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Printed page 4. PDF page 37.
occurrence flight. The indicated airspeed was 102 knots. The AFCS IAS mode then reverted into PITCH HOLD mode7 and one second later the stall warning annunciated in the cockpit for one second. The PF then stated “terrain ahead” and theOpen official document at PDF page 37ASC-AOR-16-06-001: TransAsia Airways Flight GE235
Printed page 110. PDF page 143.
AP is engaged while the vertical FD orders are not followed, the reversion is done in pitch hold mode. (AP basic mode) General information of AFCS The part 2, limitations and procedures, "procedure and techniques" contains the following general informationOpen official document at PDF page 143ASC-AOR-16-06-001: TransAsia Airways Flight GE235
Printed page 53. PDF page 86.
been observed in the stall test; as the FMA vertical mode had previously reverted to “PITCH HOLD” mode, the flight director (FD) bars provided guidance to maintain a pitch target of 8°. When the stick shaker and subsequently the stickOpen official document at PDF page 86ASC-AOR-16-06-001: TransAsia Airways Flight GE235
Printed page 109. PDF page 142.
the following : - stabilizing the aircraft around its center of gravity while holding pitch attitude and heading, wing level or bank angle (AP in basic modes). - flying automatically any upper or basic mode or anymode except GO AROUNDOpen official document at PDF page 142ASC-AOR-16-06-001: TransAsia Airways Flight GE235
Printed page 282. PDF page 315.
of engine number 2, the flight director reverted to basic mode and the FMA displayed PITCH HOLD guidance, which was contrary to the stall recovery, causing the confusion indication to the flight crew while aircraft was under an approach-to-stall condition.Open official document at PDF page 315ASC-AOR-16-06-001: TransAsia Airways Flight GE235