Cessna 414 crash during instrument approach in icing conditions

4 fatalities • Greeneville, United States of America • Landing (descent or approach)

A Cessna 414 crashed into trees and terrain during a circling approach while operating in instrument icing conditions.

What happened

During an approach to land in instrument icing conditions, the pilot was performing a circling maneuver with the landing gear extended and flaps set to 15 degrees. While flying through clouds, the aircraft began to buffet and shake significantly. The pilot transmitted an emergency message over the UNICOM frequency, notifying a fixed base operator and a lineman of engine ice. Shortly after this transmission, the aircraft entered a 60-degree bank and struck trees and the ground.

At the time of the accident, the total weight of the Cessna 414 was 6,568.52 pounds, which exceeded the maximum landing weight of 6,430 pounds. There were 1 fatality reported in the accident.

Findings

Investigation into the circumstances revealed that the alternate air induction system was not activated during the flight. Additionally, the aircraft's weight at the time of the crash was above the manufacturer's specified maximum landing weight. The pilot had previously completed one other flight in icing conditions prior to this occurrence.

Probable cause

The failure to activate the alternate air induction system during instrument icing conditions led to engine ice accumulation.

Frequently asked questions

What happened in the 2003-12-11 Cessna 414 Chancellor accident near Greeneville, United States of America?

A Cessna 414 crashed into trees and terrain during a circling approach while operating in instrument icing conditions.

Were there any fatalities in the 2003-12-11 Cessna 414 Chancellor accident?

The accident was fatal, resulting in 4 fatalities.

What aircraft was involved and where did it happen?

The accident on 2003-12-11 involved a Cessna 414 Chancellor, registration N1592T, operated by Young Forever, at Greeneville, United States of America.

What was the probable cause of the accident?

The failure to activate the alternate air induction system during instrument icing conditions led to engine ice accumulation.

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