Safety record in brief:1 NTSB accident (substantial damage, Mar 2021)3 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.
A total loss of engine power during cruise flight due to a fatigue crack in the No. 3 cylinder connecting rod shaft resulting from either preignition or detonation, which resulted in a forced landing and impact with terrain.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for WPR21LA121)
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 |
|---|---|---|---|
| 2009-10-09 R2 | Rudder Control System | Sep 12, 2011 | Airframe (150J)Certain serial numbers: 150F 15061533–15064532; 150G 15064533–15064969; 150G 15064971–15067198; 150H 15067199–15069308; 150H 649; 150J 15069309–15071128; …. Only with: FA150L S/N FA1500121-FA1500261 and FA150M S/N FA1500262-FA1500336 only when equipped with FKA150-2311 and FKA150-2316. |
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (150J) |
| 2008-22-18 | Cessna Aircraft Company 150 Series Airplanes | Dec 9, 2008 | Airframe (150J)Only with: BRS-150 Parachute System with serial number 50001 through 50006 installed via STC SA64CH. |
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.