EUROCOPTER AS 350 B3 near Somerville, TN — 2013-10-22
- Date
- 2013-10-22
- Location
- Somerville, TN, USA
- Aircraft
- EUROCOPTER AS 350 B3
- Registration
- N353HW
- Category
- Helicopter
- Highest injury
- Fatal
- Fatalities
- 3
- Phase of flight
- Climb
Probable cause
The pilot’s inadvertent encounter with night, instrument meteorological conditions while responding to an obstacle alert, resulting in an in-flight loss of helicopter control.
NTSB narrative
The flight was dispatched to pick up a patient at a hospital and transport him to another hospital near the helicopter's home base. The pilot performed a weather check, and the flight departed with two medical staff on board. Night, visual meteorological conditions prevailed at the departure helipad. Satellite tracking data revealed that the helicopter proceeded in an easterly direction, following a US highway. The helicopter then climbed in right-hand turn until the satellite data ended; the helicopter was about 1,116 feet above ground level (agl). The wreckage was found, burning, in a wooded area, about 3,300 feet south of the US highway. No eyewitnesses to the accident were located. The helicopter impacted the trees at a steep angle, and the orientation of the main wreckage was indicative of a loss of helicopter control before impact. The wreckage was largely consumed by a postcrash fire. Examination of the airframe, rotor system, and engine did not reveal evidence of a preexisting mechanical malfunction of failure. Rotational signatures on the main rotor and engine indicated that the engine was producing power at the time of the accident. The helicopter was equipped with night vision goggles (NVG) and NVG-capable lighting. The pilot had been trained on the use of NVG about 12 months before the accident. The helicopter was not equipped for flight under instrument flight rules. A review of the weather conditions revealed that, at an airport within 2 miles of the accident site, few clouds were observed at 800 feet agl, and a broken ceiling existed at 1,200 feet agl. A review of the helicopter's ground track revealed two obstacles in the immediate vicinity, an unlit, nonoperational cellular tower, 140-feet tall, and a water tower, about 115-feet tall. The helicopter was equipped with a Helicopter Terrain Avoidance Warning System (HTAWS). Although recorded HTAWS data was not available, research and flight testing revealed that the pilot may have received an in-flight obstacle alert, prompting a climb. Considering the low clouds and night conditions that probably existed along the last segment of the flight's track, it is likely that the pilot initiated a climb and inadvertently entered instrument meteorological conditions, where a loss of helicopter control occurred.
Analysis
- Primary failure mode
- VFR into IMC
- First missed decision gate
- Pilot should have aborted the flight due to deteriorating weather conditions.
NTSB coding
Evidence available
- ADS-B / radar
- Photos
- 32 docket documents
Docket documents32
- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1form
- Release of Aircraft Wreckage, NTSB Form 6120.15form
- Hospital Wing Personnel Statementsinterview
- Statement of Party Representatives to NTSB Investigationinterview
- Witness Statementsinterview
- Cell Tower Dataother
- Crew Briefing Checklist and Risk Assessment Worksheetother
- Excerpts – Company Flight Training Recordsother
- Excerpts – Maintenance Records, Airframeother
- Excerpts – Maintenance Records, Powerplantother
- FAA Operations Specifications A021other
- Flight Manifestsother
- HTAWS Flight Test Dataother
- Pilot Flight Time Data – Hospital Wingother
- Weather Dataother
- Photo 1 – Main Wreckage – Looking Eastphotos
- Photo 10 – Engine, Compressor Sectionphotos
- Photo 11 – Main Rotor Bladesphotos
- Photo 12 – Tail Rotor Drive Shaft Sectionsphotos
- Photo 13 – Tail Rotor Gearbox Section, Disassembledphotos
- Photo 14 – Tail Rotor Gearbox Section, Disassembled (Eurocopter Photo)photos
- Photo 2 – Main Wreckage – Looking Eastphotos
- Photo 3 – Main Wreckage – Looking Westphotos
- Photo 4 – Main Rotor Hub and Transmissionphotos
- Photo 5 – Enginephotos
- Photo 6 – Broken Tree Within Debris Fieldphotos
- Photo 7 – Self-supporting Lattice Towerphotos
- Photo 8 – Engine, After Recoveryphotos
- Photo 9 – Main Rotor Hub and Transmission, After Recoveryphotos
- Flight Track Dataradar
- Additional Run Reports – Hospital Wingreport
- Toxicological Reportreport
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