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Printed page label not indexed. PDF page 28.
compromised significantly the static strength of the airframe. Certainly, there was no evidence to suggest that corrosion had affected the mode of disintegration, either in the area of the explosion or at areas more remote. Similarly, there were no indicationsOpen official document at PDF page 28AAIB Aircraft Accident Report 2/90: Boeing 747-121 N739PA, Lockerbie
Printed page label not indexed. PDF page 29.
1.12.2,2 No evidence of overpressure fracture or distortion was found at the rear pressure bulkhead. Some suggestion of ‘quilting' or ‘pillowing' of skin panels between stringers and frames, indOpen official document at PDF page 29AAIB Aircraft Accident Report 2/90: Boeing 747-121 N739PA, Lockerbie
Printed page label not indexed. PDF page 37.
identified on site as containing ingested debris from within the aircraft, nonetheless had no evidence of the type of shingling seen on the blades of No 2 engine. Such evidence is usually unmistakable and its absence is a clear indicationOpen official document at PDF page 37AAIB Aircraft Accident Report 2/90: Boeing 747-121 N739PA, Lockerbie
Printed page label not indexed. PDF page 38.
aircraft and ground impact. There was no pathological indication of an in-flight fire and no evidence that any of the victims had been injured by shrapnel from the explosion. There was also no evidence which unequivocally indicated that passengers orOpen official document at PDF page 38AAIB Aircraft Accident Report 2/90: Boeing 747-121 N739PA, Lockerbie
Printed page 39. PDF page 47.
charge approximately 25 inches inboard from the fuselage skin at frame 700. There was no evidence to indicate that there was more than one explosive charge. Engine evidence To produce the fan blade tip rub damage noted on all enginesOpen official document at PDF page 47AAIB Aircraft Accident Report 2/90: Boeing 747-121 N739PA, Lockerbie
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