- Registered owner
- Matosich Andrew J
- Location
- Bigfork, MT
- Owner type
- Individual
- Serial number
- 441-0254
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Certificate issued
- February 20, 2026
- Expires
- February 28, 2033
- Mode S code
- A55061
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 24
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1979 | 4 |
|---|---|
| 1980 | 1 |
| 1983 | 1 |
| 1984 | 1 |
| 1986 | 2 |
| 1992 | 2 |
| 1996 | 2 |
| 1998 | 3 |
| 2001 | 2 |
| 2002 | 1 |
| 2003 | 1 |
| 2004 | 1 |
| 2005 | 3 |
| 2008 | 2 |
| 2009 | 1 |
| 2023 | 1 |
See all 28 ADs
Information bulletins that may apply · 5
Advisory, not mandatory.
Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N441XMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Cessna 441 aircraft
FAA incident reports
No FAA accident or incident reports matched to N441XMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Cessna 441 aircraft
Service difficulty reports · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2021FA0000404Oil Filter · brokenDURING ROUTINE 100 HOUR ENGINE MAINTENANCE, FOUND OIL FILTER ON RIGHT ENGINE PARTIALLY SEPARATED.SDR 2009FA0000420Hinge · corrodedDURING 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 EXCESSSDR 2009FA0000419Torque Tube · corrodedDURING 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.SDR 2009FA0000418Bracket · damagedWITH THE RUDDER REMOVED FOR COMPLIANCE WITH THE SID INSP, THE LWR PIVOT BRACKETS WERE FOUND EXCESSIVELY ELONGATED AND REQUIRED REPLACEMENT.SDR 2009FA0000417Pivot · corrodedDURING THE SID INSP OF THE MLG TRAILING LINK, THE PIVOT PIN WAS FOUND TO HAVE EXCESSIVE AMOUNTS OF RUST AND PITS.
STCs that may be installed · 180
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 441
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light Controller