Accident Eurocopter AS 350B3 AStar N910S,
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ASN Wikibase Occurrence # 235216
 
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Date:Monday 29 October 2018
Time:13:45
Type:Silhouette image of generic AS50 model; specific model in this crash may look slightly different    
Eurocopter AS 350B3 AStar
Owner/operator:Enbridge Energy Co Inc
Registration: N910S
MSN: 7446
Year of manufacture:2012
Total airframe hrs:2965 hours
Engine model:Turbomeca (Safran) Arriel 2D
Fatalities:Fatalities: 1 / Occupants: 1
Aircraft damage: Destroyed
Category:Accident
Location:Odanah, WI -   United States of America
Phase: En route
Nature:Survey
Departure airport:Ironwood, MI (IWD)
Destination airport:Madison, WI (MSN)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The pilot was on a scheduled pipeline patrol observation flight in a turboshaft-powered helicopter. When the pilot did not arrive at his destination, an alert notice was issued for the overdue helicopter. The helicopter wreckage was located about 22 miles west of the helicopter's departure point in a remote wooded area that was about 200 yards north of the east-west pipeline. The pilot was not in contact with air traffic control during the flight, and there was no record of a distress call. A witness working on the pipeline about 2 to 3 miles from the accident site, reported seeing the helicopter fly overhead and further reported that the helicopter looked and sounded "normal."

Visual meteorological conditions surrounded the area of the accident with 10 miles visibility and an overcast sky at 1,600 ft.

The post-crash fire consumed most of the cabin area, which limited the scope of the airframe and engine examinations. Additionally, fire damage prevented the retrieval of information from the helicopter's cockpit image and flight data monitoring system, including nonvolatile memory from the digital engine control unit and engine data recorder. However, no preimpact abnormalities were noted during the engine or airframe examinations. Further, the engine's intake axial compressor blades exhibited damage near the outer tips, and the module 5 torque nut had a slippage of about 1/16 to 1/8 inch, (2 to 4 millimeters) consistent with the engine producing power at the time of impact.

The pilot's autopsy noted moderate-to-severe coronary artery disease, scarring of the heart muscle from a previous myocardial infarction (heart attack), and changes in the blood vessels of the liver that were indicative of congestive heart failure. Thus, the pilot would have been at an increased risk for an acute coronary event causing symptoms such as shortness of breath, chest pain, palpitations, or fainting. The pilot's complete medical history was not available, and a determination of medical impairment or incapacitation could not be made based on the available evidence for the accident.

Probable Cause: The pilot's loss of helicopter control for undetermined reasons.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: CEN19FA018
Status: Investigation completed
Duration: 1 year and 5 months
Download report: Final report

Sources:

NTSB

Location

Revision history:

Date/timeContributorUpdates
19-Apr-2020 07:05 ASN Update Bot Added

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