This N-number isn't registered right now. Below is its last known registration, canceled Jan 19, 2017.
Safety record in brief:1 NTSB accident (substantial damage, Mar 1999)4 ADs may apply7 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 loss of engine power for undetermined reasons.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ATL99LA062)
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 |
|---|---|---|---|
| 2020-03-16 | Fuselage Main, Structure | Mar 9, 2020 | Airframe (210L) |
| 2012-10-04 | Wings | Jun 5, 2012 | Airframe (210L)Certain serial numbers: 210G 21058819–21058936; T210G T210-0198–T210-0307; 210H 21058937–21059061; T210H T210-0308–T210-0392; 210J 21059062–21059199; T210J 21058140; … |
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (210L) |
| 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.
AFTER TAKEOFF, PUMP CONTINUED TO RUN AFTER GEAR RETRACTION. PILOT RETURNED AND LANDED SAFELY WITHOUT INCIDENT. MX ADJUSTED GEAR ACTUATOR, OPS CHECK NORMAL.
From FAA Service Difficulty Reports; matched by N-number and serial number.ON APPROACH, LANDING GEAR WOULD NOT EXTEND. PILOT PROCEEDED TO PUMP GEAR DOWN AND LOCKED AND LANDED SAFELY WITHOUT INCIDENT. MX IS INSPECTING.
From FAA Service Difficulty Reports; matched by N-number and serial number.ROTOR BROKE AT CAM AND GEAR LOCATION/DRIVE GEAR.
From FAA Service Difficulty Reports; matched by N-number and serial number.AIRCRAFT EXPERIENCED ELECTRICAL FAILURE ON 1-26-96. MX FOUND FUEL FLOW LINE CHAFED THROUGH, SPRAYING A FUEL MIST ON CHAFED ELECTRICAL WIRES. ON 2-1-96, FLIGHT EXPRESS (FPIA) REPORTED THAT AN INSPECTION ON THE FUEL PRESSURE LINE TO THE FUEL FLOW INDICATOR BEHIND THE INSTRUMENT PANEL HAS RESULTED IN…
From FAA Service Difficulty Reports; matched by N-number and serial number.ON JANUARY 26, 1996, PILOT REPORTED ELECTRICAL FAILURE GLOW BEHIND INSTRUMENT PANEL. MAINTENANCE FOUND TRANSPONDER DIMMER WIRE SHORTED AGAINST PRESSURE LINE. REPLACED FUEL PRESSURE LINE WITH STRATOFLEX III HOSE AND FITTING. INSPECTIONS ON REMAINING FLEET OF CE210'S RESULTING WITH 75 PERCENT HAVING…
From FAA Service Difficulty Reports; matched by N-number and serial number.ON JANUARY 26, 1996, PILOT REPORTED ELECTRICAL FAILURE GLOW BEHIND INSTRUMENT PANEL. MAINTENANCE FOUND TRANSPONDER DIMMER WIRE SHORTED AGAINST PRESSURE LINE. REPLACED FUEL PRESSURE LINE WITH STRATOFLEX III HOSE AND FITTING. INSPECTIONS ON REMAINING FLEET OF CE210'S RESULTING WITH 75 PERCENT HAVING…
From FAA Service Difficulty Reports; matched by N-number and serial number.ON JANUARY 26, 1996, PILOT REPORTED ELECTRICAL FAILURE GLOW BEHIND INSTRUMENT PANEL. MAINTENANCE FOUND TRANSPONDER DIMMER WIRE SHORTED AGAINST PRESSURE LINE. REPLACED FUEL PRESSURE LINE WITH STRATOFLEX III HOSE AND FITTING. INSPECTIONS ON REMAINING FLEET OF CE210'S RESULTING WITH 75 PERCENT HAVING…
From FAA Service Difficulty Reports; matched by N-number and serial number.