This SAE Aerospace Standard (AS) defines the requirements for a threaded flexible coupling assembly, which utilizes ferrules or machined tube end fittings to join tubing and components in aircraft fuel and fuel vent or other systems. This coupling assembly is designed for use from -65 to +200 °F and at 125 psig peak working pressure, and the coupling assembly may be used in other fluid systems when requirements are within the limits. AS1710D has been reaffirmed to comply with the SAE five-year review policy.
Coupling, Fuel, Flexible, Variable Cavity, Threaded Type With Ferrules
2014-11-25
Aufsatz (Konferenz)
Englisch
COUPLING, FUEL, FLEXIBLE, VARIABLE CAVITY THREADED TYPE WITH FERRULES
SAE Technical Papers | 1982
COUPLING, FUEL, FLEXIBLE, VARIABLE CAVITY, THREADED TYPE WITH FERRULES
SAE Technical Papers | 1984
Coupling, Fuel, Flexible, Variable Cavity, Threaded Type With Ferrules
SAE Technical Papers | 2004
Coupling, Fuel, Flexible, Variable Cavity, Threaded Type With Ferrules
SAE Technical Papers | 2006
Coupling Fuel, Flexible Variable Cavity, Threaded Type with Ferrules, Metric
SAE Technical Papers | 2015