Air Cargo Unit Load Devices - Performance Requirements and Test Parameters
AS36100B
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 requirements of Title 14 CFR Part 25, except for the 9.0g forward ultimate inertia force of § 25.561 (b)(3)(ii).
Rationale:
After publication of AS36100A [2006-04], reference for TSO-C90d of 2011-09-30, certain errors or insufficiencies were identified at implementation. The present revision B corrects these and is proposed for reference by future TSO-C90e revision.
Related Topics:
Containers
Restraint systems
Center of gravity (CG)
Aircraft
Identification numbers
Heat treatment
Assembling
Fittings
Also known as: SAE AS 36100
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