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Printed page 23. PDF page 25.
cockpit. During the following seconds, all of the recorded speeds became invalid and the stall warning stopped, after having sounded continuously for 54 seconds. The altitude was then about 35,000 ft, the angle of attack exceeded 40 degrees and theOpen official document at PDF page 25Final Report: Accident on 1st June 2009 to the Airbus A330-203 registered F-GZCP operated by Air France flight AF 447
Printed page 89. PDF page 91.
led to the warning stopping. After 2 h 11 Analysis of the parameters showed that the stall warning stopped concomitant with the invalidity of the three angles of attack, and was triggered again when at least one of them becameOpen official document at PDF page 91Final Report: Accident on 1st June 2009 to the Airbus A330-203 registered F-GZCP operated by Air France flight AF 447
Printed page 88. PDF page 90.
FMGEC 1 are displayed on the right side PFD. 1.16.3.2 Analysis of the operation of the stall warning From 2 h 10 min 05 onwards, the flight control law was alternate and the stall warning triggered and stopped several timesOpen official document at PDF page 90Final Report: Accident on 1st June 2009 to the Airbus A330-203 registered F-GZCP operated by Air France flight AF 447