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|
Attributes | |
ACN | 198659 |
Time | |
Date | 199201 |
Day | Thu |
Local Time Of Day | 1201 To 1800 |
Place | |
Locale Reference | airport : mbj |
State Reference | FO |
Altitude | agl bound lower : 0 agl bound upper : 0 |
Environment | |
Flight Conditions | Mixed |
Light | Daylight |
Aircraft 1 | |
Controlling Facilities | tower : cvg |
Operator | common carrier : air carrier |
Make Model Name | Widebody, Low Wing, 2 Turbojet Eng |
Navigation In Use | Other Other |
Flight Phase | ground other : taxi landing other |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air carrier |
Function | flight crew : captain oversight : pic |
Qualification | pilot : commercial pilot : instrument pilot : atp |
Experience | flight time last 90 days : 150 flight time total : 18000 flight time type : 2600 |
ASRS Report | 198659 |
Person 2 | |
Affiliation | company : air carrier |
Function | flight crew : first officer |
Qualification | pilot : instrument pilot : commercial pilot : atp |
Events | |
Anomaly | aircraft equipment problem : critical other anomaly other anomaly other |
Independent Detector | other flight crewa |
Resolutory Action | other |
Consequence | other Other |
Supplementary | |
Primary Problem | Aircraft |
Air Traffic Incident | other |
Narrative:
After landing and attempting to use a right high speed turnoff, the nose wheel steering seemed stiff in the right turn. When the steering was brought back to neutral, the nose gear went hard left (approximately 90-110 degrees) and locked in that position. The aircraft was towed off the runway and to the gate. Maintenance found 1 of 2 spliced wires to the nose wheel steering electro hydraulic selector valve broken. No other damage was found, no scuff marks on the tires and no skid marks on the runway or high speed taxiway. In my opinion, in the event an electrical failure to this valve should occur, it should default to a neutral position. Failure at a higher speed then ours could be catastrophic.
Original NASA ASRS Text
Title: NOSE WHEEL STEERING FAILURE ON WDB AS ACFT WAS TURNED ON HIGH SPD TAXIWAY.
Narrative: AFTER LNDG AND ATTEMPTING TO USE A R HIGH SPD TURNOFF, THE NOSE WHEEL STEERING SEEMED STIFF IN THE R TURN. WHEN THE STEERING WAS BROUGHT BACK TO NEUTRAL, THE NOSE GEAR WENT HARD L (APPROX 90-110 DEGS) AND LOCKED IN THAT POS. THE ACFT WAS TOWED OFF THE RWY AND TO THE GATE. MAINT FOUND 1 OF 2 SPLICED WIRES TO THE NOSE WHEEL STEERING ELECTRO HYD SELECTOR VALVE BROKEN. NO OTHER DAMAGE WAS FOUND, NO SCUFF MARKS ON THE TIRES AND NO SKID MARKS ON THE RWY OR HIGH SPD TAXIWAY. IN MY OPINION, IN THE EVENT AN ELECTRICAL FAILURE TO THIS VALVE SHOULD OCCUR, IT SHOULD DEFAULT TO A NEUTRAL POS. FAILURE AT A HIGHER SPD THEN OURS COULD BE CATASTROPHIC.
Data retrieved from NASA's ASRS site as of July 2007 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.