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Printed page label not indexed. PDF page 1.
nose-down to regain indicated airspeed. The pitch reached 7.6° nose-down with an associated 6,240 ft/min descent rate, before the aircraft exited icing conditions, correct airspeed was regained and the autopilot pitched up. The descent had resulted in an 18 ktOpen official document at PDF page 1AAIB final report: G-ONEE
Printed page label not indexed. PDF page 3.
continued to pitch further nose-down reaching a recorded 7.6° nose-down with associated 6,240 ft/min rate of descent. The crew recalled receiving an ias disagree alert and they reported that they were about to intervene, when descending through 10,000 ft theOpen official document at PDF page 3AAIB final report: G-ONEE
Printed page label not indexed. PDF page 10.
The aircraft pitch reached 7.6° nose-down and the descent rate reached approximately 6,240 ft/min. With decreasing recorded IAS, the crew briefly manually increased the thrust. As the TAT probe temperature started to climb from freezing point, indicating that it wasOpen official document at PDF page 10AAIB final report: G-ONEE
Printed page label not indexed. PDF page 39.
pitch commands and a rapidly increasing rate of descent, reaching 7.6° nose-down and 6,240 ft/min. The event coincided with a handover of control between the PF and PM, and it is possible that this distraction delayed their recognition of theOpen official document at PDF page 39AAIB final report: G-ONEE
Printed page label not indexed. PDF page 42.
but allowed the autopilot to pitch the aircraft nose-down to -7.6° with an associated 6,240 ft/min descent rate. The crew were about to intervene when the autopilot began correcting the pitch as the aircraft exited icing conditions, and the correctOpen official document at PDF page 42AAIB final report: G-ONEE