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| Date: | Sunday 27 October 2024 |
| Time: | 08:30 |
| Type: |  Robinson R22 Beta |
| Owner/operator: | Veracity Aviation LLC |
| Registration: | N7521Z |
| MSN: | 3810 |
| Year of manufacture: | 2005 |
| Engine model: | Lycoming O-360-J2A |
| Fatalities: | Fatalities: 0 / Occupants: 1 |
| Other fatalities: | 0 |
| Aircraft damage: | Substantial |
| Category: | Accident |
| Location: | Pearland Regional Airport (LVJ/KLVJ), Houston, TX -
 United States of America
|
| Phase: | Take off |
| Nature: | Private |
| Departure airport: | Houston-Pearland Regional Airport, TX (KLVJ) |
| Houston-Pearland Regional Airport, TX (KLVJ) | |
| Investigating agency: | NTSB |
| Confidence Rating: |  Accident investigation report completed and information captured |
On October 27, 2024, about 0830 central daylight time, a Robinson Helicopter R-22 Beta, N7521Z, was substantially damaged when it was involved in an accident at the Pearland Regional Airport (LVJ), Pearland, Texas. The pilot sustained minor injuries. The helicopter was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.
The pilot stated that he increased engine power to lift off and initiated a pedal turn toward the adjacent taxiway. He recalled that the helicopter made a “violent lurch” to the right, so he lowered the collective abruptly but that did not seem to make any difference. He did not remember anything further.
Airport surveillance video footage captured the helicopter lift off and translate a short distance to the right. The right skid appeared to contact the ground again, and the helicopter immediately began rotating to the right. This was accompanied by dramatic pitch oscillations. The aft portion of the tailboom impacted the paved ramp surface, and the tailboom and empennage separated. Rotation of the helicopter continued until it collided with a nearby parked airplane.
The helicopter sustained damage to both main rotor blades, the tailboom, tail rotor assembly, and the empennage. An examination helicopter did not reveal any preimpact anomalies consistent with an inability to maintain control of the helicopter.
A review of the surveillance video indicated that the helicopter began a dynamic rollover when the right skid dragged on the ground immediately after lifting off. Based on the response of the helicopter, the pilot likely increased collective pitch to increase height but did not provide sufficient left anti-torque pedal input to counter the increased torque. The pilot was unable to regain control of the helicopter before it impacted the ground.
Probable Cause: The pilot’s failure to maintain control of the helicopter during lift off.
Accident investigation:
 |
|
Sources:
NTSB
https://data.ntsb.gov/Docket?ProjectID=195385
https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=7521Z
https://s3.amazonaws.com/mfbimages/logbook/images/aircraft/id/93380/2021031614584601-5760624_.jpg (photo)
Location
Revision history:
| Date/time | Contributor | Updates |
|---|---|---|
| 28-Oct-2024 19:17 | Captain Adam | Added |
| 01-Nov-2024 20:56 | RobertMB | Updated [Source, Embed code, Narrative, ] |
| 19-Nov-2024 19:58 | Captain Adam | Updated [Time, Narrative, Accident report, ] |
| 02-Apr-2025 22:08 | Captain Adam | Updated [Source, Narrative, ] |
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