G-ONEE: electrical failures and unreliable airspeed
Printed page label not indexed. PDF page 39.
use idle thrust and 0° pitch in the event of having to action the checklist. Further planning time was curtailed by the increasing cabin altitude prompting the crew to commence an early descent, with the unreliable airspeed discussion not completedOpen official document at PDF page 39AAIB final report: G-ONEE