AS1650D Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Procurement Specification
Revised
07/10/2017
- Features
- Issuing Committee
- Content
- This SAE Aerospace Standard (AS) 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, and is designed for use from −65 to +400 °F and at 125 psig nominal operating pressure.
- Content
- AS1650 Revision D returns vibration test to revision A test requirements. This revision encompasses changes to test specimen configurations, fixtures, fluid and vibration levels. Additionally, various changes were made to clarify proof and pressure surge test requirements.
- Pages
- 27
- Citation
- SAE International Technical Standard, Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Procurement Specification, SAE Standard AS1650D, Revised July 2017, Reaffirmed June 2005, Issued March 1992, https://doi.org/10.4271/AS1650D.