CESSNA 172P near Spruce Creek, FL — 2014-09-11
- Date
- 2014-09-11
- Location
- Spruce Creek, FL, USA
- Airport
- 7FL6
- Aircraft
- CESSNA 172P
- Registration
- N63835
- Category
- Airplane
- Highest injury
- Minor
- Fatalities
- 0
- Phase of flight
- Approach
Probable cause
A total loss of engine power due to fuel exhaustion, which resulted from the pilots’ improper preflight and in-flight fuel planning.
NTSB narrative
The flight instructor and pilot receiving instruction departed on a training flight, and the pilot stated that the fuel tanks were "almost full." After 3 hours 24 minutes of flight, which included three full-power takeoffs and climbs, the engine experienced a total loss of power on final approach to the destination airport. According to Federal Aviation Administration air traffic control records, multiple one-leg flight plans were filed for the flight. Based on this information, the estimated fuel endurance was 3 hours 20 minutes. The pilot receiving instruction stated that the fuel selector was in the "both" position throughout the flight but that, on final approach, he noticed that the fuel selector had been switched to the "right" tank position, so he moved the fuel selector back to the "both" position. Shortly thereafter, the engine stopped producing power. The flight instructor stated that the pilot inadvertently selected the "off" position instead of the "both" position when he moved the fuel selector from the "right" tank position. During the subsequent forced landing, the airplane's cabin and fuselage were damaged, but both wing fuel tanks remained intact. No signs of in-flight or postaccident fuel leakage were found. Postaccident examination showed that the left wing tank contained no fuel and that the right wing tank contained about 3 gallons of fuel. A test run of the engine was performed following the accident using the fuel found in the right wing tank. The engine started immediately, accelerated smoothly, and ran continuously with no anomalies observed. According to the airplane manufacturer, the airplane's fuel tanks had a total capacity of 43 gallons, of which 3 gallons were unusable. Based on this information, it is likely that the pilots exhausted all of the usable fuel during the flight, which resulted in a total loss of engine power on final approach to their destination airport.
Analysis
- Primary failure mode
- Fuel management
- First missed decision gate
- Pilot should have ensured fuel was adequate before flight and during approach.
NTSB coding
Evidence available
- Photos
- 9 docket documents
Docket documents9
- Air Traffic Control Overviewatc
- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1form
- Memorandum for Record - Pilot Interview Summaryinterview
- Pilot Statementinterview
- Recovery Specialist Statementinterview
- Movie 1 – Engine Start at Crash Site (Recovery Team)other
- Movie 2 - – Engine Shutdown at Conclusion of Engine Run(Recovery Team)other
- Photo 1 – Main Wreckage (Photo Courtesy of FAA)photos
- Photo 2 – Wreckage Facing Opposite Direction (Photo Courtesy of FAA)photos
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