No fatalities

2 Aug 2010: CESSNA 180B (N5177E) — MORGAN EDWARD A — Burnet, TX

Burnet, TX, United States

On 2 Aug 2010, a CESSNA 180B (registration N5177E) operated by MORGAN EDWARD A was involved in an aviation accident near Burnet, TX. No fatalities were reported. Investigators recorded the probable cause as: The failure of the tailwheel compression spring, which resulted in a loss of directional control during landing. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

A Cessna 180B experienced a runway excursion during landing after the tailwheel compression spring broke, causing loss of directional control. The pilot was uninjured; the left aileron was substantially damaged.

Accident Overview

On August 2, 2010, about 0830 central daylight time, a Cessna 180B airplane, registration N5177E, was substantially damaged during landing at Burnet Municipal Airport (BMQ) in Burnet, Texas. The private pilot was not injured. The airplane was owned and operated by a private individual under 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed, and the flight operated without a flight plan.

Flight Details

The flight originated from Llano Municipal Airport (AQO) in Llano, Texas, about 0700. The pilot reported that he was delivering the airplane to BMQ to have the tailwheel examined to troubleshoot tailwheel shimmy.

Accident Sequence

During landing, the pilot performed a three-point landing. During the rollout, the rudder pedals began to "shudder violently." The pilot was unable to control the airplane, and it exited the right side of the runway. During the runway excursion, the left wing struck the ground, substantially damaging the left aileron.

Tailwheel Examination

The tailwheel assembly was sent to a repair station by the owner and disassembled. The tailwheel compression spring (part number 3222) was found broken. The broken compression spring would allow the tailwheel to caster freely. The broken compression spring was not retained, so an examination to determine the cause of the failure could not be performed.

Contributing factors

Nose/tail landing gear — FailureAttain/maintain not possible