Piper Aircraft, Inc. PA-44-180 (Seminole): certification basis

Basis entries as written on the TCDS

1. REG

   For the basic PA-44-180 (Seminole) aeroplane the applicable certification basis is FAR 23. For details on the applicable FAR 23 amendments see A.V., note 6.

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

2. REG

   For PA-44-180 (Seminole) aeroplanes equipped with the factory installed Avidyne Entegra System option the additional certification basis for installation specific items only is CS-23 (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.

3. REG

   For PA-44-180 (Seminole) aeroplanes equipped with the factory installed Garmin G1000 Integrated Avionics System option the additional certification basis for installation specific items only is CS-23 (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.

4. REG

   For PA-44-180 (Seminole) equipped with the factory installed Garmin GFC700 AFCS option the additional certification basis for installation specific items only is CS-23 (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.

5. REG

   For PA-44-180 (Seminole) aeroplanes equipped with Piper Lycoming IO-360-B1G6 and LIO-360-B1G6 Fuel Injected Engines the additional certification basis for installation specific items only is FAR 23 and 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.

6. REG

   For PA-44-180 (Seminole) aeroplanes equipped with the factory installed Garmin G5 Standby Instrument option

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

7. REG

   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.

8. REG

   For PA-44-180 (Seminole) aeroplanes (see note 12) equipped with halon free hand-held Fire Extinguisher, the additional certification basis for installation is CS-23 (for applicable amendments see A.V., note 12).

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

9. REG

   FAR 23 for the basic PA-44-180 (Seminole) 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.

10. REG

    FAR 23 and CS-23 for PA-44-180 (Seminole) 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.

11. REG

    FAR 23 and CS-23 for PA-44-180 (Seminole) 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.

12. REG

    FAR 23 and CS-23 for PA-44-180 (Seminole) 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.

13. REG

    FAR 23 and CS-23 for PA-44-180 (Seminole) aeroplanes equipped with Piper Lycoming IO-360-B1G6 and LIO- 360-B1G6 Fuel Injected Engines (for applicable amendments see A.V. note 7)

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

14. REG

    FAR 23 and CS-23 for PA-44-180 (Seminole) aeroplanes equipped with the factory installed Garmin G5 Standby Instrument 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.

15. ◆ SPECIAL

    None for the basic PA-44-180 (Seminole) aeroplane.

16. ◆ SPECIAL

    CRI-F01, Protection from the Effects of HIRF, CRI-F02, Protection from the Effects of Lightning Strike; Indirect Effects, CRI-F05, Human Factors in Integrated Avionic Systems, for PA-44-180 (Seminole) aeroplanes equipped with the factory installed Avidyne Entegra System option.

17. ◆ SPECIAL

    CRI B-52, Human Factors in Integrated Avionic Systems, CRI F-66, Synthetic Vision, 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-44-180 (Seminole) aeroplanes equipped with the factory installed Garmin G1000 Integrated Avionics System option, or with Piper factory installed Garmin G1000NXi Phase I as installed by Piper drawing number 107600- 002, or with Piper factory installed Garmin G1000NXi Phase II as installed by Piper drawing number 107600- 002 or 107600-003.

18. ◆ 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-44-180 aeroplanes equipped with the factory installed Garmin GFC700 AFCS option Special condition “Security Protection of Aircraft Systems and Networks” (see annex 1) for aeroplanes equipped with Piper factory installed Garmin G1000NXi Phase I as installed by Piper drawing number 107600-002, or with

19. ◆ SPECIAL

    Piper factory installed Garmin G1000NXi Phase II as installed by Piper drawing number 107600-002 or 107600-003.

20. ◆ SPECIAL

    SC-B23.div-01 (B-52) Human Factors in Integrated Avionic Systems for PA-44-180 (Seminole) aeroplanes equipped with Garmin G5 Standby Instrument

21. ELOS

    FAR 23.1545(a) for the basic PA-44-180 (Seminole) aeroplane (airspeed indicator markings based on IAS instead of CAS).

22. ELOS

    b) CRI-F03, Powerplant Instruments for PA-44-180 (Seminole) aeroplanes equipped with the factory installed Avidyne Entegra System option.

23. ELOS

    c) CRI F-201, Flight Instruments, Stabilized Magnetic Compass, CRI F-203, Power Plant Instruments, Fuel Flow Indication, for PA-44-180 (Seminole) aeroplanes equipped with the factory installed Garmin G1000 Integrated Avionics System option, or with Piper factory installed Garmin G1000NXi Phase I as installed by Piper drawing number 107600-002, or with Piper factory installed Garmin G1000NXi Phase II as installed by Piper drawing number 107600-002 or 107600-003

24. ELOS

    d) None for the factory installed Garmin GFC700 AFCS option

25. ELOS

    e) F-201, Flight Instruments, Stabilized Magnetic Compass, for PA-44-180 (Seminole) aeroplanes equipped with Garmin G5 Standby Instrument

26. OTHER

    ICAO Annex 16, Volume 1 (see TCDSN for further detail)

27. Exemptions: none recorded.