7 fatalities

Aircraft Crashes After Clear Air Turbulence Upset and Engine Flameout (N50SK)

Redwater, United States of AmericaFlight

On April 4, 1986, an IAI 1124 Westwind (registration N50SK) operated by Drayton Associates was involved in an aviation accident near Redwater, United States of America in flight. 7 people were killed. Investigators recorded the probable cause as: Occurrence #1: airframe/component/system failure/malfunction – weather radar system failure; continued operation with known deficiencies. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-11Data APIEditorial standards

An aircraft crashed following an uncontrolled descent after a turbulence upset at FL370. The crew encountered a severe thunderstorm, both engines flamed out, and the aircraft overstressed during exit, causing structural failure. An improper weather briefing and radar malfunction were noted. All seven occupants were killed.

Accident Summary

An aircraft crashed during an uncontrolled descent after a turbulence upset at flight level 370. The upset occurred due to clear air turbulence associated with a VIP level 6 thunderstorm located within 7 miles of the aircraft's last known position. Following the upset, the aircraft penetrated and descended through the thunderstorm cell, which contained lightning, extreme turbulence, and severe icing. During the upset and descent, both engines flamed out. The crew's attempts to recover the aircraft were unsuccessful due to the conditions within the cell.

Flight and Weather Encounter

The crew had received an improper briefing from the Flight Service Station (FSS) and reported to the deputy controller that their weather radar was malfunctioning. SIGMET and AWW information was not provided during the briefing. As the aircraft exited the bottom of the thunderstorm cell at 4,000 feet, the crew overstressed the airframe. The overstress caused the left main landing gear door to separate, which then struck the left horizontal stabilizer, causing the stabilizer to separate due to overload. The aircraft impacted terrain at an angle of 82° nose down.

Investigation Findings

The investigation determined that the nature of the aircraft's radar malfunction could not be determined. The official findings listed multiple occurrences, including: failure of the weather radar system; continued operation with known equipment deficiencies; encounter with a thunderstorm, clear air turbulence, gusts, and downdraft; dark night conditions; improper preflight briefing by FSS personnel; hazardous weather advisory not issued; in-flight weather advisories not issued; unclear information from FSS; excessive workload on the pilot and copilot; loss of engine power (total, nonmechanical); and a subsequent uncontrolled descent leading to collision with terrain.

Probable cause

Occurrence #1: airframe/component/system failure/malfunction – weather radar system failure; continued operation with known deficiencies. Occurrence #2: in flight encounter with weather – thunderstorm, clear air turbulence, gusts, downdraft; dark night; improper preflight briefing; hazardous weather advisory not issued. Occurrence #3: in flight encounter with weather – in-flight weather advisories not issued; unclear information from FSS. Occurrence #4: loss of control – remedial action attempted; excessive workload on pilot and copilot. Occurrence #5: loss of engine power (total, nonmechanical). Occurrence #6: in flight collision with terrain/water.