Safety record in brief:1 NTSB accident (substantial damage, Jun 2024)3 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 pilot's failure to maintain directional control during landing which resulted in a ground loop.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC24LA050)
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 |
|---|---|---|---|
| 2006-10-21 | Engine Components Incorporated (ECi) Reciprocating Engine Connecting Rods | Jun 22, 2006 | Engine (O-360-C4P)Only with: ECi connecting rods P/N AEL11750 (forging P/N AEL11488) installed, rod serial numbers 54/6 and below, produced between January 2002 and January 2004. |
| 2006-06-16 | Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, and… | Apr 27, 2006 | Engine (O-360-C4P)Only with: Engines manufactured new or rebuilt, overhauled, or that had a crankshaft installed after March 1, 1999. |
| 2005-19-11 | Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, LO-360… | Oct 21, 2005 | Engine (O-360-C4P)Only with: Engines rated at 300 HP or lower, manufactured new, rebuilt, or overhauled after March 1, 1999, or that had a crankshaft installed after March 1, 1999. |
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 MAINTENANCE IT WAS NECCESARY TO REMOVE THE EXHAUST SYSTEM. WHEN EXHAUST RISER WAS REMOVED FROM MUFFLER IT WAS NOTED THAT HOLES FOR ALINGMENT PIN/CLAMP WERE NOT IN ALINGMENT WITH EACH OTHER. THIS CONDITION RESULTED IN THE EXHAUST SYSTEM BEING INSTALLED UNDER TENSION AND IF NOT CORRECTED THIS…
From FAA Service Difficulty Reports; matched by N-number and serial number.