Safety record in brief:1 NTSB accident (substantial damage, May 2009)2 ADs may apply2 service difficulty reports
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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 due to fuel starvation as a result of the pilot's failure to activate the fuel boost pump when attempting an engine restart. Contributing to the accident was the pilot's failure to use a checklist.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for WPR09CA262)
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 |
|---|---|---|---|
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (210) |
| 2008-10-02 | Cessna Aircraft Company 172, 175, 180, 182, 185, 206, 207, 208, 210, and 303 Series… | May 12, 2008 | Airframe (210)Certain serial numbers: 172S 172S10672–172S10674; 172S 172S10676; 172S 172S10678–172S10680; 172S 172S10682; 172S 172S10683; 172S 172S10685; …. Only with: Applies only to airplanes that have a P/N 2013142-18 alternate static air source selector valve installed after November 19, 2007. |
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.
DURING SCHEDULED ANNUAL INSPECTION, FOUND MOVEMENT IN THE RT WING SPAR FITTINGS, BETWEEN THE RT WING MAIN SPAR ATTACH BRACKETS AND THE FUSELAGE CARRY-THROUGH SPAR ATTACH BRACKETS. REMOVED RT WING FROM AIRCRAFT, FOUND SIGNIFICANT PITTING AND CORROSION IN BORES OF ALL ATTACH BRACKET BUSHINGS.
From FAA Service Difficulty Reports; matched by N-number and serial number.CESSNA PART NR C589510-0290. MANUFACTURED TO TSO-C91, WOULD NOT PASS G-SWITCH OPERATIONAL CHECK PER FAR 91.207(D) EVEN AFTER SLAMMING ELT INTO GROUND IN DIRECTION OF FLIGHT. ELT WOULD PUT OUT SIGNAL WHEN MANUALLY SWITCHED TO ON.
From FAA Service Difficulty Reports; matched by N-number and serial number.