Bell UH-1H accident near Dove Creek, CO

On July 16, 2013, a Bell UH-1H (helicopter) was involved in an accident near Dove Creek, CO. 1 person died. Damage to the aircraft: substantial.

Date
July 16, 2013
Place
Dove Creek, CO
Aircraft
Bell UH-1H · Helicopter
Injuries
1 fatal, 0 serious, 0 minor
Damage
Substantial
Position
37.756°N, 108.773°W
NTSB ID
20130716X92622

Official records · CEN13FA415

NTSB summary

HISTORY OF FLIGHT On July 16, 2013, about 0955 mountain daylight time, a Tamarack UH-1H helicopter, N775AR, was substantially damaged after a loss of control and ground impact near Dove Creek, Colorado. The pilot, the sole occupant, was fatally injured. The helicopter was registered to BVDS Incorporated and operated by Billings Flying Service under the provisions of 14 Code of Federal Regulations Part 133 during a seismic survey operation. Visual meteorological conditions prevailed for the local flight, which departed without a flight plan from a staging area near Dove Creek, Colorado, about 0953. According to ground witnesses at the survey location, the pilot flew inbound to their location from the left seat, hoisting a basket load with a long line rope. The pilot overshot the intended drop site and the basket load impacted the ground, followed immediately by the 150 foot long line falling straight down onto the basket load. At about the same time, the helicopter entered into a right bank, followed by a left bank. The helicopter subsequently impacted the ground in a steep left bank. PERSONNEL INFORMATION The pilot, age 27, held a commercial pilot certificate with airplane single and multiengine land, airplane instrument, and rotorcraft-helicopter ratings. The pilot also held a flight instructor certificate, with airplane single and multi-engine and rotorcraft-helicopter ratings, as well as a mechanic airframe and power plant certificate. On June 24, 2013, the pilot was issued a Class 2 medical certificate, with no restrictions. A review of the pilot's flight records indica

Probable cause

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.

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