Table of Contents

Foreword
Introduction
1 Scope
2 Normative references
3 Terms and definitions
4 Design criteria
5 Testing methods
6 Quality control
7 Markings
8 Options
9 Manufacturer's instructions
10 Operating instructions
Bibliography

Abstract

Describes the design criteria and testing methods adequate to guarantee the ultimate load and operational dependability of cargo restraint strap assemblies with a typical rated ultimate tension load capability of 22250 N (5000 lbf), as used by the airline industry in order to restrain on board civil transport aircraft during flight.

General Product Information

Published
Document Type	Standard
Status	Current
Publisher	International Organization for Standardization
Pages
ISBN
Committee	TC 20
Supersedes	ISO/DIS 16049-1 : 60.00 (2013)