NTSB CAROL · Event
Event GAA18CA030
Registry · N878MC
FAA Aircraft Registry record.
Make / Model
ROBINSON HELICOPTER R22 BETA
Year of manufacture
2005 · 12 years old at event
TCDS
H10WE · ROBINSON HELICOPTER CO
Engine
LYCOMING O-360 SERIES (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20050214
ADS-B equipped
Yes — Mode-S AC1524
Registrant of record
HELICOPTER LEASING LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The student pilot’s tension on the flight control at a low level during an autorotation, which did not allow sufficient time for the flight instructor to correct and recover control before the hard landing.
Factual narrative
The purpose of the training flight was to practice auto rotations with power recovery. The flight instructor reported that as the helicopter descended through about 40 ft, he instructed the student to increase the landing flare and roll on throttle for power recovery. As the helicopter continued to quickly descend to about 8 ft, they raised the collective and the flight instructor felt resistance in the collective. The rpms began to drag down and he tried rolling on the throttle to bring the rpms back up. The flight instructor reported that he believed that the student had tensed up on the throttle and collective as he tried to keep the helicopter level and cushion for the landing. The student pilot reported that in hindsight, he was pulling up on the collective, but his hand (wrist) was locked which prevented the governor to roll on and increase power. The helicopter subsequently landed hard, substantially damaging the fuselage. The flight instructor reported that there were no preaccident mechanical malfunctions or failures with the helicopter that would have precluded normal operation. The purpose of the training flight was to practice autorotations with power recovery. The flight instructor reported that, as the helicopter descended through about 40 ft, he instructed the student pilot to increase the landing flare and roll on throttle for power recovery. As the helicopter continued to quickly descend to about 8 ft, they raised the collective, and the flight instructor felt resistance in the collective. The rpms began to drag down, and he tried rolling on the throttle to bring the rpms back up. The flight instructor reported that he believed that the student had tensed up on the throttle and collective as he tried to keep the helicopter level and cushion for the landing. The student pilot reported that, in hindsight, he was pulling up on the collective, but his hand (wrist) was locked, which prevented the governor to roll on and increase power. The helicopter subsequently landed hard, which resulted in substantial damage the fuselage. The flight instructor reported that there were no preaccident mechanical malfunctions or failures with the helicopter that would have precluded normal operation Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- C Personnel issues-Action/decision-Action-(general)-Student/instructed pilot - C
- C Personnel issues-Psychological-Attention/monitoring-Task monitoring/vigilance-Instructor/check pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2017_GAA18CA030.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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