5 fatalities

1973-01-03: Beechcraft 90 King Air (N936K) — Morplan Inc. — Cedar Rapids, United States of America

Cedar Rapids, United States of AmericaLanding (descent or approach)

On January 3, 1973, a Beechcraft 90 King Air (registration N936K) operated by Morplan Inc. was involved in an aviation accident near Cedar Rapids, United States of America during landing or approach. 5 people were killed. Investigators recorded the probable cause as: Improper in-flight decisions on part of the pilot-in-command who exceeded the designed stress limits of the aircraft. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781233163Data APIEditorial standards

During an ILS approach to Cedar Rapids Airport in poor weather, control was lost. The twin-engine airplane crashed in an open field, killing all five occupants. Investigators determined that the left wing, left engine, and tail separated in flight.

Accident Summary

A twin-engine airplane was destroyed when it crashed in an open field several miles from Cedar Rapids Airport. The crew had initiated an ILS approach in poor weather conditions. Control of the aircraft was lost, and it dove into the ground. All five occupants were killed.

Aircraft Damage

The airplane sustained total destruction. Investigation revealed that during the flight, under poor weather conditions, the left wing, left engine, and tail separated from the aircraft. This separation rendered the aircraft uncontrollable.

Weather and Approach

Weather conditions at the time included low ceiling, fog, snow, and turbulence associated with clouds and thunderstorms. The crew began the descent for the ILS approach later than expected, and it is believed they expedited the descent.

Probable Cause

Official findings determined the probable cause was improper in-flight decisions by the pilot-in-command, who exceeded the designed stress limits of the aircraft. Contributing factors included overload failure, in-flight separation of the left wing, left engine, and tail, low ceiling, fog and snow, turbulence from clouds and thunderstorms, a late start to the ILS descent, and an expedited descent by the crew.