This N-number isn't registered right now. Below is its last known registration, canceled Oct 31, 2023.
Safety record in brief:1 NTSB accident (substantial damage, May 2022)3 ADs may apply2 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
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.
An unintentional movement of the cyclic control before takeoff, which resulted the main rotor blades contacting the fixed wire cutter.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA22LA229)
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 |
|---|---|---|---|
| 2011-08-06 | Honeywell International Inc. LTS101 Series Turboshaft Engines and LTP101 Series… | May 17, 2011 | Engine (LTS101-750B-1)Only with: Power turbine rotor P/N 4-141-290-01, -02, -03, -05, -06, -11, -12, -13, -14, or -16 installed. |
| 2009-24-12 | Honeywell International Inc. LTS101 Series Turboshaft and LTP101 Series Turboprop Engines | Jan 4, 2010 | Engine (LTS101-750B-1)Only with: Engines with certain gas generator turbine discs, P/N 4-111-015-14, installed. |
| 2001-22-07 | Honeywell International, Inc. LTP 101 Series Turboprop and LTS101 Series Turboshaft… | Nov 30, 2001 | Engine (LTS101-750B-1)Only with: Rigid tube fuel manifolds P/N 4-301-042-02, -04, -05, -06, 4-301-236-01, -02, -03, -04, 4-301-286-01, -02, or 4-301-376-01 installed. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
DURING A SCHEDULED INSPECTION, A 0.5" LONG CRACK WAS DISCOVERED IN THE TRAILING EDGE OF THE COMPOSITE HORIZONTAL STABILIZER.THE CRACK WAS IN THE ALUMINUM TRAILING EDGE STRIP ANS ALSO IN THE COMPOSITE TRAILING EDGE.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A SCHEDULED INSP , A 1 INCH LONG CRACK WAS DISCOVERED IN THE SKIN OF THE TAILBOOM VERTICAL FIN, AT THE ACCESS COVER OPENING AT THE TOP OF THE VERTICAL FIN.
From FAA Service Difficulty Reports; matched by N-number and serial number.