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Atlas / NTSB / CEN25LA337

NTSB CAROL · Event

Event CEN25LA337

2025-08-23 Caseville, Michigan, United States Minor 1 aircraft Status: Completed

Registry · N707EE

FAA Aircraft Registry record.

Make / Model

BELL OH-58A

Year of manufacture

1972 · 53 years old at event

Engine

ALLISON T63-A-700 (317 hp)

Seats / Engines

4 seats · 1 engine

Last airworthiness date

20170709

ADS-B equipped

Yes — Mode-S A96EF8

Registrant of record

ENGLER ERIC M DBA

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The front seat passenger’s inadvertent movement of the cyclic control resulting in a dynamic rollover after landing. Contributing to the accident was the pilot’s decision to leave the dual flight controls installed with a non-pilot passenger in the front seat.

Factual narrative

The pilot reported that while on a local flight he noticed a squall line approaching and elected to return to the private strip from which he had departed. During the approach, rain intensity increased, and the wind began gusting to about 15 knots. The pilot landed the helicopter, lowered the collective, and reduced power. While the main rotor was turning about 420 rpm, the helicopter suddenly rolled over onto its right side, resulting in substantial damage to the main rotor system and fuselage. The pilot reported that the dynamic rollover was likely caused by the front seat passenger inadvertently contacting the cyclic control while turning to speak with the rear seat passenger. The OH-58A flight manual notes that when carrying non-rated passengers unfamiliar with helicopter operation, the pilot should evaluate the advantages and disadvantages of stowing the copilot controls or accepting the potential hazard of leaving them installed. The Federal Aviation Administration Helicopter Flying Handbook (FAA-H-8083-21B) states, “If possible, remove front passenger flight controls and ensure all passenger personal items, such as cameras and mobile phones, are secure.” Bell Helicopter Operational Safety Notice GEN-20-50 advises that pilots emphasize avoidance of flight and engine controls during preflight briefings, especially when dual controls are installed, and further notes that removing the dual controls, if installed, remains an option to prevent inadvertent interference. The pilot reported that there were no preaccident mechanical anomalies or failures that would have precluded normal operation. 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).

  • Personnel issues-Experience/knowledge-Knowledge-Knowledge of equipment-Passenger
  • Personnel issues-Action/decision-(general)-(general)-Pilot
  • Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Lateral/bank control-Not attained/maintained
  • Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot
  • Aircraft-Aircraft systems-Flight control system-Control column section-Unintentional use/operation

Verbatim from NTSB's published report. Source file NTSB_2025_CEN25LA337.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 ↗