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Piper Aircraft, Inc. PA-32R-301 Saratoga II HP: certification basis

TCDS EASA.IM.A.239 revision 1 (6 Apr 2009) · Normal · EASA · Source TCDS

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Basis entries as written on the TCDS

  1. REG

    For the basic PA-32R-301 Saratoga II HP aeroplane the applicable certification basis is based on CAR 3 and FAR23 (for details on the applicable amendments and paragraphs see A.V., note 5).

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

  2. REG

    For PA-32R-301 Saratoga II HP aeroplanes equipped with the factory installed Avidyne Entegra System option the additional certification basis for installation specific items only is defined in CRI-A01 (for details on applicable paragraphs see A.V., note 6).

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

  3. REG

    CAR 3 and FAR 23 for the basic PA-32R-301 Saratoga II HP 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

    CAR 3, FAR 23 and JAR-23 for PA-32R-301 Saratoga II HP 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. ◆ SPECIAL

    None for the basic PA-32R-301 Saratoga II HP aeroplane

  6. ◆ SPECIAL

    CRI-F01, Protection from the Effects of HIRF

  7. ◆ SPECIAL

    CRI-F02, Protection from the Effects of Lightning Strike; Indirect Effects, CRI-F05, Human Factors in Integrated Avionic Systems,

  8. ◆ SPECIAL

    for PA-32R-301 Saratoga II HP aeroplanes equipped with the factory installed Avidyne Entegra System option

  9. ELOS

    CAR 3.757, CAR 3.777 for the basic PA-32R-301 Saratoga II HP aeroplane

  10. ELOS

    CRI-F03, Powerplant Instruments for PA-32R-301 Saratoga II HP aeroplanes equipped with the factory installed Avidyne Entegra System option

  11. OTHER

    ICAO Annex 16, Volume 1, Chapter 6

  12. Exemptions: none recorded.
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