Safety record in brief:1 NTSB accident (substantial damage, Oct 1995)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 improper installation of an intake manifold tube assembly during engine overhaul which permitted leakage into the induction system resulting in detonation and piston failure in the associated cylinder.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX96LA023)
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 |
|---|---|---|---|
| 2006-06-16 | Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, and… | Apr 27, 2006 | Engine (AEIO-360 SER)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 (AEIO-360 SER)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. |
| 2004-25-22 | Great Lakes Aircraft Company, LLC, Models 2T-1A-1 and 2T-1A-2 Airplanes | Jan 28, 2005 | Airframe (2T-1A-2)Only with: Airplanes with a Lycoming IO-360-B1F6, AIO-360-B1G6, or AEIO-360-B1G6 engine 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.
WHEN REMOVING STABILIZER BRACE WIRES AND FINE BRACE WIRES, THE HORIZONTAL STABILIZER SPARS WERE FOUND CRACKED AT THE INTERCONNECT FITTINGS. THERE IS NO REQUIREMENT TO DISSASEMBLE THE STABILIZER TO INSPECT THE SPARS AND THE PRE-FLIGHT WILL NOT DETECT ANY MOVEMENT BECAUSE OF THE TENSION OF THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.