Loss of control Accident Lockheed 18-50 Lodestar N33369, Monday 10 January 1955
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Date:Monday 10 January 1955
Time:09:38
Type:Silhouette image of generic L18 model; specific model in this crash may look slightly different    
Lockheed 18-50 Lodestar
Owner/operator:National Airlines
Registration: N33369
MSN: 18-2414
Year of manufacture:1943
Total airframe hrs:20627 hours
Engine model:Wright R-1820-G202A
Fatalities:Fatalities: 0 / Occupants: 13
Other fatalities:0
Aircraft damage: Destroyed, written off
Category:Accident
Location:St. Petersburg Airport, FL (PIE) -   United States of America
Phase: Take off
Nature:Passenger - Scheduled
Departure airport:St. Petersburg-Pinellas International Airport, FL (PIE/KPIE)
Destination airport:Sarasota-Bradenton Airport, FL (SRQ/KSRQ)
Investigating agency: CAB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
National Airlines Flight 1 originated at Orlando, Florida, destination Miami, Florida, with scheduled intermediate stops at Lakeland, Tampa, St. Petersburg, Sarasota, Ft. Meyers, and West-Palm Beach.
The flight departed Orlando at 08:05 and Lakeland was overflown as there were no passengers debarking or boarding. After a stop at Tampa the flight landed at St. Petersburg at 09:29.
The captain taxied the aircraft from the ramp to the run-up position for runway 09 then told the copilot that he was to fly the next segment of the route.
After a normal run-up, the copilot taxied the aircraft to the end of the 5010-foot runway. The airplane was lined up and the tail wheel was locked. During takeoff, as the tail had come up, the airplane began to swerve to the left. After correcting, it swerved to the right. A series of over-corrections in both directions followed. The crew noted a drop of 5 inches in manifold pressure of the left engine followed by a drop of 25 inches. The captain took over control and closed the throttles. He could not stop the turn which developed into a skid and the main landing gear collapsed, rupturing the right wing fuel tank.
The airplane came to rest on the sodded area, off the runway, heading 180 degrees from its original takeoff position. All on board safely evacuated the airplane.

PROBABLE CAUSE: "The Board determines that the probable cause of this accident was the copilot's loss of directional control during the takeoff run and the inability of the captain to regain control of the aircraft, the latter possibly due to failure of the pedal mechanism."

Accident investigation:
cover
  
Investigating agency: CAB
Report number: final report
Status: Investigation completed
Duration:
Download report: Final report

Sources:

The Lockheed Twins / Peter J Marson
Rome News-Tribune - Jan 10, 1955
CAB Report

Location

Revision history:

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