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G-ONEE: electrical failures and unreliable airspeed

Printed page label not indexed. PDF page 3.

disagree alert and they reported that they were about to intervene, when descending through 10,000 ft the indicated airspeed rose rapidly as the aircraft left icing conditions and the pitot probes cleared. The autopilot reacted to the speed increase by
Open official document at PDF page 3AAIB final report: G-ONEE

G-ONEE: electrical failures and unreliable airspeed

Printed page label not indexed. PDF page 38.

display the current cabin altitude in amber. There are no other alerts until it reaches 10,000 ft when a cabin altitude warning is generated. Approximately 10 minutes after the aircraft reached FL250 the cabin altitude began to climb from 3,000
Open official document at PDF page 38AAIB final report: G-ONEE

G-ONEE: electrical failures and unreliable airspeed

Printed page 23. PDF page 25.

35,000 ft, the angle of attack exceeded 40 degrees and the vertical speed was about -10,000 ft/min. The aeroplane's pitch attitude did not exceed 15 degrees and the engines' N1's were close to 100%. The aeroplane was subject to roll
Open 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