ERA14LA272 · Landrum Kelly T VANS RV6
Landrum Kelly T VANS RV6 · Accident: powerplant system/component malfunction/failure en route
From William M Tuck Airport (W78) to Suffolk Executive Airport (SFQ)
Event
- NTSB case
- ERA14LA272
- Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
- Accident
- InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
- Completed
- API-reported fatalities
- 0 · all aircraft and ground
- Ground fatalities
- Unknown
- OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
- General aviation
- WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
- Visual Meteorological Cond
Landrum Kelly T VANS RV6
- Aircraft type
- Landrum Kelly VANS RV6
- Category
- Airplane
- RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
- N6RP
- Operator
- Landrum Kelly T
- Onboard fatalities
- Unknown
- Route
- From William M Tuck Airport (W78), South Boston, VATo Suffolk Executive Airport (SFQ), Suffolk, VA
- Aircraft age
- About 8 years (built 2006)
- Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
- Part 91: General Aviation
- Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
- En route · cruise
- Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
- Powerplant system/component malfunction/failure
- DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
- Substantial
Cause areas
- Aircraft › Aircraft propeller/rotor
- Aircraft › Fluids/miscellaneous hardware
- Personnel issues › Action/decision
- Personnel issues › Task performance
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
According to the pilot, who was also the owner/builder of the experimental amateur-built airplane, while operating about 2,000 ft mean sea level, the engine rpm went to redline, the airplane lost thrust, and a red fluid covered the windscreen. The pilot attempted a forced landing to a field, but the airplane impacted trees, which resulted in substantial damage to the wings and fuselage.
Postaccident examination of the engine revealed no mechanical malfunctions or anomalies to the engine or gearbox. Examination of the propeller showed that the fine pitch stop nuts were missing. The propeller needle thrust bearing and mating parts were galled, burned, and damaged from rotational and thermal wear. The heat damage likely initiated at the needle thrust bearing and progressed both fore and aft to the blade pin spool and slave piston collar, respectively. The Delrin bushing melted after the heat reached the blade pin spool, which allowed the propeller pins to make bare metal contact with the spool pin slots. With the absence of stop nuts, the propeller blade angle could decrease below a 0-thrust angle, and the melted Delrin bushings allowed the propeller blade angles to decrease an additional 6 degrees in the negative direction. The cumulative effect of both events was a total loss of aerodynamic thrust.
About 28 flight hours before the accident, the pilot/builder used a viscous lubricant to grease the bearings in the propeller assembly. According to the lubricant manufacturer, the lubricant has a high viscosity and was designed for low-speed automotive and trucking applications not for aviation use. Lubricants with high viscosities can cause the bearing to skid, which can result in rapid overheating and failure of the bearing.
Probable cause
The pilot/builder's decision to use a lubricant that was not designed for high-speed aviation applications, which resulted in the failure of the propeller needle thrust bearing due to the loss of lubrication from overheating, a total loss of aerodynamic thrust, and a subsequent forced landing.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ERA14LA272
- Event ID
- 20140602X83649
- Case number
- ERA14LA272
- Dataset
- full-current
- Source SHA-256
- 5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
Source notes (4)
- Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
- Filled from the NTSB case API where the bulk record had no value: investigation status. Values present in the bulk record are kept.
- The date is the local date, which is the same as the UTC date the NTSB stores.
- API snapshot SHA-256: d348113511602b28ce1cad559f153fd37a0122fb5e3da63017f0e25b3461ecbd; retrieved 2026-09-15T23:43:23.187Z.