Refine Your Search

Topic

Search Results

Standard

COUPLING ASSEMBLY, THREADLESS, FLEXIBLE, FIXED CAVITY, SELF-BONDING

1998-03-01
HISTORICAL
AS1650
This document defines the requirements for a threadless, flexible, self-bonding coupling assembly, which, when installed on machined fixed cavity ferrules, provides a flexible connection for joining tubing and components in aircraft fuel, vent, or other systems. This assembled coupling, hereafter referred to as the assembly, is designed for use from -65 to 400 °F and at 125 psi operating pressure.
Standard

COUPLING, FUEL, FLEXIBLE, VARIABLE CAVITY THREADED TYPE WITH FERRULES

1982-05-01
HISTORICAL
AS1710
This specification 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 from -65 to 200 degrees F and at 125 psi operating pressure.
Standard

COUPLING, FUEL, FLEXIBLE, VARIABLE CAVITY, THREADED TYPE WITH FERRULES

1984-01-01
HISTORICAL
AS1710A
This specification 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 from -65 to 200 degrees F and at 125 psi peak working pressure.
X