Accident Details
On December 5, 2025, about 0858 central standard time, a Hughes 369D helicopter, registration N161LA, was substantially damaged when it impacted terrain near Pryor, Oklahoma. The pilot was fatally injured. The helicopter was operated under Title 14 Code of Federal Regulations Part 91 as an aerial observation flight.
According to the operator, the helicopter departed from a landing zone about 1 mile from the accident site approximately 28 minutes before the accident. The purpose of the flight was to visually monitor power line replacement operations.
Witness Observations
Multiple witnesses employed by the power line company reported that the helicopter was hovering above and alongside a power distribution line under construction. The helicopter was moving at a slow speed, about 4 knots, while the pilot observed a device called a “sock” being pulled along the power distribution line by ground-based equipment.
The witnesses stated that the helicopter suddenly pitched up to a near inverted attitude, flew backward, then turned and pitched straight down toward the ground. They described the sequence as resembling the helicopter “flipped over on its back and fell to the ground.”
Wreckage Examination
Examination of the accident site revealed that the helicopter impacted an open field in a nose-low attitude, about 250 ft south of the power distribution line where the ‘sock’ was being observed. The first identifiable point of contact (FIPC) was a ground impression with debris fragments consistent with the forward fuselage and cabin area, and ground penetration scars consistent with the left and right skid toes. The right skid toe and forward 2–3 ft of the right skid separated from the rest of the skid and remained impaled at the FIPC.
The main wreckage came to rest on its right side on a magnetic heading of about 040°, about 6 ft south of the FIPC. The majority of the debris field was within about a 50 ft diameter of the main wreckage. One main rotor blade was located about 110 ft south of the main wreckage, another main rotor blade about 160 ft southeast, a section of main rotor blade about 160 ft south, and one pitch horn about 170 ft south. All major components of the helicopter were accounted for at the accident site.
The wreckage was recovered to a secure facility for further examination.