- 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.
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.