Piper Aircraft, Inc. PA-28-181 (Archer III): certification basis
Basis entries as written on the TCDS
-
REG
For the basic PA-28-181 (Archer III) aeroplane the applicable certification basis is CAR 3 and FAR 23. For details on the applicable CAR 3 and 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.
-
REG
For PA-28-181 (Archer III) 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 Avidyne, 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.
-
REG
For PA-28-181 (Archer III) 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 1, 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.
-
REG
For PA-28-181 (Archer III) aeroplanes equipped with the factory installed Garmin G1000 NXI phase I and II the additional certification basis for installation specific items only is CS-23 as defined in CRI A-01 Annex A04 (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.
-
REG
For PA-28-181 (Archer III) aeroplanes equipped with the factory installed Lycoming IO-360-B4A engine the additional certification basis for installation specific items only is CS-23 as defined in CRI A-01 Annex A05 (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.
-
REG
For PA-28-181 (Archer III) aeroplanes equipped with the factory installed Garmin G5 Standby Instrument option and G3X avionics (see note 10) 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.
-
REG
For PA-28-181 (Archer III) aeroplanes equipped with main wing spar assembly defined by Piper drawing 28W57A013, 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.
-
REG
For PA-28-181 (Archer III) aeroplanes (see note 10) with the hand-held halon free Fire Extinguisher, the additional certification basis for installation is CS-23 (for applicable amendments see A.V., note 11).
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
-
REG
For PA-28-181 (Archer III) aeroplanes with factory installed Garmin G1000NXi Integrated Avionics that incorporate System Software Release 7, 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.
-
REG
CAR 3 and FAR 23 for the basic PA-28-181 (Archer III) 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.
-
REG
CAR 3 and FAR 23 and CS-23 for PA-28-181 (Archer III) 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.
-
REG
CAR 3 and FAR 23 and CS-23 for PA-28-181 (Archer III) 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.
-
REG
CAR 3 and FAR 23 and CS-23 for PA-28-181 (Archer III) aeroplanes equipped with the factory installed Garmin G1000 NXI (phase I and phase II & GFC700 AFCS)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
-
REG
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.
-
REG
CAR 3 and FAR 23 and CS-23 for PA-28-181 (Archer III) aeroplanes equipped with the factory installed Lycoming
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
-
REG
IO-360-B4A engine 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.
-
REG
CAR 3 and FAR 23 and CS-23 for PA-28-181 (Archer III) aeroplanes equipped with the factory installed Garmin G5 Standby Instrument option and G3X avionics (see note 10)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
-
REG
(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.
-
REG
CAR 3 and 14 CFR 23 and CS-23 for PA-28-181 Archer III aeroplanes with Garmin G1000NXi Integrated Avionics that incorporate System Software Release 7 (for applicable amendments see A.II.4.g).
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
-
◆ SPECIAL
None for the basic PA-28-181 (Archer III) aeroplane.
-
◆ SPECIAL
CRI-F01, Protection from the Effects of HIRF, CRI-F02, Protection from the Effects of Lightning Strike; Indirect Effects,
-
◆ SPECIAL
CRI-F05, Human Factors in Integrated Avionic Systems, for PA-28-181 (Archer III) aeroplanes equipped with the factory installed Avidyne Entegra System option.
-
◆ SPECIAL
CRI B-52, 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), PA-28-181 (Archer III) aeroplanes equipped with the factory installed Garmin G1000 Integrated Avionics System option.
-
◆ SPECIAL
SC-B23.div-01 (B-52), 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
-
◆ SPECIAL
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-28-181 (Archer III) aeroplanes equipped with the factory installed Garmin G1000 NXI (Phase I and Phase II). In addition CRI F-14 Electronic Stability and Protection (ESP) only for aeroplanes equipped with G1000 phase II option and the autopilot GFC-700.
-
◆ SPECIAL
SC-B23.div-01 (B-52) Human Factors in Integrated Avionic Systems for PA-28-181 (Archer III) aeroplanes equipped with Garmin G5 Standby Instrument and G3X avionics (see note 10).
-
ELOS
None for the basic PA-28-181 (Archer III) aeroplane
-
ELOS
CRI-F03, Powerplant Instruments for PA-28-181 (Archer III) aeroplanes equipped with the factory installed Avidyne Entegra System option.
-
ELOS
CRI F-201, Flight Instruments, Stabilized Magnetic Compass, CRI F-203, Power Plant Instruments, Fuel Flow Indication, for PA-28-181 (Archer III) aeroplanes equipped with the factory installed Garmin G1000 Integrated Avionics System option.
-
ELOS
CRI F-201, Flight Instruments, Stabilized Magnetic Compass, CRI F-203, Power Plant Instruments, Fuel Flow Indication, for PA-28-181 (Archer III) aeroplanes equipped with the factory installed Garmin G1000 NXI (Phase I and Phase II)
-
ELOS
F-201, Flight Instruments, Stabilized Magnetic Compass, for PA-28-181 (Archer III) for PA-28-181 (Archer III) aeroplanes equipped with the factory installed Garmin G5 Standby Instrument
-
OTHER
ICAO Annex 16, Volume 1, Chapter 10
- Exemptions: none recorded.