GJB 6887-2009
Procedure for low cycle fatigue test of military helicopter turboshaft engine (English Version)

Standard No.

GJB 6887-2009

Language

Chinese, Available in English version

Release Date

2009

Published By

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

Status

Withdraw

Latest

GJB 6887-2009

Scope

This specification specifies the technical requirements and test methods for the low-cycle fatigue test of the whole turboshaft engine for military helicopters. This specification is applicable to the low cycle fatigue test of the whole turboshaft engine for military helicopters.

GJB 6887-2009 Referenced Document

• GJB 242-1987 General specification for aerospace turboprop and turboshaft engines

GJB 6887-2009 history

• 2009 GJB 6887-2009 Procedure for low cycle fatigue test of military helicopter turboshaft engine