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SAE International, 09/30/2021
Publisher: SAE
File Format: PDF
$48.00$97.00
Published:30/09/2021
File Size:1 file , 340 KB
Note:This product is unavailable in Ukraine, Russia, Belarus
This document covers the general requirements for hydraulic aircraft jacks. It can be applied to tripod, unipod, and axle jacks that may be used on open ramp areas as well as in the aircraft hangar.
Throughout this Aerospace Standard, the minimum essential criteria are identified by the key word "shall". Recommended criteria are identified by use of the key word "should". Deviation from recommended criteria should only occur after careful consideration and thorough service evaluation have shown alternate methods to provide an equivalent level of safety.
The term "vertical load" throughout this Aerospace Standard is defined as the force imposed on the aircraft jack at the airframe jack point.
Guidelines for Developing and Revising SAE Nomenclature and Definitions (Stabilized: Jul 2021)
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Alloy, Corrosion and Heat-Resistant, Bars and Forgings 21Cr - 32.5Ni - 0.38Ti - 0.38Al - 45Fe Solution Heat Treated
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Steel, Corrosion Resistant, Sheet, Strip, and Plate 15Cr - 6.5Ni - 0.75Mo - 0.60Cb - 1.5Cu Solution Heat Treated, Precipitation Hardenable
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Steel, Corrosion-Resistant, Sheet, Strip, and Plate 19Cr - 9.2Ni (SAE 30304) Solution Heat Treated
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