Standard

SAE AIR6

Dec 1996 Withdrawn

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Abstract

This publication formalizes the applicable design concepts considered acceptable for "draw-through" cooling of electronic (avionic) equipment installed in subsonic and supersonic commercial jet transports. Methods other than draw-through cooling are covered in AIR 728A for high Mach number aircraft.

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Standard from SAE International
Published: 1 December 1996
Withdrawn: 1 December 1996
Document type: IS
Pages
ISBN:

Publisher SAE International
Distributor SAE International

Product Relations

Referred by: SAE AIR1174B
Referred by: SAE AIR1174A

SAE AIR6

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