What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
The pilot stated he was descending into the Mt. Pleasant (mpz) airport, and at about 2000 feet, the engine began to run rough. The pilot said he actuated the carburetor heat and increased the mixture, and the engine begain to run smooth again. Shortly after that, the engine started losing power again. The pilot stated he tried selecting the right and left tanks with the electric fuel pump on. Nothing he did helped. He was unable to maintain altitude and crashed in a corn field near the town of Salem, Iowa, which is just southwest of the Mt. Pleasant Airport. One blade of the composite propeller had no visible damage; the other blade was broken off, suggesting the aircraft was not producing power at impact. The left wing tip fuel tank had a small amount of fuel; the right wing tip tank was about half full. Compression and spark were verified at all cylinders and both magnetos. The spark plugs were clean and dry. The combination fuel sump/bowl was dislodged and open to the air. There was no fuel or fuel residue in the bowl. The fuel screen was inspected and was found to be clean. The fuel selector in the aircraft was in the left position. An eyewitness statement indicates that the aircraft was sputtering and missing, and the aircraft wings were swaying slightly side to side.
As the FAA filed it
THE PILOT STATED HE WAS DESCENDING INTO THE MT. PLEASANT (MPZ) AIRPORT, AND AT ABOUT 2000 FEET, THE ENGINE BEGAN TO RUN ROUGH. THE PILOT SAID HE ACTUATED THE CARBURETOR HEAT AND INCREASED THE MIXTURE, AND THE ENGINE BEGAIN TO RUN SMOOTH AGAIN. SHORTLY AFTER THAT, THE ENGINE STARTED LOSING POWER AGAIN. THE PILOT STATED HE TRIED SELECTING THE RIGHT AND LEFT TANKS WITH THE ELECTRIC FUEL PUMP ON. NOTHING HE DID HELPED. HE WAS UNABLE TO MAINTAIN ALTITUDE AND CRASHED IN A CORN FIELD NEAR THE TOWN OF SALEM, IOWA, WHICH IS JUST SOUTHWEST OF THE MT. PLEASANT AIRPORT.ONE BLADE OF THE COMPOSITE PROPELLER HAD NO VISIBLE DAMAGE; THE OTHER BLADE WAS BROKEN OFF, SUGGESTING THE AIRCRAFT WAS NOT PRODUCING POWER AT IMPACT. THE LEFT WING TIP FUEL TANK HAD A SMALL AMOUNT OF FUEL; THE RIGHT WING TIP TANK WAS ABOUT HALF FULL. COMPRESSION AND SPARK WERE VERIFIED AT ALL CYLINDERS AND BOTH MAGNETOS. THE SPARK PLUGS WERE CLEAN AND DRY. THE COMBINATION FUEL SUMP/BOWL WAS DISLODGED AND OPEN TO THE AIR. THERE WAS NO FUEL OR FUEL RESIDUE IN THE BOWL. THE FUEL SCREEN WAS INSPECTED AND WAS FOUND TO BE CLEAN. THE FUEL SELECTOR IN THE AIRCRAFT WAS IN THE LEFT POSITION. AN EYEWITNESS STATEMENT INDICATES THAT THE AIRCRAFT WAS SPUTTERING AND MISSING, AND THE AIRCRAFT WINGS WERE SWAYING SLIGHTLY SIDE TO SIDE.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.