This N-number isn't registered right now. Below is its last known registration, canceled Aug 18, 2016.
Safety record in brief:1 NTSB accident (substantial damage, Dec 2014)4 ADs may apply5 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 power to the right engine for reasons that could not be determined during postaccident examination and teardown and the pilot’s failure to properly configure the airplane for single-engine flight.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN15FA090)
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.
PRIOR TO DEPARTURE FROM DEN, THE PILOT REPORTED THAT THE LT PNEUMATIC PUMP WAS INOPERATIVE. MX REPLACED THE PNEUMATIC PUMP & THE ACFT DEPARTED, CRUISING AT FL200. THE PILOT NOTED A DECREASE IN POWER & DECREASING OIL PRESS. THE PILOT SHUT DOWN & SECURED THE ENG AS A PRECAUTIONARY MEASURE & DIVERTED…
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOT REPORTED THAT WHEN CONFIGURING THE ACFT FOR CRUISE FLIGHT THE LT ENGINE MANIFOLD PRESSURE DECREASED. PILOT NOTED THAT THE OIL PRESSURE WAS DECLINING AND SHUTDOWN THE ENGINE AS A PRECAUTIONARY MEASURE. OPEN
From FAA Service Difficulty Reports; matched by N-number and serial number.AFTER TAKEOFF, REPORTED SMOKE IN CABIN AND DECLARED AN EMERGENCY. FLIGHT DIVERTED. MX DISABLED HEATER AFTER CONFIRMATION OF FAILURE. HEATER WOULD NOT CYCLE OFF HOT. DUCTS AND DEBRIS WERE OVERHEATED. NO BURNED OR EVIDENCE OF CHARRED AREAS.
From FAA Service Difficulty Reports; matched by N-number and serial number.ACFT WAS INBOUND AT CRUISE. E2 ALTERNATOR WAS FLICKERING ON OFF LINE MULTIPLE TIMES AND FAILED. E1 ALTERNATOR FAILED AFTER E2. PILOT LOST ELECTRICAL POWER AND LANDED.
From FAA Service Difficulty Reports; matched by N-number and serial number.ALL FOUR AILERON PRIMARY CONTROL CABLES FOUND WORN, SEVERING SEVERAL STRANDS AT WING STATION 50.021 WHERE IS PASSES IN FRONT OF THE OUTBOARD FLAP BELLCRANK. ONE CABLE HAD 3 OF THE 7 STRANDS SEVERED. CABLES WERE COVERED WITH GREASE AND GRIME MAKING IT DIFFICULT TO INSPECT CABLE. CLEARANCE IS…
From FAA Service Difficulty Reports; matched by N-number and serial number.