Safety record in brief:1 NTSB accident (substantial damage, Sep 1992)3 ADs may apply2 service difficulty reports
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 JAMMING OF THE OIL PRESSURE PUMP CAUSED BY THE FAILURE OF THE OIL PRESSURE PUMP DRIVEN IMPELLER. THE LACK OF A SUITABLE LANDING AREA WAS A FACTOR.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CHI92LA274)
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 (172P) |
| 2011-06-02 | Cessna Aircraft Company (Cessna) Model 172 Airplanes Modified by Supplemental Type… | May 26, 2011 | Airframe (172P)Only with: Modified by STC SA01303WI (installation of TAE 125-01 or TAE 125-02-99 engine). |
| 2001-23-03 | Cessna Aircraft Company Models 172N, 172P, R172K, 172RG, F172N, F172P, FR172J, and… | Dec 27, 2001 | Airframe (172P)Certain serial numbers: 172N 17267585–17270049; 172N 17270051–17274009; 172N 17261445; 172N 17261578; 172N 17270050; 172P 17274010–17276654; … |
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 INSPECTION, FOUND THE LEFT FLAP, INBOARD HINGE FLAP SUPPORT ARMS WERE GROOVED DUE TO CHAFING BY THE AFT BEARING. THIS CONDITION IS USUALLY RELATED TO THE FORWARD BEARING CHAFING. BOTH INBOARD HINGE FLAP SUPPORT ARMS WERE CHANGED WITH NEW. SEB 95-3 ADDRESSES INSPECTING THESE SUPPORT ARMS.…
From FAA Service Difficulty Reports; matched by N-number and serial number.MAGNETO ROTOR SHAFT SHEARED .25 INCH BELOW CAM. SUBMITTER RECOMMENDS VISUAL INSPECTION OF SHAFT AT DISASSEMBLY.
From FAA Service Difficulty Reports; matched by N-number and serial number.