This Aerospace Specification establishes the requirements for a threaded flexible coupling assembly, hereafter referred to as the assembly, which utilizes ferrules or machined tube end fittings to join tubing and components in aircraft fuel, vent, or other systems. This coupling assembly is designed for use from -54 to 93 °C and at 862 kPa peak working pressure. AS coupling components referenced herein have been qualified to AS1710. Ferrule referenced herein are inch ferrules adapted to metric tubing. MA2250 has been reaffirmed to comply with the SAE five-year review policy.
Coupling Fuel, Flexible Variable Cavity, Threaded Type with Ferrules, Metric
2015-08-21
Aufsatz (Konferenz)
Englisch
Coupling, Fuel, Flexible, Variable Cavity, Threaded Type With Ferrules
SAE Technical Papers | 2014
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 | 1982
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