BEECH C24R near Titusville, FL — 2014-07-10
- Date
- 2014-07-10
- Location
- Titusville, FL, USA
- Airport
- X21
- Aircraft
- BEECH C24R
- Registration
- N6222Q
- Category
- Airplane
- Highest injury
- Minor
- Fatalities
- 0
- Phase of flight
- Cruise
Probable cause
The pilot's failure to secure the fuel strainer drain during the preflight inspection, which resulted in a total loss of engine power due to fuel exhaustion.
NTSB narrative
The pilot reported that, while conducting a preflight inspection, he looked inside the wing fuel tanks and estimated that there was about 27 gallons of fuel. He then departed on a local flight to test the avionics and autopilot system. While returning to the airport after an approximate 1-hour flight, the engine experienced a total loss of power, and the pilot attempted a forced landing on the roof of a building. The airplane crashed through the roof, which resulted in substantial damage to the wings, fuselage, and flight control surfaces. No visible fuel or fuel odor was noted at the accident site. A postaccident examination of the airplane revealed that both fuel tanks had been breached and were void of fuel. The fuel strainer sump, which sits forward of the firewall below the fuselage, was found in the open-and-locked position. When the strainer valve's tangs were pushed up and rotated counter-clockwise, the sump remained in the open-and-locked position. The sump sprang back to the closed position when the tangs were pushed up and released. Postaccident fuel consumption calculations and fuel strainer drain testing revealed that the airplane would have burned through and lost about 28 gallons of fuel during the approximate 1-hour flight with the strainer drain not properly secured.
Analysis
- Primary failure mode
- Fuel management
- First missed decision gate
- Pilot could have checked fuel levels more accurately before flight.
NTSB coding
Evidence available
- Photos
- 16 docket documents
Docket documents16
- Air Traffic Control Statementsatc
- Evidence Control Form –Strainer Sumpform
- Fuel Performance Calculationsform
- Party Formform
- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1form
- Strainer Drain Valve Informationform
- Pilot and Passenger Statementsinterview
- Beechcraft C24R Fuel System Descriptionother
- Correspondence with Airframe Manufacturerother
- Correspondence with FAAother
- Photo 1 - Airplane at Accident Site (Photo Courtesy of FAA)photos
- Photo 2 - Airplane at Recovery Facility (Photo Courtesy of FAA)photos
- Photo 3 - Fuel Strainer Sump Valvephotos
- Photo 4 - Fuel Strainerphotos
- Weather Report and Recordreport
- Release of Wreckagewreckage
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