Robinson Helicopter R44 accident near Galveston, Texas, December 31, 2024
On December 31, 2024 at about 6:20 pm local time, a 2002 Robinson Helicopter R44, registered N441HQ, was substantially damaged in an accident during takeoff near Galveston, Texas (Private Heliport airport). It was a positioning flight under general aviation rules (Part 91). No one was hurt; 1 person was on board or involved. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot’s failure to maintain terrain clearance during the takeoff from the helipad in high and gusting wind conditions, that resulted in the right skid extension embedding in the artificial turf, and a subsequent dynamic rollover sequence.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- December 31, 2024 · about 6:20 pm local time
- Place
- Galveston, Texas · Private Heliport · map
- Type
- Accident
- Injuries
- No one was hurt; 1 person was on board or involved.
- Weather
- visual conditions (good weather)
- Aircraft
- Robinson Helicopter R44 NO SERIES, built 2002 · all R44s on the register
- Registration
- N441HQ · registry record · serial 1155
- Damage
- Substantial damage
- Flight
- Positioning flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
Due to recent precipitation in the area, the heliport, consisting of a flat grass, artificial turf and dirt field, was soft. The private heliport, that is equipped with a windsock, is located about 800 ft away from the Gulf of Mexico. Due to the soft ground conditions, the operator’s fuel truck was parked farther away from the helipad. The pilot reported the purpose of the flight was to reposition the helicopter from the current helipad to another helipad at the heliport, to be near the fuel truck to obtain fuel. At the time of the takeoff, the pilot reported the wind condition originating from about 340°, was 16 to 18 kts, with gusts of 25 to 26 kts. As the pilot initiated the takeoff from the artificial turf helipad with the helicopter oriented to the north, the pilot reported the wind “helped push” the helicopter slightly rearward. During the rearward movement, the right skid extension became embedded in the artificial turf, the helicopter entered a dynamic rollover sequence, and the helicopter came to rest on its right side. The pilot was able to egress from the front right seat via the fractured windshield. The helicopter sustained substantial damage to the main rotor system, the fuselage, the tailcone, and the empennage. The pilot reported there were no preimpact mechanical malfunctions or failures with the airframe or the engine that would have precluded normal operation. According to the airframe manufacturer, there are no published wind limitations for starting and takeoff, however, in ground effect hover controllability has been substantiated in a 17 kt wind from any direction up to 9,600 ft density altitude. The operator did not have any published wind limitations for starting and takeoff, however the operator reported that the wind condition is typically 15 to 25 kts at the heliport. A review of the Federal Aviation Administration (FAA) Advisory Circular 150/5390-2D Heliport Design did not find any published guidance on the usage of artificial turf at heliports, nor was any published guidance found in the FAA Helicopter Flying Handbook FAA-H-8083-21B regarding artificial turf hazards with dynamic rollover.
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
- Dynamic rollover during takeoff defining event
- Other weather encounter during takeoff
- Evacuation during post (impact)
- Collision during takeoff/land during takeoff
The NTSB's findings
- Environmental issues › Conditions/weather/phenomena › Wind › High wind › Effect on equipment
- Environmental issues › Conditions/weather/phenomena › Wind › Gusts › Effect on equipment
- Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- Environmental issues › Physical environment › Runway/land/takeoff/taxi surface › Soft surface › Effect on equipment
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Altitude › Not attained/maintained
- Aircraft › Aircraft systems › Landing gear system › Aux gear (tail/rotorcrft skid) › Damaged/degraded
Pilot
- Certificate: commercial pilot, remote
- Ratings: instrument: helicopter; rotorcraft: helicopter
- Flight time: 550.4 hours in all; 103.1 in the last 90 days; 51.8 in the last 30 days; 474.8 as pilot in command
- Last flight review: August 20, 2024
- Medical certificate: Class 1 (without waivers/limitations)
- Seat: rgt
- Injury: no injuries
The aircraft
- Airframe total time: 3,878.2 hours
- Last inspection: 100-hour inspection, December 6, 2024
- Maximum gross weight: 2,400 lb
- Seats: 4
- Landing gear: fixed
- Engine: Lycoming Engines O-540-F1B5 (piston); 0 hours total
- Operator: Galveston Helicopter Adventures, LLC
The flight
- Flight plan: none
- Runway NA
Weather at the time
- Light: daylight
- Wind: from 360° at 17 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 66°F (19°C), dew point 46°F (8°C)
- Altimeter: 30.01 inHg
- Observation at 11:52 am from KGLS, 5 miles away
Weather report (METAR): KGLS 311752Z 36017KT 10SM CLR 19/08 A3001 RMK AO2 SLP163 T01940078 10200 20178 50011
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Photographs from the investigation 7 pictures from the NTSB's docket, as the NTSB released them
Photograph 1 – View of the front of the helicopter at the accident site
Photograph 2 – View of the bottom of the helicopter at the accident site
Photograph 3 – View of the rear of the helicopter at the accident site
Photograph 4 – View of the top of the helicopter at the accident site
Photograph 5 – View of the windsock at the accident site
Photograph 6 – View of the helipad material, an artificial turf
Photograph 7 – View of the right side skid and the artificial turfThe NTSB's photographs with the NTSB's captions, at screen size. Open a picture to see it full size or to report one that should not be shown.
Documents from the investigation the NTSB's docket: the evidence folder behind the report
10 documents, released by the NTSB on January 30, 2025. 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.
| # | Document | What it is | |
|---|---|---|---|
| 1 | Accident Photographs | PDF, 8 pages · our copy | View Download |
| 2 | Pilot/operator Aircraft Accident Report, NTSB Form 6120.1 | PDF, 10 pages | View Download |
| 3 | Accident Site Overview | PDF, 1 page | View Download |
| 4 | Pilot Flight Review Entry | PDF, 1 page | View Download |
| 5 | Robinson Helicopter Company and Operator - Email Memorandums | PDF, 2 pages | View Download |
| 6 | Robinson Helicopter Company - R-44 Pilot's Operating Handbook and Rotorcraft Flight Manual Excerpt | PDF, 1 page | View Download |
| 7 | Robinson Helicopter Company - R-44 Illustrated Parts Catalog Excerpt | PDF, 3 pages | View Download |
| 8 | Robinson Helicopter Company - Safety Notice SN-09 Many Accidents Involve Dynamic Rollover | PDF, 1 page | View Download |
| 9 | N441HQ - Video Footage #1 (.Mov File - Courtesy of Mcdonald's) | MOV file | Download |
| 10 | N441HQ - Video Footage #2 (.Mov File - Courtesy of Mcdonald's) | MOV file | 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.
