Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Sep 2017)2 ADs may apply4 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 pilot’s failure to maintain clearance from a sign while taking off from a road.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for GAA17CA549)
THE PILOT'S POOR JUDGMENT IN ATTEMPTING TO LAND UNDER THE EXISTING HIGH WIND CONDITION.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC93LA063)
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 (U206G) |
| 2009-16-03 | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating… | Sep 9, 2009 | Engine (IO 520 SERIES)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P installed. |
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 A 100 HOUR INSPECTION, A CRACK WAS FOUND ON THE REAR ATTACH BRACKET OF THE HORIZONTAL STAB.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING COURSE OF 100 HR INSPECTION, A RUST LINE WAS NOTED IN THE PAINT. UPON FURTHER INVESTIGATION THE PART WAS NOTED TO BE CRACKED. THIS PART APPEARS TO BE THE NEW STYLE STEEL PART. THIS PART WAS INSTALLED ON THE LT SIDE , THE CRACK STARTED AT THE LOWER OB CORNER RADIUS AND TRAVELED APPROXIMATELY…
From FAA Service Difficulty Reports; matched by N-number and serial number.THE HEAD OF THE BOLT ATTACHING THE REAR OF THE NOSE GEAR DRAG LINK TO THE AIRCRAFT WAS FOUND LAYING IN THE NOSE GEAR WELL. THIS BOLT IS IN A SHEAR LOAD AND SHOULD NOT HAVE BEEN SUBJECT TO ANY FORCES THAT WOULD FORCE THE HEAD OF THE BOLT TO THE POINT OF CRACKING OFF.
From FAA Service Difficulty Reports; matched by N-number and serial number.PROBLEMS ENCOUNTERED WITH SUPERIOR CYLINDERS, B OR B SERIES. NR 4 CYLINDER HAD STUCK EXHAUST VALVE AND BENT PUSH ROD. NR 1 AND NR 2 CYLINDERS HAD CRACKS EXTENDING FROM THE SPARK PLUG HOLE TO THE FIN AREA LEFT OF THE SPARK PLUG HOLE TO THE FIN AREA LEFT OF THE SPARK PLUG HOLE (WHEN FACING THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.