St. Augustine, FL, USA
N9431N
PIPER PA 28R-200
The flight instructor reported that, during a training flight to practice touch-and-go landings, while the airplane was climbing through 500 ft, the engine started to "sputter." The student pilot, who was flying the airplane, stated that she switched the fuel tanks just before the engine lost power but that she was unsure which tank she had selected. Due to the low altitude, the flight instructor took control of the airplane and performed an emergency landing in a marsh, during which the right wing and airframe sustained substantial damage. An examination of the airplane and engine did not reveal evidence any preimpact mechanical malfunctions or failures that would have precluded normal operation. Before takeoff, the airplane had 25 gallons of fuel onboard, and the airplane had been flown about 1 hour before the engine lost power. According to the engine operating manual, the engine's fuel consumption rate was 12.5 gallons per hour, which would have resulted in about half of the fuel supply still being available when the engine lost power, assuming that the supply of fuel in the selected fuel tank had not already been exhausted. However, the postaccident quantity of fuel onboard the airplane could not be verified due to the airplane having rested in the marsh after the accident. Therefore, based on the available evidence, the reason for the loss of engine power could not be determined.
On August 20, 2017, about 1120 eastern daylight time, a Piper PA-28R-200, N9431N, was substantially damaged during a forced landing after takeoff from Northeast Florida Regional Airport (SGJ) St Augustine, Florida. The flight instructor and student pilot sustained minor injuries. The airplane was privately owned, and the instructional flight was operated under the provisions of Title 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed at the time, and no flight plan was filed for the local flight, which originated from SGJ about 1035.According to the flight instructor, the purpose of the flight was to practice traffic pattern touch-and-go landings. The instructor said that during the run-up he told the student "not to forget to change the fuel tanks every 30 minutes." The flight instructor stated that they were on their fourth takeoff and were climbing through 500 ft when the engine started to "sputter." The flight instructor took control of the airplane, declared an emergency and landed the airplane in a marsh area. According to the student pilot, as they were climbing through 500 ft, she switched the fuel tanks while climbing and the engine "failed." The student pilot did not recall which fuel tank she switchd to prior to the loss of engine power. She passed the controls over to the instructor to perform the emergency landing. Examination of the airplane by a Federal Aviation Administration Inspector revealed the right wing and airframe was buckled. A cursory examination of the engine did not reveal any anomalies that would have precluded normal operation. Due to the airplane resting in the marsh the amount of fuel remaining in the wing tanks could not be determined. Prior to take off the airplane had a total of 25 gallons of fuel on board. According to the Lycoming engine operator's manual, the IO-360C series engine fuel consumption is 12.5 gallons per hour at performance cruise. The airplane was flown for about an hour prior to the loss of engine power.
A total loss of engine power for reasons that could not be determined because examination of the airplane and engine did not reveal evidence of any preimpact mechanical malfunctions or failures that would have precluded normal operation and because the amount of fuel onboard the airplane could not be verified.
Source: NTSB Aviation Accident Database
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