# N108AX: Mcdonnell-Douglas DC-10-30, registration cancelled 2011-08-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 3, 2011
- Status when cancelled: Triennial form not returned
- Airframe: [Mcdonnell-Douglas DC-10-30](https://openairdocs.org/model/mcdonnell-douglas-dc-10-30) (registry code 3023501)
- Engine: [GE CF6-50 series](https://openairdocs.org/engine/ge-cf6-50-series) (registry code 30018)
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs)
- Serial number: 47927
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 7, 1997
- Certificate issued: November 4, 2004
- Last registry action: August 18, 2008
- Mode S code: A02282
- 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/N108AX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=108AX
- Page: https://openairdocs.org/deregistered/N108AX-2011-08-03

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-10-30: https://openairdocs.org/model/mcdonnell-douglas-dc-10-30.md

## Service difficulty reports (38)

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

- [SDR CNMA20100003](https://openairdocs.org/sdr/CNMA20100003), Jan 28, 2010: ACCESS DOOR. LEAKING. AT 370 FL COULD NOT CONTROL CABIN CLIMB IN AUTO, STANBY, OR MANUAL CLIMBING AT 1000 FT IAW MIN HAD TO DESCENT TO MAINTAIN 9500 FT CABIN AT FL 290. FOUND FWD AVI
- [SDR CNMA20090015](https://openairdocs.org/sdr/CNMA20090015), Jul 13, 2009: FUEL TANK. LEAKING. RT WING LEAKING FUEL IN FLIGHT.
- [SDR CNMA20090055](https://openairdocs.org/sdr/CNMA20090055), Aug 8, 2008: SEAT TRACK. CORRODED. LIGHT CORROSION ON SEAT TRACK (N6) LT UNDER THRESHOLD PAX DOOR 4 LT REMOVE THRESHOLD PLATE AND DRAIN VALVES ON DOOR NR 4 LT OK DONE AS AMM 53-10-01, REV 81. REM
- [SDR CNMA20090054](https://openairdocs.org/sdr/CNMA20090054), Aug 8, 2008: SKIN. DENTED. DENT ON FUSELAGE SKIN STA 729 - LONGERON 43. PERFORM REPAIR IAW SRM 53-20-00 FIG SH3, REV 45, VOL I, OK PERFORM REPAIR AS REQUIRED.
- [SDR CNMA20090053](https://openairdocs.org/sdr/CNMA20090053), Aug 8, 2008: FLOORBEAM. CORRODED. CORROSION ON FLOOR SUPPORT AT STA 815 X19. FABRICATED AND INSTALLED NEW PN ADA7326-1 IAW DWG ADA7326 AND 7548 AND SRM 51-35-01, STEP 1, VOL II, REV 94.
- [SDR CNMA20090052](https://openairdocs.org/sdr/CNMA20090052), Aug 8, 2008: FLOORBEAM. CORRODED. LIGHT CORROSION ON FLOORBEAM AT STA 859 X-72. REMOVED CORROSION IAW SRM 51-21-01, ERV 94, VOL II OUT OF LIMITS. REPLACED PN ADD 7160-2 IAW SRM 51-35-01, VOL II,
- [SDR CNMA20090051](https://openairdocs.org/sdr/CNMA20090051), Aug 8, 2008: FLOORBEAM. CORRODED. CORROSION ON FLOOR SUPPORT TEE AT AFTER PRESSURE BULKHEAD, STA 2007. X-40 - X-60, AND X 20. PERFORMED REPAIR IAW SRM 53-40-00, FIG 16, REF 94, VOL I.
- [SDR CNMA20090050](https://openairdocs.org/sdr/CNMA20090050), Aug 8, 2008: SUPPORT. CRACKED. GALLEY SUPPORT CORRODED AT STA 459 XX24. REPLACED PN ACA7366-501 IAW DWG ACA7365 AND SRM51-35-01, VOL II, REV 94.
