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|
Attributes | |
ACN | 1232386 |
Time | |
Date | 201501 |
Local Time Of Day | 1201-1800 |
Place | |
Locale Reference | ZZZ |
State Reference | US |
Aircraft 1 | |
Make Model Name | MD-11 |
Operating Under FAR Part | Part 121 |
Flight Phase | Landing |
Flight Plan | IFR |
Component | |
Aircraft Component | Aileron Control System |
Person 1 | |
Function | Captain Pilot Not Flying |
Events | |
Anomaly | Aircraft Equipment Problem Critical |
Narrative:
During flight control check the ailerons did not respond appropriately. Movement of the control yoke was not correct as the control wheel would not return to a neutral position. In other words; with full right or left aileron input the yoke would remain in that position without returning to center position being very difficult to move. Returned to the gate and entered the information into the log book. Maintenance worked on the issue for some time. Maintenance said that they had found some corrosion around a cannon plug that was giving info to the FCC (I believe that is what they said.) in any case; the airplane passed all the checks and was returned to service. The airplane worked well before takeoff and during all phases until the landing phase when the autopilot was turned off. The first officer and I had discussed the situation and decided it would be a good idea to shut off the autopilot and make sure all was well. After the autopilot went to dual land the first officer turned off the autopilot and quickly realized we were again having the same issue with poor aileron movement. I took the airplane and tested the controls. The ailerons were not responding well. We declared an emergency. I added about 15 knots of speed and they worked better. Ref was 156 knots which put the speed about 170 knots. We briefly discussed a G/a and decided the airplane was stable and in a good position to make a safe landing. Aileron movement was very restricted. The first officer did an outstanding job of flying a stable approach and because of this and the lack of crosswinds we were in a good position to continue to a safe landing. We were asked if we still needed assistance after landing; we declined and went to the gate where we wrote up the problem as well as briefed maintenance. The ailerons reacted as though we were fighting against the auto pilot.
Original NASA ASRS Text
Title: MD11 Captain reports discovering very stiff ailerons during the control check and returns to the gate for maintenance. Maintenance finds nothing definite after several hours of checking. The hydraulics are powered up and the ailerons are found to be normal and the flight departs. All is normal until final approach when the autopilot is switched off and the ailerons are found to be nearly frozen. The approach is continued to a successful landing.
Narrative: During flight control check the ailerons did not respond appropriately. Movement of the control yoke was not correct as the control wheel would not return to a neutral position. In other words; with full right or left aileron input the yoke would remain in that position without returning to center position being very difficult to move. Returned to the gate and entered the information into the log book. Maintenance worked on the issue for some time. Maintenance said that they had found some corrosion around a cannon plug that was giving info to the FCC (I believe that is what they said.) In any case; the airplane passed all the checks and was returned to service. The airplane worked well before takeoff and during all phases until the landing phase when the autopilot was turned off. The First Officer and I had discussed the situation and decided it would be a good idea to shut off the autopilot and make sure all was well. After the autopilot went to dual land the First Officer turned off the autopilot and quickly realized we were again having the same issue with poor aileron movement. I took the airplane and tested the controls. The ailerons were not responding well. We declared an emergency. I added about 15 knots of speed and they worked better. Ref was 156 knots which put the speed about 170 knots. We briefly discussed a G/A and decided the airplane was stable and in a good position to make a safe landing. Aileron movement was very restricted. The First Officer did an outstanding job of flying a stable approach and because of this and the lack of crosswinds we were in a good position to continue to a safe landing. We were asked if we still needed assistance after landing; we declined and went to the gate where we wrote up the problem as well as briefed maintenance. The ailerons reacted as though we were fighting against the auto pilot.
Data retrieved from NASA's ASRS site 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.