Standard

SAE AS8009A

Oct 1996 Withdrawn

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Language English

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Abstract

This Aerospace Standard (AS) specifies minimum performance requirements for primary pressure altimeter systems other than air data computers. This AS covers altimeter systems that measure and display altitude as a function of atmospheric pressure. The pressure transducer may be contained within the instrument display case or located remotely. Requirements for air data computers are specified in AS8002. Some requirements for nontransducing servoed altitude indicators are included in AS791. The instrument system specified herein does not include aircraft pressure lines. Unless otherwise specified, whenever the term "instrument" is used, it is to be understood to be the complete system of pressure transducer components, any auxiliary equipment, and display components. The test procedures specified herein apply specifically to analog type instruments. Digital instruments or automatic test instrumentation may require other test procedures. Such differing procedures shall be justified prior to use.

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Standard from SAE International
Published: October 29 1996
Withdrawn: September 21 2005
Document type: IS
Pages
ISBN:

Publisher: SAE International
Distributor: SAE International

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Refers: SAE AS791
Replaced by: SAE AS8009B
Refers: SAE AIR1075
Replaces: SAE AS8009

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Version history History (2)

SAE AS8009A

SAE AS8009

Abstract

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