HB 6167.5-2014 Environmental conditions and test procedures for airborne equipment of civil airplane.Part 5: Operational shocks and crash safety test (English Version)
This part specifies the flight impact and crash safety test conditions and test methods for civil aircraft airborne equipment. The flight shock test in this part is applicable to all equipment installed on fixed-wing aircraft and helicopters. The crash safety test in this part is applicable to equipment installed in the cockpit and other areas of the aircraft. Separation during emergency landing will endanger the occupants and fuel. Safety equipment for systems or emergency escape equipment. This test cannot meet the requirements of China Civil Aviation Regulations (CCAR) for all equipment, such as seats and seat restraints.
HB 6167.5-2014 Referenced Document
HB 6167.1-2014 Environmental conditions and test procedures for airborne equipment of civil airplane.Part 1: General principles
HB 6167.6-2014 Environmental conditions and test procedures for airborne equipment of civil airplane.Part 6: Vibration test
HB 6167.5-2014 history
2014HB 6167.5-2014 Environmental conditions and test procedures for airborne equipment of civil airplane.Part 5: Operational shocks and crash safety test
1989HB 6167.5-1989 Environmental conditions and test methods for airborne equipment of civil aircraft Flight shock and crash safety tests