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CEN20CA192

2020-05-22 · Carbondale, Illinois, United States · None · 1 aircraft · Status: Completed

Airport MDH

Current FAA registration · N5183X

Make / Model
CHAMPION 7GCBC
Year of manufacture
1969 · 51 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19690423
ADS-B equipped
Yes — Mode-S A681FE

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's excessive brake input while he attempted to maintain directional control during landing roll.

Factual narrative

The pilot reported that the accident occurred during a wheel landing in the tailwheel-equipped airplane on a hard surface runway. The pilot stated that upon touchdown the airplane began to swerve side-to-side due to the airplane's "natural instability" on the ground. The pilot attempted to maintain directional control by pulling full aft on the control stick and applying maximum braking; however, his excessive brake input while the airplane was in a level pitch attitude caused the airplane to pitch down and the propeller to impact the runway before the airplane pivoted back onto the tailwheel. The airplane came to rest upright on the runway. The tailwheel crushed the lower portion of the rudder when it landed hard on the runway. The pilot reported that there were no mechanical anomalies with the airplane that would have precluded normal operation. A postaccident examination confirmed flight control continuity and found no issues with the wheel brakes or the tailwheel. The pilot reported that the accident occurred during a wheel landing in the tailwheel-equipped airplane on a hard surface runway. The pilot stated that upon touchdown the airplane began to swerve side-to-side due to the airplane's "natural instability" on the ground. The pilot attempted to maintain directional control by pulling full aft on the control stick and applying maximum braking; however, his excessive brake input while the airplane was in a level pitch attitude caused the airplane to pitch down and the propeller to impact the runway before the airplane pivoted back onto the tailwheel. The airplane came to rest upright on the runway. The tailwheel crushed the lower portion of the rudder when it landed hard on the runway. The pilot reported that there were no mechanical anomalies with the airplane that would have precluded normal operation. A postaccident examination confirmed flight control continuity and found no issues with the wheel brakes or the tailwheel. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • C Aircraft-Aircraft systems-Landing gear system-Brake-Incorrect use/operation - C
  • C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Surface speed/braking-Incorrect use/operation - C
  • C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C

Verbatim from NTSB's published report. Source file NTSB_2020_CEN20CA192.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.