CESSNA 336 near Mobile, AL — 2014-07-03
- Date
- 2014-07-03
- Location
- Mobile, AL, USA
- Aircraft
- CESSNA 336
- Registration
- N3804U
- Category
- Airplane
- Highest injury
- Serious
- Fatalities
- 0
- Phase of flight
- Initial climb
Probable cause
The pilot’s inadequate preflight fuel planning during which he did not ensure that there was adequate fuel in the main tanks for the flight, which resulted in a loss of engine power.
NTSB narrative
The pilot reported that he was performing mosquito control spraying operations at 100 ft above ground level (agl) when the rear engine began to sputter and lose power. He switched to the auxiliary fuel tank; however, this did not remedy the situation. He then climbed the airplane to 500 ft agl and continued to troubleshoot the problem by again switching fuel tanks and turning the electric boost pumps on. Shortly thereafter, the front engine began to lose power. Unable to regain full power on both engines, the pilot chose to perform a forced landing in an open field. The airplane touched down on soft soil and stopped abruptly, which resulted in extensive damage to the airplane. Both fuel selectors were found in the right main fuel tank positions. An examination of the fuel system revealed that the main fuel tanks contained only residual fuel and that the auxiliary tanks contained an adequate amount of fuel. Examination of the fuel lines revealed that both supply lines from the gascolators to the engine-driven fuel pumps were contaminated and obstructed with a granular, powder-like substance. The engines ran normally when operated in a test cell after the accident. The auxiliary fuel tanks were designed for level, cruise flight only. The auxiliary tanks fed directly to the fuel selector and had no boost pumps available. It is likely that, due to the fuel system's design, adequate fuel pressure could not be regained once the main tanks were depleted and the pilot switched to the auxiliary tanks. The contamination in the fuel lines might have further restricted fuel flow to the engines. The loss of engine power might have been prevented if the pilot had maintained an adequate amount of fuel in the main tanks.
Analysis
- Primary failure mode
- Fuel management
- First missed decision gate
- Pilot should have switched to main fuel tanks before engine power loss.
NTSB coding
Evidence available
- Photos
- 24 docket documents
Docket documents24
- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1form
- FAA Inspector Statementinterview
- Statement of Party Representatives to NTSB Investigationinterview
- Documentation of Annual Inspectionother
- Evidence Controlother
- Excerpts – Airframe Logbookother
- Excerpts – Forward Engine Logbookother
- Excerpts – Rear Engine Logbookother
- NTSB Memorandum of Record MOB Weatherother
- Photo 1 – View of Aircraft Wreckage from Left Side (Photo Courtesy of FAA)photos
- Photo 10 – Rear Engine Fuel Strainer Bowlphotos
- Photo 11 – Debris Found Inside Rear Engine Fuel Strainer Bowlphotos
- Photo 12 – Debris Inside Right Main Sump Tankphotos
- Photo 13 – Front Engine Fuel Supply Line Debrisphotos
- Photo 14 – Front Engine Fuel Strainer Corrosionphotos
- Photo 2 – View of Aircraft Wreckage from Aft (Photo Courtesy of FAA)photos
- Photo 3 – View of Aircraft Wreckage from Right Side (Photo Courtesy of FAA)photos
- Photo 4 – View of Aircraft Wreckage from Front (Photo Courtesy of FAA)photos
- Photo 5 – View of Forward Fuselage and Front Engine (Photo Courtesy of FAA)photos
- Photo 6 – View of Aft Fuselage and Rear Engine (Photo Courtesy of FAA)photos
- Photo 7 – Cockpit Engine Controls (Photo Courtesy of FAA)photos
- Photo 8 – Cockpit Fuel Selector Handles (Photo Courtesy of FAA)photos
- Photo 9 – Rear Engine Fuel Supply Line Debrisphotos
- Continental Motors Front and Rear Engine Run Reportsreport
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