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This work aims to validate the effect for Failure Condition of landing gear system by case analysis. Based on the real aviation accident data, this paper does the case analysis of failure condition effect for civil aircraft landing gear system. The results obtained in this research include failure condition effects that according to the actual situation and the traceability between theory analysis and real case. This paper provides supporting material for landing gear system Functional Hazard Assessment and supports the safety and certification of the aircraft.
Inspec keywords: failure (mechanical); aircraft; air safety; gears; hazards; failure analysis; aerospace safety; design engineering
Subjects: Aerospace industry; Health and safety aspects; Statistics; Maintenance and reliability