OO-SJA
FlightFinder has no observed route profile for this registration. The documented safety events below are available independently of live flight tracking.
Safety history
- March 29, 1981AccidentHull loss
It was determined that the explosion of the engine n°3 was the consequence of the disintegration of a blade located on the 10th stage of the compressor due to fatigue cracks. The following contributing factors were identified: - The approach was completed with one engine inoperative. Full accident record