SAE AS1650D
Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Procurement Specification
Historical
Standard by SAE International, 2017-07-10
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About This Item
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 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.
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Standard Details
- Publication Date: 2017-07-10
- Standard Status: historical
- Publisher: SAE International
- Document Type: Aerospace Standard
- Subject: Fittings, Fuel systems, Fuel systems modules, Environmental testing, Failure modes and effects analysis, Aluminum alloys, Hoses, Conductivity, Defense industry
- Official SAE: Doi link
Document History
- New Version Available: AS1650F (2018-10-24)
- Previous Version: AS1650E (2017-12-07)
- This Version: AS1650D (2017-07-10)
- Previous Version: AS1650C (2016-02-26)
- Previous Version: AS1650B (2010-08-24)
- Previous Version: AS1650A (2005-06-02)
- Previous Version: AS1650 (1998-03-01)
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