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 ↗.
Search this event elsewhere
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