This N-number isn't registered right now. Below is its last known registration, canceled Mar 24, 2014.
Safety record in brief:2 NTSB accidents (substantial damage at worst, latest May 2011)3 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 decision to initiate a go-around after a bounced landing at an airport where go-arounds were not advised and his failure to maintain adequate airspeed during the go-around.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for WPR11FA232)
THE PILOT'S MISJUDGEMENT OF CLEARANCE FROM A PARKED AIRCRAFT WHILE TAXIING.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX90LA254)
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 |
|---|---|---|---|
| 2023-05-16 | Reciprocating Engine Power Section | Mar 15, 2023 | Engine (TSIO-520-M) |
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (T207A) |
| 2009-16-03 | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating… | Sep 9, 2009 | Engine (TSIO-520-M)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 ACFT WAS TAKEN OUT OF SERVICE DUE TO A BLADE THAT ROTATED FREELY IN THE HUB AND WAS NOT CONNECTED TO THE PITCH CHANGE MECHANISM. THE PROPELLER WAS DISASSEMBLED AND THE RETENTION AREA OF ONE BLADE WAS FOUND TO BE CRACKED APPROX 3 INCHES ACROSS THE RETENTION AREA OF ONE BLADE WAS FOUND TO BE…
From FAA Service Difficulty Reports; matched by N-number and serial number.WHEN THE FUEL SELECTOR VALVE IS SELECTED TO THE RT TANK, FUEL IS BEING DELIVERED FROM THE LT TANK, VISE VERSA. THIS WAS DISCOVERED DURING A SHORT FLIGHT IN WHICH THE PILOT NOTICED THE RT TANK FUEL GAUGE WAS DROPPING WHEN THE LT TANK WAS SELECTED. THIS WAS LATER CONFIRMED DURING AN INSPECTION IN…
From FAA Service Difficulty Reports; matched by N-number and serial number.FWD RT STABILIZER FITTING CRACKED. FOUND CRACKED FITTING UPON ANNUAL INSPECTION OF EMPENNAGE. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.OIL FILTER INTERNAL GASKET WAS OUT OF PLACE AND COVERING INLET PASSAGE OF FILLER BODY. APPEARS TO BE MANUFACTURE DEFECT. SUBMITTER ADVISES A CLOSER INSPECTION OF OIL FILTER PRIOR TO INSTALLATION TO INSURE GASKET IS NOT BLOCKING INLET HOLE.
From FAA Service Difficulty Reports; matched by N-number and serial number.