Piper Aircraft, Inc. PA-46-701TP: certification basis
Basis entries as written on the TCDS
-
REG
For the basic PA-46-701TP aeroplane, the applicable certification basis is 14 CFR Part 23 and CS-23. For details on the applicable FAR 23 and CS-23 certification basis see F.V., note 6.
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
-
REG
14 CFR Part 23 and CS-23 for the basic PA-46-701TP aeroplane, (for applicable amendments see F.II.4)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
-
◆ SPECIAL
CRI B-52, Human Factors
-
◆ SPECIAL
CRI B-01, Handling characteristics for high performance aircraft
-
◆ SPECIAL
CRI E-58, Turbine engine installation, rain ingestion
-
◆ SPECIAL
CRI F-601, Security Protection of Aircraft Systems and Networks
-
ELOS
CRI B-101, Longitudinal control forces
-
ELOS
CRI D-601, Material strength properties
-
ELOS
CRI E-601, Fuel flow, no pilot action required after engine start
-
ELOS
CRI E-602, Digital only display of powerplant instruments and omission of coloured caution and normal operating range arcs
-
ELOS
CRI F-606, Flight instruments, stabilized magnetic compass
-
OTHER
ICAO Annex 16, Volume I, Part II, Chapter 10, Amendment 13, in accordance with CS-36, Amdt. 6 ICAO Annex 16, Volume II, Part II, Amendment 10, in accordance with CS-34, Amdt. 4
- Exemptions: none recorded.