Bell Helicopter Textron Canada 429 accident near Elba, New York, April 26, 2022
On April 26, 2022 at about 5:00 pm local time, a 2017 Bell Helicopter Textron Canada 429, registered N507TJ, was substantially damaged in an accident during maneuvering near Elba, New York (Genesee County Airport). It was an instructional flight under general aviation rules (Part 91). 2 people were killed. The weather was visual conditions (good weather).
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The NTSB's probable cause their words, unchanged
The pilots’ inappropriate flight control inputs while in vortex ring state, which resulted in main rotor blade contact with the tail boom and a subsequent in-flight breakup. Also causal was the flight instructor’s inadequate monitoring of the flight.
Source: NTSB aviation accident database, copy made October 4, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- April 26, 2022 · about 5:00 pm local time
- Place
- Elba, New York · Genesee County Airport · map
- Type
- Accident
- Injuries
- 2 people were killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Bell Helicopter Textron Canada 429 NO SERIES, built 2017 · all 429s on the register
- Registration
- N507TJ · no longer on the register · serial 57332
- Damage
- Substantial damage
- Flight
- Instructional flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The flight instructor was providing recurrent training to the operator’s pilots. During the first training flight of the day, a pilot who received instruction from the flight instructor described that the instructor told him to perform a vortex ring state (VRS) recovery maneuver, which the pilot accomplished, but shortly afterwards, the instructor requested that the pilot perform the maneuver again. During the second entry into VRS, the helicopter developed a very high descent rate, and the pilot was surprised when the flight instructor pilot did not intervene as the helicopter got deeper into the state. The pilot, feeling uncomfortable at that point, exited the very high descent rate on his own rather than waiting for further guidance from the instructor. The remainder of the first flight was uneventful. The second training flight of the day was the accident flight. A review of the recovered parametric data for this flight showed that the helicopter had been performing training maneuvers, and that shortly before the accident the helicopter was operating within the VRS envelope with a vertical descent rate between -800 to -1,300 feet per minute (fpm). This was consistent with the instructor directing the accident pilot to enter VRS for training purposes. Shortly thereafter, multiple abrupt control inputs were recorded, which including a forward cyclic input, followed by a nearly full-aft cyclic input within 1 second, as well as a concurrent full-down collective input with an increasing left pedal input. Based on contact signatures found on the helicopter’s main rotor blades and tailboom after the accident, it is likely that these abrupt control inputs resulted in the main rotor blades contacting the tail boom and the subsequent in-flight breakup of the helicopter. The parametric data and physical evidence observed during a postaccident examination of the wreckage revealed no evidence of any mechanical malfunctions or failures of the helicopter that would have precluded recovery from VRS. Based on this information, the reasons why the pilot(s) might have applied these abrupt control inputs could not be determined. Given the contextual commentary from the pilot of the previous training flight, it is likely the flight instructor did not provide adequate information to the accident pilot on how he would receive training for VRS, to include how they would identify, enter, and exit VRS.
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
- Inflight upset during maneuvering
- Abrupt maneuver during maneuvering defining event
- Part(s) separation from AC during maneuvering
- Settling with power/vortex ring state during maneuvering
The NTSB's findings
- Personnel issues › Psychological › Attention/monitoring › Task monitoring/vigilance › Instructor/check pilot
- Personnel issues › Action/decision › Action › Delayed action › Instructor/check pilot
- Aircraft › Aircraft propeller/rotor › Main rotor system › Main rotor blade system › Capability exceeded
- Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
Flight instructor
- Certificate: airline transport pilot, flight instructor, commercial pilot
- Ratings: multi-engine land; single-engine land; instructor: helicopter; instructor: instrument helicopter; instrument: airplane; instrument: helicopter; rotorcraft: helicopter; rotorcraft: unmanned (suas)
- Flight time: 2,850 hours in all; 500 in this make and model
- Medical certificate: Class 1 (with waivers/limitations)
- Seat: left
- Injury: fatal
Pilot
- Certificate: airline transport pilot, flight instructor, commercial pilot
- Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: helicopter; instructor: instrument airplane; instructor: instrument helicopter; instrument: helicopter; rotorcraft: helicopter
- Flight time: 6,030 hours in all; 580 in this make and model
- Medical certificate: Class 2 (with waivers/limitations)
- Seat: rgt
- Injury: fatal
The aircraft
- Airframe total time: 1,039 hours
- Last inspection: continuous airworthiness programme, April 24, 2022
- Maximum gross weight: 7,000 lb
- Landing gear: fixed
- Engine 1: Pratt & Whitney PW207 (turboshaft); 1,039 hours total
- Engine 2: Pratt & Whitney PW207 (turboshaft); 0 hours total
- Fire on the ground
- Operator: Mercy Flight INC
The flight
- Departed from: CVQ Batavia NY at 3:10 pm
- Flight plan: none
- A second pilot was aboard
Weather at the time
- Light: daylight
- Wind: from 290° at 10 knots
- Visibility: 10 statute miles
- Sky: broken clouds at 3,400 ft
- Temperature: 54°F (12°C), dew point 39°F (4°C)
- Altimeter: 30.07 inHg
- Observation at 12:54 pm from ROC, 21 miles away
Weather report (METAR): KROC 261654Z 29010KT 10SM BKN034 BKN050 OVC150 12/04 A3007 RMK AO2 SLP188 T01170044
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flig | 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 ERA22FA207.
