NEBERT VANS RV-10 near Toledo, OR — 2014-05-31
- Date
- 2014-05-31
- Location
- Toledo, OR, USA
- Aircraft
- NEBERT VANS RV-10
- Registration
- N62DN
- Category
- Airplane
- Highest injury
- Fatal
- Fatalities
- 2
- Phase of flight
- Maneuvering
Probable cause
A total loss of engine power due to fuel starvation because of a blocked fuel line that resulted from the pilot’s improper maintenance practices and the pilot’s subsequent failure to maintain adequate airspeed while attempting a forced landing, which led to the airplane exceeding its critical angle-of-attack and experiencing an aerodynamic stall.
NTSB narrative
The pilot, who was also the builder of the experimental kit airplane, departed for a cross-country flight from his home airport. The passenger reported that, following a normal departure, the airplane continued the takeoff climb through some cloud wisps and ascended above a lower cloud cover with an overcast layer above. Suddenly, the engine experienced a total loss of power. The pilot maneuvered the airplane toward the closest airport, but, when he realized that the airplane would not be able to glide to the airport, he attempted to make an off-airport landing. The airplane stalled and then collided with terrain in an open area of a paper mill. Ground scar analysis and wreckage fragmentation revealed that the airplane descended in a steep, near-vertical, nose-down, left-wing-down attitude before it impacted terrain. The pilot installed a fuel flow transducer about 2 to 3 weeks before the accident and used heavy applications of room temperature vulcanization (RTV) silicone to seal the fuel lines. A friend of the pilot, who was also a mechanic, reported that he had observed the pilot about a year earlier using heavy applications of RTV silicone to seal parts during a condition inspection and that he had mentioned to the pilot that this was an improper practice. A bead of RTV silicone was found in the fuel line, and it is likely that it blocked the inlet of the transducer and starved the engine of fuel. Additionally, subsequent to the loss of engine power, the pilot failed to maintain sufficient airspeed while maneuvering to locate a suitable off-airport landing site and flew the airplane beyond its critical angle-of-attack, which resulted in a stall and loss of airplane control.
Analysis
- Primary failure mode
- Engine power loss
- First missed decision gate
- Pilot could have checked fuel system before flight to ensure proper operation.
NTSB coding
Evidence available
- Photos
- 9 docket documents
Docket documents9
- Statement of Party Representatives to NTSB Investigationinterview
- Witness Statementsinterview
- Floscan Transducer Manualother
- Fuel System Schematic Excerptsother
- Pilot’s Blog Postingother
- Fuel System Examination (6 Embedded Images)photos
- Tests and Research (5 Embedded Images)photos
- Wreckage and Impact (8 Embedded Images)photos
- Toxicological Reportreport
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