No fatalities

1991-01-11: Beechcraft 200 Super King Air (N200MR) — United Executive Jet — Vichy-Rolla National, United States of America

Vichy-Rolla National, United States of AmericaLanding (descent or approach)

On January 11, 1991, a Beechcraft 200 Super King Air (registration N200MR) operated by United Executive Jet was involved in an aviation accident near Vichy-Rolla National, United States of America during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: A restricted visual outlook and go-around was not performed by the pilot. Factors related to the accident were a dark night, fog and glare, ice covered runway and whiteout conditions. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781212317Data APIEditorial standards

While executing a VOR approach on a dark, foggy night, the pilot lost depth perception and ground contact after turning on landing lights short final, resulting in a hard landing that damaged the wing spar, engine mount, and propeller. The runway was covered with 3 inches of mirror-smooth ice, causing glare. All four occupants were uninjured.

Incident Overview

During the execution of a VOR approach on a dark, foggy night, the pilot turned on the landing lights while on short final. This action led to a loss of depth perception and ground contact. A hard landing ensued before corrective action could become effective, resulting in damage to the wing spar, engine mounting support, and propeller.

Environmental Conditions

The runway and the entire airport were covered with approximately three inches of mirror-smooth ice. This created considerable glare, which compounded the already challenging visibility conditions. The night was dark and foggy, further reducing visual cues.

Occupant Outcome

All four occupants of the aircraft escaped the incident without injury.

Damage

Damage was sustained to the wing spar, engine mounting support, and propeller due to the hard landing.

Probable cause

A restricted visual outlook and go-around was not performed by the pilot. Factors related to the accident were a dark night, fog and glare, ice covered runway and whiteout conditions.