N7521Z is a 2005 Robinson Helicopter R22 BETA. It is a rotorcraft with 2 seats, powered by a Lycoming O-360 series rated at 180 horsepower. The registration is active, with the registrant based in Seguin, TX. Its standard airworthiness certificate was issued in Apr 2005. It has been registered to its current owner since Apr 2021. This page also carries 1 NTSB event.
- 21 years old
2021
2005
That's everything on file so far — TailWiki checks the FAA registry daily and adds new entries as N7521Z's record changes.
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 about 18 inches of manifold pressure to lift off and he started a pedal turn toward the adjacent taxiway. He recalled the helicopter made a “violent lurch” to the right and he lowered the collective abruptly but that did not seem to make any difference. The pilot did not remember anything further.
Airport surveillance video footage showed 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 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 of the helicopter confirmed flight control continuity from the cyclic and collective cockpit controls to the main rotor. Tail rotor control continuity was confirmed from the cockpit anti-torque pedals to the tailboom separation. Damage to the tail rotor control system aft of the tailboom separation was consistent with the impact damage. The examination did not reveal any preimpact anomalies consistent with an inability to maintain control of the helicopter.
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