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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
Printed page 66. PDF page 66.
coming from a repair on the left inner elevon o the tail cone anti-collision light, o a severely fire-damaged inspection panel from the wing lower surface, o seven inspection panels identified as coming from the upper surface of the leftOpen final report at PDF page 66Final report: Concorde F-BTSC, 25 July 2000
Printed page 142. PDF page 142.
OBSERVED Leave the gear extended unless safety conditions require it. [...]" � Fire or Severe Engine Damage Procedure Page II-04.20.1 specifies that the first actions to take are: "GEAR, on takeoff...........................................................................Open final report at PDF page 142Final report: Concorde F-BTSC, 25 July 2000
Printed page 175. PDF page 175.
and 2 suffered simultaneous surges leading to slight loss of thrust on engine 1 and a severe loss on engine 2. � The surge on engine 1 was most likely caused by ingestion of hot gases or solid debris, probablyOpen final report at PDF page 175Final report: Concorde F-BTSC, 25 July 2000
Printed page 176. PDF page 176.
by a violent fire. � Many pieces of the aircraft found along the track indicate that severe damage to the aircraft's structure was caused in flight by the fire. � Even with the engines operating normally, the significant damage causedOpen final report at PDF page 176Final report: Concorde F-BTSC, 25 July 2000