Standard Practice for Design, Alteration, and Certification of Aircraft Electrical Wiring Systems

Importancia y uso:

4.1 Design—The design procedures defined in this practice are intended to provide acceptable guidance in the original design of electrical systems.

4.2 Alteration—The alteration procedures defined in this practice are intended to provide acceptable guidance for modification of general aviation aircraft. Design of any modification shall follow the practices and processes defined in the design sections of this practice.

4.3 Certification—Certification guidance provided in this practice is intended to provide generally accepted procedures and processes for certification of original and modified electrical systems and equipment. Requirements for certification shall be coordinated with the applicable National Aeronautics Association/Civil Aeronautics Administration (NAA/CAA) regulatory agency.

Subcomité:

F39.01

Referida por:

F3231_F3231M-23, F3316_F3316M-19, F2799-14R19, F3060-20

Volúmen:

15.09

Número ICS:

49.060 (Aerospace electric equipment and systems)

Palabras clave:

aircraft; aircraft electrical wiring systems; alteration; aviation; certification; design; helicopter; rotorcraft; rotorcraft electrical wiring systems;