AS5385A Cargo Restraint Straps - Design Criteria and Testing Methods

Revised

07/15/2002

Features
Issuing Committee
Scope
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:
  1. 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
  2. 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.
Meta TagsDetails
DOI
https://doi.org/10.4271/AS5385A
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.
Additional Details
Publisher
Published
Jul 15, 2002
Product Code
AS5385A
Content Type
Technical Standard
Status
Revised
Language
English

Revisions