The principle of damage tolerance in structural design of an aircraft is based on the: - ATPL

Question id 184 - Aircraft General Knowledge - Airframe, Systems, Powerplant - ATPL - Airline Transport Pilot license

Fact That There Is No Need To Inspect The Structure.

Replacement of parts after a given number of cycles or hours of use.

Monitoring of critical parameters and the replacement of parts if a limit value is exceeded.

Capability to withstand a certain amount of weakening of the structure without catastrophic Failure.