Aviation Crash Map

Robinson R44 N616HS

8 July 2018 · Williamsburg, Virginia, United States · Fatal

Summary

On 8 July 2018 at about 20:33 local time, a Robinson R44 registered N616HS was involved in an accident near Williamsburg, Virginia, United States. 2 people were on board and one died. One person on the ground also died. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 20:33
Classification
Accident
Location
Williamsburg, Virginia, United States
Nearest airport
Williamsburg-Jamestown (JGG)
Coordinates
37.2883, -76.7294
Aircraft
Robinson R44
Registration
N616HS
Category
Helicopter
Year built
2004
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Williamsburg → Stafford
Aircraft damage
Destroyed
Weather
VMC
Light
Day
NTSB number
ERA18FA187

People

1 person died, including 1 on the ground.

On board Died Serious Minor Uninjured On the ground
2 1 0 0 0 1

Probable cause

The pilot's failure to safely operate the helicopter due to his impaired cognitive and physical abilities, which resulted in a loss of control.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

On the morning of the accident, the pilot flew the helicopter cross-country to attend a meeting at another airport. He departed on the return flight to his home airport later that afternoon and climbed the helicopter to an altitude of about 1,700 ft, leveled off, and the groundspeed increased. About 3 minutes after takeoff, the helicopter entered a right descending turn that continued until it impacted a condominium building at a high vertical speed. Witnesses reported that the helicopter rocked "back and forth unsteadily" before it suddenly pitched downward to impact the roof of the building. Examination of the wreckage revealed no anomalies that would have precluded normal operation. The engine crankshaft gear bolt was found unthreaded and the alignment pin for the crankshaft gear was found sheared. The locking tab designed to prevent rotation of the bolt was found attached and intact. Examination of the bolt, locking tab, and accessory gears revealed no pre-impact damage. Had the bolt unthreaded during flight, the engine would have stopped running; however, the engine oil coolers exhibited grinding damage consistent with the engine rotating at the time of impact, and witnesses reported hearing the engine running continuously until the impact. It is therefore likely that the bolt unthreaded during the accident sequence. The forward-facing accessory case cover was found impact damaged and partially missing. Had the accessory gear train stopped rotating due to impact or from fragments of the cover or debris in the gear mesh, the crankshaft could continue to rotate briefly, allowing the bolt to unthread without damaging the locking tab. The 85-year-old pilot was diagnosed with Parkinson's disease about 3 years before the accident. He experienced tremors in both hands, which was treated with medication and surgery with some success. The tremors consistently affected his left hand more than the right, and he reported that the tremors were more pronounced later in the day. Although the severity of his tremors or to what degree they may have affected his ability to fly the helicopter could not be determined, it is possible that they may have had more of an effect during the accident flight than on the day's earlier flight. In the 2 years preceding the accident, the pilot's doctors noted mild dementia and mild cognitive impairment. His dementia was treated with medication (which he subsequently discontinued), and reportedly improved, although his mild cognitive impairment persisted. His doctors also noted that the pilot had impaired measures of simple attention and visual scanning and tracking speed, and mild, relative difficulty with sustained attention. They recommended that the pilot not fly due to concerns with his attention, reaction time, and judgment. It is likely that impairment resulted from one or more of the pilot's well-documented progressive impaired cognitive and physical abilities negatively affected his ability to safely operate the helicopter and led to the loss of control.

Quoted verbatim from the NTSB record.

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