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Air Cargo Unit Load Devices - Performance Requirements and Test Parameters
- Aerospace Standard
Published June 06, 2016 by SAE International in United States
Downloadable datasets availableAnnotation ability available
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).
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.
|Aerospace Standard||Air Cargo Unit Load Devices – Testing Methods|
|Aerospace Standard||Air Cargo Unit Load Devices – Load Distribution Model|
Data Sets - Support Documents
|Unnamed Dataset 1||LIST OF CURRENT PAGES|
|Unnamed Dataset 2|
|Unnamed Dataset 3|
|Unnamed Dataset 4|
|Table 1||ULD sizes|
|Table 2||ULD configurations|
|Table 3||Testing restraint conditions|
Committee AGE-2 reports to the Aerospace General Projects Division. The main, or governing committee, AGE-2, is composed of the most experienced members, mainly from the airlines, airframe manufacturers, and support equipment manufacturers, to provide leadership and guidance for the Membership to implement the work is drawn with reasonable balance from airlines, airframe manufacturers, support equipment manufacturers, and others with special aircraft related expertise. Members serve based on their knowledge, expertise, and experience and not as agents or representatives of any organization.
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