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Accidents · NTSB LAX08FA233 · Final report

Hughes 369D accident near Price, Utah, July 19, 2008

On July 19, 2008 at about 9:40 pm local time, a Hughes 369D (helicopter), registered N400BE, was destroyed in an accident during takeoff near Price, Utah (Carbon County Regional airport). It was a personal flight under general aviation rules (Part 91). 3 people were killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilot's inadequate preflight performance planning for the takeoff and the loading that exceeded the lift performance capability of the helicopter.

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

What the record shows

Date
July 19, 2008 · about 9:40 pm local time
Place
Price, Utah · Carbon County Regional · map
Type
Accident
Injuries
3 people were killed.
Weather
visual conditions (good weather)
Aircraft
Hughes 369D · all 369Ds on the register
Registration
N400BE · no longer on the register · serial 470115D
Damage
Destroyed
Flight
Personal flight · general aviation rules (Part 91)

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

Prior to departure, the helicopter was refueled, a child passenger was replaced with an adult, and additional baggage (exact weight unknown) was added. While fueling, the pilot had a discussion with another pilot stating that the conditions at the airport may make the departure more difficult. The helicopter was observed taking off to the south and then making a right turn towards the northwest. As the helicopter approached the perimeter fence of the airport it was observed to be descending. The accident site was located about .5 nm from the last observed position. The first identified point of impact appeared to be where the left skid tube hit the ground. The ground scar was not in line with the direction of the debris energy path, but was about 270 degrees to the right. The on-scene examination of the accident site indicated that the helicopter first impacted the ground with its left skid, in a more vertical than horizontal vector. The main rotor blades displayed low rotor damage signatures. At the time of the accident the density altitude was computed to be 9,330 feet mean sea level (msl), and the pressure altitude was computed to be 5,827 feet msl. A conservative weight of the helicopter was calculated to be approximately 2,823 pounds. The helicopter’s certified gross weight is 3,000 pounds. The calculated hover performance in ground effect (HIGE) was determined to be at least 63 pounds over the performance capabilities of the helicopter. The calculated hover performance out of ground effect (HOGE) was determined to be at least 223 pounds over the performance capabilities of the helicopter. Witnesses reported the winds at the time of the accident as 10 knots out of the south. Post accident examination of the airframe and engine components found no anomalies that would have precluded normal operation.

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

  1. Preflight or dispatch event during prior to flight
  2. Loss of control in flight during takeoff defining event
  3. Miscellaneous/other during uncontrolled descent
  4. Hard landing during landing

The NTSB's findings

  • cause Personnel issues › Task performance › Planning/preparation › Performance calculations › Pilot
  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › (general) › Capability exceeded

Pilot

  • Certificate: private
  • Ratings: single-engine land; rotorcraft: helicopter
  • Flight time: 2,044 hours in all; 1,318 as pilot in command
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 4,148 hours
  • Last inspection: annual inspection, July 1, 2007
  • Maximum gross weight: 3,000 lb
  • Seats: 5
  • Landing gear: fixed
  • Engine: Rolls-Royce 250 (turboshaft); 0 hours total
  • Fire on the ground
  • Operator: Bbp Air LLC

The flight

  • Departed from: KPUC Price UT at 9:40 pm
  • Destination: U77 Spanish Fork UT
  • Flight plan: none

Weather at the time

  • Light: daylight
  • Wind: at 10 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 93°F (34°C), dew point 34°F (1°C)
  • Altimeter: 30.04 inHg
  • Observation at 9:53 pm from PUC, 1 miles away

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers2

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.