Columbus – Greeneville

The pilot was on a circling approach for landing in instrument icing conditions. The landing gear were extended and the flaps were lowered to 15°. The alternate air induction system was not activated. The surviving passenger stated when the airplane came out of the clouds and the airplane started to buffet and shake. The pilot was heard to state on the UNICOM frequency by the fixed base operator and a lineman, "Emergency engine ice." The airplane was observed to make a 60-degree angle of bank and collided with trees and terrain. The Pilot's Operating Handbook states the airplane will stall at 129 miles per hour with the landing gear and flaps down at 15-degrees. The maximum landing weight for the Cessna 414 is 6,430 pounds. The total aircraft weight at the crash site was 6,568.52 pounds. Witnesses who knew the pilot stated the pilot had flown one other known flight in icing conditions before the accident flight.

Flight / Schedule

Columbus – Greeneville

Registration

N1592T

MSN

414-0372

Year of Manufacture

1972

Operator

Young Forever

Date

December 11, 2003 at 10:47 AM

Type

CRASH

Flight Type

Executive/Corporate/Business

Flight Phase

Landing (descent or approach)

Crash Site

Airport (less than 10 km from airport)

Crash Location

Greeneville Tennessee

Region

North America • United States of America

Coordinates

36.1632°, -82.8310°

Crash Cause

Human factor

Narrative Report

On December 11, 2003 at 10:47 AM, Columbus – Greeneville experienced a crash involving Cessna 414 Chancellor, operated by Young Forever, with the event recorded near Greeneville Tennessee.

The flight was categorized as executive/corporate/business and the reported phase was landing (descent or approach) at a airport (less than 10 km from airport) crash site.

5 people were known to be on board, 4 fatalities were recorded, 1 survivors were identified or estimated. This corresponds to an estimated fatality rate of 80.0%.

Crew on board: 1, crew fatalities: 1, passengers on board: 4, passenger fatalities: 3, other fatalities: 0.

The listed crash cause is human factor. The pilot was on a circling approach for landing in instrument icing conditions. The landing gear were extended and the flaps were lowered to 15°. The alternate air induction system was not activated. The surviving passenger stated when the airplane came out of the clouds and the airplane started to buffet and shake. The pilot was heard to state on the UNICOM frequency by the fixed base operator and a lineman, "Emergency engine ice." The airplane was observed to make a 60-degree angle of bank and collided with trees and terrain. The Pilot's Operating Handbook states the airplane will stall at 129 miles per hour with the landing gear and flaps down at 15-degrees. The maximum landing weight for the Cessna 414 is 6,430 pounds. The total aircraft weight at the crash site was 6,568.52 pounds. Witnesses who knew the pilot stated the pilot had flown one other known flight in icing conditions before the accident flight.

Aircraft reference details include registration N1592T, MSN 414-0372, year of manufacture 1972.

Geospatial coordinates for this crash are approximately 36.1632°, -82.8310°.

Fatalities

Total

4

Crew

1

Passengers

3

Other

0

Crash Summary

The pilot was on a circling approach for landing in instrument icing conditions. The landing gear were extended and the flaps were lowered to 15°. The alternate air induction system was not activated. The surviving passenger stated when the airplane came out of the clouds and the airplane started to buffet and shake. The pilot was heard to state on the UNICOM frequency by the fixed base operator and a lineman, "Emergency engine ice." The airplane was observed to make a 60-degree angle of bank and collided with trees and terrain. The Pilot's Operating Handbook states the airplane will stall at 129 miles per hour with the landing gear and flaps down at 15-degrees. The maximum landing weight for the Cessna 414 is 6,430 pounds. The total aircraft weight at the crash site was 6,568.52 pounds. Witnesses who knew the pilot stated the pilot had flown one other known flight in icing conditions before the accident flight.

Cause: Human factor

Occupants & Outcome

Crew On Board

1

Passengers On Board

4

Estimated Survivors

1

Fatality Rate

80.0%

Known people on board: 5

Operational Details

Schedule / Flight

Columbus – Greeneville

Operator

Young Forever

Flight Type

Executive/Corporate/Business

Flight Phase

Landing (descent or approach)

Crash Site

Airport (less than 10 km from airport)

Region / Country

North America • United States of America

Aircraft Details

Registration

N1592T

MSN

414-0372

Year of Manufacture

1972