| Crash location | 37.870000°N, 96.690000°W
Reported location is a long distance from the NTSB's reported nearest city. This often means that the location has a typo, or is incorrect. |
| Nearest city | El Dorado, KS
37.817240°N, 96.862252°W 10.1 miles away |
| Tail number | N61024 |
|---|---|
| Accident date | 03 Feb 2018 |
| Aircraft type | Cessna 150 |
| Additional details: | None |
The pilot reported that en route, he noticed a drop in the airplane's engine RPM. He noted that the fuel shut off valve was open, and the gas gauges showed half full in the right tank and quarter full in the left tank. He added that the carburetor heat was off, the mixture was full rich, and then the engine quit running. During the third attempt to restart the engine, it briefly started and then quit again. Subsequently, during an off-airport landing in a field, the airplane nosed over.
The airplane sustained substantial damage to the empennage and fuselage.
The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. He added, that he had filled the gas "to the top" (22.5 gallons) prior to departure and had flown for 3.7 hours.
The 1969 Cessna 150 owner's manual states that the airplane's maximum range was 4.1 hours with no reserve at 75% power at 7,000 ft.
The pilot further reported in a telephone conversation with the National Transportation Safety Board investigator-in-charge that, he did not consult the emergency checklist as it was placed in the glovebox.
FAA inspectors drained the fuel tanks about 5 days after the accident and reported that there was no evidence of fuel leakage around the fuel caps or on the ground. They drained about 8-12 ounces from the left wing tank and about ¾ of a gallon from the right wing tank. The FAA added that the engine showed proper continuity and the magnetos were operational. The engine was not run due to a fractured intake manifold just above the carburetor base flange. The fracture damage to the intake manifold was consistent with impact damage.
The pilot’s improper fuel planning, which resulted in a total loss of engine power due to fuel exhaustion and a subsequent off-airport landing and nose-over.