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Accidents · NTSB ERA23LA011 · Final report

Bell Textron Canada LTD 505 accident near Fort Myers, Florida, October 8, 2022

On October 8, 2022 at about 10:02 pm local time, a 2021 Bell Textron Canada LTD 505 (helicopter), registered N5DF, was substantially damaged in an accident during approach (IFR final approach) near Fort Myers, Florida. It was a personal flight under general aviation rules (Part 91). 4 people were seriously injured. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilot’s execution of a landing approach with a right, quartering tailwind, low forward airspeed, and high power demand that, when combined, resulted in a loss of tail rotor effectiveness and helicopter control.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
October 8, 2022 · about 10:02 pm local time
Place
Fort Myers, Florida · map
Type
Accident
Injuries
4 people were seriously injured.
Weather
visual conditions (good weather)
Aircraft
Bell Textron Canada LTD 505, built 2021
Registration
N5DF · registry record · serial 65340
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

The pilot, who owned the helicopter, was proceeding to a landing zone to drop off passengers. As he initiated his approach, the prevailing wind was a right, quartering tailwind. His approach was near vertical, with no forward airspeed. The helicopter began to rotate to the right, then the rotation accelerated, and the pilot was unable to maintain helicopter control. The helicopter impacted the ground and came to rest on its left side, and the pilot and all three passengers were seriously injured. The main rotor struck a reinforced concrete light pole during the impact sequence, and the main rotor hub and blades separated from the main rotor mast. This resulted in an engine overspeed and blade shedding of the free turbine blades, by design, to prevent rupture of the free turbine disk. Postaccident examination of the airframe, engine, digital engine control unit, and data from integrated avionics revealed no evidence of a preexisting mechanical malfunction or failure that would have precluded normal operation. Recorded data revealed that during the approach, engine power demand exceeded engine power available, resulting in a loss of tail rotor effectiveness (LTE), after which the pilot was unable to recover control of the helicopter.

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

  1. Loss of control in flight during approach (IFR final approach) defining event
  2. Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent

The NTSB's findings

  • Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Directional control › Not attained/maintained
  • Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot
  • Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
  • Environmental issues › Conditions/weather/phenomena › Wind › Tailwind › Effect on operation

Pilot

  • Certificate: private
  • Ratings: rotorcraft: helicopter
  • Flight time: 917 hours in all; 455 in this make and model; 63 in the last 90 days
  • Last flight review: May 17, 2022
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: rgt
  • Injury: serious injuries

Passenger

  • Seat: left

Passenger

  • Seat: left
  • Injury: serious injuries

Passenger

  • Seat: rgt
  • Injury: serious injuries

The aircraft

  • Airframe total time: 221 hours
  • Last inspection: continuous airworthiness programme, July 27, 2022; 39 hours since
  • Maximum gross weight: 3,680 lb
  • Seats: 5
  • Landing gear: fixed
  • Engine: Safran Helicopter Engines Arrius 2R (turboshaft); 221 hours total
  • Fire on the ground

The flight

  • Departed from: NA Bokeelia FL at 9:43 pm
  • Flight plan: none

Weather at the time

  • Light: daylight
  • Wind: from 060° at 11 knots
  • Visibility: 10 statute miles
  • Sky: broken clouds at 4,000 ft
  • Temperature: 84°F (29°C), dew point 70°F (21°C)
  • Altimeter: 30.01 inHg
  • Observation at 5:53 pm from KFMY, 6 miles away

Weather report (METAR): METAR KFMY 082153Z 06011KT 10SM BKN040 29/21 A3001 RMK ZMAFD

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers3

Documents from the investigation the NTSB's docket: the evidence folder behind the report

21 documents, released by the NTSB on April 25, 2024. 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.

#DocumentWhat it is
1 NTSB Memorandum of Record - Pilot's Written Statement PDF, 3 pages View Download
2 NTSB Memorandum of Record - Left Rear Seat Passenger Interview PDF, 1 page View Download
3 Memorandum for Record - Left Rear Seat Passenger Written Statement PDF, 3 pages View Download
4 NTSB Memorandum of Record - Right Rear Seat Passenger Interview PDF, 2 pages View Download
5 NTSB Memorandum of Record - Right Rear Seat Passenger Written Statement PDF, 2 pages View Download
6 Lee County Florida Sheriffs Office Written Witness Statements PDF, 13 pages View Download
7 Excerpts - Pilot Logbook PDF, 12 pages View Download
8 Bell Helicopter Training Certificates PDF, 2 pages View Download
9 Excerpts - Maintenance Logbooks PDF, 5 pages View Download
10 NTSB Mor - Weather Observations PDF, 1 page View Download
11 Investigation Photographs PDF, 8 pages View Download
12 NTSB Wreckage Examination Summary PDF, 8 pages View Download
13 NTSB Powerplant Examination Summary PDF, 6 pages View Download
14 Cockpit Display - Specialist's Factual Report PDF, 16 pages View Download
15 Attachment 1 to Cockpit Display - Specialist's Factual Report data file Download
16 Release of Aircraft Wreckage, NTSB Form 6120.15 PDF, 1 page View Download
17 Evidence Control Form PDF, 3 pages View Download
18 Surveillance Camera Video video View Download
19 ERA23LA011 Survival Factors Group Factual Report PDF, 25 pages View Download
20 ERA23LA011 Survival Factors Attachment 1 Detailed Injury List PDF, 3 pages View Download
21 Onboard Image Recorder - Group Chairman's Factual Report PDF, 14 pages 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.