This standard specifies the methods and requirements for calibration of fatigue and static strength (including damage tolerance and stiffness) test systems in aircraft and its component strength and stiffness test projects. This standard applies to various military aircraft and helicopters, as well as to various civilian aircraft. This standard can be used as one of the basis for the test client (hereinafter referred to as the client) to formulate a test task statement or sign a contract with the test contractor (hereinafter referred to as the contractor). It can also be adopted by the client and the contractor through negotiation.
HB 7295-1996 history
1996HB 7295-1996 Aircraft Strength and Stiffness Ground Test System Calibration Method and Requirements