Standard

SAE AS4751

Jan 2013 Withdrawn

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Abstract

This SAE Aerospace Standard (AS) establishes the requirements for a grooved clamp coupling and flanges suitable for joining intermediate pressure and temperature ducting in aircraft pneumatic systems. The rigid coupling joint assembly, hereafter referred to as “the joint”, shall operate within the temperature range of -65 °F external ambient to +800 °F internal fluid.

Document information

Standard from SAE International
Published: 7 January 2013
Document type: IS
ISBN:

Publisher SAE International
Distributor SAE International

Product Relations

Refers: SAE AS4108
Referred by: SAE AIR869B
Refers: SAE AIR869
Refers: SAE AMS5901
Refers: SAE AMSW6858
Refers: SAE AS478J
Refers: SAE AS8879
Refers: SAE AMS5510
Refers: SAE AMS5732
Refers: SAE AS478
Refers: SAE AMS5737
Refers: SAE AMS5525
Refers: SAE AMS5513
Refers: SAE AMS5518
Refers: SAE AMS5516

SAE AS4751

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Abstract

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Abstract

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