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Printed page 18. PDF page 26.
fuselage frame, clearly originating from the crown region above the forward upper deck. Datum line All grid references relating to items bearing actual explosive evidence, together with those attached to heavily distorted items found to originate immediately adjacent to thOpen official document at PDF page 26AAIB Aircraft Accident Report 2/90: Boeing 747-121 N739PA, Lockerbie
Printed page label not indexed. PDF page 44.
geographical position of the aircraft at the moment the loud sound was recorded on the CVR. The datum line, discussed at paragraph 1.12.1.6, was derived from a detailed analysis of the distribution of specific items of wreckage, including those exhibitingOpen official document at PDF page 44AAIB Aircraft Accident Report 2/90: Boeing 747-121 N739PA, Lockerbie
Printed page label not indexed. PDF page 48.
Speed of initial disintegration The distribution of wreckage in the bands between the datum line and the 250, 300, 600 and 900 metre lines was examined in detail. The positions of these items of structure on the aircraft are shownOpen official document at PDF page 48AAIB Aircraft Accident Report 2/90: Boeing 747-121 N739PA, Lockerbie
Printed page 41. PDF page 49.
fuselage. Assuming the original ground speed of 434 Kts, the elapsed flight times from the datum to each of the parellel lines were calculated to be: Distance (metres) 250 300 600 900 Time (seconds) 1,1 1.3 2.7 4.0 Thus, thereOpen official document at PDF page 49AAIB Aircraft Accident Report 2/90: Boeing 747-121 N739PA, Lockerbie