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CEN25LA408 · Bell Helicopter Textron Canada 206L-3

22 Aug 2025 · Picayune, MS, United States

925DT Bell Helicopter Textron Canada 206L-3 · Accident: hard landing during autorotation

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Event

NTSB case
CEN25LA408
Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Accident
InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
Ongoing
Event fatalities
Unknown
Ground fatalities
Unknown
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
General aviation
WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
Visual Meteorological Cond

Bell Helicopter Textron Canada 206L-3

Aircraft type
Bell 206
Category
Helicopter
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N17TL
Operator
925DT
Onboard fatalities
Unknown
Route
From not recordedTo not recorded
Aircraft age
About 33 years (built 1992)
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 91: General Aviation
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
Autorotation
Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
Hard landing
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Substantial

Cause areas

No findings designated as a cause are recorded in the NTSB data yet.

Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.

NTSB narrative

On August 22, 2025, about 1130 central daylight time, a Bell Helicopter Textron Canada 206L-3 helicopter, N17TL, was substantially damaged when it was involved in an accident near Picayune, Mississippi. The pilot and passenger were not injured. The helicopter was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The purpose of the flight was to inspect a hangar being built for the operator at the Picayune Municipal Airport in Picacyune, Mississippi. The pilot stated that he does a few practice maneuvers during each flight and on this flight, he was practicing a “quick stop” simulated emergency procedure. At the conclusion of the maneuver, while the pilot was pulling up on the collective to recover, he heard the low rotor RPM warning horn sound. The pilot verified that the throttle control was at full RPM; however, he noticed that the helicopter was no longer responding to the collective control. The pilot chose to immediately enter an autorotation from about 50 ft and when the helicopter contacted the taxiway, the left skid collapsed, the helicopter skidded about 15 ft, and came to a stop upright which resulted in substantial damage to the tailboom. The accident was not reported to the NTSB until February 26, 2026. During the intervening period, the helicopter was sold for salvage by the accident owner’s insurance company, and the airframe was disassembled for repair by the new owner. Due to the current disposition of the airframe, examination is not feasible. The accident was not known to the FAA until the new owner attempted to register the helicopter with the FAA in January 2026. At the time of notification, only the Rolls-Royce 250-C30P turboshaft engine was able to be secured for further examination. The disposition of the turboshaft engine between the accident and its recovery for further examination could not be determined. The engine will be examined at a future date.

Verbatim NTSB factual narrative from the NTSB dataset

Sources

NTSB record CEN25LA408
Event ID
20260302202581
Case number
CEN25LA408
Dataset
full-current
Source SHA-256
5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
Source notes (4)
  • Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
  • Filled from the NTSB case API where the bulk record had no value: investigation status, coordinates. Values present in the bulk record are kept.
  • The date is the local date, which is the same as the UTC date the NTSB stores.
  • API snapshot SHA-256: ac8da5fb871b5f043941cac442ef60a128b948f6a8322d53a2d3b34a60be68f9; retrieved 2026-09-16T20:53:21.924Z.