AS5385C Cargo Restraint Straps - Design Criteria and Testing Methods

Reaffirmed

11/26/2012

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/upper deck cargo systems and meeting the requirements of NAS 3610 or AS36100, 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.
Rationale
Content
AS5385C has been reaffirmed to comply with the SAE five-year review policy.
Meta TagsDetails
DOI
https://doi.org/10.4271/AS5385C
Pages
21
Citation
SAE International Technical Standard, Cargo Restraint Straps - Design Criteria and Testing Methods, SAE Standard AS5385C, Reaffirmed November 2012, Revised January 2007, Issued September 2000, https://doi.org/10.4271/AS5385C.
Additional Details
Publisher
Published
Nov 26, 2012
Product Code
AS5385C
Content Type
Technical Standard
Status
Reaffirmed
Language
English

Revisions