Standard Test Method for Freezing Point of Aviation Fuels
Importancia y uso:
4.1 The freezing point of an aviation fuel is the lowest temperature at which the fuel remains free of solid hydrocarbon crystals that can restrict the flow of fuel through filters if present in the fuel system of the aircraft. The temperature of the fuel in the aircraft tank normally falls during flight depending on aircraft speed, altitude, and flight duration. The freezing point of the fuel must always be lower than the minimum operational tank temperature.
4.2 Freezing point is a requirement in Specifications D910, D1655, and D7566.
Subcomité:
D02.07
Referida por:
D1655-25, D7153-22AE01, D7547-23, D7566-25, D3699-25, D7153-22AE01, D6615-25, D0910-24, D6227-24A, D8603-25, D5972-25, D7223-21, D8631-25, D5972-25, D8147-24, D7154-15R21E01, D7154-15R21E01, D7719-21A, D8615-25, D8434-21, D7153-22AE01, D4054-25, D7960-21, D7826-25A, D8164-21
Volúmen:
05.01
Número ICS:
75.160.20 (Liquid fuels)
Palabras clave:
aviation gasoline; aviation turbine fuels; crystallization point; determination; freezing point; low temperature tests; manual method; petroleum products; physical tests;
$ 1,246
Norma
D2386
Versión
25a
Estatus
Active
Clasificación
Test Method
Fecha aprobación
2025-10-01
