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Printed page 138. PDF page 138.
that when engines 1 and 2 suffered their first surges, the aircraft was subjected to a severe loss of thrust almost like a double engine failure, the longitudinal acceleration was then halved (figure longitudinal acceleration on Concorde (nx)). It wasOpen final report at PDF page 138Final report: Concorde F-BTSC, 25 July 2000
Printed page 175. PDF page 175.
nominal thrust before suffering, at the moment of takeoff, a second surge leading to a severe loss of thrust; engine 2, in a slight recovery phase, also surged for the second time at that moment. � The second surge onOpen final report at PDF page 175Final report: Concorde F-BTSC, 25 July 2000
Printed page 176. PDF page 176.
forward propagation of the flame causing a very large fire under the aircraft's wing and severe loss of thrust on engine 2 then engine 1. In addition, the impossibility of retracting the landing gear probably contributed to the retention andOpen final report at PDF page 176Final report: Concorde F-BTSC, 25 July 2000
Printed page 17. PDF page 17.
thrown against the underside of the left wing and the rupture of a part of tank 5. A severe fire broke out under the left wing and around the same time engines 1 and 2 suffered a loss of thrust,Open final report at PDF page 17Final report: Concorde F-BTSC, 25 July 2000