Standard

SAE AS36100

Feb 2005 Withdrawn

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Language English

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Abstract

This SAE Aerospace Standard (AS) defines the minimum performance requirements and test parameters for air cargo unit load devices requiring approval of airworthiness for installation in an approved aircraft cargo compartment and restraint system that complies with the cargo restraint and occupant protection requirements of Title 14 CFR Part 25, except for the 9.0 g forward ultimate inertia force of § 25.561 (b)(3)(ii).

Document information

Standard from SAE International
Published: 10 February 2005
Withdrawn: 12 December 2011
Document type: IS
Pages
ISBN:

Publisher SAE International
Distributor SAE International

Product Relations

Referred by: SAE ARP1840B
Referred by: SAE ARP1554D
Referred by: SAE ARP5486
Referred by: SAE ARP36104A
Referred by: SAE AS1677D
Referred by: SAE AS5896
Referred by: SAE AS5385D
Referred by: SAE AS36102B
Referred by: SAE AS1825C
Referred by: SAE AS36102A
Referred by: SAE AS5385C
Referred by: SAE ARP36103A
Referred by: SAE ARP5596B
Replaced by: SAE AS36100A
Referred by: SAE AS36101A
Referred by: SAE AS36102
Referred by: SAE AS1825B
Referred by: SAE ARP36104
Referred by: SAE ARP5596A
Referred by: SAE ARP36103
Referred by: SAE AS36101
Referred by: SAE ARP5596

SAE AS36100

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Abstract

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Abstract

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