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TransAsia Airways 235

Printed page I. PDF page 6.

pusher. After the engine number 1 was shut down, the loss of power from both engines was not detected and corrected by the crew in time to restart engine number 1. The crew did not respond I
Open official document at PDF page 6ASC-AOR-16-06-001: TransAsia Airways Flight GE235

TransAsia Airways 235

Printed page V. PDF page 10.

warnings in a timely and effective manner. 8. The loss of power from both 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
Open official document at PDF page 10ASC-AOR-16-06-001: TransAsia Airways Flight GE235

TransAsia Airways 235

Printed page 177. PDF page 210.

Conclusion effective manner. (1.11, 1.18, 2.3.3) 8. The loss of power from both 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
Open official document at PDF page 210ASC-AOR-16-06-001: TransAsia Airways Flight GE235

TransAsia Airways 235

Printed page 289. PDF page 322.

(Recommend to delete it. Please refer to note 2.) 8. The loss of power from both engines was not detected and corrected by the crew in time to restart an engine.Due to the total power loss of both engines, it
Open official document at PDF page 322ASC-AOR-16-06-001: TransAsia Airways Flight GE235

TransAsia Airways 235

Printed page 285. PDF page 318.

loss of communication channel, power from both engines encountering consecutive was not detected and activation of MASTER corrected by the crew in WARNINGs, the time to restart workload of flight crew enginenumber The crew was beyond normal did not respond
Open official document at PDF page 318ASC-AOR-16-06-001: TransAsia Airways Flight GE235