Runway excursion during Lubbock Airport facility inspection

No fatalities • Lubbock, United States of America • Takeoff (climb)

An aircraft sustained significant damage after losing directional control during a takeoff roll at Lubbock Airport.

What happened

While conducting an inspection of the facilities at Lubbock Airport, the crew of an aircraft was performing a takeoff roll. During this phase of flight, the pilot lost control of the plane, causing it to veer off the runway. The aircraft eventually came to a stop with its undercarriage in a raised position.

There were no injuries reported among the three crew members involved in the incident. However, the aircraft was determined to be a total loss due to damage sustained during the excursion.

Findings

Investigations into the accident identified several contributing factors related to the loss of control. The primary reason for the event was that the crew failed to maintain directional control and failed to reach or sustain necessary flying speed. Additional technical and operational issues noted include:

  • An improper level-off maneuver
  • Asymmetric engine power causing the aircraft to veer
  • The tailwheel being in an unlocked position

Probable cause

The crew's failure to maintain directional control and achieve sufficient airspeed, compounded by asymmetric engine power and an unlocked tailwheel.

Frequently asked questions

What happened in the 1971-03-11 Douglas DC-3 accident near Lubbock, United States of America?

An aircraft sustained significant damage after losing directional control during a takeoff roll at Lubbock Airport.

Were there any fatalities in the 1971-03-11 Douglas DC-3 accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 1971-03-11 involved a Douglas DC-3, registration N25, operated by Federal Aviation Administration - FAA, at Lubbock, United States of America.

What was the probable cause of the accident?

The crew's failure to maintain directional control and achieve sufficient airspeed, compounded by asymmetric engine power and an unlocked tailwheel.

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