AS1650B Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Procurement Specification
Revised
08/24/2010
- Features
- Issuing Committee
- Content
- 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.
- Content
- 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.
- Pages
- 1
- Citation
- SAE International Technical Standard, Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Procurement Specification, SAE Standard AS1650B, Revised August 2010, Reaffirmed June 2005, Issued March 1992, https://doi.org/10.4271/AS1650B.