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MIA05CA051

2005-01-18 · Gulf Port, Mississippi, United States · None · 1 aircraft · Status: Completed

Airport KGPT

Current FAA registration · N26498

Make / Model
ROBINSON HELICOPTER R22 BETA
Year of manufacture
1988 · 17 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19880628
ADS-B equipped
Yes — Mode-S A2918D

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The student pilot's inadequate flare and his failure to maintain rotor rpm which resulted in a hard landing. Also causal was the instructor's inadequate supervision of the flight.

Factual narrative

On January 18, 2005, at approximately 1220 central standard time, a Robinson R22, N26498, registered to and operated by Vortex Helicopters Inc., experienced a hard landing. Visual meteorological conditions prevailed at the time and no flight plan was filed for the Title 14 CFR Part 91 instructional flight. The flight instructor and student pilot reported no injuries, and the helicopter incurred substantial damage. The flight originated from Vortex Heliport, Long Beach, Mississippi, earlier that day, about 1200. The instructor stated, the student entered a well maintained 70-knot glide prior to performing the autorotation recovery. The student flared too high, 10 to 12 feet agl and kept the throttle closed, preventing the governor from restoring the rpm needed to recover from the maneuver. The lack of sufficient lift and low altitude did not allow him to slow the decent. The skids and the tailboom of the helicopter incurred substantial damage from the hard landing. The student pilot stated, everything at the time of the flare was normal; however, the instructor took control of the aircraft and felt him trying to roll the throttle on, but for some reason, the student was unable to release the throttle. The helicopter landed hard from about 5 to 6 feet above the ground. The instructor stated, the student entered a well maintained 70-knot glide prior to performing the autorotation recovery. The student flared too high, 10 to 12 feet agl and kept the throttle closed, preventing the governor from restoring the rpm needed to recover from the maneuver. The lack of sufficient lift and low altitude did not allow him to slow the descent. The skids and the tailboom of the helicopter incurred substantial damage from the hard landing. The student pilot stated, everything at the time of the flare was normal; however, the instructor took control of the aircraft and felt him trying to roll the throttle on, but for some reason, the student was unable to release the throttle. The helicopter landed hard from about 5 to 6 feet above the ground. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2005_MIA05CA051.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.