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|
Attributes | |
ACN | 781801 |
Time | |
Date | 200804 |
Place | |
Locale Reference | airport : zzz.airport |
State Reference | US |
Altitude | msl single value : 6500 |
Environment | |
Flight Conditions | VMC |
Light | Dusk |
Aircraft 1 | |
Controlling Facilities | tracon : zzz.tracon tower : elp.tower |
Operator | general aviation : instructional |
Make Model Name | Eclipse 500 |
Operating Under FAR Part | Part 91 |
Flight Phase | cruise : level |
Route In Use | enroute : on vectors |
Flight Plan | IFR |
Person 1 | |
Affiliation | other |
Function | instruction : instructor oversight : pic |
Qualification | pilot : cfi pilot : multi engine pilot : atp |
Experience | flight time last 90 days : 180 flight time total : 23000 flight time type : 400 |
ASRS Report | 781801 |
Events | |
Anomaly | aircraft equipment problem : critical |
Independent Detector | other flight crewa |
Resolutory Action | flight crew : landed in emergency condition flight crew : diverted to another airport |
Supplementary | |
Problem Areas | Aircraft |
Primary Problem | Aircraft |
Narrative:
Simulated single engine climb for airwork when student trimmed the rudder for the failed engine; this is when the rudder trim 'froze' in the full left position. Alternate was used to be available. A check at the rudder freedom was done and yielded only a couple of degrees of motion to the right. We therefore decided to divert to the nearest airfield in which the crosswind would be from the right of the nose. We diverted to ZZZ and landed. Winds were from the right 290 degrees/15 KTS. The landing was uneventful. Callback conversation with reporter revealed the following information: the landing was completely uneventful and the aircraft was taxied to the ramp. Since the EA50 rudder trim is interfaced through the central aircraft computer it was decided to completely power down the aircraft and allow the computer to reboot. This had the desired effect and the rudder trim functioned normally afterward. The exact problem with the central aircraft computer that caused this incident is unknown.
Original NASA ASRS Text
Title: EA50 INSTRUCTOR REPORTS RUDDER TRIM STUCK IN THE FULL LEFT POSITION DURING TRAINING.
Narrative: SIMULATED SINGLE ENG CLB FOR AIRWORK WHEN STUDENT TRIMMED THE RUDDER FOR THE FAILED ENG; THIS IS WHEN THE RUDDER TRIM 'FROZE' IN THE FULL L POS. ALTERNATE WAS USED TO BE AVAILABLE. A CHK AT THE RUDDER FREEDOM WAS DONE AND YIELDED ONLY A COUPLE OF DEGS OF MOTION TO THE R. WE THEREFORE DECIDED TO DIVERT TO THE NEAREST AIRFIELD IN WHICH THE XWIND WOULD BE FROM THE R OF THE NOSE. WE DIVERTED TO ZZZ AND LANDED. WINDS WERE FROM THE R 290 DEGS/15 KTS. THE LNDG WAS UNEVENTFUL. CALLBACK CONVERSATION WITH RPTR REVEALED THE FOLLOWING INFO: THE LANDING WAS COMPLETELY UNEVENTFUL AND THE ACFT WAS TAXIED TO THE RAMP. SINCE THE EA50 RUDDER TRIM IS INTERFACED THROUGH THE CENTRAL ACFT COMPUTER IT WAS DECIDED TO COMPLETELY POWER DOWN THE ACFT AND ALLOW THE COMPUTER TO REBOOT. THIS HAD THE DESIRED EFFECT AND THE RUDDER TRIM FUNCTIONED NORMALLY AFTERWARD. THE EXACT PROBLEM WITH THE CENTRAL ACFT COMPUTER THAT CAUSED THIS INCIDENT IS UNKNOWN.
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.