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TransAsia Airways 235

Printed page V. PDF page 10.

engines was not detected and corrected by the crew in time to restart an engine. The aircraft stalled during the attempted restart at an altitude from which the aircraft could not recover from loss of control. 9. Flight crew coordination,
Open official document at PDF page 10ASC-AOR-16-06-001: TransAsia Airways Flight GE235

TransAsia Airways 235

Printed page 160. PDF page 193.

seconds to impact, which was insufficient for a successful restart and fly away. The aircraft stalled during the attempted restart at an altitude from which the aircraft could not recover. During the simulation test (refer to 1.16.2), the investigation team
Open official document at PDF page 193ASC-AOR-16-06-001: TransAsia Airways Flight GE235

TransAsia Airways 235

Printed page 177. PDF page 210.

engines was not detected and corrected by the crew in time to restart an engine. The aircraft stalled during the attempted restart at an altitude from which the aircraft could not recover from loss of control. (1.11, 1.18, 2.3.5) 9.
Open official document at PDF page 210ASC-AOR-16-06-001: TransAsia Airways Flight GE235

TransAsia Airways 235

Printed page 290. PDF page 323.

warnings, thereby could not have been aware of the total power loss of both engines. The aircraft stalled during the attempted restart at an altitude from which the aircraft could not recover from loss of control. Findings 1. The engine
Open official document at PDF page 323ASC-AOR-16-06-001: TransAsia Airways Flight GE235

TransAsia Airways 235

Printed page II. PDF page 7.

Aviation Occurrence Report to the stall warnings in a timely and effective manner. The aircraft stalled and continued descent during the attempted engine restart. The remaining altitude and time to impact were not enough to successfully restart the engine and
Open official document at PDF page 7ASC-AOR-16-06-001: TransAsia Airways Flight GE235

TransAsia Airways 235

Printed page 284. PDF page 317.

failure. If timely and effective perception of all three analyzing such engine manner. The aircraft flight crew to misjudge failure caused by the stalled and continued the engine number 1 wiring anomaly, descent during the failed, thus CM1 continue explaining
Open official document at PDF page 317ASC-AOR-16-06-001: TransAsia Airways Flight GE235