Amateur-built Exec 162F accident near Argyle, New York, August 7, 2021
On August 7, 2021 at about 10:00 pm local time, a 2003 amateur-built Exec 162F (helicopter), registered N162KJ, was destroyed in an accident during maneuvering near Argyle, New York. It was a personal flight under general aviation rules (Part 91). 2 people were killed. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot’s abrupt control inputs, which resulted in a lowG condition, main rotor mast bumping, and the subsequent severing of the tail boom by a main rotor blade.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- August 7, 2021 · about 10:00 pm local time
- Place
- Argyle, New York · map
- Type
- Accident
- Injuries
- 2 people were killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Amateur-built Exec 162F, built 2003
- Registration
- N162KJ · registry record · serial 6692
- Damage
- Destroyed
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
A witness reported observing the helicopter flying southbound at an altitude of about 50 to 75 ft above ground level. The witness stated that the helicopter was “having issues” and “could not stay up in the air.” The witness further stated that the helicopter seemed as if it were “bouncing” as it flew across a field. Just after the helicopter flew over a tree line, the witness heard a “loud sound” and “watched the [rotor] just stop.” The helicopter then “fell straight down.” Examination of the wreckage revealed that the lower inboard ends of the main rotor blade grips were bent upward and that both had semicircular indentations with the same diameter as the rotor mast. This damage was consistent with the blade grips contacting the mast, commonly referred to as mast bumping, which occurs due to excessive flapping motion of rotor blades (specifically, up-and-down motion of the blade tips). The aft tailboom was separated from the helicopter and found about halfway along the 400-ft-long wreckage path. An impact mark consistent with the shape of the main rotor blade was found at the forward end of the separated section, consistent with a main rotor blade severing the tailboom. Teetering rotor systems, such as the one on the accident helicopter, are particularly susceptible to mast bumping during low-G conditions, which can result from abrupt forward (nose-down) cyclic inputs. The witness’s description of the helicopter appearing to bounce as it was flying is consistent with repeated abrupt control inputs resulting in oscillating low-G conditions. These inputs likely led to the mast bumping and excessive blade flapping, which resulted in a main rotor blade contacting the tailboom. The reason for the pilot’s abrupt control inputs could not be determined. Toxicology testing of the pilot’s specimens detected ethanol and npropanol, diphenhydramine), trazadone, and a metabolite of clonazepam. The ethanol was detected in the pilot’s blood at low levels (below those considered to be impairing) and was not detected in his urine. That information, along with the presence of n-propanol in the pilot’s blood, suggested that the ethanol was from sources other than ingestion and that it likely was not a factor in the accident. The diphenhydramine results were also below the therapeutic level; therefore, that medication was not likely a factor. The pilot had been denied a Federal Aviation Administration medical certificate due to his medical history, which included bipolar disorder and depression. The detection of trazadone (which was well below therapeutic levels) and a metabolite of clonazepam indicated that he had been taking these medications to treat diagnosed conditions. However, the toxicological results suggested that the pilot’s use of these medications was likely not a factor in the accident. Toxicology testing also detected Delta-9-tetrahydocannabinol (THC), which showed that the pilot had used cannabis. Although the effects of THC can last a few hours, THC can be detected in the body for days or weeks. Thus, the investigation could not determine if the pilot’s use of cannabis could have been impairing and influenced his behavior during the accident flight.
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
- Abrupt maneuver during maneuvering defining event
- Mast bumping during maneuvering
- Part(s) separation from AC during maneuvering
- Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
The NTSB's findings
- Aircraft › Aircraft propeller/rotor › Main rotor system › Main rotor mast/swashplate › Related operating info
- Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
Pilot
- Certificate: private
- Ratings: single-engine land
- Flight time: 500 hours in all
- Medical certificate: None
- Seat: left
- Injury: fatal
The aircraft
- Maximum gross weight: 1,500 lb
- Seats: 2
- Landing gear: fixed
- Engine: Rotorway RI162F (piston); 0 hours total
- Fire on the ground
The flight
- Departed from: Argyle NY
- Flight plan: none
Weather at the time
- Light: daylight
- Wind: from 210° at 4 knots
- Visibility: 10 statute miles
- Sky: scat at 9,000 ft
- Temperature: 81°F (27°C), dew point 70°F (21°C)
- Altimeter: 30.01 inHg
- Observation at 5:54 pm from DDH, 22 miles away
Weather report (METAR): KDDH 072154Z AUTO 21004KT 10SM SCT090 27/21 A3001 RMK AO2 SLP158 T02670206
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | |||
| Passengers | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
8 documents, released by the NTSB on August 30, 2023. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.
| # | Document | What it is | |
|---|---|---|---|
| 1 | Witness Interviews | PDF, 5 pages | View Download |
| 2 | Excerpts from Pilot's Logbook | PDF, 6 pages | View Download |
| 3 | Investigative Photographs | PDF, 5 pages | View Download |
| 4 | Wreckage Examination | PDF, 37 pages | View Download |
| 5 | Wreckage Diagram | PDF, 1 page | View Download |
| 6 | Toxicological Report | PDF, 2 pages | View Download |
| 7 | Medical Factual Report | PDF, 6 pages | View Download |
| 8 | Release of Aircraft Wreckage, NTSB Form 6120.15 | PDF, 1 page | View Download |
The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.
Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
