JAL B747SR accident, 1985


 

Actual life

(reversals)

Max. stress

(MPa)

Theoretical prediction

(reversals)

12,319

650

Initial fatigue damage

9,090

Crack initiation period

11,970

 

It was determined that the cause of this accident was MSD originating from a mis-repaired lap joint in the rear pressure bulkhead structure. An attempt was made to apply the presented approach in order to estimate a probable crack initiation scenario that might precede fatal MSD. Detailed fracture mechanics consideration of this issue may be found in the work by Terada, H., A Proposal on Damage Tolerant Testing for Structural Integrity of Aging Aircraft--Learning from JAL Accident in 1985, Fracture Mechanics: 25-th Volume, STP 1220, F.Erdogan,Ed., American Society for Testing and Materials, Philadelphia,1995.

 

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