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Accidents · NTSB DEN02FA076 · Final report

Amateur-built Doug 2000 accident near Ogden, Utah, July 17, 2002

On July 17, 2002, a amateur-built Doug 2000 (gyroplane), registered N2058T, was destroyed in an accident near Ogden, Utah (Ogden-Hinckley airport). It was a personal flight under general aviation rules (Part 91). 2 people were killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

the pilot's failure to obtain and maintain adequate main rotor rpm, resulting in blade flapping and subsequent blade contact with the airframe, severing of the tailboom, and causing loss of aircraft control. Contributing factors were the high gusty winds, and the pilot's lack of proper certification.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
July 17, 2002
Place
Ogden, Utah · Ogden-Hinckley · map
Type
Accident
Injuries
2 people were killed.
Weather
visual conditions (good weather)
Aircraft
Amateur-built Doug 2000
Registration
N2058T · no longer on the register · serial H2-02-13-535
Damage
Destroyed
Flight
Personal flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

Main rotor blade rpm was seen to slow as the pilot waited for landing traffic to clear the runway. The pilot was then cleared for takeoff on runway 34. Wind was reported to be from 320 degrees at 16 knots, gusting to 23 knots. Main rotor rpm was seen to increase as the gyroplane began its takeoff roll. After it had lifted off and climbed 200 to 400 feet, witnesses saw something separate from the gyroplane and it fall to the ground. An endorsement in the pilot's logbook indicated he was competent for "solo day flight...with winds less than 15 knots and crosswind component less than 8 knots." He was not rated in gyroplanes. Wreckage examination revealed the rectangular boxed beam tail boom was twisted and severed about 2 feet in front of the vertical stabilizer. The vertical stabilizer leading edge bore chop marks. The rudder was shattered. A diagonal crease mark was noted on the left surface of the vertical stabilizer, running from the upper leading edge to the lower trailing, near the tail wheel. Both rudder cables were severed. The outboard portions of all four pusher propeller blades were severed at the same angle. Both main rotor blades were bent downward at the hub, and one blade was severed. The pilot's toxicology screen was positive for nordiazepam, oxazepam, and temazepam. These are metabolites of benzodiazepine. The most common benzodiazepine, Valium, prescribed under the name of Restoril, is a tranquilizer used in the treatment of anxiety, and is contraindicated for flying. Since benzodiazepines were not detected in blood, the pilot most likely was not under its influence. The aircraft's flight manual gives the following warnings: "Attempting takeoff at full engine power with initial rotor speed less than 150 rpm will lead to blade flapping. In this condition the rotor will contact the ground."

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

Pilot

  • Certificate: commercial pilot
  • Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane
  • Flight time: 1,231 hours in all; 30 in this make and model; 1,060 as pilot in command; 467 on instruments
  • Last flight review: April 20, 2001
  • Medical certificate: Class 2 (valid medical--w/ waivers/lim.)
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 80 hours
  • Last inspection: condition inspection, June 26, 2002; 78 hours since
  • Maximum gross weight: 1,500 lb
  • Seats: 2
  • Landing gear: fixed
  • Engine: Subaru EJ25 (piston); 0 hours total
  • Fire on the ground

The flight

  • Departed from: OGD Ogden UT
  • Flight plan: none
  • Runway 34, 5,352 ft by 150 ft

Weather at the time

  • Light: daylight
  • Wind: from 300° at 13 knots, gusting 23
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 90°F (32°C), dew point 52°F (11°C)
  • Altimeter: 30.00 inHg
  • Observation at 11:53 pm from OGD

Injuries

FatalSeriousMinorNone
Crew1
Passengers1

Documents from the investigation the NTSB's docket: the evidence folder behind the report

The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.

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.