1 fatality

1997-03-02: Beechcraft 200 Super King Air (N117WM) — Coast Hotels & Casinos — Salt Lake City, United States of America

Salt Lake City, United States of AmericaLanding (descent or approach)

On March 2, 1997, a Beechcraft 200 Super King Air (registration N117WM) operated by Coast Hotels & Casinos was involved in an aviation accident near Salt Lake City, United States of America during landing or approach. One person was killed. Investigators recorded the probable cause as: The pilot's failure to maintain adequate airspeed on the ILS approach, resulting in a stall. Factors included: low visibility; the pilot's selection of the improper DME for the approach; his resulting failure to attain the proper descent profile for the… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781206270Data APIEditorial standards

Aircraft stalled on ILS approach due to low airspeed, improper DME selection, low visibility, and insufficient altitude for recovery.

ILS Approach and Altitude Deviations

The flight was conducting a coupled ILS approach with 1/2 mile visibility in snow showers. Three successive fixes on the localizer are defined by DME paired with the ILS. Prior to the ILS DME commissioning 6 months before the accident, the DME fixes were defined by a VORTAC 4.7 nautical miles past the ILS DME. The aircraft was 800 feet high at the first fix and 1,500 feet high at the second, but approximately on altitude 4.7 nautical miles past the first and second fixes, respectively. It passed the outer marker 900 feet high and captured the glide slope from above about 1.8 nautical miles from the threshold, 500 feet above decision height and 700 feet above touchdown.

Stall and Crash

The aircraft was on glide slope for 28 seconds, during which time its speed decayed to stall speed. It then dropped below glide slope and crashed 1.3 nautical miles short of the threshold.

Cockpit Configuration

The pilot's FLT DIR DME-1/ DME-2 switch, which controls the DME display on the pilot's HSI, was found set to DME-2; the NAV-2 radio was set to the VORTAC frequency. Up to 800 feet may be required for stall recovery.

Probable cause

The pilot's failure to maintain adequate airspeed on the ILS approach, resulting in a stall. Factors included: low visibility; the pilot's selection of the improper DME for the approach; his resulting failure to attain the proper descent profile for the approach; and insufficient altitude available for stall recovery.