GJB 67.2A-2008
Military airplane structural strength specification.Part 2:Flight loads (English Version)

Standard No.

GJB 67.2A-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 6792-2009

Latest

GJB 6792-2009

Replace

GJB 67.2-1985

Scope

This Part specifies the requirements for structural strength and stiffness of military aircraft under flight loads. 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 67.2A-2008 Referenced Document

• GJB 185 Manned aircraft (fixed wing) flight quality
• GJB 2874 Flight quality of fly-by-wire aircraft
• 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 67.1A-2008 Military airplane structural strength specification.Part 1: General specigcation
• GJB 67.9A-2008 Military airplane structural strength specification.Part 9:Ground tests

GJB 67.2A-2008 history

• 2009 GJB 6792-2009 Specification for optical fibre coloring inks
• 2008 GJB 67.2A-2008 Military airplane structural strength specification.Part 2:Flight loads
• 1985 GJB 67.2-1985 Military Aircraft Strength and Stiffness Specification Flight Loading

GJB 67.2A-2008 Military airplane structural strength specification.Part 2:Flight loads has been changed from GJB 67.2-1985 Military Aircraft Strength and Stiffness Specification Flight Loading.