Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Procurement Specification

Standard:
Revised:
  • 2010-08-24
 
  • HISTORICAL Access the latest revision: AS1650D
Publisher:
  • SAE International
Pages:
23
Scope:

This aerospace specification 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 psig nominal operating pressure.

Rationale:

AS1650 Rev. B corrects the placement and title of paragraph 4.6.6. Revision B adds PRI QPL/QML requirements, deletes gunfire vibration requirements, reduces impulse peak pressure requirements and provides a general document update.

History:
Standard Published Revision Status
AS1650D 2017-07-10 Latest Revised
2016-02-26 Historical Revised
2010-08-24 Historical Revised
2005-06-02 Historical Reaffirmed
1998-03-01 Historical Reaffirmed
AKA:
  • SAE AS 1650
Sector:
Topic:
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