Safety record in brief:1 NTSB accident (substantial damage, Aug 1996)2 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.
fuel starvation for undetermined reason(s). Factors relating to the accident were: the crop, and the uphill terrain condition in the emergency landing area.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CHI96LA292)
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 (210E) |
| 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.
THE LT AND RT MAIN GEAR SADDLES WERE REPLACED 3-14-1977 AT TACH 1448.0 IAW AD76-14-07R2 AND SE75-26 THEY WERE DUE FOR A DY PENETRANT CHECK 1300 HRS LATER. THE DYE PENETRENT CHECK WAS DONE 42HRS EARLY TO CONINCIDE WITH OTHER MX. BOTH SADDLES WERE DISCOVERED TO HAVE A .2500" LONG CRACK ACROSS THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.THE LT AND RT MAIN GEAR SADDLES WERE REPLACED 3-14-1977 AT TACH 1448.0. IAW AD76-14-07R2 AND SE75-26 THEY WERE DUE FOR A DY PENETRANT CHECK 1300 HRS LATER. THE DYE PENETRENT CHECK WAS DONE 42HRS EARLY TO CONINCIDE WITH OTHER MAINTENANCE. BOTH SADDLES WERE DISCOVERED TO HAVE A .2500" LONG CRACK…
From FAA Service Difficulty Reports; matched by N-number and serial number.