The principle of damage tolerance in structural design of an aircraft is based on the:
Domanda 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. |
