According to the pilots, while in cruise flight at 6,500 feet mean sea level, the engine lost partial power. The flight instructor applied full rich mixture and carburetor heat. Maintaining partial engine power, the flight diverted to a nearby airport. The pilots were unable to activate the pilot-controlled lighting at the airport and elected to utilize the airport's rotating beacon to locate the runway. The runway was located; however, the airplane was not in a position to make a landing, and the flight instructor applied full power in order to perform a go-around. During the go-around the engine experienced a total loss of power, and the flight instructor subsequently executed a forced landing to a nearby road. During the landing, the airplane struck a utility pole and nosed over. A postaccident test run of the engine revealed no evidence of any mechanical anomalies. According to postaccident photographs of the cockpit, the audio control panel was selected to Comm 1; however, Comm 2 was the radio that was set to the airport's common traffic advisory frequency, which was used for the pilot-controlled lighting. The airplane was operating in conditions conducive to serious carburetor icing at cruise power at the time of the accident. The probability existed that the airplane was operated in an area conducive to induction icing, and, although the flight instructor applied carburetor heat, the accumulation of the ice was greater than the application of heat could melt. It is further possible that during the go-around the abrupt throttle movement to the full power setting caused the total loss of engine power.

The National Transportation Safety Board determines the probable cause(s) of this accident to be:

Index for Mar2012 | Index of months