Standard

SAE AS1960A

Nov 2024 Published

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Language English

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Abstract

This specification defines the requirements for a grooved clamp coupling and flanges suitable for joining intermediate pressure and temperature ducting in aircraft air systems. The rigid coupling joint assembly, hereafter referred to as "the joint", shall operate within the temperature range of -65 °F to +800 °F.

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Standard from SAE International
Published: 6 November 2024
Document type: IS
Pages
ISBN:

Publisher SAE International
Distributor SAE International

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Replaces: SAE AS1960

SAE AS1960A

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SAE AS1960A

SAE AS1960

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SAE AS1960A

SAE AS1960

Abstract

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