# N907AX: 1968 Douglas DC-9-31, registration cancelled 2009-08-28 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 28, 2009 - Status when cancelled: Sale reported - Airframe: [Douglas DC-9-31](https://openairdocs.org/model/douglas-dc-9-31) (registry code 3022065) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 47203 - Year built: 1968 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: August 2, 1982 - Last registry action: August 28, 2009 - Mode S code: AC8943 - Location: [Guthrie, OK](https://openairdocs.org/faa-place/OK/Guthrie) - Owner type: Individual - Owner's area on the map: 35.8679° N, 97.4344° W: Placed by OpenAirDocs at the center of ZIP code 73044, within about 9 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N907AX - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=907AX - Page: https://openairdocs.org/deregistered/N907AX-2009-08-28 From the FAA registry file of October 28, 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 Douglas DC-9-31: https://openairdocs.org/model/douglas-dc-9-31.md ## Service difficulty reports (88, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ABXA070307](https://openairdocs.org/sdr/ABXA070307), Aug 10, 2007: INTERCOSTAL. CORRODED. AFT LOWER CARGO INTERCOSTAL WAS CORRODED AT THE NUT PLATES AND ON THE UPPER SURFACE BETWEEN STA 980 AND 996 AT LONGERON 28 LEFT. REMOVED AND REPLACED INTERCOSTA - [SDR ABXA070286](https://openairdocs.org/sdr/ABXA070286), Aug 10, 2007: INTERCOSTAL. CORRODED. AFT LOWER CARGO INTERCOSTAL WAS CORRODED AT THE NUT PLATES AND ON THE UPPER SURFACE BETWEEN STA 980 AND 996 AT LONGERON 28 LEFT. REMOVED AND REPLACED INTERCOSTA - [SDR ABXA070306](https://openairdocs.org/sdr/ABXA070306), Aug 7, 2007: SKIN. CORRODED. LEFT FLAP UPPER OUTBOARD SURFACE HAD SKIN BULGING AND CUPPED RIVETS. REMOVED SEGMENT FOR REPAIR AND REINSTALLED IAW DC9 SRM 51-30-1. - [SDR ABXA070285](https://openairdocs.org/sdr/ABXA070285), Aug 7, 2007: SKIN PANEL. CORRODED. LEFT FLAP UPPER OUTBOARD SURFACE HAD SKIN BULGING AND CUPPED RIVETS. REMOVED FLAP SEGMENT FOR REPAIR AND REINSTALLED IAW DC9 SRM 51-30-1. - [SDR ABXA050205](https://openairdocs.org/sdr/ABXA050205), Aug 24, 2005: ROD END. WORN. LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. PLACED GEAR LEVER IN UPLATCH CHECK POSITION AND GEAR DOOR OPEN LIGHT CAME ON. RECYCLED GEAR AND B - [SDR ABXA050204](https://openairdocs.org/sdr/ABXA050204), Aug 24, 2005: DOWNLOCK SWITCH. DEFECTIVE. LEFT MAIN GEAR UNSAFE LIGHT STAYED ON AFTER GEAR RETRACTION, RECYCLED GEAR AND GEAR UNSAFE LIGHT WENT OUT. FOUND NR 5 PIN ON DOWNLOCK SWITCH DIRTY, CLEANED RECE - [SDR ABXA050224](https://openairdocs.org/sdr/ABXA050224), Jul 26, 2005: FRAME. CRACKED. SHEAR TIE CRACKED FS 1087, LONGERON 2 RIGHT. REMOVED AND REPLACED SHEAR TIE IAW DC-9 SRM 51-30-5. - [SDR ABXA050181](https://openairdocs.org/sdr/ABXA050181), Jul 26, 2005: FITTING. CRACKED. AFT LOWER BAG BIN DOOR NR 1 