Casualties unknown

2000-07-21: Steel/vans RV6 (N64ME) — Winnemucca, NV

Winnemucca, NV, US

On July 21, 2000, a Steel/vans RV6 (registration N64ME) was involved in an aviation accident near Winnemucca, NV. Investigators recorded the probable cause as: A loss of power due to overheating resulting from the failure of the engine build-up facility to install a vernatherm. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

After engine oil temperature exceeded limits, an amateur-built airplane lost power, overran the runway, and nosed over on soft soil. Investigation found a missing vernatherm.

Event Narrative

A flight that originated in the San Francisco Bay area was en route to Oshkosh, Wisconsin. During cruise, the pilot observed the engine oil temperature approaching the upper limit and decided to land at an airport to allow the engine to cool. After approximately one hour on the ground, the pilot conducted a detailed preflight inspection and engine run-up, which revealed no abnormalities. Departure was then initiated for the next planned stop.

About ten minutes after departure, the engine oil temperature again rose to the red line limit. The pilot elected to turn back toward the airport. Shortly thereafter, the oil temperature exceeded the red line, and the engine began to lose power. The pilot reduced throttle and set up for a forced landing on a highway. The engine power partially returned, prompting the pilot to attempt continuing to the airport. However, the engine lost power short of the facility.

The pilot reported being able to reach the runway but was too low to execute any traffic pattern maneuvers and too high for a normal landing. The airplane touched down slightly faster than normal near the midpoint of the runway and could not stop before overrunning the pavement end. The airplane then encountered soft, sandy soil and nosed over.

Investigation Findings

Disassembly of the engine revealed that the vernatherm—a component that controls oil flow through the oil cooler—was not installed. Its absence allowed the oil supply to bypass the cooler entirely. Engine records indicated that the powerplant had been built approximately 90 flight hours prior to the accident by a firm specializing in performance improvement rebuilds for the experimental aircraft market. The engine was a basic Lycoming IO-360 with several modifications aimed at power enhancement.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X21515. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.