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. AS1650 Revision C provides additional test clarification and end use system limits. Reference document changes for order and general terms and units of measure have been shortened to match current industry nomenclature.
Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Procurement Specification
2016-02-26
Conference paper
English
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