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SAE AS1650 Rev F

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

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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, is designed for use from -65 to +400 °F and at 125 psig nominal operating pressure. AS1650 was not designed for the new certification requirements for flammable leakage zones and fuel tanks for lightning protection and assembly redundancy. As such, their use and installation may require additional efforts and equipment to support new FAA CFR compliance. The AS7510 flexible coupling should be the preferred coupling for use in flammable leakage zones and fuel tanks that require service life and functionality for lightning protection and part redundancy.

SDO SAE: SAE International
Document Number AS1650
Publication Date Oct. 24, 2018
Language en - English
Page Count 29
Revision Level F
Supercedes
Committee
Publish Date Document Id Type View
Oct. 24, 2018 AS1650F Revision
Dec. 7, 2017 AS1650E Revision
July 10, 2017 AS1650D Revision
Feb. 26, 2016 AS1650C Revision
Aug. 24, 2010 AS1650B Revision
May 1, 1999 AS1650A Revision
March 1, 1992 AS1650 Revision