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Printed page IV. PDF page 9.
intermittent discontinuity between torque sensor and auto feather unit (AFU) number 2 was probably caused by the compromised soldering joints inside the AFU number 2. Flight Operations 3. The flight crew did not reject the take off when the automaticOpen official document at PDF page 9ASC-AOR-16-06-001: TransAsia Airways Flight GE235
Printed page 69. PDF page 102.
Each of those fault codes occurred on the flight prior to the occurrence and was most probably caused by the power-up sequence of the EEC, DCU, AFU, and air data computer (ADC). 1.16.5.4 Wiring Harnesses The wiring harnesses connecting theOpen official document at PDF page 102ASC-AOR-16-06-001: TransAsia Airways Flight GE235
Printed page 176. PDF page 209.
intermittent discontinuity between torque sensor and auto feather unit (AFU) number 2 was probably caused by the compromised soldering joints inside the AFU number 2. (1.6, 1.11, 1.16.5, 2.2) Flight Operations 3. The flight crew did not reject the takeOpen official document at PDF page 209ASC-AOR-16-06-001: TransAsia Airways Flight GE235