Cargo Restraint Straps - Design Criteria and Testing Methods

Standard:
Scope:

1.1 This SAE Aerospace Standard (AS) 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 22250 N (5000 lbf) rated ultimate tension load capability, as used by the airline industry in order to restrain cargo on board civil transport aircraft during flight:

Rationale:

Revision D eliminates D5 and D6 end fittings, revises the flammability test burn rate consistent with FAA regulations amendment 111, and renumbers paragraphs per current requirements for SAE standards.

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Training / Education
2017-10-27
Standard
1954-05-01