Ground Loop Results in Structural Damage After Heavy Braking During Tundra Landing

Casualties unknown • Palmer, AK, US

A private pilot experienced a ground loop after applying heavy braking during a landing on a remote tundra site with a tail-wheel aircraft.

What happened

The incident occurred while a private pilot was operating a tail-wheel equipped airplane fitted with tundra tires in a remote, unpaved environment. The pilot reported that the approach speed at touchdown was excessive for the conditions. Immediately after contact with the ground, the pilot applied heavy braking to slow the aircraft.

The application of excessive brake pressure caused the left main wheel to lock up completely. This sudden loss of traction on one side resulted in a rapid yaw to the left, known as a ground loop. The aircraft rotated sharply around its vertical axis while still moving forward, leading to significant structural contact with the ground.

The investigation

Post-incident examination of the airframe revealed extensive damage consistent with the forces generated during an uncontrolled ground loop. The right wing lift strut was compromised, likely due to the asymmetric loading and twisting of the fuselage during the rotation. Both horizontal stabilizers sustained damage, indicating that the tail section struck the ground or obstacles with considerable force.

Additionally, the right elevator was damaged, suggesting that the control surfaces were subjected to abnormal aerodynamic loads or physical impact during the event. The tundra tires, while designed for rough terrain, could not prevent the loss of directional control once the brake lock occurred.

Findings

The primary factor in this accident was the pilot's decision to land at a speed that required heavy braking to achieve a safe stop on the available surface. The locking of the left brake eliminated directional stability, making the ground loop inevitable. The configuration of the aircraft, specifically the tail-wheel setup, makes it inherently more susceptible to ground looping if directional control is not maintained through differential steering rather than just braking.

The damage sustained to the right wing strut, stabilizers, and elevator highlights the severity of the forces involved in such incidents. Proper speed management during the final phase of flight is critical to avoid the need for aggressive braking maneuvers that can lead to loss of control on soft or uneven surfaces.

Probable cause

The pilot's failure to maintain directional control during landing, resulting from excessive airspeed and heavy braking that locked the left wheel.

Frequently asked questions

What happened in the 1996-09-08 Piper PA-18 accident near Palmer, AK?

A private pilot experienced a ground loop after applying heavy braking during a landing on a remote tundra site with a tail-wheel aircraft.

What aircraft was involved and where did it happen?

The accident on 1996-09-08 involved a Piper PA-18, registration N9116D, at Palmer, AK.

What was the probable cause of the accident?

The pilot's failure to maintain directional control during landing, resulting from excessive airspeed and heavy braking that locked the left wheel.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001208X06660. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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