AS5385A Cargo Restraint Straps - Design Criteria and Testing Methods
Revised
07/15/2002
- Features
- Issuing Committee
- Content
- 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:
-
a
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
-
b
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.
-
a
- Pages
- 23
- Citation
- SAE International Technical Standard, Cargo Restraint Straps - Design Criteria and Testing Methods, SAE Standard AS5385A, Revised July 2002, Issued September 2000, https://doi.org/10.4271/AS5385A.