Cargo Restraint Straps - Design Criteria and Testing Methods

Standard:
Revised:
  • 2017-05-08
 
  • CURRENT
Publisher:
  • SAE International
Pages:
21
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.

History:
Standard Published Revision Status
AS5385D 2017-05-08 Latest Revised
2012-11-26 Historical Reaffirmed
2004-11-17 Historical Revised
2002-07-15 Historical Revised
2000-09-01 Historical Issued
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