This N-number isn't registered right now. Below is its last known registration, canceled Sep 6, 2019.
Safety record in brief:1 NTSB accident (substantial damage, May 2017)9 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.
An engine crankcase overpressurization and the subsequent loss of engine oil for reasons that could not be determined, which resulted in the failure of the No. 6 cylinder connecting rod due to a lack of lubrication.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA17LA185)
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 |
|---|---|---|---|
| 2013-11-11 | Engine Oil Pressure | Aug 1, 2013 | Airframe (182S)Certain serial numbers: 172R 17280001–17281618; 172S 172S8001–172S11256; 182S 18280001–18280944; 182T 18280945–18282357; T182T T18208001–T18209089; 206H 20608001–20608349; … |
| 2008-10-02 | Cessna Aircraft Company 172, 175, 180, 182, 185, 206, 207, 208, 210, and 303 Series… | May 12, 2008 | Airframe (182S)Certain serial numbers: 172S 172S10672–172S10674; 172S 172S10676; 172S 172S10678–172S10680; 172S 172S10682; 172S 172S10683; 172S 172S10685; …. Only with: Applies only to airplanes that have a P/N 2013142-18 alternate static air source selector valve installed after November 19, 2007. |
| 2007-05-10 | Cessna Aircraft Company Models 172R, 172S, 182S, 182T, T182T, 206H, and T206H Airplanes | Apr 11, 2007 | Airframe (182S)Certain serial numbers: 172R 17280001–17281262; 172S 172S8001–172S9994; 182S 18280001–18280944; 182T 18280945–18281701; T182T T18208001–T18208453; 206H 20608001–20608250; … |
| 2005-19-11 | Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, LO-360… | Oct 21, 2005 | Engine (IO-540 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. |
| 2004-15-18 | Cessna Aircraft Company Models 172R, 172S, 182S, 182T, T182T, 206H, and T206H Airplanes | Sep 12, 2004 | Airframe (182S)Certain serial numbers: 172R 17280001–17281073; 172R 17281075–17281127; 172R 17281130; 172S 172S8001–172S9195; 172S 172S9197; 172S 172S9198; …. Only with: Equipped with a KAP 140 autopilot computer system P/N 065-00176-2501, -2602, -5001, -5101, -5201, -5402, or -7702 (all serial numbers). |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2004-05-24 | Lycoming Engines (Formerly Textron Lycoming) AEIO-540, IO-540, LTIO-540, O-540, and… | Mar 30, 2004 | Engine (IO-540 SER)Only with: Engines with crankshaft gear retaining bolts P/N STD-2209 installed; excludes O-540-F series engines subject to AD 99-03-05 with bolt not since replaced, engines with bolt installed at original assembly or replaced by Lycoming per SB 554 after November 10, 1998, engines with bolt from replacement kits 05K19987, 05K23325, 05K23326, 05K23327, 05K23335 or 05K23336, and engines with single-drive dual magnetos. |
| 2000-02-14 | Cessna Aircraft Company Model 182S Airplanes | Mar 17, 2000 | Airframe (182S)Certain serial numbers: 182S 18280001–18280286 |
| 98-01-14 | Cessna Aircraft Company Model 182S Airplanes | Feb 23, 1998 | Airframe (182S) |
| 98-01-01 | Cessna Aircraft Company Models 172R and 182S Airplanes | Feb 2, 1998 | Airframe (182S)Certain serial numbers: 172R 17280003–17280171; 172R 17280173–17280175; 172R 17280177–17280179; 172R 17280182–17280184; 172R 17280186; 172R 17280189; … |
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.
AFTER REMOVAL OF THE CYLINDER, FOUND THAT THE CRANKSHAFT MAIN BEARINGS FROM THE NR 6 CYLINDER WERE CRUSHED AND PARTS OF THEM MISSING, LATER FOUND THE REMAINING PIECES OF BEARING MATERIAL AND PIECES OF THE CONNECTING ROD END CAP, NUTS AND BOLTS IN THE OIL SUMP. THE CRANK LOB WAS FOUND DISCOLORED…
From FAA Service Difficulty Reports; matched by N-number and serial number.