Standard Practice for Structural Compliance of Very Light Aeroplanes

Importancia y uso:

4.1 The purpose of this practice is to establish simplified methods that can be used to satisfy the materials, processes, and methods of fabrication requirements of Specification F3114 and the fatigue strength evaluation requirements of Specification F3115 for very light aeroplanes as defined in 1.1.

4.2 EASA CM-S-006 provides additional guidance regarding the relevant requirements for aeroplanes defined in 1.1.

Subcomité:

F44.30

Referida por:

F3264-24, F3115_F3115M-23

Volúmen:

15.09

Número ICS:

49.020 (Aircraft and space vehicles in general)

Palabras clave:

composite light aircraft; composite structures; normal category; small aeroplane; small airplane;