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Printed page 20. PDF page 53.
is designed to automatically feather the propeller during takeoff and approach if the engine torque decreased below 18.5 percent rated torque. The auto-feather logic and control circuits with interlock features provided arming control and prevented auto-feather of the opOpen official document at PDF page 53ASC-AOR-16-06-001: TransAsia Airways Flight GE235
Printed page 22. PDF page 55.
indicator on the cockpit center panel. When armed, the ATPCS ‘ARM' illuminated green. If one engine's torque decreased below 18.5 percent, the ATPCS relayed an uptrim (engine power increase) command to the other engine. The uptrim resulted in increasing theOpen official document at PDF page 55ASC-AOR-16-06-001: TransAsia Airways Flight GE235
Printed page 148. PDF page 181.
the ATPCS was to automatically feather the propeller during take off in the case of engine failure, and then increase engine power (uptrim) to the opposite operating engine. The ATPCS monitors both engine torque signals, when one engine decreased belowOpen official document at PDF page 181ASC-AOR-16-06-001: TransAsia Airways Flight GE235