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Printed page 73. PDF page 106.
purposes only. 3D X-ray analysis (see Figure 1.16-11) of the sensor indicated that the coil wires had broken at the outside of the bend due to the impact. Figure 1.16-10 External view of ENG 2 torque sensor left S/N CH1468Open official document at PDF page 106ASC-AOR-16-06-001: TransAsia Airways Flight GE235
Printed page 148. PDF page 181.
open circuit. The X-ray analysis (see Figure 1.16-10) of the sensor indicated that the coil wires had broken at the outside of the bend due to the impact. The AFU examination results indicated that the compromised soldering joints inside ENGOpen official document at PDF page 181ASC-AOR-16-06-001: TransAsia Airways Flight GE235