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TransAsia Airways 235

Printed page I. PDF page 6.

the required corrective actions. This led the pilot flying (PF) to retard power of the operative engine number 1 and shut down it ultimately. The loss of thrust during the initial climb and inappropriate flight control inputs by the PF
Open official document at PDF page 6ASC-AOR-16-06-001: TransAsia Airways Flight GE235

TransAsia Airways 235

Printed page V. PDF page 10.

Executive Summary operative engine number 1. 6. The flight crew's non-compliance with TransAsia Airways ATR72-600 standard operating procedures - Abnormal and Emergency Procedures for an engine flame out
Open official document at PDF page 10ASC-AOR-16-06-001: TransAsia Airways Flight GE235

TransAsia Airways 235

Printed page 176. PDF page 209.

identification and nature of the actual propulsion system malfunction and he reduced power on the operative engine number 1. (1.11, 1.18, 2.3.3) 6. The flight crew's non-compliance with TransAsia Airways ATR72-600 standard operating procedures - Abnormal and Emergency Procedures for
Open official document at PDF page 209ASC-AOR-16-06-001: TransAsia Airways Flight GE235

TransAsia Airways 235

Printed page 297. PDF page 330.

identification and nature of the actual propulsion system malfunction and he reduced power on the operative engine number 1. * Recommendation : Modify as below * 3.1.5 Following the uncommanded autofeather of engine number 2, the flight crew failed to
Open official document at PDF page 330ASC-AOR-16-06-001: TransAsia Airways Flight GE235

TransAsia Airways 235

Printed page 283. PDF page 316.

the SOP. flying (PF) to retard engine failure. 2. The wiring anomaly of power of the operative Particularly before the the engine system caused engine number 1and shut autofeather of engine an engine failure which down it ultimately. The number
Open official document at PDF page 316ASC-AOR-16-06-001: TransAsia Airways Flight GE235

TransAsia Airways 235

Printed page 284. PDF page 317.

populated residential area, flying (PF) to retard the flight director and the power of the operative FMA displayed PITCH engine number 1and shut HOLD guidance, which down it ultimately. The was contrary to the stall loss of thrust during the
Open official document at PDF page 317ASC-AOR-16-06-001: TransAsia Airways Flight GE235