CEN25LA381

NTSB accident investigation · Bell Helicopter Textron Canada 505 · Fort Worth, TX · August 27, 2025

Accident · No injuriesClass 4 · LimitedFinal report
Date
August 27, 2025, 13:10 local (18:10 UTC)
Place
Fort Worth, TX · Lane 3 at Bell South Airfield Heliport
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Emergency descent
Aircraft
N505GRBell Helicopter Textron Canada 505
Defining event
Autorotation: Hard landing
Weather
Visual (VMC) · Day
Status
Completed · report October 17, 2025
Report
Approved by Office Director
Investigation class
Class 4 - Basic report with no Prelim publish
NTSB office
Central Region
Parties
FAA North Texas FSDO
FAA report
20250827013099A
Case key
201009

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

The manufacturer flight instructor’s failure to maintain proper airspeed and a proper descent rate during a demonstrated hover out of ground effect (HOGE) autorotation, which resulted in a hard landing. Contributing to the accident was the manufacturer flight instructor’s failure to perform corrective action during the HOGE autorotation with a power recovery in a timely manner.

Findings · 6

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Use of equip/info: aircraft controlPersonnel issues › Task performance · Instructor/check pilotBell Helicopter Textron Canada 505: 3 casesAll aircraft: 9,295 casesProbable cause
Performance/control parameters: descent rateAircraft › Aircraft oper/perf/capability · Not attained/maintainedBell Helicopter Textron Canada 505: 1 caseAll aircraft: 242 casesProbable cause
Action: incorrect action performancePersonnel issues › Action/decision · Instructor/check pilotBell Helicopter Textron Canada 505: 2 casesAll aircraft: 1,386 casesProbable cause
Performance/control parameters: airspeedAircraft › Aircraft oper/perf/capability · Not attained/maintainedBell Helicopter Textron Canada 505: 1 caseAll aircraft: 1,681 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The purpose of the flight with the manufacturer flight training academy was for a flight instructor to provide instruction to another flight instructor, who was a customer. About one hour into the flight at the manufacturer’s private flight training heliport, the manufacturer flight instructor was demonstrating a hover out of ground effect (HOGE) autorotation from a straight-in approach with termination on the lane. This was the first HOGE autorotation for the manufacturer flight instructor of the day. At the time of the maneuver, the manufacturer flight instructor reported the wind direction was variable, and the wind speed was light and variable with no gusting. He reported that he was late entering the HOGE autorotation due to a heliport traffic pattern restriction for noise abatement purposes. Near the end of the HOGE autorotation, with about 35 kts airspeed, he performed a small flare by pulling the nose up slightly. About 45 ft agl, he noticed the descent rate accelerated, requiring him to make a small input with the collective. He further noticed that the descent rate became excessive. About 20 ft agl he began pulling the collective to the top stop and he leveled the skids. The helicopter landed hard on the dry asphalt lane, the skids partially collapsed, and the helicopter came to rest upright on the right side of the lane with little forward motion. The helicopter sustained substantial damage to the underside of the fuselage. The manufacturer flight instructor reported there were no preimpact mechanical malfunctions or failures with the airframe or the engine that would have precluded normal operation. The manufacturer flight training academy reported that the accident was a mismanagement of the flight controls, and the manufacturer flight instructor should have identified the situation the helicopter was in sooner and executed a power recovery to arrest the descent rate. Postaccident investigation revealed that the manufacturer flight instructor, who had been employed with the manufacturer flight training academy for nine years, did not complete the required flight risk assessment tool before the instructional flight. The estimated density altitude for the closest meteorological reporting station was 2,484 ft.

Aircraft

Registration
N505GR
Reported as
Bell Helicopter Textron Canada 505 (NO SERIES)
Category
Helicopter
Serial number
65011
Built
2017
Airframe hours
2,120
Engine
Safran Helicopter Engines Arrius 2R, 505 horsepower, turbo shaft
Damage
Substantial damage
Flight
Instructional · Part 91
Operator
Bell Training Academy, doing business as Bell Training Academy
Registered owner
Bell Textron Inc.
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · July 18, 2025 · 20.6 hours before
Departed
0TE2 · Hurst, TX
Destination
XS04 · Fort Worth, TX
Airport
XS04 · Bell South Airfield, runway Lane 3, 1,600 × 60 ft, asphalt
Equipment
Angle of attack indicator, ADS-B, Electronic primary flight display, Electronic multifunction display

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew · 2

As NTSB recorded them. NTSB leaves out names.

Role
Flight instructor
Age
52
Injuries
None
Certificates
Commercial, Flight instructor, Airline transport
Airplane ratings
Single-engine land
Instrument ratings
Airplane, Helicopter
Medical
Class 2, With waivers/limitations
Last flight review
November 20, 2024
Seat
Left
Restraint
4-point
Flight hours
6,855 total · 718 in this make and model · 5,495 as pilot in command · 114 in the last 90 days · 16 in the last 30 days · 3 in the last 24 hours
Role
Pilot
Age
57
Injuries
None
Certificates
Commercial, Flight instructor
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Without waivers/limitations
Seat
Right
Restraint
4-point

Weather

Conditions
Visual (VMC) · Day
Wind
110° at 5 knots
Visibility
10 statute miles
Lowest ceiling
3,300 ft broken
Temperature
86 °F, dew point 68 °F
Altimeter
30.15 inHg
Observed at
KGPM, 8 nm away
METAR
KGPM 271755Z AUTO 11005KT 10SM BKN033 30/20 A3015 RMK AO2 T03030203 10303 20211

Docket · 7

The files NTSB released with the investigation on October 17, 2025, on NTSB’s docket system: statements, records, photos and specialists’ reports. 190 MB in all.

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.