GJB 67.6A-2008
Military airplane structural strength specification.Part 6:Repeated loads,dusrability and damage tolerance (English Version)

Standard No.

GJB 67.6A-2008

Language

Chinese, Available in English version

Release Date

2008

Published By

Military Standard of the People's Republic of China-General Armament Department

Status

Be replaced 2009-08

Replace By

GJB 6786-2009

Latest

GJB 6786-2009

Replace

GJB 67.6-1985

Scope

This part specifies durability, damage tolerant design and verification requirements for military aircraft structures, and repetitive loads acting on aircraft. This part applies to the ordering, design and verification of various military aircraft (excluding helicopters). This part is also one of the basis for signing the contract, and the specific model should be implemented according to the terms of the contract.

GJB 67.6A-2008 Referenced Document

• GJB 67.10A-2008 Military airplane structural strength specification.Part 10: Flight tests
• GJB 67.12A-2008 Military airplane structural strength sepcification.Part 12: Documents and reports
• GJB 67.14-2008 Military airplane structural strength specification.Part 14: Composite structures
• GJB 67.1A-2008 Military airplane structural strength specification.Part 1: General specigcation
• GJB 67.2A-2008 Military airplane structural strength specification.Part 2:Flight loads
• GJB 67.4A-2008 Military airplane structural strength specification .Part 4:Ground loads
• GJB 67.8A-2008 Military airplane structural strength specification.Part 8: Vibration and aeroacoustic durability
• GJB 67.9A-2008 Military airplane structural strength specification.Part 9:Ground tests

GJB 67.6A-2008 history

• 2009 GJB 6786-2009 Resistors,fixed,wire wound power type,including space level general specification for
• 2008 GJB 67.6A-2008 Military airplane structural strength specification.Part 6:Repeated loads,dusrability and damage tolerance
• 1985 GJB 67.6-1985 Military aircraft strength and stiffness specifications, reliability requirements and fatigue loads

GJB 67.6A-2008 Military airplane structural strength specification.Part 6:Repeated loads,dusrability and damage tolerance has been changed from GJB 67.6-1985 Military aircraft strength and stiffness specifications, reliability requirements and fatigue loads.