N441JK

Cancelled 2026

Deregistered aircraft · 1980 Cessna 441 · AiResearch TPE331 series

Cancelled
May 28, 2026
Exported to
Australia
Status when cancelled
Valid registration
Serial number
441-0197
Year built
1980
Type
Fixed wing multi engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
May 18, 1989
Certificate issued
December 26, 2025
Last registry action
December 26, 2025
Mode S code
A54F26
Owner when cancelled
Gateway Air Center Inc
Location
Merced, CA
Owner type
Corporation

From the FAA registry file of October 31, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

Service difficulty reports · 5

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR 2009FA0000409Bearing · looseWITH THE LT MAIN GEAR REMOVED FROM THE WING FOR SID INSP, THE AFT TRUNNION BRG WAS FOUND VERY LOOSE IN THE AFT TRUNNION SUPPORT.May 12, 2009 · N441JK · Cessna 441 · Main Landing Gear Attach SectionSDR 2009FA0000408Pivot · corrodedDURING THE SID INSP OF THE MLG TRAILING LINK, THE PIVOT PIN WAS FOUND TO HAVE EXCESSIVE AMOUNTS OF RUST AND PITS.May 12, 2009 · N441JK · Cessna 441 · Main Landing Gear Strut/Axle/TruckSDR 2009FA0000407Drag Brace · damagedDURING THE SID INSP THE NLG WAS REMOVED FOR INSP. THE DRAG BRACE RT BRG PLATE HOLES WERE ALL FOUND EXCESSIVLY ELONGATED REQUIRING STRUCTURAL REPAIR. SUSPECT DAMAGE WAS CAUSED BY NORMAL TOWING OVER THE LIFE OF THE ACFT. THIS WOULD NOT BE DETECTED UNLESS THE May 12, 2009 · N441JK · Cessna 441 · Landing Gear Retraction/Extension SystemSDR 2009FA0000406Hinge · 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 BEARINGS CAUSING EXCMay 12, 2009 · N441JK · Cessna 441 · Passenger/Crew DoorsSDR 2003FA0001068Clamp · crackedREPORTED SMOKE IN COCKPIT UPON TAKEOFF. A/C RETURNED IMMEDIATELY AND PERFORMED NORMAL LANDING. INSP REVEALED A CRACKED V-BRAND CLAMP CONNECTING BLEED AIR SUPPLY LINES IN RT WING ROOT AREA ADJACENT TO SURFACE DEICE PRESSURE REGULATORS. SMOKE WAS DETERMINED TSep 24, 2003 · N441JK · Cessna 441 · Engine Bleed Air System