This N-number isn't registered right now. Below is its last known registration, canceled Feb 17, 2017.
Safety record in brief:1 NTSB accident (destroyed damage, Sep 2016)5 ADs may apply3 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.
A dual loss of engine power for undetermined reasons after the pilot's improper decision to attempt another maneuver after recovering from a perceived compressor stall, rather than returning to the airport.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA16FA311)
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 |
|---|---|---|---|
| 2021-05-19 | Tail Rotor Control System | May 7, 2021 | Airframe (S-61N)Only with: Arm assembly part number S6140-62614-009 installed; certificated in any category including restricted. |
| 2013-05-17 | Sikorsky Aircraft Corporation Helicopters | Apr 26, 2013 | Airframe (S-61N)Only with: With a fuel system 40 micron fuel filter element P/N 52-0505-2 or 52-01064-1 installed. |
| 2004-15-22 | Sikorsky Aircraft Corporation Model S-61L, S-61N, S-61-NM, and S-61R Helicopters | Sep 7, 2004 | Airframe (S-61N) |
| 2001-18-06 | General Electric Company T58 and CT58 Series Turboshaft Engines | Oct 18, 2001 | Engine (CT58-140-1) |
| 98-26-02 | Sikorsky Aircraft Corporation Model S- 61A, D, E, L, N, NM, R, and V Helicopters | Jan 20, 1999 | Airframe (S-61N)Only with: Main rotor shaft P/N S6135-20640-001, S6135-20640-002, or S6137-23040-001 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.
INTERGRANULAR CORROSION FOUND ON AFT LOWER SKIN OF ACFT, LOCATED AT AREA OF FS 292 - 323, WL 85, BL 35R OUTER RT SIDE OF AFT FUEL BAY. CORROSION MOSTLY LEVEL 1. LEVEL 3 IN ONE AREA APPROX 3 INCH AREA. REPAIRED CORROSION & FABRICATED FILLER & DOUBLER IAW EO15038-303 REV IR, SRM SA CHAPTER 4 & AMM…
From FAA Service Difficulty Reports; matched by N-number and serial number.THE FLIGHT CREW, DURING POST FLIGHT INSPECTION, DISCOVERED THAT THE AFT LT TRANSMISSION OIL COOLER ACCESS PANEL WAS MISSING.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING POST FLIGHT INSPECTION, THE FLIGHT CREW DISCOVERED THAT THE LT SIDE TRANSMISSION MX PANEL WAS MISSING. REPLACED PANEL, REMOVED FROM THAT WAS INSPECTED & FOUND TO BE IN A SERVICEABLE CONDITION, THE PANEL WAS REPLACED IAW S-61MM CH 53-30-0. PANEL PN S6120-62610-62610-37.
From FAA Service Difficulty Reports; matched by N-number and serial number.