Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Jun 2016)4 ADs may apply1 service difficulty report
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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 maintain a proper airspeed during the landing approach, which resulted in an improper flare and hard landing.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN16LA231)
ON GROUND ENCOUNTER WITH A WIND GUST AND FAILURE OF THE PILOT TO MAINTAIN DIRECTIONAL CONTROL OF THE AIRPLANE DURING THE LANDING ROLL, RESULTING IN THE COLLISION WITH A RAVINE
From NTSB records; matched by serial number.Read NTSB report (search CAROL for MIA91LA097)
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.
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.
CARB HEAT SHAFT WAS FOUND TO BE SHEARED AT RIVET HOLE DURING ACCIDENT INVESTIGATION. SHEARING OF THE SHAFT DID NOT APPEAR TO BE RELATED TO THE ACCIDENT.
From FAA Service Difficulty Reports; matched by N-number and serial number.