Safety record in brief:1 NTSB accident (substantial damage, Apr 2005)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 fracture of the left brake master cylinder piston rod, which resulted in the total failure of the left-side brake system and the subsequent loss of directional control during landing roll. An additional cause was the encountered ground-loop.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CHI05LA099)
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 (195A)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 (195A) |
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.
TAILWHEEL STRUT STUCK FULLY EXTENDED FOR LANDING. SYSTEM DESIGN DOES NOT PERMIT STEERING WHILE STRUT IS IN THIS CONDITION. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.