Piper Aircraft, Inc. PA-34-220T: certification basis

Basis entries as written on the TCDS

1. REG

   For the basic PA-34-220T (Seneca V) aeroplane the applicable certification basis is FAR 23. For details on the applicable FAR 23 amendments see A.V., note 6. For PA-34-220T (Seneca V) aeroplanes equipped with the factory installed Avidyne Entegra System option 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 A.V., note 7). For PA-34-220T (Seneca V) aeroplanes equipped with the factory installed Garmin G600/GNS430W/GWX68 and KTA-870 option the additional certification basis for installation specific items only is CS-23 as defined in CRI-A01-G600, release1, issue 1, or later revision (for details on applicable paragraphs see A.V., note 7). For PA-34-220T (Seneca V) aeroplanes equipped with the factory installed Garmin G1000 Integrated Avionics System option the additional certification basis for installation specific items only is CS-23 as defined in CRI A-01 G1000, issue 2, or later revision (for details on applicable paragraphs see A.V., note 7).

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

2. REG

   For PA-34-220T (Seneca V) aeroplanes equipped with the factory installed Garmin GFC700 AFCS option the additional certification basis for installation specific items only is CS-23 as defined in CRI-A01 (for details on applicable paragraphs see A.V., note 7). For PA-34-220T (Seneca V) aeroplanes equipped with the Piper factory installed optional Garmin International G1000NXi Phase I/II installed in accordance with Piper Top Drawing 107200-004, the additional certification basis for installation specific items only is CS-23 as defined in A.V. note 7).

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

3. REG

   FAR 23 for the basic PA-34-220T (Seneca V) aeroplane (for applicable amendments see A.II.4)

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

4. REG

   FAR 23 and CS-23 for PA-34-220T (Seneca V) aeroplanes equipped with the factory installed Avidyne Entegra System option (for applicable amendments see A.II.4)

   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-34-220T (Seneca V) aeroplanes equipped with the factory installed Garmin G600/GNS430W/GWX68 and KTA-870 option (for applicable amendments see A.II.4)

   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-34-220T (Seneca V) aeroplanes equipped with the factory installed Garmin G1000 Integrated Avionics System option (for applicable amendments see A.II.4)

   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-34-220T (Seneca V) aeroplanes equipped with the factory installed Garmin GFC700 AFCS option (for applicable amendments see A.II.4)

   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-34-220T (Seneca V) aeroplanes equipped with the Piper factory installed optional Garmin International G1000NXi Phase I/II installed in accordance with Piper Top Drawing 107200-004 (for applicable amendments see A.II.4)

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

9. ◆ SPECIAL

   None for the basic PA-34-220T (Seneca V) aeroplane.

10. ◆ SPECIAL

    CRI-F01, Protection from the Effects of HIRF

11. ◆ SPECIAL

    CRI-F02, Protection from the Effects of Lightning Strike; Indirect Effects, CRI-F05, Human Factors in Integrated Avionic Systems, for PA-34-220T (Seneca V) aeroplanes equipped with the factory installed Avidyne Entegra System option. Special Condition SC-B23.div-01 “Human Factors in Integrated Avionic Systems“ (see Annex 1, Ref. CRI B- 52), CRI-F52, Protection from the Effects of HIRF

12. ◆ SPECIAL

    CRI-F54, Protection from the Effects of Lightning Strike; Indirect Effects, CRI-F66, Synthetic Vision, for PA-34-220T (Seneca V) aeroplanes equipped with the factory installed Garmin G600 option. Special Condition SC-B23.div-01 “Human Factors in Integrated Avionic Systems“ (see Annex 1, Ref. CRI B- 52),

13. ◆ SPECIAL

    CRI F-66, Synthetic Vision, FAR 23.1308(a)(b)(c), Amdt. 23-61, Protection of the effects of HIRF (formerly CRI F-52), FAR 23.1306, Amdt. 23-61, Protection of the effects of lightning strike, indirect effects (formerly CRI F-54), for PA-34-220T (Seneca V) aeroplanes equipped with the factory installed Garmin G1000 Integrated Avionics System option. Special Condition SC-B23.div-01 “Human Factors in Integrated Avionic Systems“ (see Annex 1, Ref. CRI B- 52), Special condition “Security Protection of Aircraft Systems and Networks” (see Annex 1, Ref. CRI F-90) For PA-34-220T (Seneca V) aeroplanes equipped with the Piper factory installed optional Garmin International G1000NXi Phase I/II installed in accordance with Piper Top Drawing 107200-004

14. ◆ 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-34-220T (Seneca V) aeroplanes equipped with the factory installed Garmin GFC700 AFCS option

15. ELOS

    None for the basic PA-34-220T (Seneca V) aeroplane.

16. ELOS

    CRI-F03, Powerplant Instruments for PA-34-220T (Seneca V) aeroplanes equipped with the factory installed Avidyne Entegra System option.

17. ELOS

    c) None for the factory installed G600 option

18. ELOS

    d) FAR 23.1303(c), Amdt. 23-62, Use of a stabilized magnetic compass as minimum flight instrumentation, for the factory installed G1000 Integrated Avionics System option

19. ELOS

    e) None for the factory installed Garmin GFC700 AFCS option

20. ELOS

    f) ESF for CS 23.1305 (b)(4) “powerplant instruments, fuel flow indication” (see Annex 1, Ref. CRI F-203), ESF for CS 23.1303 (c) “FLIGHT INSTRUMENTS, Stabilized Magnetic Compass” (see Annex 1, Ref. CRI

21. ELOS

    F-201) for PA-34-220T (Seneca V) aeroplanes equipped with the Piper factory installed optional Garmin International G1000NXi Phase I/II installed in accordance with Piper Top Drawing 107200-004

22. OTHER

    ICAO Annex 16, Volume 1, Chapter 10

23. Exemptions: none recorded.