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ERA21FA317 · Rotorway Exec 162F

7 Aug 2021 · Argyle, NY, United States

Rotorway Exec 162F · Accident: abrupt maneuver while maneuvering

From Argyle, NY to an unrecorded destination

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Event

NTSB case
ERA21FA317
Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Accident
InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
Completed
API-reported fatalities
2 · all aircraft and ground
Ground fatalities
Unknown
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
General aviation
WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
Visual Meteorological Cond

Rotorway Exec 162F

Aircraft type
Rotorway EXEC 162
Category
Helicopter
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N162KJ
Operator
Unknown
Onboard fatalities
Unknown
Route
From Argyle, NYTo not recorded
Aircraft age
About 18 years (built 2003)
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 91: General Aviation
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
Maneuvering
Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
Abrupt maneuver
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Destroyed

Cause areas

  • Aircraft › Aircraft propeller/rotor
  • Personnel issues › Task performance

Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.

NTSB narrative

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.

Probable cause

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.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record ERA21FA317
Event ID
20210808103652
Case number
ERA21FA317
Dataset
full-current
Source SHA-256
5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
Source notes (4)
  • Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
  • Filled from the NTSB case API where the bulk record had no value: investigation status, coordinates, cause areas. Values present in the bulk record are kept.
  • The date is the local date, which is the same as the UTC date the NTSB stores.
  • API snapshot SHA-256: c055a748947309acd43f4f57ccf3b9ec5a1840b484b3686f7b33d7d89d29f1ce; retrieved 2026-09-15T07:32:56.373Z.