BELL UH-1H near Dove Creek, CO — 2013-07-16
- Date
- 2013-07-16
- Location
- Dove Creek, CO, USA
- Aircraft
- BELL UH-1H
- Registration
- N775AR
- Category
- Helicopter
- Highest injury
- Fatal
- Fatalities
- 1
- Phase of flight
- Maneuvering
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.
Contributing factors
Contributing to the accident was an inadequate analysis of the hydraulic fluid leak by the pilot and mechanic.
NTSB narrative
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.
Analysis
- Primary failure mode
- Loss of control
- First missed decision gate
- Pilot could have aborted the drop after overshooting the intended site.
NTSB coding
Evidence available
- Photos
- 17 docket documents
Docket documents17
- Hover Performance Chartform
- Release of Aircraft Wreckage, NTSB Form 6120.15form
- 1st Interview With Mechanicinterview
- 2nd Interview With Mechanicinterview
- 3rd Interview With Mechanicinterview
- Interview With Director of Maintenanceinterview
- Interview With Ground Witness #1interview
- Interview With Ground Witness #2interview
- Interview With Ground Witness #3interview
- Interview With Operator's Co-ownerinterview
- Statement of Party Representatives to NTSB Investigationinterview
- Aircraft Weighing Recordother
- Photo 1 View of helicopter at accident sitephotos
- Photo 2 Side view of helicopter at accident sitephotos
- Photo 3 Basket load at accident sitephotos
- Excerpt of US Army Flight Characteristics reportreport
- Toxicological Reportreport
Related mishaps
- MIGHTYFLY INC MF-100
2026-03-02 · Atwater, CA
- KAMAN AEROSPACE CORP K-1200
2025-08-22 · Eagle, CO
- ROBINSON HELICOPTER COMPANY R44 II
2025-07-04 · Pecos, TX
- EUROCOPTER AS 350 B2
2024-12-10 · Los Alamitos, CA
- ENSTROM HELICOPTER CORP 280C
2024-10-09 · Vale, OR
- ROBINSON HELICOPTER R44
2024-09-06 · Grand Forks, ND