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Printed page IV. PDF page 9.
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 automatic take offOpen official document at PDF page 9ASC-AOR-16-06-001: TransAsia Airways Flight GE235
Printed page 148. PDF page 181.
outside of the bend due to the impact. The AFU examination results indicated that the compromised soldering joints inside ENG 2 AFU which formed part of the connection between ENG 2 torque sensor and the AFU No.2 had increased anOpen official document at PDF page 181ASC-AOR-16-06-001: TransAsia Airways Flight GE235
Printed page 150. PDF page 183.
April 2014 respectively and the service periods89 were less than one year. The similar compromised soldering joints were found in these two units. The engine manufacturer (P&WC) had been aware of AFU-related technical issues causing uncommanded autofeather events since 20Open official document at PDF page 183ASC-AOR-16-06-001: TransAsia Airways Flight GE235
Printed page 176. PDF page 209.
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 take off whenOpen official document at PDF page 209ASC-AOR-16-06-001: TransAsia Airways Flight GE235