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About This Item

 

Full Description

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).

 

Document History

  1. SAE AS36100B

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    Air Cargo Unit Load Devices - Performance Requirements and Test Parameters

    • Most Recent
  2. SAE AS36100A


    Air Cargo Unit Load Devices - Performance Requirements and Test Parameters

    • Historical Version