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Cargo Restraint Straps - Design Criteria and Testing Methods
- Aerospace Standard
Published July 15, 2002 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This Standard aims at identifying the design criteria and testing methods adequate to guarantee the ultimate load and operational dependability of cargo restraint strap assemblies with a typical 22 250 N (5,000 lbf) rated ultimate tension load capability, as used by the airline industry in order to restrain on board civil transport aircraft during flight:
cargo loaded and tied down onto airworthiness certified air cargo pallets, themselves restrained into aircraft lower deck or main deck cargo systems meeting the requirements of NAS 3610, or
non-unitized individual pieces of cargo, or pieces of cargo placed onto an unrestrained (“floating”) pallet into either lower deck or main deck containerized cargo compartments of an aircraft.
|Aerospace Standard||Cargo Restraint Straps - Design Criteria and Testing Methods|
|Aerospace Material Specification||Glass, Laminated, Aircraft Glazing|
Data Sets - Support Documents
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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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