The pilot's failure to maintain directional control on landing rollout resulting in an inadvertent ground loop, and on-ground collision between the left wing and the runway. Contributing to the accident was the pilot's total lack of experience in kind of aircraft.
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 (1)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
THE CRANKSHAFT APPEARS TO HAVE FRACTURED AT THE CRANK PIN. SEPARATING THE CRANK PIN AND ROD ASSEMBLY FROM THE PROPELLER SHAFT. THE AIRCRAFT WAS IN THE PROCESS OF BEING FERRIED CROSS COUNTRY. THE AIRCRAFT IS USED FOR AEROBATIC PERFORMANCES. (SW15200318971)
From FAA Service Difficulty Reports; matched by N-number and serial number.