SAE AS1710, revision B

Coupling, Fuel, Flexible, Variable Cavity Threaded Type With Ferrules

Month of publication: 1992-07-01

Date reaffirmed: May 2004

Developed by committee: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

Annotation and contents

Source of this annotation and contents: SAE.

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, vent or other systems. This coupling assembly is designed for use for -65 to 200 degrees F and at 125 psi peak working pressure, and the coupling assembly may be used in other fluid systems when requirements are within the limits.