Casualties unknown

2004-03-11: Cessna C195A (N9869A) — Gila Bend, AZ

Gila Bend, AZ, US

On March 11, 2004, a Cessna C195A (registration N9869A) was involved in an aviation accident near Gila Bend, AZ. Investigators recorded the probable cause as: The tail wheel locking prevented the pilot from steering, resulting in a ground loop. 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 private pilot ground looped while attempting to land during a checkout flight when the tail wheel locked, preventing rudder input and causing an uncontrolled right turn.

Overview

During a checkout flight intended to familiarize a private pilot with a newly purchased airplane, the aircraft experienced a ground loop while attempting to land. The incident occurred when the tail wheel locked, rendering the rudder ineffective and causing the airplane to veer uncontrollably.

Flight Details

The purpose of the flight was for a certified flight instructor (CFI) to provide a checkout to the private pilot. The pilot had completed approximately four full stall landings prior to the accident landing. During each of those landings, the pilot consistently drifted to the left during the landing roll.

Incident Description

On the next landing attempt, the pilot touched down and again drifted to the left. The CFI instructed the pilot to input left rudder to correct the drift. However, the pilot was unable to steer because the tail wheel had become locked. As a result, the airplane began a long turn to the right and subsequently ground looped in the same direction.

Pilot Experience

The pilot had purchased the airplane the day before the accident and had accumulated a total of 3.6 hours of flight time in the same make and model. This limited experience in the specific aircraft type may have been a factor in the difficulty managing the directional control during landing.

Mechanical Status

The pilot reported that there were no preimpact mechanical malfunctions or failures with the airplane, apart from the tail wheel locking issue that occurred during the landing roll. The locking of the tail wheel was the direct mechanical impediment that prevented the pilot from maintaining directional control.

Probable cause

The tail wheel locking prevented the pilot from steering, resulting in a ground loop.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20040406X00423. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.