HB 6167.5-1989
Environmental conditions and test methods for airborne equipment of civil aircraft Flight shock and crash safety tests (English Version)
- Standard No.
- HB 6167.5-1989
- Language
- Chinese, Available in English version
- Release Date
- 1989
- Published By
- Professional Standard - Aviation
- Status
- 2014-10
- Replace By
- HB 6167.5-2014
- Latest
- HB 6167.5-2014
- Scope
- This standard specifies the test conditions and test methods for civil aircraft impact and collision safety (collision impact and crash acceleration). It is an integral part of the "Environmental Conditions and Test Methods for Civil Aircraft Airborne Equipment" series of standards. The flight impact test is used to verify whether the airborne equipment maintains normal working condition when and after the impact encountered by the aircraft during normal flight, and whether the performance parameters remain within the specified tolerance range. Such shocks may occur during taxiing, landing, or when the aircraft suddenly encounters gusts of wind while in flight. The crash safety test is used to verify whether equipment installed in the aircraft cockpit and other areas will separate from its mounting brackets during an emergency landing, which may endanger the safety of the occupants, fuel system, fault recording system or emergency exhaust device.
HB 6167.5-1989 history
- 2014 HB 6167.5-2014 Environmental conditions and test procedures for airborne equipment of civil airplane.Part 5: Operational shocks and crash safety test
- 1989 HB 6167.5-1989 Environmental conditions and test methods for airborne equipment of civil aircraft Flight shock and crash safety tests
