Aerospatiale AS 355F2 accident near Beekmantown, New York, October 30, 2018
On October 30, 2018 at about 8:11 pm local time, a 1981 Aerospatiale AS 355F2 (helicopter), registered N372CA, was destroyed in an accident during maneuvering (hover) near Beekmantown, New York. It was an external-load flight under external-load helicopter rules (Part 133). 2 people were killed and 2 people were seriously injured. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot's failure to keep the helicopter clear of a utility pole while hovering with a tailwind, which resulted in a dynamic rollover into active power lines.
Source: NTSB aviation accident database, copy made October 4, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- October 30, 2018 · about 8:11 pm local time
- Place
- Beekmantown, New York · map
- Type
- Accident
- Injuries
- 2 people were killed and 2 people were seriously injured.
- Weather
- visual conditions (good weather)
- Aircraft
- Aerospatiale AS 355F2 F1, built 1981 · all AS 355F2s on the register
- Registration
- N372CA · registry record · serial 5028
- Damage
- Destroyed
- Flight
- External-load flight · external-load helicopter rules (Part 133)
The NTSB's narrative final · quoted from the NTSB record
The pilot, pilot-rated passenger, and two linemen were conducting a flight to temporarily install a block (a large pulley used for fiber-optic wire) on a utility pole that was part of a set of high-tension power lines. The pilot was seated in the front right seat, and one of the linemen was seated outside of the helicopter on a bench that was externally attached to the right side of the landing gear. The pilot-rated passenger, who was observing the flight for training purposes, was seated in the front left seat, and the other lineman was seated in the aft left seat. The power lines were aligned northwest/southeast, which required the pilot to approach the utility pole on a southeasterly heading so that the pole would be to the right of the pilot and lineman. For the lineman to install the block on the utility pole, the pilot had to hover the helicopter next to the pole. The wind conditions about the time of the accident were such that the helicopter would have encountered a tailwind. The pilot-rated passenger, the lineman seated in the aft left seat, and witnesses on the ground all stated that, while the helicopter was hovering next to the utility pole, the helicopter's right skid struck the pole a few times. The helicopter rolled over, became entangled in energized power lines, and caught fire. All four of the occupants survived the impact with the power lines and jumped to the ground to escape the burning wreckage. The pilot and the lineman seated on the bench did not survive the fall. A postimpact fire consumed most of the helicopter while it was entangled in the power lines, and sections of the helicopter dropped from the power lines as it burned. Examination of the wreckage and both engines revealed no preimpact mechanical deficiencies that would have precluded normal operation. The surviving lineman stated that he had flown with the pilot earlier that day and that the pilot had difficulty keeping the helicopter steady due to the strong wind, so the lineman temporarily installed a block before the helicopter returned to the base. Before the accident flight, the pilots, linemen, their foreman, the owner and a representative of the helicopter company and representatives of the linemen's employer held a safety meeting and agreed that, although the wind was too strong to fully install a block, the wind was "okay" to temporarily install another block. Given that the pilot had difficulty holding the helicopter steady while hovering with a tailwind on the previous flight the pilot most likely also had difficulty hovering the helicopter with the tailwind that was present about the time of the accident. The helicopter's subsequent impact with the utility pole resulted in a dynamic rollover into the power lines.
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
What happened, in order
- Collision with terrain or object (not controlled flight into terrain) during maneuvering (hover)
- Dynamic rollover during maneuvering (hover) defining event
- Loss of control in flight during maneuvering (hover)
- Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
The NTSB's findings
- cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- cause Environmental issues › Conditions/weather/phenomena › Wind › Tailwind › Response/compensation
- cause Environmental issues › Conditions/weather/phenomena › Wind › Tailwind › Effect on operation
- cause Environmental issues › Physical environment › Object/animal/substance › Pole › Response/compensation
Pilot
- Certificate: airline transport pilot, flight instructor
- Ratings: single-engine land; instructor: airplane single-engine; instructor: helicopter; instructor: instrument helicopter; instrument: airplane; instrument: helicopter; rotorcraft: helicopter
- Flight time: 16,500 hours in all
- Last flight review: October 16, 2018
- Medical certificate: Class 1 (with waivers/limitations)
- Seat: rgt
- Injury: fatal
Pilot-Rated Passenger
- Certificate: commercial pilot
- Ratings: instructor: helicopter; instructor: instrument helicopter; instrument: helicopter; rotorcraft: helicopter
- Flight time: 2,000 hours in all; 300 in this make and model; 34 in the last 90 days; 5 in the last 30 days; 1,940 as pilot in command; 1,000 on instruments
- Last flight review: January 6, 2018
- Medical certificate: Class 2 (without waivers/limitations)
- Seat: left
- Injury: serious injuries
The aircraft
- Airframe total time: 9,905.1 hours
- Last inspection: 100-hour inspection, October 28, 2018; 1 hours since
- Maximum gross weight: 5,600 lb
- Seats: 6
- Landing gear: fixed
- Engine 1: Allison 250-C20F (turboshaft); 11,611 hours total
- Engine 2: Allison 250-C20F (turboshaft); 8,115 hours total
- Fire in flight and on the ground
- Operator: Catalyst Aviation LLC
The flight
- Departed from: None Plattsburgh NY at 8:02 pm
- Destination: Beekmantown NY
- Flight plan: none
- A second pilot was aboard
Weather at the time
- Light: daylight
- Wind: from 290° at 7 knots
- Visibility: 10 statute miles
- Sky: overcast at 3,100 ft
- Temperature: 39°F (4°C), dew point 28°F (-2°C)
- Altimeter: 30.02 inHg
- Observation at 7:53 pm from PBG, 6 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | |||
| Passengers | 1 | 2 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.
About this page
Everything above comes from the NTSB's public accident database: the narrative, probable cause and findings are the NTSB's own words, and the coded tables behind its report (pilot, aircraft, flight, weather, injuries, sequence of events) are written out in plain English. Pilots' ages, home towns and medical details are left out on purpose. The documents and photographs are the NTSB's docket, the folder of records gathered during the investigation, shown as the NTSB released them (the NTSB redacts some personal details first) and listed under the NTSB's own titles. This site's own text never names pilots, passengers or anyone else involved. A preliminary report describes what is known soon after the event and can change; the final report, with the probable cause, usually follows one to two years later and this page is refreshed when it does. Case number ERA19FA035.
