Part-66 Module 11 Practice Questions - EASA Part-66 Module 11 - Aeroplane Aerodynamics, Structures And Systems Exam

In a 'fail-safe' airframe structural design philosophy, structural integrity after a single failure is assured because:

Multiple load paths exist so remaining structure carries the load until the failure is detected Every component is replaced at a fixed flight-hour life regardless of condition The component is designed never to crack within the aircraft's life Inspections are eliminated because the part cannot fail

Correct Answer:

Multiple load paths exist so remaining structure carries the load until the failure is detected

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