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|
Attributes | |
ACN | 559994 |
Time | |
Date | 200209 |
Day | Thu |
Local Time Of Day | 1201 To 1800 |
Place | |
Locale Reference | airport : stl.airport |
State Reference | MO |
Altitude | agl single value : 0 |
Environment | |
Light | Daylight |
Aircraft 1 | |
Controlling Facilities | tower : ord.tower |
Operator | common carrier : air carrier |
Make Model Name | B737-300 |
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 : atp |
Experience | flight time last 90 days : 63 |
ASRS Report | 559994 |
Person 2 | |
Affiliation | company : air carrier |
Function | flight crew : first officer |
Events | |
Anomaly | other anomaly other |
Independent Detector | other flight crewa other flight crewb |
Resolutory Action | none taken : detected after the fact |
Consequence | other other |
Supplementary | |
Problem Areas | Aircraft Airport |
Primary Problem | Ambiguous |
Narrative:
Captain's takeoff. V1 was 128 KTS. At about 115 KTS, airplane abruptly swerved nose left for 1/2 seconds, which I immediately countered with right rudder. I felt no input on the rudder pedals during this yaw, and experienced no resistance on the rudder pedals as I corrected back to centerline. The airplane was completely controllable as I corrected. It seemed inappropriate to initiate a high speed rejected takeoff. Since this yaw was very brief, the aircraft experienced no further yaw problems for the remainder of the flight to den. We consulted dispatch and air carrier maintenance controller at cruise altitude, to discuss the problem and continued to a normal landing.
Original NASA ASRS Text
Title: B737-300 CREW HAD THE ACFT YAW TO THE L DURING TKOF ROLL AT STL.
Narrative: CAPT'S TKOF. V1 WAS 128 KTS. AT ABOUT 115 KTS, AIRPLANE ABRUPTLY SWERVED NOSE L FOR 1/2 SECONDS, WHICH I IMMEDIATELY COUNTERED WITH R RUDDER. I FELT NO INPUT ON THE RUDDER PEDALS DURING THIS YAW, AND EXPERIENCED NO RESISTANCE ON THE RUDDER PEDALS AS I CORRECTED BACK TO CTRLINE. THE AIRPLANE WAS COMPLETELY CONTROLLABLE AS I CORRECTED. IT SEEMED INAPPROPRIATE TO INITIATE A HIGH SPD REJECTED TKOF. SINCE THIS YAW WAS VERY BRIEF, THE ACFT EXPERIENCED NO FURTHER YAW PROBS FOR THE REMAINDER OF THE FLT TO DEN. WE CONSULTED DISPATCH AND ACR MAINT CTLR AT CRUISE ALT, TO DISCUSS THE PROB AND CONTINUED TO A NORMAL LNDG.
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.