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|
Attributes | |
ACN | 237905 |
Time | |
Date | 199303 |
Day | Sat |
Local Time Of Day | 1201 To 1800 |
Place | |
Locale Reference | airport : mht |
State Reference | NH |
Altitude | agl bound lower : 0 agl bound upper : 0 |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Operator | general aviation : personal |
Make Model Name | Small Aircraft, High Wing, 1 Eng, Fixed Gear |
Flight Phase | landing other |
Flight Plan | None |
Person 1 | |
Affiliation | Other |
Function | flight crew : single pilot |
Qualification | pilot : private |
Experience | flight time last 90 days : 4 flight time total : 200 flight time type : 67 |
ASRS Report | 237905 |
Person 2 | |
Affiliation | government : faa |
Function | controller : local |
Qualification | controller : non radar |
Events | |
Anomaly | conflict : ground critical other anomaly other anomaly other |
Independent Detector | other flight crewa |
Resolutory Action | none taken : unable |
Consequence | other |
Supplementary | |
Primary Problem | Flight Crew Human Performance |
Air Traffic Incident | Pilot Deviation |
Narrative:
While doing a wheel landing at the manchester airport, the aircraft swerved to the left. Applying full right rudder had no effect. Differential braking stopped the swerve, but I was unable to realign the plane with the runway before it left the pavement. The plane left the runway and rolled into a mixture of melting snow and mud. When the plane hit a foot-deep snowdrift, it flipped over onto its back. I feel that this problem can be prevented by greater experience with wheel lndgs, and in particular by learning to lower the tailwheel before the rudder loses its effectiveness. A contributing factor to the early loss of rudder effectiveness is that I had about a 5 KT tailwind during this landing. A tailwind will cause the rudder to lose effectiveness earlier than expected. In the future, I will be more aware of this factor.
Original NASA ASRS Text
Title: TAIL DRAGGER PLT LOSES CTL OF ACFT ON LNDG PROC ROLLOUT IN DOWNWIND LNDG.
Narrative: WHILE DOING A WHEEL LNDG AT THE MANCHESTER ARPT, THE ACFT SWERVED TO THE L. APPLYING FULL R RUDDER HAD NO EFFECT. DIFFERENTIAL BRAKING STOPPED THE SWERVE, BUT I WAS UNABLE TO REALIGN THE PLANE WITH THE RWY BEFORE IT LEFT THE PAVEMENT. THE PLANE LEFT THE RWY AND ROLLED INTO A MIXTURE OF MELTING SNOW AND MUD. WHEN THE PLANE HIT A FOOT-DEEP SNOWDRIFT, IT FLIPPED OVER ONTO ITS BACK. I FEEL THAT THIS PROB CAN BE PREVENTED BY GREATER EXPERIENCE WITH WHEEL LNDGS, AND IN PARTICULAR BY LEARNING TO LOWER THE TAILWHEEL BEFORE THE RUDDER LOSES ITS EFFECTIVENESS. A CONTRIBUTING FACTOR TO THE EARLY LOSS OF RUDDER EFFECTIVENESS IS THAT I HAD ABOUT A 5 KT TAILWIND DURING THIS LNDG. A TAILWIND WILL CAUSE THE RUDDER TO LOSE EFFECTIVENESS EARLIER THAN EXPECTED. IN THE FUTURE, I WILL BE MORE AWARE OF THIS FACTOR.
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.