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|
Attributes | |
ACN | 772328 |
Time | |
Date | 200801 |
Local Time Of Day | 1201 To 1800 |
Place | |
Locale Reference | airport : atl.airport |
State Reference | GA |
Altitude | agl single value : 0 |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Operator | common carrier : air carrier |
Make Model Name | B757-200 |
Operating Under FAR Part | Part 121 |
Flight Phase | ground : takeoff roll |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air carrier |
Function | flight crew : captain oversight : pic |
Qualification | pilot : commercial pilot : flight engineer pilot : instrument pilot : multi engine pilot : atp |
Experience | flight time last 90 days : 90 flight time total : 14000 flight time type : 2500 |
ASRS Report | 772328 |
Events | |
Anomaly | aircraft equipment problem : less severe non adherence : company policies |
Independent Detector | aircraft equipment other aircraft equipment : eicas other flight crewa |
Resolutory Action | flight crew : rejected takeoff |
Supplementary | |
Problem Areas | Aircraft Flight Crew Human Performance |
Primary Problem | Aircraft |
Narrative:
During takeoff roll at approximately 85-90 KTS I noticed a right hydraulic pump message on the upper EICAS; with an associated pressure light on the right engine driven hydraulic pump on the overhead panel. I made the command decision to abort the takeoff. Autobrakes were applied at approximately 100 KTS. The aircraft was returned to the gate uneventfully. No passenger injuries were reported. No damage to the aircraft was apparent. Wheel brakes did not overheat. All applicable fom; logbook and quick reference manual procedures were referenced and complied with. Factor in the decision to abort: the aircraft on the previous segment was returned to the gate with total right hydraulic failure. The right main gear anti-skid assembly was replaced and the aircraft returned to service. When the hydraulic pump came on I thought I may have lost all hydraulics on the right system.
Original NASA ASRS Text
Title: B757 FLT CREW EXPERIENCES HYDRAULIC PUMP FAILURE DURING TKOF AND CAPT ELECTS TO REJECT AT 100 KTS AND RETURN TO THE GATE.
Narrative: DURING TKOF ROLL AT APPROX 85-90 KTS I NOTICED A R HYD PUMP MESSAGE ON THE UPPER EICAS; WITH AN ASSOCIATED PRESSURE LIGHT ON THE R ENG DRIVEN HYD PUMP ON THE OVERHEAD PANEL. I MADE THE COMMAND DECISION TO ABORT THE TKOF. AUTOBRAKES WERE APPLIED AT APPROX 100 KTS. THE ACFT WAS RETURNED TO THE GATE UNEVENTFULLY. NO PAX INJURIES WERE RPTED. NO DAMAGE TO THE ACFT WAS APPARENT. WHEEL BRAKES DID NOT OVERHEAT. ALL APPLICABLE FOM; LOGBOOK AND QUICK REF MANUAL PROCS WERE REFED AND COMPLIED WITH. FACTOR IN THE DECISION TO ABORT: THE ACFT ON THE PREVIOUS SEGMENT WAS RETURNED TO THE GATE WITH TOTAL R HYD FAILURE. THE R MAIN GEAR ANTI-SKID ASSEMBLY WAS REPLACED AND THE ACFT RETURNED TO SVC. WHEN THE HYD PUMP CAME ON I THOUGHT I MAY HAVE LOST ALL HYDS ON THE R SYS.
Data retrieved from NASA's ASRS site as of May 2009 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.