Asymmetrical flap configuration leads to Fairchild accident during takeoff practice

No fatalities • Las Vegas-Harry Reid (McCarran), United States of America • Takeoff (climb)

A Fairchild aircraft veered off the runway and cartwheeled during a simulated no-flap takeoff procedure due to an asymmetrical flap setting.

What happened

During a training maneuver involving a full-flap landing followed by a transition to a no-flap takeoff configuration, the Fairchild experienced a loss of directional control. As the aircraft reached rotation speed, it veered toward the left side of the runway. The aircraft subsequently cartwheeled off the paved surface, eventually coming to a stop approximately 557 feet to the left of the runway centerline and 6000 feet from the end of the takeoff area.

Post-accident inspection revealed an irregular flap configuration during the flight. While the right inboard and outboard flaps were found in the fully extended position, the left side of the wing was asymmetrical; specifically, the left inboard flap was only extended to 17 degrees, and the left outboard flap was completely retracted.

Probable cause

The accident was caused by an asymmetrical flap condition resulting from a jammed flap gearbox and a malfunctioning rotary actuator, compounded by insufficient maintenance and a failure of the warning system.

Frequently asked questions

What happened in the 1965-04-16 Fairchild F27 accident near Las Vegas-Harry Reid (McCarran), United States of America?

A Fairchild aircraft veered off the runway and cartwheeled during a simulated no-flap takeoff procedure due to an asymmetrical flap setting.

Were there any fatalities in the 1965-04-16 Fairchild F27 accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 1965-04-16 involved a Fairchild F27, registration N757L, operated by Bonanza Airlines, at Las Vegas-Harry Reid (McCarran), United States of America.

What was the probable cause of the accident?

The accident was caused by an asymmetrical flap condition resulting from a jammed flap gearbox and a malfunctioning rotary actuator, compounded by insufficient maintenance and a failure of the warning system.

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