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Printed page IV. PDF page 9.
education, and improvement purposes. Findings Related to Probable Causes Powerplant 1. An intermittent signal discontinuity between the auto feather unit (AFU) number 2 and the torque sensor may have caused the automatic take off power control system (ATPCS): NotOpen official document at PDF page 9ASC-AOR-16-06-001: TransAsia Airways Flight GE235
Printed page 149. PDF page 182.
and were higher than the prescribed values in CMM when the ribbon was moved by hand. Intermittent signal discontinuity produces an unstable torque signal to AFU and can adversely affect the functioning of the ATPCS, including unreliable arming and inadvertentOpen official document at PDF page 182ASC-AOR-16-06-001: TransAsia Airways Flight GE235
Printed page 175. PDF page 208.
education, and improvement purposes. 3.1 Findings Related to Probable Causes Powerplant 1. An intermittent signal discontinuity between the autofeather unit (AFU) number 2 and the torque sensor may havecaused the automatic takeoff power control system 175Open official document at PDF page 208ASC-AOR-16-06-001: TransAsia Airways Flight GE235
Printed page 148. PDF page 181.
No.2 had increased an unstable signal path resistance, therefore, may have produced an intermittent discontinuity of the torque signal. Continuity of the signal was required to ensure that the ATPCS system functioned as expected. The disrupted signal probably resulted inOpen official document at PDF page 181ASC-AOR-16-06-001: TransAsia Airways Flight GE235