- [SDR CNMA20090049](https://openairdocs.org/sdr/CNMA20090049), Aug 8, 2008: FITTING. CORRODED. CORROSION ON FITTING GALLEY AT STA 879, X44. REMOVED CORROSION IAW SRM 51-21-24 VOL II, REV 94 WITHOUT LIMITS DEPTH MATERIAL REMOVED 3.5 MM. FABRICATED PN AWD77
- [SDR CNMA20090048](https://openairdocs.org/sdr/CNMA20090048), Aug 8, 2008: FLOORBEAM. CORRODED. LIGHT CORROSION ON FLOOR SUPPORT AT STA 815 X-18. FABRICATED AND INSTALLED NEW PN ADA7326-1 IAW DWG 7696 AND ADA7548 AND SRM 51-35-01 STEP 1, VOL II REV 94.
- [SDR CNMA20090047](https://openairdocs.org/sdr/CNMA20090047), Aug 8, 2008: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT AT STA 859 - 893 X73. REPLACED PN ADA7160-1 IAW DWG ADA7160 AND DWG 7163 AND MM 20-50-02 REV 81.
- [SDR CNMA20090046](https://openairdocs.org/sdr/CNMA20090046), Aug 8, 2008: FLOOR SUPPORT. CORRODED. LIGHT CORROSION ON FLOORBEAM SUPPORT BETWEEN STA 1820-1887 X36. REMOVED BEAM IAW SRM 51-31-01 VOL II REV 94. FABRICATED PN AGA7085-1 ED INSTALLED IAW DWG ASA 71
- [SDR CNMA20090045](https://openairdocs.org/sdr/CNMA20090045), Aug 8, 2008: TRACK. CORRODED. FOUND CORROSION ON DOWN TRACK AT STA 1871-2007 AND X=107.25. REMOVED CORROSION IAW SRM 51-21-01 V II REV 94 DIMENSIONS OUT OF LIMITS (120 X 50 X 2,3 MM). REPLAC
- [SDR CNMA20090044](https://openairdocs.org/sdr/CNMA20090044), Aug 8, 2008: TRACK. CORRODED. FOUND CORROSION ON DOWN TRACK AT STA 1902 - 2007 AND X=75.25. CORROSION REMOVED IAW SRM 51-21-01 V G REV 94 DIMENTIONS ARE OUT OF LIMITS (240 X 8T X 2,4 MM) FAB
- [SDR CNMA20090043](https://openairdocs.org/sdr/CNMA20090043), Aug 8, 2008: TRACK. CORRODED. FOUND CORROSION ON DOWN TRACK AT STA 1887-2007 AND X=27.50. REMOVED BEAM IAW SRM 51-31-01, VOL II, REV 94 AND MM 20-50-02 REV 81. FABRICATED PN ASA7087-1 IAW DW
- [SDR CNMA20090041](https://openairdocs.org/sdr/CNMA20090041), Aug 8, 2008: SKIN. CRACKED. HFEC INSP ON HS IAW J/C 10AD-904 SB 455-18. FOUND ONE CRACK INDICATION 37MM LENGTH ON OUTER SECTION UPPER AFTER SKIN PANEL RT SIDE. PERFORMED STOP DRILL AS REQU
- [SDR CNMA20090042](https://openairdocs.org/sdr/CNMA20090042), Aug 8, 2008: CARGO TRACK. CORRODED. FOUND CORROSION ON DOWN TRACK AT STA 1931.500 -2007 AND X=8.50. REMOVED BEAM IAW SRM 51-31-01 VOL I REV 94 AND MM 20-50-02 REV 81. FABRICATED PN AGA7088-1 IAW D
- [SDR CNMA20090041A](https://openairdocs.org/sdr/CNMA20090041A), Aug 8, 2008: DOOR FRAME. CRACKED. FWD CARGO NEAR DOOR JAMB PANEL NR 127AR CRACKED. REMOVED PANEL 127AR AMM 20-50-02 REV 81. WELD PER DPS 10225 INSTALLED PANEL 127AR IAW MM 20-50-02 REV 81.
