Casualties unknown

Aircraft Stall and Collision During Instrument Approach in Icing Conditions (N948CC)

Reno, NV, US

On March 14, 2002, a Beech E90 (registration N948CC) was involved in an aviation accident near Reno, NV. Investigators recorded the probable cause as: The pilot's inadequate approach airspeed for the existing adverse meteorological conditions followed by his delayed remedial action to avert stalling and subsequent loss of airplane control. 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 2026-06-10Data APIEditorial standards

An aircraft stalled and collided with a building during an instrument approach in snow showers and freezing fog. The pilot was not informed of a visibility decrease below his minimum requirement, and the empennage deice boots were found dysfunctional.

Accident Overview and Flight Context The accident occurred during the return portion of a round-trip flight while the aircraft was on final approach to the pilot's alternate airport due to a weather-induced diversion. Moderate-intensity snow showers and freezing fog were present. During the initial approach, the reported visibility was 1 1/2 miles. About the time the pilot passed the final approach fix, the visibility decreased to 1/2 mile, but the pilot was not informed of the decrease below his 1-mile minimum requirement. ## Approach and Loss of Control During an instrument approach, upon descending to the prescribed minimum descent altitude, about 1/2 mile from the missed approach point, the pilot failed to maintain flying airspeed. The airplane stalled, rolled left, and in an uncontrolled descent collided with a commercial building 0.96 nm from the runway's displaced threshold. ## Airspeed and Pilot Actions The pilot had maintained the recommended 140-knot approach speed in the icing conditions until about 3 1/2 miles from the runway. Thereafter, the airplane's speed gradually decreased until reaching about 75 knots. After the airplane started vibrating, the pilot increased engine power, but his action was not timely enough to avert stalling. ## Maintenance and Deice System Findings Company mechanics maintained the airplane. On previous occasions, overheat conditions had occurred wherein the environmental ducting melted and heat was conducted to the adjacent pneumatic tube that provides deice air to the empennage boots. During the accident investigation, the deice tube was found completely melted closed, thus rendering all of the empennage deice boots dysfunctional.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20020403X00453. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.