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|
Attributes | |
ACN | 895650 |
Time | |
Date | 201006 |
Local Time Of Day | 1801-2400 |
Place | |
Locale Reference | ZZZ.ARTCC |
State Reference | US |
Environment | |
Light | Night |
Aircraft 1 | |
Make Model Name | B757 Undifferentiated or Other Model |
Operating Under FAR Part | Part 121 |
Flight Phase | Climb |
Component | |
Aircraft Component | Hydraulic System Pump |
Person 1 | |
Function | Pilot Not Flying Captain |
Qualification | Flight Crew Air Transport Pilot (ATP) |
Person 2 | |
Function | First Officer Pilot Flying |
Events | |
Anomaly | Aircraft Equipment Problem Critical |
Narrative:
Just prior to reaching top of climb; we received a 'left hydraulic pump' EICAS message with associated 'press' light illuminated in the left hyp pump switch. QRH calls for affected pump switch off. We complied and then received a lower EICAS message 'power xfer unit.' we checked MEL and operating manual for explanation of message. Both references stated that the power xfer unit message is a 'failure of circuitry for power transfer unit protection.' we had a three way conversation with the dispatcher and a maintenance person. After a lengthy conversation; it was determined that the ptu (power transfer unit) was not operating properly and given the condition of the engine driven pump; any further degradation of the left hydraulic system would put the aircraft in real jeopardy. I elected to divert and we obtained a clearance and since we were on the edge of making an overweight landing; requested arff to be mobilized and available upon landing.
Original NASA ASRS Text
Title: B757 flight crew experienced an engine driven hydraulic pump failure nearing top of climb on an oceanic flight. An indication of PTU failure was also received; the crew diverted for maintenance.
Narrative: Just prior to reaching top of climb; we received a 'L HYD PUMP' EICAS message with associated 'press' light illuminated in the L HYP PUMP SWITCH. QRH calls for affected pump switch off. We complied and then received a lower EICAS message 'POWER XFER UNIT.' We checked MEL and operating manual for explanation of message. Both references stated that the POWER XFER UNIT message is a 'Failure of circuitry for power transfer unit protection.' We had a three way conversation with the Dispatcher and a maintenance person. After a lengthy conversation; it was determined that the PTU (power transfer unit) was not operating properly and given the condition of the engine driven pump; any further degradation of the left hydraulic system would put the aircraft in real jeopardy. I elected to divert and we obtained a clearance and since we were on the edge of making an overweight landing; requested ARFF to be mobilized and available upon landing.
Data retrieved from NASA's ASRS site as of April 2012 and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.