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Printed page V. PDF page 10.
implemented by the engine manufacturer to address this issue before the occurrence was not sufficiently effective. The engine manufacturer has issued a modification addressing the specific VOpen official document at PDF page 10ASC-AOR-16-06-001: TransAsia Airways Flight GE235
Printed page 151. PDF page 184.
countermeasures implemented by the engine manufacturer to address the AFU continuity problems were not sufficiently effective and require further solutions. During this occurrence investigation, the engine manufacturer, Pratt & Whitney Canada, informed the investigation team that a pOpen official document at PDF page 184ASC-AOR-16-06-001: TransAsia Airways Flight GE235
Printed page 177. PDF page 210.
implemented by the engine manufacturer to address this issue before the occurrence was not sufficiently effective. The engine manufacturer has issued a modification addressing the specific finding of this investigation. This new modification is currently implemented in alOpen official document at PDF page 210ASC-AOR-16-06-001: TransAsia Airways Flight GE235
Printed page 290. PDF page 323.
failure before the occurrence was before the occurrence was investigation in the cases not sufficiently effective. not sufficiently effective. and found the internal The engine manufacturer The engine manufacturer circuit board contact has issued a modification has issuedOpen official document at PDF page 323ASC-AOR-16-06-001: TransAsia Airways Flight GE235