Pensacola - Saint Louis

About 20 minutes after takeoff the pilot reported the right engine had lost power and the aircraft would not maintain altitude. Vectors were provided for an emergency landing, but the aircraft crashed in a wooded area about 3 miles from the airport. There was evidence that the gear and flaps had been extended and the aircraft had entered a turn before impacting. Both props had evidence of low to moderate power and neither was feathered. An exam revealed unsymmetrical wear on the blades of the right turbocharger; its thrust spacer, pn 406990-9004, was worn and there was evidence of oil leakage. The 13 qt, right engine oil system had only 6.85 qts of oil remaining. Both turbochargers had been installed during an annual inspection in april 1983 and previously had been overhauled. The aircraft was estimated to be 844 lbs over its max weight limit and the aircraft cg limit was exceeded by about 4.8 inches. Six of the passengers were not restrained by seat belts. An associate estimated that the pilot had only 4 to 6 hours of rest in the previous 3 to 4 days. All eight occupants were killed.

Flight / Schedule

Pensacola - Saint Louis

Registration

N2960Q

MSN

421A-0060

Year of Manufacture

1968

Date

June 21, 1983 at 11:31 PM

Type

CRASH

Flight Type

Executive/Corporate/Business

Flight Phase

Landing (descent or approach)

Crash Site

Airport (less than 10 km from airport)

Crash Location

Atmore Alabama

Region

North America • United States of America

Coordinates

31.0238°, -87.4939°

Crash Cause

Technical failure

Narrative Report

On June 21, 1983 at 11:31 PM, Pensacola - Saint Louis experienced a crash involving Cessna 421A Golden Eagle I, operated by Odom Flying Service, with the event recorded near Atmore Alabama.

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.

8 people were known to be on board, 8 fatalities were recorded, 0 survivors were identified or estimated. This corresponds to an estimated fatality rate of 100.0%.

Crew on board: 1, crew fatalities: 1, passengers on board: 7, passenger fatalities: 7, other fatalities: 0.

The listed crash cause is technical failure. About 20 minutes after takeoff the pilot reported the right engine had lost power and the aircraft would not maintain altitude. Vectors were provided for an emergency landing, but the aircraft crashed in a wooded area about 3 miles from the airport. There was evidence that the gear and flaps had been extended and the aircraft had entered a turn before impacting. Both props had evidence of low to moderate power and neither was feathered. An exam revealed unsymmetrical wear on the blades of the right turbocharger; its thrust spacer, pn 406990-9004, was worn and there was evidence of oil leakage. The 13 qt, right engine oil system had only 6.85 qts of oil remaining. Both turbochargers had been installed during an annual inspection in april 1983 and previously had been overhauled. The aircraft was estimated to be 844 lbs over its max weight limit and the aircraft cg limit was exceeded by about 4.8 inches. Six of the passengers were not restrained by seat belts. An associate estimated that the pilot had only 4 to 6 hours of rest in the previous 3 to 4 days. All eight occupants were killed.

Aircraft reference details include registration N2960Q, MSN 421A-0060, year of manufacture 1968.

Geospatial coordinates for this crash are approximately 31.0238°, -87.4939°.

Fatalities

Total

8

Crew

1

Passengers

7

Other

0

Crash Summary

About 20 minutes after takeoff the pilot reported the right engine had lost power and the aircraft would not maintain altitude. Vectors were provided for an emergency landing, but the aircraft crashed in a wooded area about 3 miles from the airport. There was evidence that the gear and flaps had been extended and the aircraft had entered a turn before impacting. Both props had evidence of low to moderate power and neither was feathered. An exam revealed unsymmetrical wear on the blades of the right turbocharger; its thrust spacer, pn 406990-9004, was worn and there was evidence of oil leakage. The 13 qt, right engine oil system had only 6.85 qts of oil remaining. Both turbochargers had been installed during an annual inspection in april 1983 and previously had been overhauled. The aircraft was estimated to be 844 lbs over its max weight limit and the aircraft cg limit was exceeded by about 4.8 inches. Six of the passengers were not restrained by seat belts. An associate estimated that the pilot had only 4 to 6 hours of rest in the previous 3 to 4 days. All eight occupants were killed.

Cause: Technical failure

Occupants & Outcome

Crew On Board

1

Passengers On Board

7

Estimated Survivors

0

Fatality Rate

100.0%

Known people on board: 8

Operational Details

Schedule / Flight

Pensacola - Saint Louis

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

N2960Q

MSN

421A-0060

Year of Manufacture

1968