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Atlas / NTSB / CEN25LA287

NTSB CAROL · Event

Event CEN25LA287

2025-07-26 New Holstein, Wisconsin, United States Airport · 8D1 None 1 aircraft Status: Completed

Registry · N83PS

FAA Aircraft Registry record.

Make / Model

AEROTEK PITTS S-2A

Year of manufacture

1977 · 48 years old at event

Engine

LYCOMING AEIO-360 SER (180 hp)

Seats / Engines

2 seats · 1 engine

Last airworthiness date

19770513

ADS-B equipped

Yes — Mode-S AB5757

Registrant of record

BURT DONALD H

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot’s loss of direction control during landing due to an unapproved tailwheel assembly and tail spring that resulted in a tailwheel shimmy and a subsequent ground loop.

Factual narrative

The pilot reported that during landing on the asphalt runway, with a passenger in the front seat, the airplane had a significant tailwheel shimmy. The pilot attempted to stop the shimmy by lifting the tailwheel off the runway as the airplane continued to decelerate. As the speed decreased, the tailwheel settled back onto the runway and shimmied again, but directional control was maintained. However, the shimmy eventually became more adverse, and the pilot was unable to maintain directional control of the airplane. The airplane ground looped to the left, came to rest adjacent to the runway, and sustained substantial damage to the right wing and empennage. Postaccident examination revealed that an unapproved tailwheel assembly and tail spring were installed. The tailwheel created a negative castor angle and reduced trail, which was exacerbated by the additional weight of the rear occupant, and resulted in the tailwheel shimmy during landing. 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).

  • Aircraft-Aircraft systems-Landing gear system-Nose/tail landing gear-Malfunction
  • Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Attain/maintain not possible
  • Aircraft-Aircraft systems-Landing gear system-Nose/tail landing gear-Incorrect service/maintenance

Verbatim from NTSB's published report. Source file NTSB_2025_CEN25LA287.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 (stall). 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 ↗