Safety record in brief:1 NTSB accident (substantial damage, Oct 2022)3 ADs may apply
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Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
The pilot’s execution of a landing approach with a right, quartering tailwind, low forward airspeed, and high power demand that, when combined, resulted in a loss of tail rotor effectiveness and helicopter control.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA23LA011)
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 |
|---|---|---|---|
| 2023-24-09 | Engine Indicating System | Jan 17, 2024 | Engine (ARRIUS 2R) |
| 2021-11-19 | Fuselage Main, Structure | Jul 16, 2021 | Airframe (505)Serial numbers per Attachment A of Bell Alert Service Bulletin 505-19-12, Revision A, dated July 11, 2019. Only with: Truss assembly P/N SLS-030-056-015 with a serial number listed in Attachment A of Bell ASB 505-19-12 Rev A installed. |
| 2020-19-05 | Bell Helicopter Textron Canada Limited Helicopters | Oct 8, 2020 | Airframe (505)Serial numbers per Table 1 of Bell Alert Service Bulletin 505-19-13, dated July 2, 2019 (swashplate assembly S/Ns). Only with: Swashplate assembly P/N 206-010-450-123 with an S/N listed in Table 1 of Bell ASB 505-19-13 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.