LANDRUM KELLY T VANS RV6 near Suffolk, VA — 2014-05-31
- Date
- 2014-05-31
- Location
- Suffolk, VA, USA
- Aircraft
- LANDRUM KELLY T VANS RV6
- Registration
- N6RP
- Category
- Airplane
- Highest injury
- Minor
- Fatalities
- 0
- Phase of flight
- Descent
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.
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.
Analysis
- Primary failure mode
- Mechanical failure
- First missed decision gate
- Pilot could have selected a different emergency landing site earlier.
NTSB coding
Evidence available
- Photos
- 13 docket documents
Docket documents13
- Materials Laboratory Parts Return Formform
- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1form
- Excerpt from Propeller Hub Instructionsother
- Excerpt from Propeller Logbookother
- Fly-in Event Instructionsother
- Record of Conversationsother
- Vari-Prop System Descriptionother
- Photograph 1: Airplane at Rest at Accident Site (Courtesy of Recovery Team)photos
- Photograph 2: Airplane at Rest at Accident Site (Courtesy of Recovery Team)photos
- Photograph 3: Propeller Hub (Courtesy of Recovery Team)photos
- Gearbox/Propeller Exam Factual Reportreport
- Weather Report and Recordreport
- Release of Wreckagewreckage
Related mishaps
- VANS RV-7A
2024-12-22 · Gila Bend, AZ
- PIPER PA-32R-301
2024-10-17 · Van, TX
- CESSNA 170A
2024-09-11 · Marshall, IN
- AERONCA 11AC
2024-07-27 · Winchester, CA
- TITAN T51
2024-05-12 · Novi, MI
- Kitfox Series 5
2024-04-05 · Yucca Grove, CA