Casualties unknown

2001-05-18: Piper PA-22-150 (N3170Z) — Concord, CA

Concord, CA, US

On May 18, 2001, a Piper PA-22-150 (registration N3170Z) was involved in an aviation accident near Concord, CA. Investigators recorded the probable cause as: The pilot's failure to maintain directional control during the landing roll due to overcorrection in a crosswind condition. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

A light aircraft experienced a ground loop after overcorrecting for a crosswind during the landing roll. The pilot lost directional control while attempting to counteract a rightward veer, resulting in the airplane circling off the runway.

What happened

The accident occurred during the landing phase of flight. Prior to touchdown, the pilot observed a 90-degree crosswind with a speed of 10 knots. As the aircraft touched down and began its landing roll, it started to veer toward the right side of the runway.

In response to this deviation, the pilot applied full left rudder and utilized the brakes to correct the trajectory. However, this input proved excessive, causing the airplane to overcorrect sharply to the left. The pilot was unable to regain control or align the aircraft with the runway heading. Consequently, the airplane entered a continuous left turn, completing a circle on the ground before coming to rest.

The investigation

Following the incident, an examination of the aircraft was conducted to determine if any mechanical failures contributed to the loss of control. The pilot reported that no mechanical anomalies were detected with the airplane prior to or during the event. The investigation confirmed that the aircraft's systems functioned normally, pointing to pilot input and environmental factors as the primary elements in the sequence of events.

Findings

The analysis indicates that the loss of directional control was directly linked to the pilot's reaction to the crosswind conditions. While the initial veer to the right was a common challenge during crosswind landings, the application of full left rudder and braking resulted in an overcorrection. This excessive input caused the aircraft to swing violently to the opposite side, making it impossible for the pilot to recover the runway centerline. The resulting ground loop was the direct outcome of this control error.

Safety message

This incident highlights the critical importance of smooth, progressive control inputs during crosswind landings. Overcorrection can quickly lead to a loss of directional control, especially on paved surfaces where traction is high. Pilots are reminded to maintain appropriate rudder pressure and avoid abrupt braking or steering adjustments when correcting for runway drift.

Probable cause

The pilot's failure to maintain directional control during the landing roll due to overcorrection in a crosswind condition.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20010604X01070. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.