000 Phase III option

21. ELOS

    CRI F-201, Flight Instruments, Stabilized Magnetic Compass, CRI F-203, Power Plant Instruments, Fuel Flow Indication, for PA-46-350P (Malibu Meridian) aeroplanes equipped with the factory installed Garmin G1000 NXI Integrated Avionics

22. OTHER

    ICAO Annex 16, Volume 1, Chapter 6 if equipped with HC-I2YR-1BF/F8074 propeller (2-bladed)

23. OTHER

    ICAO Annex 16, Volume 1, Chapter 10 if equipped with HC-I3YR-1E/7890K propeller (3-bladed)

24. OTHER

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

25. Exemptions: none recorded.