This N-number isn't registered right now. Below is its last known registration, canceled Feb 11, 2023.
Safety record in brief:5 NTSB accidents (substantial damage at worst, latest Aug 2020)4 ADs may apply
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 excessive speed while landing on a wet grass runway, which resulted in a runway excursion and impact with a fence.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for WPR20CA250)
The pilot's failure to maintain directional control of the airplane after encounter wind gusts during landing roll resulting in the airplane ground looping to the left and the right wing, right horizontal stabilizer, and right elevator contacting the runway and receiving substantial damage.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for MIA01LA123)
THE PILOT'S FAILURE TO MAINTAIN PROPER RUNWAY ALIGNMENT DURING THE LANDING ROLL.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CHI93LA092)
THE PILOT'S INADEQUATE COMPENSATION FOR THE UNFAVORABLE WIND CONDITIONS.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX89LA306)
THE CFI INDICATED THAT THE TAILWHEEL BEGAN TO SHIMMY DURING ROLLOUT. AS FORWARD CONTROL YOKE PRESSURE WAS APPLIED THE SHIMMY WENT AWAY, HOWEVER, AS THE ACFT BEGAN TO SLOW DOWN, THE TAILWHEEL WAS LOWERED AND BEGAN TO SHIMMY AGAIN. AS THE ACFT CONTINUED TO SLOW IT VEERED TO THE RIGHT. THE CFI APPLIED LEFT RUDDER. INITIALLY THE ACFT CONTINUED TO THE RIGHT. SUBSEQUENTLY IT ROLLED LEFT, DRAGGING ITS…
From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX87LA277)
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.