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8 matching PDF pages. Showing 6 short source excerpts. Open the document for full context.
Printed page 17. PDF page 17.
1 and 2 suffered a loss of thrust, severe for engine 2, slight for engine 1. By 14 h 43 min 13 s, as the PF commenced the rotation, the controller informed the crew the presence of flames behind theOpen final report at PDF page 17Final report: Concorde F-BTSC, 25 July 2000
Printed page 39. PDF page 39.
wind 090 8 kt cleared for takeoff", the crew replied "45 90 takeoff 26 right". At 14 h 43 min 13 s the controller stated "... 45 90 you have flames ... you have flames behind you". The crew acknowledgedOpen final report at PDF page 39Final report: Concorde F-BTSC, 25 July 2000
Printed page 47. PDF page 47.
final transcript. 14 h 43 min 10.1 s, noise followed, from 14 h 43 min 11 s to 14 h 43 min 13.8 s, by a change in the background noise. In the same time period the FO announces "watchOpen final report at PDF page 47Final report: Concorde F-BTSC, 25 July 2000
Printed page 48. PDF page 48.
14 h 43 min 13.4 s, message from the controller indicating flames at the rear and read back by the FO. 14 h 43 min 16.4 s, FE "(stop) ". 14 h 43 min 20.4 s, FE "Failure eng... failureOpen final report at PDF page 48Final report: Concorde F-BTSC, 25 July 2000
Printed page 129. PDF page 129.
min 12.3 s Surge. The EGT, P7, 14 h 43 min 12.7 s N1, N2, Aj show and deviations. 14 h 43 min 13.3 s Surge. 14 h 43 min 12.0 s and The Nx is recorded at its minimalOpen final report at PDF page 129Final report: Concorde F-BTSC, 25 July 2000
Printed page 161. PDF page 161.
stabilisation of the flame. This is consistent with the controller's comment which, at 14 h 43 min 13.4 s, indicated extensive flames at the rear of the aircraft. A few tenths of a second after the change in the backgroundOpen final report at PDF page 161Final report: Concorde F-BTSC, 25 July 2000