Casualties unknown

1992-07-22: Beech 23 (N2359J) — Gary L. Smith — Fall River Mill, CA

Fall River Mill, CA, US

On July 22, 1992, a Beech 23 (registration N2359J) operated by Gary L. Smith was involved in an aviation accident near Fall River Mill, CA. Investigators recorded the probable cause as: THE PILOTS DECISION TO TURN DOWN WIND AT A CRITICAL PHASE OF THE GO AROUND WITH INADEQUATE AIRSPEED RESULTING IN A STALL MUSH UNCONTROLLED DESCENT. 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

During a go-around from a crosswind landing attempt, the pilot turned into a direct tailwind. Witnesses observed the aircraft bank sharply and descend from low altitude.

Accident Overview

The pilot was attempting to land in a 20-knot right crosswind with gusts to about 25 knots. According to the Pilot's Operating Handbook (POH), the airplane's demonstrated crosswind component is 13 knots. The pilot initiated a go-around, and during the initial climb turned a close left crosswind, which placed the airplane in a direct tailwind of 20 knots or more.

Witness Observations

Witnesses reported that the aircraft never exceeded 100 feet in altitude. After narrowly missing a water tank, the airplane suddenly banked 90 degrees to the left and fell to the ground. Witnesses stated that the airplane was very low and had positive engine power at the time.

Local Wind Conditions

According to local area pilots, under the wind conditions on the day of the accident, the area just southwest of the airport is capable of severe turbulence, wind shears, and down drafts associated with a southwesterly airflow over and between Mount Haney and Saddle Mountain.

Weight and Balance

Weight and balance computations were performed using three different fuel loads and other estimated weights. All three calculations placed the center of gravity at the forward CG limits.

Post-Accident Examination

During the on-scene accident investigation, a lubricant container was found in the tail cone area. Close examination of the area revealed evidence of can contact and rubbing on the stabilator servo tab rod. The rod was found bent.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X15173. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.