SAE AS1710B-2004
Coupling, Fuel, Flexible, Variable Cavity, Threaded Type With Ferrules

Standard No.

SAE AS1710B-2004

Release Date

2004

Published By

Society of Automotive Engineers (SAE)

Status

Be replaced

Replace By

SAE AS1710C-2006

Latest

SAE AS1710D-2014

Scope

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 psi peak working pressure, and the coupling assembly may be used in other fluid systems when requirements are within the limits.

SAE AS1710B-2004 history

• 2014 SAE AS1710D-2014 Coupling, Fuel, Flexible, Variable Cavity, Threaded Type With Ferrules
• 2009 SAE AS1710D-2009 Coupling, Fuel, Flexible, Variable Cavity, Threaded Type With Ferrules
• 2006 SAE AS1710C-2006 Coupling, Fuel, Flexible, Variable Cavity Threaded Type With Ferrules
• 2004 SAE AS1710B-2004 Coupling, Fuel, Flexible, Variable Cavity, Threaded Type With Ferrules
• 1992 SAE AS1710B-1992 Coupling@ Fuel@ Flexible@ Variable Cavity@ Threaded Type with Ferrules
• 1984 SAE AS1710A-1984 COUPLING, FUEL, FLEXIBLE, VARIABLE CAVITY, THREADED TYPE WITH FERRULES
• 1982 SAE AS1710-1982 COUPLING, FUEL, FLEXIBLE, VARIABLE CAVITY THREADED TYPE WITH FERRULES