This N-number isn't registered right now. Below is its last known registration, canceled Jun 8, 2017.
Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Aug 1992)6 ADs may apply2 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.
FAILURE OF THE PILOT TO FEATHER THE FAILED ENGINE PROPELLER. A FACTOR WAS: POWER LOSS FOR UNDETERMINED REASONS.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DEN92FA081)
THE PILOT DISCOVERED THAT THE GEAR WOULD NOT EXTEND ELECTRICALLY. MANUAL EXTENSION WAS ATTEMPTED, BUT THE CRANK WOULD NOT TURN IN EITHER DIRECTION. WHILE APPLYING PRESSURE TO THE CRANKS, THE CHAIN DRIVE FAILED. THE PLANE WAS LANDED WITH THE GEAR RETRACTED. DISASSEMBLY OF THE EMERGENCY EXTENSION SYSTEM REVEALED THAT A SHAFT, PN 0843400-50, WAS BENT AND GOUGE MARKS WERE FOUND ON A TOOTH OF A BEVEL…
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DEN82DA079)
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 (402A) |
| 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. |
| 2009-04-04 | Cessna Aircraft Company Models 401, 401A, 401B, 402, 402A, and 402B Airplanes | Mar 2, 2009 | Airframe (402A)Certain serial numbers: 401 655; 401 401-0001–401-0322; 401A 655; 401A 401A0001–401A0132; 401B 401B0001–401B0221; 402 402-0001–402-0322; … |
| 2005-20-25 | The Cessna Aircraft Company Models 401, 401A, 401B, 402, 402A, 402B, 402C, 404, 411… | Nov 9, 2005 | Airframe (402A)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. |
| 2005-12-12 | Cessna Aircraft Company Models 401, 401A, 401B, 402, 402A, 402B, 411, and 411A Airplanes | Jun 22, 2005 | Airframe (402A) |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2000-01-16 | Cessna Aircraft Company 300 and 400 Series Airplanes | Feb 15, 2000 | Airframe (402A) |
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.
INLET ON DUCT DEFORMED DUE TO HEAT RESTRICTING AIR FLOW (PILOT DEFROST). SUBMITTER FABRICATED NEW DUCT OUT OF FIBERGLASS USING OLD DUCT AS PATTERN. DAMAGE DIFFICULT TO DETECT. SUBMITTER SUGGESTS REMOVING HOSE, CABIN FIREWALL, TO INSPECT.
From FAA Service Difficulty Reports; matched by N-number and serial number.INLET ON DUCT DEFORMED DUE TO HEAT RESTRICTING AIR FLOW. (COPILOT DEFROST.) SUBMITTER FABRICATED NEW DUCT OUT OF FIBERGLASS USING OLD DUCT AS PATTERN. DAMAGE DIFFICULT TO DETECT. SUBMITTER SUGGESTS REMOVING HOSE, CABIN FIREWALL, TO INSPECT.
From FAA Service Difficulty Reports; matched by N-number and serial number.