SAE AS1650A
Superseded
View Superseded by
Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Procurement Specification
Hardcopy , PDF
English
06-02-2005
08-24-2010
| DocumentType |
Standard
|
| Pages |
29
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
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.
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