Casualties unknown

2001-08-05: Beech B36TC (N1109T) — Weaverville, CA

Weaverville, CA, US

On August 5, 2001, a Beech B36TC (registration N1109T) was involved in an aviation accident near Weaverville, CA. Investigators recorded the probable cause as: the pilot's selection of the wrong runway, which resulted in an attempted takeoff uphill in a prevailing tailwind toward rising terrain and high obstacles. 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

An aircraft on takeoff from runway 36 at an airport struck trees beyond the departure end. The pilot had been advised by a briefer to use that runway despite signage prohibiting takeoff. The aircraft weight exceeded the maximum gross weight, and density altitude was high.

Accident Overview

Ground witnesses at the airport observed the pilot depart uphill on runway 36 into rising terrain. The aircraft collided with trees just beyond the runway's departure end.

Runway and Signage

Runway 36 is 2,980 feet long with a 50-foot pavement width and a 3.5 percent uphill gradient. The terrain north of the airport rises more steeply. An airport warning sign states in red: "This R/W Closed for takeoff use R/W 18."

Pre-Takeoff Communication

On the day of the accident, the pilot contacted the FAA Rancho Murieta Automated Flight Service Station at 0823. The pilot questioned the briefer about takeoff procedures and an "X" marked on the runway. After discussion, the briefer told the pilot to take off on runway 36 (uphill), contrary to the signage and FAA Airport/Facility Directory remarks.

Source of Briefer's Information

According to the briefer, his source for airport procedures was the FAA Airport/Facility Directory. The directory entry for the airport initially stated: "Airport closed to touch and go; go arounds; takeoff from runway 36 and landings on runway 18." Later in the entry, another note read: "Land runway 36 takeoff runway 18 due to steep 3.5 percent uphill airport gradient and steeper rising terrain to the north."

Aircraft Weight and Performance

The maximum gross weight of the airplane is 3,850 pounds. Based on known and estimated weights, the accident aircraft weighed about 3,939 pounds, or 89 pounds above the maximum takeoff weight. According to the Pilot's Operating Handbook (POH) and best available information, the airplane would have required 3,750 feet of level, paved, dry runway for takeoff with zero flaps to clear a 50-foot obstacle.

Weather Conditions

Witnesses at the airport estimated temperatures in the mid-90s to over 100 degrees Fahrenheit, with wind out of the south. Based on this information, the density altitude was estimated between 4,000 and 4,800 feet mean sea level (msl).

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20010820X01733. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.