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Air France 4590 (Concorde)

Printed page 28. PDF page 28.

nozzle used to optimise performance. The secondary exhaust nozzle also incorporates the thrust reverser. Reheat provides 18% extra thrust at takeoff. The secondary exhaust nozzle also allows reverse thrust to be provided. � Manufacturers: Rolls Royce and SNECMA � Type:
Open final report at PDF page 28Final report: Concorde F-BTSC, 25 July 2000

Air France 4590 (Concorde)

Printed page 89. PDF page 89.

The dispatcher's work screen indicated QFU 27. In addition, the non-availability of thrust reverser engine 2 thrust reverser (secondary nozzle) led to a reduction of 2.5% in the maximum weight in operation. Based on data on the wind (a twelve
Open final report at PDF page 89Final report: Concorde F-BTSC, 25 July 2000

Air France 4590 (Concorde)

Printed page 140. PDF page 140.

the maximum energy indicated in the Flight Manual (70 MJ), increased by 10%, � use of thrust reversers on engines 1, 3 and 4. With this set of hypotheses, it appears that the residual speed of the aircraft at the
Open final report at PDF page 140Final report: Concorde F-BTSC, 25 July 2000

Air France 4590 (Concorde)

Printed page 158. PDF page 158.

flight. According to his calculations, taking into account the unavailability of the thrust reverser and with the elements at his disposal, not all of which were in fact correct since the data from the AOGE software had not been updated,
Open final report at PDF page 158Final report: Concorde F-BTSC, 25 July 2000

Air France 4590 (Concorde)

Printed page 171. PDF page 171.

maintenance. 2.6 Maintenance at Continental Airlines The loss of the wear strip from the thrust reverser door on the Continental Airlines DC-10 originated from lack of rigorous maintenance. In fact, over a period of little more than a month, the
Open final report at PDF page 171Final report: Concorde F-BTSC, 25 July 2000

Air France 4590 (Concorde)

Printed page 174. PDF page 174.

was cut by a metallic strip present on the runway. � The metallic strip came from the thrust reverser cowl door of engine 3 on a DC 10 that had taken off five minutes before the Concorde. � This metallic
Open final report at PDF page 174Final report: Concorde F-BTSC, 25 July 2000