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Atlas / NTSB / CEN10LA457

NTSB CAROL · Event

Event CEN10LA457

2010-08-02 Burnet, Texas, United States Airport · BMQ None 1 aircraft Status: Completed

Registry · N5177E

FAA Aircraft Registry record.

Make / Model

CESSNA 180B

Year of manufacture

1959 · 51 years old at event

Engine

CONT MOTOR O-470 SERIES (230 hp)

Seats / Engines

4 seats · 1 engine

Last airworthiness date

19590309

ADS-B equipped

Yes — Mode-S A67EC2

Registrant of record

ABRAHAM EDWARD C

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The failure of the tailwheel compression spring, which resulted in a loss of directional control during landing.

Factual narrative

On August 2, 2010, about 0830 central daylight time, a Cessna 180B airplane, N5177E, was substantially damaged during landing at Burnet Municipal Airport (BMQ), Burnet, Texas. The private pilot was not injured. The airplane was owned and operated by a private individual under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed for the flight, which operated without a flight plan. The flight originated from the Llano Municipal Airport (AQO), Llano, Texas about 0700. The pilot reported he was delivering the airplane to BMQ to have the tailwheel examined to troubleshoot tailwheel shimmy. He performed a three point landing and during 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 hit the ground, substantially damaging the left aileron. The tailwheel assembly was sent to a repair station by the owner and disassembled. The tailwheel compression spring (part number 3222) was found broken. Failure of the 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. The pilot was flying to an airport with a maintenance facility to have a tailwheel shimmy repaired. Upon arrival at the destination airport, the pilot performed a three point landing, and, during the landing roll, 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 hit the ground. Postaccident disassembly of the tailwheel revealed that the tailwheel compression spring had broken. The failure of the compression spring allowed the tailwheel to caster freely making controllability of the airplane on the ground difficult. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).

  • C Aircraft-Aircraft systems-Landing gear system-Nose/tail landing gear-Failure - C
  • C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Attain/maintain not possible - C

Verbatim from NTSB's published report. Source file NTSB_2010_CEN10LA457.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

What the literature says.

Academic papers and agency reports matching this event's aircraft type or causal vocabulary (runway excursion, maintenance). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.

Browse the full corpus — academia portal ↗