Standard

SAE AS36100

Feb 2005 Withdrawn

Existing or new amendments and versions must be purchased separately.

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).

Products specifications

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Withdrawn: December 12 2011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

Publisher: SAE International
Distributor: SAE International

Product Relations

Referred by: SAE ARP1554D
Referred by: SAE ARP1840B
Referred by: SAE ARP5486
Referred by: SAE ARP36104A
Referred by: SAE AIR36106A
Referred by: SAE AS1677D
Referred by: SAE AS5896
Referred by: SAE AIR36108
Referred by: SAE ARP5595B
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 AIR36107A
Referred by: SAE ARP5595A
Referred by: SAE AS36101A
Referred by: SAE AS36102
Referred by: SAE AS1825B
Referred by: SAE AIR36106
Referred by: SAE AIR36107
Referred by: SAE ARP36104
Refers: SAE AS33601
Referred by: SAE ARP5596A
Referred by: SAE ARP36103
Referred by: SAE AS36101
Referred by: SAE ARP5596
Referred by: SAE ARP5595

Extended editions Extended editions (0)

Version history Related Corrigenda and Amendments (0)

Abstract

Products specifications

Product Relations