AS5385D Cargo Restraint Straps - Design Criteria and Testing Methods

Revised

05/08/2017

Features
Issuing Committee
Scope
Content
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:
  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
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/AS5385D
Pages
21
Citation
SAE International Technical Standard, Cargo Restraint Straps - Design Criteria and Testing Methods, SAE Standard AS5385D, Revised May 2017, Reaffirmed November 2012, Issued September 2000, https://doi.org/10.4271/AS5385D.
Additional Details
Publisher
Published
May 8, 2017
Product Code
AS5385D
Content Type
Technical Standard
Status
Revised
Language
English

Revisions