Neefjes Lancair 360 MK-II near Milford, UT — 2011-02-27
- Date
- 2011-02-27
- Location
- Milford, UT, USA
- Aircraft
- Neefjes Lancair 360 MK-II
- Registration
- N989TT
- Category
- Airplane
- Highest injury
- Fatal
- Fatalities
- 1
- Phase of flight
- Descent
Probable cause
The pilot's loss of control of the airplane due to spatial disorientation after inadvertently entering instrument meteorological conditions. Contributing to the accident were the pilot's inadequate preflight preparation, his en route decision-making, and his distraction due to a partial loss of engine power due to a restriction in a fuel injection nozzle.
Contributing factors
Contributing to the accident were the pilot's inadequate preflight preparation, his en route decision-making, and his distraction due to a partial loss of engine power due to a restriction in a fuel injection nozzle.
NTSB narrative
The pilot, who was not instrument rated, intended to fly to his destination while remaining in visual meteorological conditions (VMC). While en route, he entered an area where the clouds started to close in on him. Although the air traffic controller whom he was communicating with advised the pilot that there was an airport with VMC a short distance behind him, the pilot elected to attempt to proceed to his destination. As he continued, weather conditions became such that the pilot elected to land at an alternate airport. While being vectored to the alternate airport, the airplane's engine began to run rough, which, according to recorded engine analyzer data, was due to a restriction of the fuel flow in the orifice of the no. 1 cylinder injector nozzle. While attempting to deal with the rough running engine and maneuvering toward the alternate airport, the pilot inadvertently entered the clouds, and most likely lost control of the airplane due to spatial disorientation. The airplane then descended near vertically into the terrain. There was no record of the pilot receiving a weather briefing either from an FAA-contracted Flight Service Station or from either Direct User Access Terminal Service (DUATS) provider.
Analysis
- Primary failure mode
- Engine power loss
- First missed decision gate
- Pilot did not file a flight plan or obtain a weather briefing before departure.
NTSB coding
Evidence available
- ATC audio
- FDR / data
- ADS-B / radar
- Photos
- 30 docket documents
Docket documents30
- Evidence Control Formform
- Evidence Control Formsform
- Release of Aircraft Wreckage, NTSB Form 6120.15form
- Statement of Party Representatives to NTSB Investigationinterview
- Accident Site Location on Google Earthother
- Engine Monitor Dataother
- NEXRAD Reflectivity - Accident at Red Dot Near Centerother
- Precision Airmotive Engine Data Analysisother
- Precision Airmotive Fuel System Testsother
- Image 1. On-scene photo of entire airplane, shot from left rear, and showing location of primary fuselage fractures.photos
- Image 10. Close-up photo of the electrode end of both sparkplugs from cylinder number 1.photos
- Image 11. Photo of the inside of the barrel of the number 1 cylinder.photos
- Image 12. Photo of the dome of the piston from the number one cylinder.photos
- Image 13. Photo of the toe and push rod cup of the rockers from the number 1 cylinder.photos
- Image 14. Photo of the inside of the vacuum pump, showing impact damage to rotor.photos
- Image 15. Photo showing coils and leads from LSE Plasma II CD Ignition system.photos
- Image 2. Photo of interior of right fuel tank, showing outlet filter screen and quantity sensor.photos
- Image 3. Photo of interior of left fuel tank, showing outlet filter screen and quantity sensor.photos
- Image 4. Photo of right and left electric fuel pumps.photos
- Image 5. Photo of fuel injection throttle body just prior to disassembly for inspection.photos
- Image 6. Photo of electrode end of sparkplugs from the top of each cylinder.photos
- Image 7. Photo of electrode end of sparkplugs from the bottom of each cylinder.photos
- Image 8. Photo showing the orifice in the discharge end of the fuel injection nozzle from each cylinder.photos
- Image 9. Photo showing the inner surface of the filter element from the fuel gasculator.photos
- Visible Satellite Imagery - Accident at Red Dotphotos
- Weather Radar Cloud Temperaturesradar
- Lycoming Engine Reportreport
- Toxicological Reportreport
- Transcript of Radio Communicationstranscript
- Release of Parts (Engine Alalyzer)wreckage
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