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Printed page 47. PDF page 55.
corrosion induced weaknesses, which had then been exploited by the explosive forces. No evidence of fatigue cracking was found in the bonded joints. Inter-surface corrosion was present on most lap joints but only one very small region of corrosion hadOpen official document at PDF page 55AAIB Aircraft Accident Report 2/90: Boeing 747-121 N739PA, Lockerbie
Printed page 56. PDF page 64.
Airworthiness and had been maintained in compliance with the regulations. There was no evidence of any defect or malfunction in the aircraft that could have caused or contributed to the accident. The structure was in good condition and the minimalOpen official document at PDF page 64AAIB Aircraft Accident Report 2/90: Boeing 747-121 N739PA, Lockerbie