Safety record in brief:1 NTSB accident (substantial damage, Apr 1992)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 PILOT'S MISMANGEMENT OF THE FUEL IN THAT HE DELAYED SELECTION OF A FUEL TANK WITH USABLE FUEL, AND THE EXCESSIVE FINAL LANDING SPEED. FACTORS WERE THE PILOT'S FAILURE TO EXTEND THE FLAPS AND THE ROUGH/UNEVEN TERRAIN BECAUSE OF THE RAILROAD SPUR.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ATL92LA088)
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 |
|---|---|---|---|
| 2014-20-12 | Fuselage | Nov 12, 2014 | Airframe (17-30A) |
| 2009-16-03 | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating… | Sep 9, 2009 | Engine (IO 520 SERIES)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P 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.
CRANKSHAFT IS BROKEN IN AREA OF NR6, NR5 ROD JOURNAL. CRANKSHAFT BROKE ON APPROACH TO LANDING AS PROP RPM CONTROL WAS ADVANCED ON SHORT FINAL. ENGINE POWER UNDER VERY LOW POWER. ENGINE HAS NOT BEEN DISASSEMBLED YET. THERE IS ALREADY AN AD NOTE TO TAKE THESE SHAFTS OUT OF SERVICE. IT WAS A NON VAR…
From FAA Service Difficulty Reports; matched by N-number and serial number.