PLT STATED THAT IMMEDIATELY AFTER TOUCHDOWN, THE RIGHT WHEEL SEEMED TO DRAG. RIGHT DRIFT WAS INITIALLY CORRECTED BY USE OF OPPOSITE AILERON TO REDUCE WEIGHT ON RIGHT WHEEL AND RUDDER FOR DIRECTIONAL CONTROL. HOWEVER, AS THE ACFT SLOWED WEIGHT SETTLED ON THE RIGHT WHEEL, THE ACFT SWEREVED TO THE RIGHT AND NOSED OVER. POST-MISHAP EXAMINATION OF ACFT BRAKE REVEALED NO DISCREPANCIES.
AFTER A BRIEF STOP AT OAKS, ND, FOR FUEL, THE PLT TOOK OFF TO FLY ABOUT 5 MI TO HIS PRIVATE STRIP IN AN ALFALFA FIELD. DURING THE LANDING ROLL, THE GEAR HIT A GOPHER MOUND & THE ACFT NOSED OVER.
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
No ADs published since 1998 matched this airframe or engine model.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (0)
No Service Difficulty Reports found for this airframe since 1995.