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Printed page 54. PDF page 62.
hold, directly caused the loss of the aircraft. The direct explosive forces produced a large hole in the fuselage structure and disrupted the main cabin floor. Major cracks continued to propagate from the large hole under the influence of theOpen official document at PDF page 62AAIB Aircraft Accident Report 2/90: Boeing 747-121 N739PA, Lockerbie
Printed page 56. PDF page 64.
reveal positive evidence of an explosive event. The direct explosive forces produced a large hole in the fuselage structure and disrupted the main cabin floor. Major cracks continued to propagate from the large hole under the influence of the serviceOpen official document at PDF page 64AAIB Aircraft Accident Report 2/90: Boeing 747-121 N739PA, Lockerbie
Printed page 18. PDF page 26.
model of the aircraft at Appendix B, Figures B-5 to B-8. The trail contained numerous large items from the forward fuselage. The flight deck and nose of the aircraft fell in the curved part of this trail close to Lockerbie.Open official document at PDF page 26AAIB Aircraft Accident Report 2/90: Boeing 747-121 N739PA, Lockerbie
Printed page 47. PDF page 55.
From this large jagged hole, three of the fractures continued to propagate away from the hole instead of terminating at the boundary. One fracture propagated longitudinally rearwards as far as thOpen official document at PDF page 55AAIB Aircraft Accident Report 2/90: Boeing 747-121 N739PA, Lockerbie
Printed page label not indexed. PDF page 56.
propagating outwards away from the main hole. Critical crack considerations The three very large tears extending beyond the boundary of the petalled region resulted in a critical reduction of fuselage structural integrity. Calculations were carried out at the Royal AerospaceOpen official document at PDF page 56AAIB Aircraft Accident Report 2/90: Boeing 747-121 N739PA, Lockerbie
Printed page 40. PDF page 42.
of the heating element and evacuation by the purge holes, the crystals accumulate in large numbers in the probe tube. As a result, a physical barrier is created inside the probe that will disturb the measurement of total pressure, thisOpen official document at PDF page 42Final Report: Accident on 1st June 2009 to the Airbus A330-203 registered F-GZCP operated by Air France flight AF 447