The U.S. aircraft register, updated daily
Accidents · NTSB CEN13FA415 · Final report

Bell UH-1H accident near Dove Creek, Colorado, July 16, 2013

On July 16, 2013 at about 3:55 pm local time, a 1977 Bell UH-1H (helicopter), registered N775AR, was substantially damaged in an accident during maneuvering (hover) near Dove Creek, Colorado. It was an external-load flight under external-load helicopter rules (Part 133). 1 person was killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

Pilot-induced oscillations caused by the loss of hydraulic assist of the flight controls due to an excessive loss of hydraulic fluid during a critical phase of flight, which resulted in ground impact. Contributing to the accident was an inadequate analysis of the hydraulic fluid leak by the pilot and mechanic.

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

What the record shows

Date
July 16, 2013 · about 3:55 pm local time
Place
Dove Creek, Colorado · map
Type
Accident
Injuries
1 person was killed.
Weather
visual conditions (good weather)
Aircraft
Bell UH-1H, built 1977 · all UH-1Hs on the register
Registration
N775AR · registry record · serial 65-10067
Damage
Substantial damage
Flight
External-load flight · external-load helicopter rules (Part 133)

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

The helicopter pilot flew inbound to a seismic survey location hoisting a basket load with a long-line rope. The pilot overshot the intended drop site, and the basket load and long-line impacted the ground after the pilot likely initiated a load release. The helicopter then entered a right bank, followed by a steep left bank, and subsequently impacted the ground. Postaccident examination of the helicopter revealed evidence consistent with a loss of hydraulic fluid from the flight control system due to a hydraulic leak of a check valve fitting near the tail rotor servo. As the pilot approached the survey location, the loss of hydraulic pressure most likely resulted in very-high collective control forces and pilot-induced oscillations. The director of maintenance stated that the pilot and a mechanic were aware of the hydraulic fluid leak and had ordered replacement parts; however, they had not yet been installed. He stated that they did not expect the leak to cause a significant issue. Thus, it is likely that they did not foresee the leak causing a significant flight hazard.

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. Collision with terrain or object (not controlled flight into terrain) during maneuvering (hover)
  2. Loss of control in flight during maneuvering (hover) defining event

The NTSB's findings

  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Lateral/bank control › Attain/maintain not possible
  • cause Aircraft › Fluids/misc hardware › Fluids › Hydraulic fluid › Incorrect service/maintenance
  • factor Personnel issues › Action/decision › Info processing/decision › Understanding/comprehension › Pilot
  • factor Personnel issues › Action/decision › Info processing/decision › Understanding/comprehension › Ground crew

Pilot

  • Certificate: flight instructor, commercial pilot
  • Ratings: multi-engine land; multi-engine sea; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: helicopter; instrument: airplane; rotorcraft: helicopter
  • Flight time: 5,000 hours in all; 1,800 in this make and model; 25 in the last 30 days; 5,000 as pilot in command
  • Last flight review: February 26, 2013
  • Medical certificate: Class 2 (without waivers/limitations)
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 14,798 hours
  • Last inspection: annual inspection, June 5, 2013; 41 hours since
  • Seats: 15
  • Landing gear: fixed
  • Engine: Lycoming T53-L-13B (turboshaft); 0 hours total

The flight

  • Departed from: Dove Creek CO at 3:53 pm
  • Destination: Dove Creek CO
  • Flight plan: none

Weather at the time

  • Light: daylight
  • Wind: from 300° at 4 knots
  • Visibility: 10 statute miles
  • Sky: overcast at 8,500 ft
  • Temperature: 70°F (21°C), dew point 54°F (12°C)
  • Altimeter: 30.25 inHg
  • Observation at 3:53 pm from KCEZ, 21 miles away

Injuries

FatalSeriousMinorNone
Flight crew1

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.