9 fatalities

1968-03-17: Beechcraft E18 (N3400) — Black Hills Glass & Mirror Company — Rapid City, United States of America

Rapid City, United States of AmericaLanding (descent or approach)

On March 17, 1968, a Beechcraft E18 (registration N3400) operated by Black Hills Glass & Mirror Company was involved in an aviation accident near Rapid City, United States of America during landing or approach. 9 people were killed. Investigators recorded the probable cause as: Improper compensation for wind conditions on part of the pilot who failed to maintain flying speed. Inadequate preflight preparation and unfavorable wind component were also reported. Improperly loaded aircraft was considered as a contributing factor. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781238960Data APIEditorial standards

On final approach to Rapid City Airport, a pilot encountered gusty winds and lost control, resulting in a crash and explosion. All nine occupants were killed. The probable cause includes improper wind compensation and inadequate preflight preparation.

Accident Details

On final approach to Rapid City Airport, the pilot encountered gusty winds and lost control of the airplane. The aircraft crashed in a huge explosion in a field. All nine occupants were killed.

Probable Cause

The official investigation determined the probable cause to be improper compensation for wind conditions on the part of the pilot, who failed to maintain flying speed. Inadequate preflight preparation and unfavorable wind component were also reported. An improperly loaded aircraft was considered as a contributing factor. Additionally, gusting wind up to 20 knots exceeded rearward center of gravity limits.

Investigation Findings

The investigation highlighted several factors: the pilot's failure to properly compensate for wind conditions, inadequate preflight preparation, and an unfavorable wind component. The aircraft's load distribution was found to be improper, contributing to loss of control. Gusty winds of up to 20 knots were present and exceeded the aircraft's rearward center of gravity limits, exacerbating the situation.