TOTAL LOSS OF ENGINE POWER DUE TO FUEL EXHAUSTION. CONTRIBUTING TO THE ACCIDENT WAS THE FAILURE OF THE PILOT TO LEAN THE FUEL/AIR MIXTURE DURING CRUISE FLIGHT WHICH INCREASED THE FUEL CONSUMPTION FOR THE FLIGHT.
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.
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.
Engine fuel and control · float · stickingJun 6, 2004
ON SHORT FINAL THE ENGINE LOST POWER. A DECISION WAS MAKE TO MAKE AN OFF FIELD LANDING IN A CORNFIELD. FOLLOW-UP STATIC RUN SHOW NO PROBLEMS AND TEST FLIGHT WAS SCHEDULED. DURING THE TEST FLIGHT ENGINE POWER LOSS TOOK PLACE ON SHORT FINAL. CARBURETOR WAS REMOVED AND INSPECTED FINDING MARKS ON THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.