- [SDR CNMA20090040](https://openairdocs.org/sdr/CNMA20090040), Aug 8, 2008: STIFFENER. CORRODED. CTR WHEEL WELL AFT CLOSING BULKHEADS WITH A STIFFENER CORRODED. REPLACED PN AYB7080-9, REF DWG BOE AYB 7080 IAW SRM 51-35-01, REV 94, VOL I, STEP 9.
- [SDR CNMA20090039](https://openairdocs.org/sdr/CNMA20090039), Aug 8, 2008: SUPPORT. CORRODED. NR 2 GALLEY SUPPORT CORRODED AT STA 465 RT AND LT SIDE. REMOVED CORROSION IAW SRM 51-21-01, VOL II, REV 94 WITHOUT LIMITS DEPTH MATERIAL REMOVED 4 MM. FABRICATE
- [SDR CNMA20090038](https://openairdocs.org/sdr/CNMA20090038), Aug 8, 2008: SUPPORT. CORRODED. NR 2 GALLEY SUPPORT CORRODED AT STA 435, RT AND LT SIDE. REMOVED CORROSION IAW SRM 51-21-01, VOL II, REV 94 WITHOUT LIMITS DEPTH MATERIAL REMOVED 3 MM. FABRICAT
- [SDR CNMA20090037](https://openairdocs.org/sdr/CNMA20090037), Aug 8, 2008: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT BETWEEN STA 440 / 453, XO. FABRICATED AND INSTALLED NEW PN ACA7374-1 IAW DWG ACA7374 AND 7365 AND SRM 51-35-01 V I REV 94 STEP 1.
- [SDR CNMA20090036](https://openairdocs.org/sdr/CNMA20090036), Aug 8, 2008: SUPPORT. CRACKED. CTR CARGO DOOR EXTERNAL FAIRING SUPPORT CRACKED (AFT POSITION). PERFORM REPAIR IAW SRM 53-00-01, FIG 8, SHEET 2, REV 94.
- [SDR CNMA20090035](https://openairdocs.org/sdr/CNMA20090035), Aug 8, 2008: FLOORBEAM. CRACKED. CTR CARGO COMPT, FLOOR STRUCTURE, AT STA 1523 (FWD BULKHEAD) NR 4 ANGULARS CRACKED. OPEN PANELS 183JE-183FE FWD BULKHEAD CTR CARGO COMPARTMENT IAW AMM 20-50-02 
- [SDR CNMA20090034](https://openairdocs.org/sdr/CNMA20090034), Aug 8, 2008: FLOOR SUPPORT. CRACKED. AFT CARGO COMPT FLOOR SUPPORT STRUCTURE AT STA 1921 LT SIDE ANGULAR CRACKED. PERFORMED REPAIR IAW SRM 53-00-01, FIG 8, SHT 1, REV 94 (VOL I).
- [SDR CNMA20090033](https://openairdocs.org/sdr/CNMA20090033), Aug 8, 2008: PANEL. DAMAGED. PYLON NR 2 PANEL, 457BT DAMAGED. REPAIRED IAW SRM 54-00-01, FIG 1A SHEET 1 REV 94 VOL J.
