Buffalo – Saint Louis

While taxiing to Runway 23 the flight received an IFR (Instrument Plight Rules) clearance from ARTC (Air Route Traffic Control). Normal pre-takeoff checks were performed and the takeoff roll was started at 1640. The aircraft became airborne after using approximately one-half of the 5.630-foot runway. Immediately after leaving the ground the gear was raised and the first officer saw the left feathering button light come on dimly which indicated that the left propeller was in the process of being feathered by the auto-feathering system. After definitely determining the light was on and visually checking the left propeller, the auto-feathering system was disarmed and the captain., in an effort to stop the feathering cycle, pulled the feathering button to neutral. This effort was unsuccessful. the left propeller feathered, and the engine stopped. During the climb an air speed of 140 m.p.h. was reached and maintained., the right engine remaining at full takeoff power. Approximately 250 feet above the ground a shallow left turn was started and the first officer was ordered to reinstate the left engine. the captain believing the aircraft would climb no farther. In the effort to restart the left engine by unfeathering the left propeller. only 600 r.p.m. could be obtained and the captain felt a buffeting through the control yoke. The aircraft at this time had progressed in the left turn approximately 180 degrees from the takeoff direction and the captain. fearing he would be unable to clear obstructions. Including high tension lines, decided to make a wheels-up landing. The landing was made in a field approximately one mile south of the airport. When the aircraft stopped, the passengers and crew evacuated it in an expeditious and orderly manner. The airplane was damaged beyond repair.

Flight / Schedule

Buffalo – Saint Louis

Aircraft

Convair CV-240

Registration

N94244

MSN

88

Year of Manufacture

1948

Date

January 20, 1954 at 04:42 PM

Type

CRASH

Flight Type

Scheduled Revenue Flight

Flight Phase

Takeoff (climb)

Crash Site

Airport (less than 10 km from airport)

Crash Location

Buffalo New York

Region

North America • United States of America

Coordinates

42.8864°, -78.8781°

Crash Cause

Technical failure

Narrative Report

On January 20, 1954 at 04:42 PM, Buffalo – Saint Louis experienced a crash involving Convair CV-240, operated by American Airlines, with the event recorded near Buffalo New York.

The flight was categorized as scheduled revenue flight and the reported phase was takeoff (climb) at a airport (less than 10 km from airport) crash site.

24 people were known to be on board, 0 fatalities were recorded, 24 survivors were identified or estimated. This corresponds to an estimated fatality rate of 0.0%.

Crew on board: 3, crew fatalities: 0, passengers on board: 21, passenger fatalities: 0, other fatalities: 0.

The listed crash cause is technical failure. While taxiing to Runway 23 the flight received an IFR (Instrument Plight Rules) clearance from ARTC (Air Route Traffic Control). Normal pre-takeoff checks were performed and the takeoff roll was started at 1640. The aircraft became airborne after using approximately one-half of the 5.630-foot runway. Immediately after leaving the ground the gear was raised and the first officer saw the left feathering button light come on dimly which indicated that the left propeller was in the process of being feathered by the auto-feathering system. After definitely determining the light was on and visually checking the left propeller, the auto-feathering system was disarmed and the captain., in an effort to stop the feathering cycle, pulled the feathering button to neutral. This effort was unsuccessful. the left propeller feathered, and the engine stopped. During the climb an air speed of 140 m.p.h. was reached and maintained., the right engine remaining at full takeoff power. Approximately 250 feet above the ground a shallow left turn was started and the first officer was ordered to reinstate the left engine. the captain believing the aircraft would climb no farther. In the effort to restart the left engine by unfeathering the left propeller. only 600 r.p.m. could be obtained and the captain felt a buffeting through the control yoke. The aircraft at this time had progressed in the left turn approximately 180 degrees from the takeoff direction and the captain. fearing he would be unable to clear obstructions. Including high tension lines, decided to make a wheels-up landing. The landing was made in a field approximately one mile south of the airport. When the aircraft stopped, the passengers and crew evacuated it in an expeditious and orderly manner. The airplane was damaged beyond repair.

Aircraft reference details include registration N94244, MSN 88, year of manufacture 1948.

Geospatial coordinates for this crash are approximately 42.8864°, -78.8781°.

Fatalities

Total

0

Crew

0

Passengers

0

Other

0

Crash Summary

While taxiing to Runway 23 the flight received an IFR (Instrument Plight Rules) clearance from ARTC (Air Route Traffic Control). Normal pre-takeoff checks were performed and the takeoff roll was started at 1640. The aircraft became airborne after using approximately one-half of the 5.630-foot runway. Immediately after leaving the ground the gear was raised and the first officer saw the left feathering button light come on dimly which indicated that the left propeller was in the process of being feathered by the auto-feathering system. After definitely determining the light was on and visually checking the left propeller, the auto-feathering system was disarmed and the captain., in an effort to stop the feathering cycle, pulled the feathering button to neutral. This effort was unsuccessful. the left propeller feathered, and the engine stopped. During the climb an air speed of 140 m.p.h. was reached and maintained., the right engine remaining at full takeoff power. Approximately 250 feet above the ground a shallow left turn was started and the first officer was ordered to reinstate the left engine. the captain believing the aircraft would climb no farther. In the effort to restart the left engine by unfeathering the left propeller. only 600 r.p.m. could be obtained and the captain felt a buffeting through the control yoke. The aircraft at this time had progressed in the left turn approximately 180 degrees from the takeoff direction and the captain. fearing he would be unable to clear obstructions. Including high tension lines, decided to make a wheels-up landing. The landing was made in a field approximately one mile south of the airport. When the aircraft stopped, the passengers and crew evacuated it in an expeditious and orderly manner. The airplane was damaged beyond repair.

Cause: Technical failure

Occupants & Outcome

Crew On Board

3

Passengers On Board

21

Estimated Survivors

24

Fatality Rate

0.0%

Known people on board: 24

Operational Details

Schedule / Flight

Buffalo – Saint Louis

Flight Type

Scheduled Revenue Flight

Flight Phase

Takeoff (climb)

Crash Site

Airport (less than 10 km from airport)

Region / Country

North America • United States of America

Aircraft Details

Aircraft

Convair CV-240

Registration

N94244

MSN

88

Year of Manufacture

1948