Amateur-built Dominator accident near Gilbert, Minnesota, November 15, 2024
On November 15, 2024 at about 10:15 pm local time, a amateur-built Dominator (gyroplane), registered UNREG, was substantially damaged in an accident during maneuvering (low-alt flying) near Gilbert, Minnesota. It was a personal flight under general aviation rules (Part 91). 1 person was seriously injured. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
A total loss of engine power and subsequent autorotation to a swamp, that resulted in a rollover. Contributing to the pilot’s delayed egression from the gyroplane, was the lack of a restraint system cutting device.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- November 15, 2024 · about 10:15 pm local time
- Place
- Gilbert, Minnesota · map
- Type
- Accident
- Injuries
- 1 person was seriously injured.
- Weather
- visual conditions (good weather)
- Aircraft
- Amateur-built Dominator NO SERIES
- Registration
- UNREG · no longer on the register · serial Unknown
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The non-certificated pilot departed from the airport in the unregistered experimental gyroplane for a local area flight. Shortly after departure, the experimental 2-stroke engine sustained a total loss of engine power. The pilot initiated an autorotation to a swamp. After successfully landing the gyroplane, the pilot began the shutdown process. However, due to the “spongy and soft” ground, the gyroplane began to “wobble,” and the gyroplane rolled over to the right. The pilot was then pinned under the gyroplane, and he was unable to release the lap belt. About an hour later, he found his cellular phone and contacted first responders who were able to later extract him from the gyroplane. The single seat gyroplane, with no airframe serial number, sustained substantial damage to the main rotor system and the empennage. Postaccident examination revealed that the gyroplane had an empty weight of about 405 pounds, that exceeded the 254-pound empty weight limit for powered ultralight vehicles. The pilot reported the gyroplane held “5 to 6 gallons” of fuel, as powered ultralight vehicles are not to exceed a 5-gallon fuel capacity per regulation. When the pilot purchased the gyroplane several months prior to the accident, it came with no documentation, and thus the maintenance history for the airframe and the engine was undetermined. The engine manufacturer has previously published a warning that states, “This engine, by its design, is subject to sudden stoppage.” As a lesson learned, the pilot suggested to have a cutting device available if an occupant is unable to activate the release mechanism for a restraint system.
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
What happened, in order
- Loss of engine power (total) during maneuvering (low-alt flying) defining event
- Autorotation Off-field or emergency landing
- Roll over during landing
- Evacuation during post (impact)
The NTSB's findings
- Aircraft › Aircraft power plant › Engine (reciprocating) › (general) › Failure
- Environmental issues › Physical environment › Runway/land/takeoff/taxi surface › Soft surface › Effect on equipment
- Aircraft › Aircraft systems › Equipment/furnishings › Flight compartment equipment › Incorrect use/operation
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › (general) › Attain/maintain not possible
Pilot
- Certificate: student
- Flight time: 325 hours in all; 15 in the last 90 days; 270 as pilot in command
- Medical certificate: None
- Seat: sngl
- Injury: serious injuries
The aircraft
- Last inspection: inspection type not recorded
- Seats: 1
- Landing gear: fixed
- Engine: Rotax Aircraft Engines 582 UL (piston); 0 hours total
The flight
- Departed from: EVM Eveleth MN at 10:05 pm
- Flight plan: none
Weather at the time
- Light: daylight
- Wind: from 230° at 3 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 46°F (8°C), dew point 39°F (4°C)
- Altimeter: 30.05 inHg
- Observation at 4:05 pm from KEVM, 1 miles away
Weather report (METAR): KEVM 152205Z AUTO 23003KT 10SM CLR 08/04 A3005 RMK AO1
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Photographs from the investigation 4 pictures from the NTSB's docket, as the NTSB released them
Photograph 1 – View of the fuselage and the engine at the accident site
Photograph 2 – View of the empennage and the engine at the accident site
Photograph 3 – View of the cockpit at the accident site
Photograph 4 – View of the aircraft recovered from the accident site and inside of a hangarThe NTSB's photographs with the NTSB's captions, at screen size. Open a picture to see it full size or to report one that should not be shown.
Documents from the investigation the NTSB's docket: the evidence folder behind the report
5 documents, released by the NTSB on April 22, 2025. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.
| # | Document | What it is | |
|---|---|---|---|
| 1 | Pilot/operator Aircraft Accident Report, NTSB Form 6120.1 | PDF, 16 pages | View Download |
| 2 | Accident Photographs | PDF, 5 pages · our copy | View Download |
| 3 | Eveleth Police Department - Unregistered Aircraft Accident Report | PDF, 2 pages | View Download |
| 4 | Federal Aviation Administration - Unregistered Aircraft Examination Report | PDF, 1 page | View Download |
| 5 | Rotax Aircraft Engines 582 Ul Series Operators Manual - Safety Information | PDF, 4 pages | View Download |
The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.
Other NTSB records under UNREG the same tail number, which may have belonged to a different aircraft at the time
Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
