This N-number isn't registered right now. Below is its last known registration, canceled Dec 20, 2019.
Safety record in brief:1 NTSB accident (substantial damage, Sep 2018)4 ADs may apply8 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 properly adjust the fuel/air mixtures, which resulted in a partial loss of engine power to both engines due to fuel starvation and a subsequent forced landing to a field.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN18LA373)
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 |
|---|---|---|---|
| 2016-17-08 | Elevator Tab Control System | Sep 12, 2016 | Airframe (T310R) |
| 2009-16-03 | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating… | Sep 9, 2009 | Engine (TSIO-520 SER)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. |
| 2000-01-16 | Cessna Aircraft Company 300 and 400 Series Airplanes | Feb 15, 2000 | Airframe (T310R) |
| 98-04-28 | Cessna Aircraft Company Models T303, 310R, T310R, 335, 340A, 402B, 402C, 404, F406, 414… | Mar 13, 1998 | Airframe (T310R) |
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.
COUPLING FLANGE BURNT AND CORRODED CAUSING EXHAUST LEAK. AIRCRAFT UNDERWENT ANNUAL INSPECTION AND IMPORT C OF A SUBSEQUENTLY ISSUED BY SO-FSDO-05 NINE MONTHS PRIOR TO THIS SHOP VISIT. THE ERODED, BURNT END OF THE COUPLING WAS MISSING MATERIAL, AND IS LOCATED UNDER THE METAL SEGMENTED 'V' BAND…
From FAA Service Difficulty Reports; matched by N-number and serial number.ENGINE BEAM FOUND SEVERELY CORRODED FROM EXPOSURE TO HOT EXHAUST GASSES DUE TO LEAKING EXHAUST PIPE FLANGES AND CLAMPS. OTHER DAMAGE FOUND INVOLVED THE FIREWALL ACCESS PANEL WHICH COVERS THE FUEL CROSSFEED LINE IN WHICH MOSTLY ALL OF THE ATTACHING SCREW HEADS WERE EITHER BURNT OR CORRODED AWAY.
From FAA Service Difficulty Reports; matched by N-number and serial number.COUPLING FLANGE BURNT AND CORRODED CAUSING EXHAUST LEAK. AIRCRAFT UNDERWENT ANNUAL INSPECTION AND IMPORT C OF A SUBSEQUENTLY ISSUED BY SO-FSDO-05 NINE MONTHS PRIOR TO THIS SHOP VISIT. THE ERODED, BURNT END OF THE COUPLING WAS MISSING MATERIAL AND IS LOCATED UNDER THE METAL SEGMENTED V-BAND CLAMPS…
From FAA Service Difficulty Reports; matched by N-number and serial number.COUPLING FLANGE BURNT AND CORRODED CAUSING EXHAUST LEAK. AIRCRAFT UNDERWENT ANNUAL INSPECTION AND IMPORT C OF A SUBSEQUENTLY ISSUED BY SO-FSDO-05 NINE MONTHS PRIOR TO THIS SHOP VISIT. THE ERODED, BURNT END OF THE COUPLING WAS MISSING MATERIAL AND IS LOCATED UNDER THE METAL SEGMENTED 'V' BAND…
From FAA Service Difficulty Reports; matched by N-number and serial number.COUPLING FLANGE BURNT AND CORRODED CAUSING EXHAUST LEAK. AIRCRAFT UNDERWENT ANNUAL INSPECTION AND IMPORT C OF A SUBSEQUENTLY ISSUED BY SO-FSDO-05 NINE MONTHS PRIOR TO THIS SHOP VISIT. THE ERODED, BURNT END OF THE COUPLING WAS MISSING MATERIAL AND IS LOCATED UNDER THE METAL SEGMENTED 'V' BAND…
From FAA Service Difficulty Reports; matched by N-number and serial number.COUPLING FLANGE BURNT AND CORRODED CAUSING EXHAUST LEAK. AIRCRAFT UNDERWENT ANNUAL INSPECTION AND IMPORT C OF A SUBSEQUENTLY ISSUED BY SO-FSDO-05 NINE MONTHS PRIOR TO THIS SHOP VISIT. THE ERODED, BURNT END OF THE COUPLING WAS MISSING MATERIAL AND IS LOCATED UNDER THE METAL SEGMENTED 'V' BAND…
From FAA Service Difficulty Reports; matched by N-number and serial number.PART WAS FOUND CRACKED 330 DEGREES AROUND WELD AND WAS VISIBLE BY OPENING THE OUTBOARD COWLING DOOR.
From FAA Service Difficulty Reports; matched by N-number and serial number.THIS NEW FAA-PMA PART WAS NOT FORMED PROPERLY AND COULD NOT BE INSTALLED WITHOUT CAUSING UNDUE STRESS ON MATING PARTS. THE PART WAS TAGGED AND RETURNED TO DISTRIBUTOR AND ANOTHER NEW PART ORDERED FOR THE AIRCRAFT. (THE ANGLE OF THE BEND IN THE PIPE WAS NOT CORRECT).
From FAA Service Difficulty Reports; matched by N-number and serial number.