Safety record in brief:1 NTSB accident (substantial damage, Sep 2021)4 ADs may apply3 service difficulty reports
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The pilot experiencing an episode of impaired behavior and incapacitation for reasons that could not be determined based on the available information.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for WPR21LA350)
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 |
|---|---|---|---|
| 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. |
| 2005-20-25 | The Cessna Aircraft Company Models 401, 401A, 401B, 402, 402A, 402B, 402C, 404, 411… | Nov 9, 2005 | Airframe (404)Certain serial numbers: 401 655; 401 401-0001–401-0322; 401A 655; 401A 401A0001–401A0132; 401B 401B0001–401B0221; 402 402-0001–402-0322; …. Only with: Equipped with an avionics bus circuit breaker switch P/N CM3589-50, 593-250-101, 593-250-102, W31-X2M5A-50, or W31-X1000-50. |
| 2000-01-16 | Cessna Aircraft Company 300 and 400 Series Airplanes | Feb 15, 2000 | Airframe (404) |
| 98-04-28 | Cessna Aircraft Company Models T303, 310R, T310R, 335, 340A, 402B, 402C, 404, F406, 414… | Mar 13, 1998 | Airframe (404) |
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.
ENGINE FAILED IN FLIGHT. NR 5 AND NR 6 CONNECTING ROD (CRANK END) PROTRUDING THROUGH TOP OF ENGINE CASE. HOLES IN BOTH SIDES OF CASE BELOW NR 5 AND NR 6 CYLINDERS ABOVE OIL PAN FLANGE. THE ENGINE HAS BEEN IN SERVICE SINCE 07/2016. IT IS A FACTORY REBUILT ENGINE.
From FAA Service Difficulty Reports; matched by N-number and serial number.FOUND BOTH LEFT AND RIGHT T CHANNELS CRACKED APPROX 8 INCHES. THESE CHANNELS ARE LOCATED ON THE FORWARD CORNERS OF THE NOSE WHEEL WELL BOX ASSY AND ACCESSED FROM THE NOSE BAGGAGE AREA. POSSIBLE CAUSE FOR CRACKING DUE TO EXCESSIVE SIDE LOADING WHILE TAXIING. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number.FUEL STAINS WERE NOTED AROUND SEVERAL INTAKE TUBES. IN REMOVING THE COLLARS FROM THE CYLINDERS TO GAIN ACCESS TO THE INJECTORS, TWO OF THE INTAKE TUBES WERE FOUND CRACKED AROUND THE RADIUS OF THE FLANGE.
From FAA Service Difficulty Reports; matched by N-number and serial number.