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, expect for the 9.0 g forward ultimate inertia force of 25.561 (b)(3)(ii).
SAE AS 36100A-2006由美国机动车工程师协会 US-SAE 发布于 2006-04-01。
SAE AS 36100A-2006 在中国标准分类中归属于: V50 航空运输与地面设备综合,在国际标准分类中归属于: 49.120 货运设备。
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