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Pan Am 103 (Lockerbie)

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3. CONCLUSIONS 56 3.a ‘Findings . 56 3.b Cause 57 4. SAFETY RECOMMENDATIONS. . . . . . .t~-t:~<CSest*‘C«CSH 2. APPENDICES Appendix Appendix Appendix Appendix Appendix Appendix Appendix A. Personnel involved in the investigatio
Open official document at PDF page 7AAIB Aircraft Accident Report 2/90: Boeing 747-121 N739PA, Lockerbie

Pan Am 103 (Lockerbie)

Printed page label not indexed. PDF page 16.

through a large cargo door on the right side of the aircraft. Internal fuselage cavities Because of the conventional skin, frame and stringer type of construction, common to all large public transport aircraft, the fuselage was effectively divided into a
Open official document at PDF page 16AAIB Aircraft Accident Report 2/90: Boeing 747-121 N739PA, Lockerbie

Pan Am 103 (Lockerbie)

Printed page label not indexed. PDF page 17.

noted that a similar communication did not exist between the upper and lower cabins because there were no air conditioning/depressurisation passages to bypass the upper deck floor.) Aircraft weight and centre of gravity The aircraft was loaded within its permitted
Open official document at PDF page 17AAIB Aircraft Accident Report 2/90: Boeing 747-121 N739PA, Lockerbie

Pan Am 103 (Lockerbie)

Printed page label not indexed. PDF page 25.

1.12.1.4 velocity. The impact had caused almost complete crushing of the structure on the left side. The radome and right nose landing gear door had detached in the air and were recovered in the southern trail. Examinat
Open official document at PDF page 25AAIB Aircraft Accident Report 2/90: Boeing 747-121 N739PA, Lockerbie

Pan Am 103 (Lockerbie)

Printed page label not indexed. PDF page 29.

must have remained attached to the wing centre section at the time of its impact. Because of the high degree of fragmentation and the relative insignificance of the wing in terms of the overall explosive damage pattern, a reconstruction of
Open official document at PDF page 29AAIB Aircraft Accident Report 2/90: Boeing 747-121 N739PA, Lockerbie

Pan Am 103 (Lockerbie)

Printed page label not indexed. PDF page 30.

of the structure of the fin revealed evidence of in-flight damage to the leading edge caused by the impact of structure or cabin contents. This damage was not severe or extensive and the general break-up of the fin did not
Open official document at PDF page 30AAIB Aircraft Accident Report 2/90: Boeing 747-121 N739PA, Lockerbie