N441XCessna 441
Safety record in brief:No NTSB accidents or incidents since 19825 ADs may apply5 service difficulty reports
Registration
FAA Aircraft Registry · Oct 17, 2026- Registered owner
- Individual owner
- City, state
- Bigfork, MT
- Certificate issued
- Feb 20, 2026
- Expires
- Feb 28, 2033
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Cessna
- Model
- 441
- Serial number
- 441-0254
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 10
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A55061
Engine
- Type
- Turbo-prop
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2026 – nowIndividual ownerBigfork, MT · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (5)
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 |
|---|---|---|---|
| 2005-20-25 | The Cessna Aircraft Company Models 401, 401A, 401B, 402, 402A, 402B, 402C, 404, 411… | Nov 9, 2005 | Airframe (441)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. |
| 2003-09-09 | Cessna Aircraft Company Models 441 and F406 Airplanes | Jun 24, 2003 | Airframe (441)Certain serial numbers: 441 0001–0362; 441 698; F406 0001–0089 |
| 98-04-28 | Cessna Aircraft Company Models T303, 310R, T310R, 335, 340A, 402B, 402C, 404, F406, 414… | Mar 13, 1998 | Airframe (441) |
| 97-25-04 | Cessna Aircraft Company Models 208, 208A, 208B, 425, and 441 Airplanes | Jan 21, 1998 | Airframe (441) |
| 95-25-10 | Cessna Model 441, 500, 550, and 560 Series Airplanes | Jan 22, 1996 | Airframe (441)Serial numbers per Allied Signal Aerospace Service Bulletins 103576-21-4054, 103576-21-4056, and 103648-21-4055. Only with: Equipped with Allied Signal outflow/safety valves identified in Allied Signal Aerospace Service Bulletins 103576-21-4054, 103576-21-4056, and 103648-21-4055. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (5)
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.
- Servicing · oil filter · brokenDec 14, 2021
DURING ROUTINE 100 HOUR ENGINE MAINTENANCE, FOUND OIL FILTER ON RIGHT ENGINE PARTIALLY SEPARATED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · pivot · corrodedMay 14, 2009
DURING THE SID INSP OF THE MLG TRAILING LINK, THE PIVOT PIN WAS FOUND TO HAVE EXCESSIVE AMOUNTS OF RUST AND PITS.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Stabilizers · bracket · damagedMay 14, 2009
WITH THE RUDDER REMOVED FOR COMPLIANCE WITH THE SID INSP, THE LWR PIVOT BRACKETS WERE FOUND EXCESSIVELY ELONGATED AND REQUIRED REPLACEMENT.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 5 reportsShow fewer reports
- Flight controls · torque tube · corrodedMay 14, 2009
DURING THE SID INSP, FOUND THE RUDDER TORQUE TUBE HAD SOME RUST. THIS CAN ONLY BE FOUND WITH THE RUDDER REMOVED. REMOVING THE RUDDER IS NOT REQUIRED EXCEPT DURING THE SID INSP.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · hinge · corrodedMay 14, 2009
DURING THE SID INSP, THE UPPER CABIN DOOR WAS REMOVED FOR INSP. THE HINGE PIVOT BOLTS COULD NOT BE REMOVED BECAUSE THE BOLTS, BUSHINGS AND BRGS WERE ALL RUSTED SOLID. THIS CAUSED THE BOLTS TO PIVOT IN THE FUSELAGE STRUCTURE INSTEAD OF THE BRGS CAUSING EXCESSIVE WEAR OF THE FUSELAGE DOOR MOUNT…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026