This N-number isn't registered right now. Below is its last known registration, canceled Apr 3, 2020.
Safety record in brief:1 NTSB accident (substantial damage, Aug 2018)2 ADs may apply1 service difficulty report
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.
The in-flight separation of the tail rotor blade due to fatigue, which resulted in the subsequent emergency landing and dynamic rollover.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN18LA313)
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 |
|---|---|---|---|
| 2021-26-09 | Tail Rotor Head | Jan 19, 2022 | Airframe (B-2)Only with: Tail rotor (T/R) hub part number 161-1 or 2951 installed. |
| 2014-20-16 | Brantly International, Inc. Helicopters | Nov 12, 2014 | Airframe (B-2)Only with: Main rotor blade P/N 248-101, 248-202, or 248-404 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.
INVESTIGATION REVEALED THE TAIL ROTOR AND UPPER TAIL ROTOR GEARBOX ASSEMBLY TO BE MISSING FROM THE PRIMARY ACCIDENT SITE AND WAS LOCATED APPROXIMATELY ONE-HALF MILE AWAY BY THE AIRCRAFT OWNER. THE GEARBOX DRIVE SHAFT WAS SHEARED AND REMAINED WITH THE HELICOPTER DURING THE ACCIDENT SEQUENCE. THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.