Safety record in brief:1 NTSB accident (substantial damage, Mar 1989)4 ADs may apply
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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 COMPENSATE FOR THE LOSS OF LIFT DUE TO ICE ACCUMULATION ON THE WINGS, HIS FAILURE TO CONTROL THE RATE OF DESCENT, AND POOR INFLIGHT DECISION MAKING. CONTRIBUTING TO THE ACCIDENT WAS THE PILOT'S FATIGUE.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for SEA89LA054)
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 |
|---|---|---|---|
| 2020-21-22 | Fuselage; 55, Stabilizers | Dec 7, 2020 | Airframe (A185F) |
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (A185F) |
| 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. |
| 98-23-02 | Cessna Aircraft Company 180 and 185 Series Airplanes | Dec 22, 1998 | Airframe (A185F)Only with: Airglas Engineering Company (AECI) Model LW3600-180 or LW3600-180A fixed penetration wheel skis installed per STC SA213AL. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
No Service Difficulty Reports found for this airframe since 1995.