AS1650F Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Procurement Specification

Revised

10/24/2018

Features
Issuing Committee
Scope
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, 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.
Rationale
Content
Revise pressure surge test fixture in Figure 7 and clarify allowable leakage description for the vibration test in 4.6.3.3.3.
Meta TagsDetails
DOI
https://doi.org/10.4271/AS1650F
Pages
29
Citation
SAE International Technical Standard, Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Procurement Specification, SAE Standard AS1650F, Revised October 2018, Reaffirmed June 2005, Issued March 1992, https://doi.org/10.4271/AS1650F.
Additional Details
Publisher
Published
Oct 24, 2018
Product Code
AS1650F
Content Type
Technical Standard
Status
Revised
Language
English