Safety record in brief:1 NTSB accident (substantial damage, May 1999)2 ADs may apply1 service difficulty report
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 fatigue fracture of the left main landing gear spring at the clamping mechanism, as a result of fretting.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for FTW99LA156)
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 |
|---|---|---|---|
| 2004-21-08 R1 | Aileron Control System | May 9, 2013 | Airframe (195B)Only with: Equipped with at least one P/N 0322709 or P/N 0322709-1 inboard aileron hinge bracket. |
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (195B) |
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.
UPON LANDING ROLL-OUT, AIRCRAFT SLOWED TO APPROXIMATELY 20 KNOTS. THE LEFT MAIN GEAR SEPARATED THE AIRCRAFT. THREE PASSENGERS ON BOARD THE AIRCRAFT STATED THE LANDING WAS VERY SMOOTH. POST-ACCIDENT INVESTIGATION REVEALED WHAT COULD HAVE BEEN A SMALL FRACTURE IN THE LEFT MAIN GEAR SPRING WHERE IT…
From FAA Service Difficulty Reports; matched by N-number and serial number.