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.
Rationale: AS1650 Revision D returns vibration test to revision A test requirements. This revision encompasses changes to test specimen configurations, fixtures, fluid and vibration levels. Additionally, various changes were made to clarify proof and pressure surge test requirements.
Also known as: SAE AS 1650
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