Skip to content

GAA17CA551

2017-09-24 · Santa Barbara, California, United States · None · 1 aircraft · Status: Completed

Airport SBA

Current FAA registration · N177SR

Make / Model
ROBINSON HELICOPTER R22 BETA
Year of manufacture
2001 · 16 years old at event
Engine
LYCOMING O-360 SERIES (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20011115
ADS-B equipped
Yes — Mode-S A134CE

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The student pilot’s unstabilized hover, which resulted in ground contact and a dynamic rollover. Contributing to the accident was the flight instructor’s delayed remedial action.

Factual narrative

According to the flight instructor in the skid-equipped helicopter, he was providing hover instruction to his airplane rated student, about three feet above the ground. The instructor reported that he allowed the student to make the necessary flight control inputs, as he guarded the controls. The area was level, with 1ft tall weeds. The helicopter began to drift laterally and descend. The right skid contacted the weeds and the helicopter rolled onto its right-side. The instructor reported that, "I was not quick enough in lowering the collective to prevent full rollover." The helicopter sustained substantial damage to the tailboom and engine mounts. Per the National Transportation Safety Board's Pilot Aircraft Accident Report, the instructor reported that the accident could have been prevented by instructing hover practice at a, "higher altitude and away from obstacles that may serve as a pivot point leading to dynamic rollover." The pilot reported that there were no preaccident mechanical malfunctions or failures with the helicopter that would have precluded normal operation. According to the flight instructor in the skid-equipped helicopter, he was providing hover instruction to his airplane-rated student about 3 ft above the ground. The instructor reported that he allowed the student to make the necessary flight control inputs as he guarded the controls. The area was level with 1-ft-tall weeds. The helicopter began to drift laterally and descend. The right skid contacted the weeds, and the helicopter rolled onto its right side. The instructor reported that "I was not quick enough in lowering the collective to prevent full rollover." The helicopter sustained substantial damage to the tailboom and engine mounts. Per the National Transportation Safety Board's Pilot Aircraft Accident Report, the instructor reported that the accident could have been prevented by instructing hover practice at a "higher altitude and away from obstacles that may serve as a pivot point leading to dynamic rollover." 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

FAA avdata. C = Cause, F = Factor.

  • C Personnel issues-Task performance-Use of equip/info-Aircraft control-Student/instructed pilot - C
  • C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Altitude-Not attained/maintained - C
  • C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Lateral/bank control-Not attained/maintained - C
  • F Personnel issues-Action/decision-Action-Delayed action-Instructor/check pilot - F

Verbatim from NTSB's published report. Source file NTSB_2017_GAA17CA551.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.