# N360AX: 1972 Mcdonnell Douglas DC-10-10, registration cancelled 2004-02-13

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 13, 2004
- Status when cancelled: Triennial form not returned
- Airframe: [Mcdonnell Douglas DC-10-10](https://openairdocs.org/model/mcdonnell-douglas-dc-10-10) (registry code 3022110)
- Engine: [GE CF6-6 series](https://openairdocs.org/engine/ge-cf6-6-series) (registry code 30020)
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs)
- Serial number: 46706
- Year built: 1972
- Type of aircraft: Fixed wing multi engine
- Engine type: 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](https://openairdocs.org/faa-owner/OMNI%20DC-10%20LEASING%20LLC)
- Location: [Tulsa, OK](https://openairdocs.org/faa-place/OK/Tulsa)
- Owner type: Corporation
- Owner's area on the map: 36.1540° N, 95.9928° W: Placed by OpenAirDocs: center of Tulsa, OK, within about 8 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N360AX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=360AX
- Page: https://openairdocs.org/deregistered/N360AX-2004-02-13

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.

ADs and bulletins for the Mcdonnell Douglas DC-10-10: https://openairdocs.org/model/mcdonnell-douglas-dc-10-10.md

## Service difficulty reports (10)

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

- [SDR CNMA200100029](https://openairdocs.org/sdr/CNMA200100029), Aug 6, 2001: BEARING. FAILED. DURING 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 
- [SDR CNMA200100004](https://openairdocs.org/sdr/CNMA200100004), Dec 10, 2000: DOUBLER. CORRODED. AFT CARGO PIT FS 1921 LOWER REPAIR DOUBLER CORRODED FROM LONGERON 50L TO 50R. REMOVED FASTENERS. REMOVED CORROSION, TREATED, PRIMED, AND REINSTALLED DOUBLER IAW
- [SDR CNMA200100008](https://openairdocs.org/sdr/CNMA200100008), Dec 9, 2000: SEAT TRACK. CORRODED. A 20 INCH SECTION OF SEAT TRACK CORRODED INBOARD OF L2 DOOR. REPAIRED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00.
- [SDR CNMA200100005](https://openairdocs.org/sdr/CNMA200100005), Dec 9, 2000: PLATE. CORRODED. LOWER BEACON MOUNTING PLATE CORRODED. REMOVED, CLEANED, TREATED AND PRIMED MOUNTING PLATE. MOUNTING PLATE REINSTALLED.
- [SDR CNMA200100011](https://openairdocs.org/sdr/CNMA200100011), Dec 7, 2000: SPAR. CORRODED. DURING 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
- [SDR CNMA200100007](https://openairdocs.org/sdr/CNMA200100007), Dec 6, 2000: LONGERON. CORRODED. LONGERON 49R BETWEEN FS 1975 AND FS 1986 EXFOLIATED AT AFT END. ACCOMPLISHED LONGERON REPAIR IAW SRM 53-10-00.
- [SDR CNMA200100006](https://openairdocs.org/sdr/CNMA200100006), Dec 6, 2000: STRINGER. CORRODED. STRINGER 49R AT FS 1986 CORRODED COMPLETELY THROUGH. INSTALLED NEW SECTION OF STRINGER IAW SRM 53-10-00.
- [SDR CNMA200100003](https://openairdocs.org/sdr/CNMA200100003), Dec 1, 2000: FLOORBEAM. CORRODED. LEVEL 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 2
- [SDR CNMA200100001](https://openairdocs.org/sdr/CNMA200100001), Sep 21, 2000: SWITCH. MISALIGNED. AIRCRAFT DEPARTED KMSP. UNABLE TO PRESSURIZE MAIN CABIN ABOVE 5000 FEET MSL. L1 DOOR WARNING INDICATION LIGHT ILLUMINATED AFTER TAKEOFF. L1 DOOR HAD APPROXIMATE
- [SDR 20001011AP008](https://openairdocs.org/sdr/20001011AP008), May 12, 2000: PIVOT. BROKEN. DURING 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 HIN

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