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Printed page 3. PDF page 36.
feathered. At 1052:43 the PF stated “i will pull back engine one throttle”. The PM responded “wait a second cross check”, but the ENG 1 power lever angle (PLA6) had already been retarded from 75 degrees to 66 degrees. TheOpen official document at PDF page 36ASC-AOR-16-06-001: TransAsia Airways Flight GE235
Printed page 214. PDF page 247.
(pitch trim 倚枧) 10 52 43.0 CAM [sound of pitch trim] 䫱ᶨᶳ cross check 10 52 43.6 CAM-2 [wait a secondcross check] 10 52 44.8 CAM (sound of single cavalry charge) 10 52 46.1 CAM-1 heading mode 10 52 46.6Open official document at PDF page 247ASC-AOR-16-06-001: TransAsia Airways Flight GE235