This N-number isn't registered right now. Below is its last known registration, canceled Mar 30, 2020.
Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Jul 2019)7 ADs may apply9 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.
A ductile overstress fracture failure of the right main landing gear bell crank assembly pivot bolt, which resulted in a collapse of the right main landing gear.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC19LA039)
THE ACFT SKIDDED SIDEWAYS DURING LANDING ON AN ICY RWY. THE NOSE GEAR COLLAPSED SIDEWAYS WHEN IT COLLIDED WITH A SNOWBANK AT THE RWYS EDGE. THERE WERE NO INJURIES.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for MKC84LA048)
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 (402B) |
| 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. |
| 2009-04-04 | Cessna Aircraft Company Models 401, 401A, 401B, 402, 402A, and 402B Airplanes | Mar 2, 2009 | Airframe (402B)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 (402B)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 (402B) |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2000-01-16 | Cessna Aircraft Company 300 and 400 Series Airplanes | Feb 15, 2000 | Airframe (402B) |
| 98-04-28 | Cessna Aircraft Company Models T303, 310R, T310R, 335, 340A, 402B, 402C, 404, F406, 414… | Mar 13, 1998 | Airframe (402B) |
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.
PILOT EXPERIENCED LT ENGINE FAILURE IN-FLIGHT DUE TO AN OIL LEAK. AFTER LANDING, INVESTIGATED OIL LEAK AND FOUND THAT THE OIL FILTER ADAPTER ASSEMBLY HAD CRACKED AND BROKEN OFF BELOW THE OIL FILTER, CAUSING THE LOSS OF OIL. INSTALLED NEW OIL FILTER ADAPTER, PN 641639.
From FAA Service Difficulty Reports; matched by N-number and serial number.ON A MX CK FLIGHT, AFTER CHANGING THE NR1 AND THE NR5 CYLINDERS, THE PILOT SAW SMOKE FROM THE LT ENG NACELLE. HE SECURED THE ENG AND RETURNED TO THE HANGAR. UPON OUR INVESTIGATION WE FOUND THAT THE OIL LEVEL WAS STILL ABOUT THE SAME AND THERE WAS INDICATIONS OF AN OIL LEAK BELOW THE ROCKER BOX…
From FAA Service Difficulty Reports; matched by N-number and serial number.OIL TEMP INDICATOR INDICATED FULL HOT READING ON INITIAL CLIMB. A/C RETURNED TO AIRPORT. OIL TEMP SENSOR WAS REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE WITH NORMAL OPERATING INDICATIONS.
From FAA Service Difficulty Reports; matched by N-number and serial number.ON SHORT FINAL, HEARD A THUD IN FLOORBOARDS. JUST AFTER PUTTING GEAR DOWN. AIRCRAFT HAD A SLIGHT YAW AND ROLL AND LANDED UNEVENTFULLY. TAXIED IN, SELECTED FLAPS UP AND SHUTDOWN AIRCRAFT. DURING POSTFLIGHT NOTICED FLAPS WERE STILL FULLDOWN. MAINTENANCE INSPECTION FOUND BROKEN FLAP CONTROL CABLE.…
From FAA Service Difficulty Reports; matched by N-number and serial number.BETWEEN SLC & TWF PILOT REPORTED A LOUD BOOMING/STRIKING NOISE, AS IF HE HAD HIT A BIRD. UPON INVESTIGATION HE NOTICED THE ESCAPE HATCH WAS MISSING. HE NOTIFIED SALT LAKE CENTER OF THE SITUATION. NO OTHER DAMAGE WAS NOTICED. THE PILOT SLOWED THE AIRCRAFT AND CONTINUED SAFELY TO TWF.
From FAA Service Difficulty Reports; matched by N-number and serial number.ON SHORT FINAL THE CABLE BROKE AND THE LEFT FLAP RETRACTED WHICH CAUSED A SPLIT FLAP CONDITION. REPLACED CABLE . INSPECTED THE OTHER FLAP CABLES, NO DEFECTS NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number.HINGE ATTACHMENT DOUBLER CRACKED FOR UPPER RADIUS CORNER FORWARD AND DOWN. CRACK LENGTH, APPROXIMATELY 1.25 INCHES.
From FAA Service Difficulty Reports; matched by N-number and serial number.RETRACT ATTACH EAR CASTING BROKEN. SPACER P/N S133-4P32 AND BOLT P/N 464 P4-26 REPLACED WITH 1 'AN' 5 BOLT AND OVERTORQUED CAUSING UNDO STRESS TO CASTING.
From FAA Service Difficulty Reports; matched by N-number and serial number.LEFT ENGINE WENT TO NORMALLY ASPIRATED, DUE TO LT TURBO VALVE FAILURE.
From FAA Service Difficulty Reports; matched by N-number and serial number.