What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) Shortly after departure from a private airstrip in Callao, Missouri, pilot states that the engine began to run rough, with the engine tachometer fluctuating between 1800 and 2000 RPM. Carburetor heat was applied with no apparent change to engine performance. At that point, the pilot decided to return to the local airstrip. While approaching the airstrip, the pilot noted that the tachometer was indicating between 1100 and 1300 RPM. Pilot states that due to the lack of available power and rising terrain he decided to approach straight-in for a downwind landing. The aircraft landed on the wet grass/muddy runway, sliding off the end and impacting a gravel road (fireworks ave), at which time the nose wheel assembly broke off. This caused the aircraft to pitch nose down, flipping the aircraft upside down upon a barbed-wire fence on the east side of fireworks ave. post accident inspection found no engine compression on number two cylinder. Subsequent tear-down inspection revealed piston head erosion with damage extending completely through the piston. This condition is consistent with a piston exposed to an elevated operating temperature.
As the FAA filed it
(-23) SHORTLY AFTER DEPARTURE FROM A PRIVATE AIRSTRIP IN CALLAO, MISSOURI, PILOT STATES THAT THE ENGINE BEGAN TO RUN ROUGH, WITH THE ENGINE TACHOMETER FLUCTUATING BETWEEN 1800 AND 2000 RPM. CARBURETOR HEAT WAS APPLIED WITH NO APPARENT CHANGE TO ENGINE PERFORMANCE. AT THAT POINT, THE PILOT DECIDED TO RETURN TO THE LOCAL AIRSTRIP. WHILE APPROACHING THE AIRSTRIP, THE PILOT NOTED THAT THE TACHOMETER WAS INDICATING BETWEEN 1100 AND 1300 RPM. PILOT STATES THAT DUE TO THE LACK OF AVAILABLE POWER AND RISING TERRAIN HE DECIDED TO APPROACH STRAIGHT-IN FOR A DOWNWIND LANDING. THE AIRCRAFT LANDED ON THE WET GRASS/MUDDY RUNWAY, SLIDING OFF THE END AND IMPACTING A GRAVEL ROAD (FIREWORKS AVE), AT WHICH TIME THE NOSE WHEEL ASSEMBLY BROKE OFF. THIS CAUSED THE AIRCRAFT TO PITCH NOSE DOWN, FLIPPING THE AIRCRAFT UPSIDE DOWN UPON A BARBED-WIRE FENCE ON THE EAST SIDE OF FIREWORKS AVE. POST ACCIDENT INSPECTION FOUND NO ENGINE COMPRESSION ON NUMBER TWO CYLINDER. SUBSEQUENT TEAR-DOWN INSPECTION REVEALED PISTON HEAD EROSION WITH DAMAGE EXTENDING COMPLETELY THROUGH THE PISTON. THIS CONDITION IS CONSISTENT WITH A PISTON EXPOSED TO AN ELEVATED OPERATING TEMPERATURE.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.
Other reports on N275SW · 1
Matched to the same aircraft by N-number and date.