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TransAsia Airways 235

Printed page V. PDF page 10.

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, communication, and threat and error management (TEM) were less
Open official document at PDF page 10ASC-AOR-16-06-001: TransAsia Airways Flight GE235

TransAsia Airways 235

Printed page 160. PDF page 193.

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 found that the flight director bars provided a
Open official document at PDF page 193ASC-AOR-16-06-001: TransAsia Airways Flight GE235

TransAsia Airways 235

Printed page 177. PDF page 210.

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. Flight crew coordination, communication, and threat and error management
Open official document at PDF page 210ASC-AOR-16-06-001: TransAsia Airways Flight GE235

TransAsia Airways 235

Printed page 290. PDF page 323.

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 1. The engine 1. In addition to the AFU Related
Open official document at PDF page 323ASC-AOR-16-06-001: TransAsia Airways Flight GE235

TransAsia Airways 235

Printed page 288. PDF page 321.

flight crew attempted restart at an possibility to clarify the might not be able to altitude from which the false perception of the handle such event aircraft could not flight crew to misjudge immediately. Let along recoverfrom loss of the
Open official document at PDF page 321ASC-AOR-16-06-001: TransAsia Airways Flight GE235