N360AX

Cancelled 2004

Deregistered aircraft · 1972 Mcdonnell Douglas DC-10-10 · GE CF6-6 series

Cancelled
February 13, 2004
Status when cancelled
Triennial form not returned
Serial number
46706
Year built
1972
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
May 6, 1972
Certificate issued
September 13, 1997
Last registry action
December 16, 2003
Mode S code
A40C62
Owner when cancelled
Omni Dc-10 Leasing LLC
Location
Tulsa, OK
Owner type
Corporation

From the FAA registry file of November 5, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

Service difficulty reports · 10

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

SDR CNMA200100029Bearing · failedDURING CLIMBOUT #3 ENGINE OIL STRAINER CLOGGED LIGHT CAME ON AND THROTTLE WAS REDUCED AND LIGHT WENT OUT. SHORTLY THERE AFTER OIL QTY DROPPED TO "0" AND ENGINE WAS SHUT DOWN PER COM PROCEDURES. ACCOMPLISHED FUEL DUMP INFLIGHT. REMOVED AND REPLACED RADIAL MID Aug 6, 2001 · N360AX · Doug DC1010 · Turbine Engine Accessory DriveSDR CNMA200100004Doubler · corrodedAFT CARGO PIT FS 1921 LOWER REPAIR DOUBLER CORRODED FROM LONGERON 50L TO 50R. REMOVED FASTENERS. REMOVED CORROSION, TREATED, PRIMED, AND REINSTALLED DOUBLER IAW SRM 51-31-01.Dec 10, 2000 · N360AX · Doug DC1010 · Fuselage Main, Plate/SkinSDR CNMA200100008Seat Track · corrodedA 20 INCH SECTION OF SEAT TRACK CORRODED INBOARD OF L2 DOOR. REPAIRED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00.Dec 9, 2000 · N360AX · Doug DC1010 · Fuselage, Seat/Cargo Attach FittingsSDR CNMA200100005Plate · corrodedLOWER BEACON MOUNTING PLATE CORRODED. REMOVED, CLEANED, TREATED AND PRIMED MOUNTING PLATE. MOUNTING PLATE REINSTALLED.Dec 9, 2000 · N360AX · Doug DC1010 · Fuselage Main, Plate/SkinSDR CNMA200100011Spar · corrodedDURING C-CHECK, FOUND LEFT WING AFT SPAR T-CAP FASTENER HOLE CORRODED AT STA XORS 582. CORROSION WAS REMOVED BY SPOTFACING FASTENER HOLE FROM LOWER SIDE OF HOLE AND INSTALLING A FILLER AND DOUBLER USING 7075-T6 .125 THICKNESS. MAJOR REPAIR APPROVED BY 8110-3Dec 7, 2000 · N360AX · Doug DC1010 · Wing SparSDR CNMA200100007Longeron · corrodedLONGERON 49R BETWEEN FS 1975 AND FS 1986 EXFOLIATED AT AFT END. ACCOMPLISHED LONGERON REPAIR IAW SRM 53-10-00.Dec 6, 2000 · N360AX · Doug DC1010 · Fuselage Main, Longeron/StringerSDR CNMA200100006Stringer · corrodedSTRINGER 49R AT FS 1986 CORRODED COMPLETELY THROUGH. INSTALLED NEW SECTION OF STRINGER IAW SRM 53-10-00.Dec 6, 2000 · N360AX · Doug DC1010 · Fuselage Main, Longeron/StringerSDR CNMA200100003Floorbeam · corrodedLEVEL 2 CORROSION FOUND ON FLOORBEAM STATION 1841 LEFT TO RIGHT DURING C-CHECK INSPECTION. REMOVED DAMAGED AREA ON LT SIDE FROM LBL 25-30 AND RT SIDE FROM LBL 25-35. FABRICATED L-ANGLE REPAIR AND FILLER IAW SRM 53-00-01.Dec 1, 2000 · N360AX · Doug DC1010 · Fuselage Main, Floor BeamSDR CNMA200100001Switch · misalignedAIRCRAFT DEPARTED KMSP. UNABLE TO PRESSURIZE MAIN CABIN ABOVE 5000 FEET MSL. L1 DOOR WARNING INDICATION LIGHT ILLUMINATED AFTER TAKEOFF. L1 DOOR HAD APPROXIMATELY ONE-EIGHT INCH TO ONE-QUARTER INCH GAP BETWEEN DOOR AND DOOR FRAME. INITIATED PROCDEURES TO DSep 21, 2000 · N360AX · Doug DC1010 · Door Warning SystemSDR 20001011AP008Pivot · brokenDURING ROUTINE ''A'' CHECK, A LUBE CARD WAS ISSUED FOR THE HORIZ STAB, WHICH INCLUDED THE HINGE FITTING PIVOT SHAFT. DURING THIS TASK, IT WAS NOTED THAT THE HINGE PIVOT SHAFT AND SLEEVE HAD MIGRATED APPROXIMATELY .125 INCH OUT OF THE HINGE FITTING. FURTHER IMay 12, 2000 · N360AX · Doug DC1010 · Flight Control System