GJB 67.7A-2008 (English Version) PDF

Standard No.: GJB 67.7A-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 6787-2009
Latest: GJB 6787-2009
Replace: GJB 67.7-1995

Scope: This part specifies the requirements and analysis, ground tests and flight tests required to prevent flutter, divergence and other aeroelastic instabilities during aircraft design and manufacture. This section provides analysis and test requirements to identify and establish some criteria and parameters as minimum standards for structural design, the airframe should be able to meet these requirements. 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 67.7A-2008 Referenced Document

GJB 67.12A-2008 Military airplane structural strength sepcification.Part 12: Documents and reports
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 67.6A-2008 Military airplane structural strength specification.Part 6:Repeated loads,dusrability and damage tolerance
GJB 67.9A-2008 Military airplane structural strength specification.Part 9:Ground tests

2009 GJB 6787-2009 Resistors,chip,fixed,film,zero,ohm,including space level,general specification for
2008 GJB 67.7A-2008 Military airplane structural strength specigcation.Part 7: Aeroelasticity
1985 GJB 67.7-1985 Military Aircraft Strength and Stiffness Specification Aeroelastic Instabilities