- Location: West Alton, MO
- Accident Number: CEN25FA307
- Date & Time: August 7, 2025, 10:59 Local
- Registration: N173AL
- Aircraft: Hughes 369D
- Injuries: 2 Fatal
- Flight Conducted Under: Part 133: Rotorcraft ext. load
On August 7, 2025, about 1059 central daylight time, a Hughes (MD Helicopters) 369D helicopter, N173AL, was destroyed when it was involved in an accident near West Alton, Missouri. The pilot and crewmember were fatally injured. The helicopter was operated as a Title 14 Code of Federal Regulations Part 133 external load flight.
According to the available Automatic Dependent Surveillance – Broadcast (ADS-B) data for the helicopter, the pilot departed from the north bank of the river about 1025. He appeared to make three trips to the powerline support tower on the south bank of the river and then return to the original position on the north bank. The final ADS-B data point was recorded at 1035. No further ADS-B data was recorded.
A witness located on the tow vessel reported that the helicopter pilot and lineman appeared to be attempting to attach a safety marker (orange ball) to one of the power lines. The lineman appeared to be standing on the left skid, wearing a safety harness. On the second attempt, as the pilot brought the helicopter closer to the power lines at which time the tail of the helicopter struck the line.
From the witness’ vantage point, it appeared that the tailboom partially separated from the airframe with a portion of it “dangling.” The helicopter then pivoted, and the cockpit hit the line which caused sparks similar to when an electrical transformer fails. The helicopter then fell onto the barge deck and a postimpact fire ensued. The witness did not recall seeing the helicopter on fire during flight, only the sparks when the fuselage struck the line. The crew moved the tow vessel alongside the barge and used its pilothouse fire station to extinguish the fire. A subsequent inspection of the barge did not reveal any structural damage or any release of the barge contents.
The helicopter main wreckage consisted of the fuselage, engine, main rotor transmission, main rotor hub, and forward portion of the tail boom (fragmented into two sections). One main rotor blade was located about 150 ft from the main wreckage. A 7-foot segment of a second main rotor blade was located about 176 ft from the main wreckage. Finally, a main rotor blade tip, about 6-inches in length, was located about 26 ft from the main wreckage. The remaining main rotor blades and the aft portion of the tail boom, including the tail rotor and horizontal stabilizer, were not present with the wreckage and presumed to have landed in the river.
The video data recorder onboard the tow vessel was retained for examination and download. A search of the river bottom in the vicinity of the accident site using side-scan sonar equipment is planned. The helicopter wreckage was retained for possible further examination.
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