Piper Aircraft, Inc. PA-32R-301 Saratoga II HP: certification basis
/aircraft/easa/EASA.IM.A.239/pa-32r-301-saratoga-ii-hp/basis.csv
Basis entries as written on the TCDS
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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.
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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.
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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.
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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.
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◆ SPECIAL
None for the basic PA-32R-301 Saratoga II HP aeroplane
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◆ SPECIAL
CRI-F01, Protection from the Effects of HIRF
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◆ SPECIAL
CRI-F02, Protection from the Effects of Lightning Strike; Indirect Effects, CRI-F05, Human Factors in Integrated Avionic Systems,
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◆ SPECIAL
for PA-32R-301 Saratoga II HP aeroplanes equipped with the factory installed Avidyne Entegra System option
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ELOS
CAR 3.757, CAR 3.777 for the basic PA-32R-301 Saratoga II HP aeroplane
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ELOS
CRI-F03, Powerplant Instruments for PA-32R-301 Saratoga II HP aeroplanes equipped with the factory installed Avidyne Entegra System option
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OTHER
ICAO Annex 16, Volume 1, Chapter 6
- Exemptions: none recorded.