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CEN20CA193

2020-05-22 · Ionia, Michigan, United States · None · 1 aircraft · Status: Completed

Airport Y70

Current FAA registration · N5179D

Make / Model
CESSNA 182A
Year of manufacture
1958 · 62 years old at event
Engine
CONT MOTOR O-470 SERIES (230 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19580522
ADS-B equipped
Yes — Mode-S A67F07

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's failure to maintain directional control during landing. Contributing was the pilot getting his shoe caught in the rudder pedal.

Factual narrative

The pilot was performing an instrument approach to the runway following a local flight. The airplane was configured with full flaps and the pilot's intention was to perform a three-point landing. The wind was reported as calm; however, the pilot reported seeing smoke that indicated there was a light crosswind from the right. After touching down on the runway the tailwheel began to "shimmy violently," and the airplane began to drift to the left. The pilot applied rudder to get the airplane to track "a straight path" and then turned right to correct back to the runway's centerline. To recorrect to the centerline, the pilot applied full left rudder. At that point, either the pilot's "left shoe caught on something and jammed the pedal, or the left rudder pedal [became] stuck in the full left rudder position." The pilot couldn't move the pedal to maintain directional control and the airplane ground looped causing substantial damage to the right aileron and the right elevator. A postaccident examination showed no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. The pilot was performing an instrument approach to the runway following a local flight. The airplane was configured with full flaps and the pilot's intention was to perform a three-point landing. The wind was reported as calm; however, the pilot reported seeing smoke that indicated there was a light crosswind from the right. After touching down on the runway the tailwheel began to "shimmy violently," and the airplane began to drift to the left. The pilot applied rudder to get the airplane to track "a straight path" and then turned right to correct back to the runway's centerline. To recorrect to the centerline, the pilot applied full left rudder. At that point, either the pilot's "left shoe caught on something and jammed the pedal, or the left rudder pedal [became] stuck in the full left rudder position." The pilot couldn't move the pedal to maintain directional control and the airplane ground looped causing substantial damage to the right aileron and the right elevator. A postaccident examination showed no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
  • C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Attain/maintain not possible - C
  • F Personnel issues-Miscellaneous-(general)-(general)-Pilot - F

Verbatim from NTSB's published report. Source file NTSB_2020_CEN20CA193.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

Matched on aircraft type. All research papers