AS1650A: Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Procurement Specification - Technical Standard

Features

Issuing Committee: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

Scope

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.

Meta Tags

Topics: Parts
Environmental testing
Conductivity
Failure modes and effects analysis
Aluminum alloys
Aviation fuels
Assembling
Test procedures
Pressure
Test facilities

Details

DOI: https://doi.org/10.4271/AS1650A

Pages: 29

Citation: SAE International Technical Standard, Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Procurement Specification, SAE Standard AS1650A, Reaffirmed June 2005, Revised May 1999, Issued March 1992, https://doi.org/10.4271/AS1650A.

Additional Details

Publisher: SAE International

Published: Jun 2, 2005

Product Code: AS1650A

Content Type: Technical Standard

Status: Reaffirmed

Language: English

Historical