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DEN04CA061

2004-04-14 · Nephi, Utah, United States · None · 1 aircraft · Status: Completed

Airport U14

Current FAA registration · N555UH

Make / Model
ROBINSON HELICOPTER R22
Year of manufacture
2004 · 0 years old at event
Engine
LYCOMING O-360 SERIES (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20040211
ADS-B equipped
Yes — Mode-S A713C8

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

the flight instructor's failure to maintain control of the helicopter resulting in a hard landing.

Factual narrative

On April 14, 2004, at approximately 0930 mountain daylight time, a Robinson R22, N555UH, was substantially damaged during a hard landing at Nephi, Utah. The flight instructor and pilot receiving instruction were not injured. Visual meteorological conditions prevailed. No flight plan had been filed for the flight being conducted under the provisions of Title 14 CFR Part 91. The cross-country flight had departed Provo, Utah, at 0800. According to the flight instructor, they were practicing 180 degree autorotations and had just successfully completed one. Prior to the second maneuver, the pre-landing checks were completed and the maneuver was entered at an altitude of 700 feet agl and at an airspeed of 75 knots. The flight instructor stated "at approximately 150 feet agl, [the] decent rate increase[d] dramatically." He said that he attempted to recover and flare with "aft cyclic and down collective" with no effect. He added full throttle and "raised" collective, in attempt to land in a "skid level attitude." During the impact with the ground, both skids collapsed and the main rotor blade severed the tail boom. The helicopter rotated "three or four times" before coming to rest off of the left side of the runway. An examination of the systems revealed no anomalies. The flight instructor said, while practicing 180 degree autorotations, and "at approximately 150 feet agl, [the] descent rate increase[d] dramatically.' The flight instructor stated that he attempted to recover and flare with aft cyclic and down collective. He then added full throttle and raised the collective, in an attempt to land in a "skid level attitude." The helicopter, however, struck the ground hard, collapsing both skids and allowing the main rotor blade to sever the tail boom. The helicopter rotated "three or four times" before coming to rest off of the left side of the runway. An examination of the helicopters systems revealed no anomalies. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2004_DEN04CA061.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

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