Standard Practice for Aeroplane Turbine Fuel System Hot Weather Operations

Importancia y uso:

4.1 This specification provides designers of general aviation aeroplanes a process for evaluating and testing a fuel system under hot weather conditions to ensure safety during flight. The specification is applicable to kerosene-type turbine engine fuels and fuel systems for traditional general aviation aeroplanes.

Subcomité:

F44.40

Referida por:

F3063_F3063M-24, F3264-24

Volúmen:

15.09

Número ICS:

75.160.20 (Liquid fuels)

Palabras clave:

cavitation; fuel system testing; heat rejection; hot fuel; hot weather operation; hot weather testing; turbine fuel hot weather; turbine fuel testing; vapor formation; vapor lock;