Safety record in brief:1 NTSB accident (substantial damage, May 2017)4 ADs may apply
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The pilot’s loss of helicopter control on approach to land due to a vortex ring state (settling with power) condition, which resulted in a hard landing.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN17LA192)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2024-20-07 | Various Helicopters | Dec 5, 2024 | Airframe (R66)Only with: Only helicopters modified by the applicable STC (SR00831LA, SR00780LA, SR01687LA, SR00856LA, SR01855LA, SR02244LA, SR01779LA, SR01459LA, SR01535LA, SR00932LA, SR02049LA, SR02484LA, or SR01902LA). |
| 2021-04-12 | Robinson Helicopter Company Helicopters | Apr 12, 2021 | Airframe (R66)Only with: Tail rotor drive shaft assembly P/N D224-3 without B900-11 modification installed. |
| 2019-07-02 | Robinson Helicopter Company Helicopters | May 17, 2019 | Airframe (R66)Certain serial numbers: R66 0003–0789; R66 0791; R66 0794; R66 0796 |
| 2016-26-04 | Robinson Helicopter Company Helicopters | Feb 8, 2017 | Airframe (R66)Only with: R44/R44 II with main rotor blade P/N C016-7 Revision AA through AE installed; R66 with main rotor blade P/N F016-2 Revision A through E installed. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
No Service Difficulty Reports found for this airframe since 1995.