Safety record in brief:1 NTSB accident (substantial damage, Nov 2014)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 partial loss of engine power during climb after takeoff for a reasons that could not be determined because postaccident engine examination revealed no evidence of mechanical malfunctions or failures.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA15LA063)
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 |
|---|---|---|---|
| 2025-23-08 | Hoses and Tubes | Dec 2, 2025 | Airframe (182Q)Only with: Equipped with an affected part as defined in paragraph (g)(1) of this AD installed in accordance with STC SA03302AT. |
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (182Q) |
| 2009-04-05 | Cessna Aircraft Company Models 182Q and 182R Airplanes | Mar 27, 2009 | Airframe (182Q)Only with: Equipped with SMA diesel engine Model SR305-230-1 (or SR305-230 converted to SR305-230-1 per SMA SB-01-76-002) installed under STC SA03302AT. |
| 2007-09-01 | Cessna Aircraft Company Models 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, and 182R… | Apr 25, 2007 | Airframe (182Q)Only with: Air Plains Services Corporation STC SA00152WI installed and a ground power receptacle mounted on the firewall (forward ground power receptacle). |
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.