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 9.0g forward ultimate inertia force of § 25.561 (b)(3)(ii).
SAE AS36100A-2011 history
1970SAE AS36100C-2020 Air Cargo Unit Load Devices – Performance Requirements and Test Parameters
2016SAE AS36100B-2016 Air Cargo Unit Load Devices – Performance Requirements and Test Parameters
2011SAE AS36100A-2011 Air Cargo Unit Load Devices – Performance Requirements and Test Parameters
2006SAE AS36100A-2006 Air Cargo Unit Load Devices - Performance Requirements and Test Parameters
2005SAE AS36100-2005 Air Cargo Unit Load Devices - Performance Requirements and Test Parameters