- [SDR CNMA20090032](https://openairdocs.org/sdr/CNMA20090032), Aug 8, 2008: BEAM. CRACKED. CTR CARGO COMP STA 1781 NR 3 LT BEAM OF ZONE PLENUM CRACKED. REMOVED BEAM IAW MM 20-50-02 REV 81. PERFORMED DRILL NEW BEAM IAW DWG AF)7011-3. REPLACED BEAM IAW 
- [SDR CNMA20090031](https://openairdocs.org/sdr/CNMA20090031), Aug 8, 2008: FLOORBEAM. CRACKED. CTR CARGO COMP FLOOR UNLOAD BEAM CRACKED AT STA 1690 (UPPER FLANGE) PERFORMED REPAIR IAW SRM 53-70-00 FIG 3 REV 93 VOL J. PERFORMED PAINTING IAW SRM 51-21-02 VO
- [SDR CNMA20090030](https://openairdocs.org/sdr/CNMA20090030), Aug 8, 2008: STRUCTURE. CRACKED. RT OTBD FLAP INBD RIB CLOSURE HAS AN ANGULAR CRACK. REMOVED RT OTBD FLAP, INBD T/E SECTION. REMOVED ALL SCREWS SIZED IAW SRM 51-31-01 VOL 2 REV 93. REMOVED RT O
- [SDR CNMA20090029](https://openairdocs.org/sdr/CNMA20090029), Aug 8, 2008: PANEL. CRACKED. LT OTBD FLAP, OTBD HINGE PANEL 526JL, CRACKED. PERFORMED REPAIR IAW SRM 57-00-01, FIG 10.
- [SDR CNMA20090025](https://openairdocs.org/sdr/CNMA20090025), Aug 8, 2008: PANEL. CRACKED. LT WING OTBD FLAP INBD HINGE PANEL 535DL CRACKED. PERFORMED REPAIR IAW SRM 57-00-01, FIG 4, SH1, VOL I, REV 94.
- [SDR CNMA20090028](https://openairdocs.org/sdr/CNMA20090028), Aug 8, 2008: SUPPORT. CRACKED. LT OTBD FLAP, INBD HINGE STRUCTURE UNDER PANEL 535JL, SUPPORT CRACKED. REPLACED SUPPORTS CRACKED UNDER PANEL 535JL IAW SRM 51-35-01 VOL II REV 93.
- [SDR CNMA20090027](https://openairdocs.org/sdr/CNMA20090027), Aug 8, 2008: PANEL. CRACKED. LT OTBD FLAP, INBD HINGE PANEL 535JL CRACKED. REMOVED EXISTING REPAIR IAW SRM 51-31-01 VII PERFORMED WELD IAW DPS10225. REINSTALLED OLD REPAIR IAW SRM 51-35-02 
- [SDR CNMA20090026](https://openairdocs.org/sdr/CNMA20090026), Aug 8, 2008: PANEL. DELAMINATED. LT INBD FLAP, OTBD HINGE, PANEL 541JL UNGLUED. PERFORMED REPAIR IAW DWG ARC 2541.
- [SDR CNMA20090024](https://openairdocs.org/sdr/CNMA20090024), Aug 8, 2008: PANEL. CRACKED. LT WING OTBD FLAP INBD HINGE PANEL 535DL CRACKED. PERFORMED REPAIR IAW SRM 57-00-01, FIG 4, SH1, VOL I, REV 94.
- [SDR CNMA20090023](https://openairdocs.org/sdr/CNMA20090023), Aug 8, 2008: STRUCTURE. DENTED. DENT AT STA 1853.93 LONG 47 REPAIR NEXT C CHK. PERFORMED SANDING AS REQUESTED AS DPS 9.316. PERFORMED REPAIR IAW SRM 53-20-00, FIG 6 (SHT 3) V.I. REV 93. PERFOR
- [SDR CNMA20090022](https://openairdocs.org/sdr/CNMA20090022), Aug 8, 2008: SKIN. DENTED. DENT 30 INCH, FWD OF R1 DOOR SILL - DENT 6 INCH LONG WITHIN LIMITS IAW SRM VOL I-53-20-00 PERFORM PERMANENT REPAIR. REMOVED DUCT IAW 20-50-02 AND MANIFOLD AIR C
- [SDR CNMA20090021](https://openairdocs.org/sdr/CNMA20090021), Aug 8, 2008: SKIN. DENTED. UNDER RT PITOT TUBE HAS FUSELAGE DENT PERFORM PERMANENT REPAIR. REMOVED ELECTRICAL EQUIPMENT TO ACCESS ZONE. REMOVE BRACKET AS AMM 77-13-01 (TRANSDUCER NOT INST

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