BEAM FORWARD END FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1. - [SDR ABXA050180](https://openairdocs.org/sdr/ABXA050180), Jul 25, 2005: FRAME. CRACKED. LONGERON 23 LEFT CRACKED AT FRAME, FS 200. REPAIRED AREA IAW DC-9 SRM 53-02. - [SDR ABXA050223](https://openairdocs.org/sdr/ABXA050223), Jul 24, 2005: SKIN. CORRODED. SKIN LONGERON 30, FS 680 TO FS 737 WAS CORRODED. BLENDED CORROSION AND REPAIRED DAMAGED AREAS IAW DC-9 SRM. - [SDR ABXA050144](https://openairdocs.org/sdr/ABXA050144), Jun 6, 2005: ANNUNCIATOR. MALFUNCTIONED. AFTER EMERGENCY POWER CHECK, LOWER CARGO FIRE, TAIL COMP TEMP HIGH, APU FIRE, AND DC EMERGENCY BUSS OFF LIGHTS ILLUMINATED. REMOVED AND REPLACED ANNUNCIATOR PAN - [SDR ABXA030457](https://openairdocs.org/sdr/ABXA030457), Nov 19, 2003: INTERCOSTAL. CRACKED. INTERCOSTAL CRACKED AT STA 389 BUTTLINE XERO AT FLOORBEAM ATTACH POINT. REPAIRED IAW DC-9 SSRM DWG K05159. - [SDR ABXA030456](https://openairdocs.org/sdr/ABXA030456), Nov 14, 2003: FITTING. CRACKED. LONGERON 29 LEFT END FITTING CRACKED ON OUTBOARD SIDE FS 756. REPAIRED LONGERON 29 LEFT AT STA 756 IAW DC-9 SRM 53-02. - [SDR ABXA030455](https://openairdocs.org/sdr/ABXA030455), Nov 14, 2003: FITTING. CRACKED. LONGERON 29 RIGHT END FITTING CRACKED ON OUTBOARD SIDE FS 756. REPAIRED LONGERON 29 RIGHT AT STA 756 IAW DC-9 SRM 53-02. - [SDR ABXA030454](https://openairdocs.org/sdr/ABXA030454), Nov 14, 2003: FRAME. CORRODED. LEVEL II CORROSION OF FRAME FS 218, LONGERON 28 LT. REMOVED DAMAGED FRAME AND INSTALLED NEW SECTION OF FRAME STA 218, LONGERON 26 LT LONGERON 26 RT IAW DC-9 SRM - [SDR ABXA030453](https://openairdocs.org/sdr/ABXA030453), Nov 14, 2003: FITTING. CRACKED. LT MLG WW OUTBOARD APPROXIMATELY FS 730 SUPPORT BRACKET CRACKED FOR UPPER INBOARD BONDED PANEL LINK. REPLACED FITTING IAW DC-9 SRM 51-30-1. - [SDR ABXA010886](https://openairdocs.org/sdr/ABXA010886), May 20, 2002: SWITCH. DEFECTIVE. DURING INITIAL GEAR EXTENSION, THE NOSE LANDING GEAR LIGHT FLICKERED ON AND OFF AND CONTINUED TO DO SO UNTIL THE GEAR WAS RAISED. FOUND NOSE LANDING GEAR DOWN L - [SDR ABXA010814](https://openairdocs.org/sdr/ABXA010814), Apr 2, 2002: FITTING. CRACKED. NR 6 TEE CRACKED APPROXIMATELY 1 INCH LONG AT LONGERON 14. REPLACED THE NR 6 TEE IAW DC-9 SRM. - [SDR ABXA010815](https://openairdocs.org/sdr/ABXA010815), Apr 1, 2002: CONTROL COLUMN. CRACKED. CAPTAIN'S CONTROL COLUMN SHOWED CRACK INDICATIOIN AND WAS BLENDED BEYOND LIMITS. REPLACED CAPTAIN'S CONTROL COLUMN IAW DC-9 SRM 51-30-1 AND 51-30-2. - [SDR ABXA000378](https://openairdocs.org/sdr/ABXA000378), Aug 3, 2000: FITTING. CRACKED. NR 5 SLAT OUTBOARD ATTACH FITTING WAS CRACKED. REPLACED NR 5 SLAT IAW DC9 MM 27-80-1. - [SDR ABXA000377](https://openairdocs.org/sdr/ABXA000377), Jul 27, 2000: SKIN. CRACKED. LEFT WING NR 4 SLAT END FITTING WAS CRACKED. REPLACED NR 4 SLAT IAW DC9 MM 27-80-01. - [SDR ABXA000386](https://openairdocs.org/sdr/ABXA000386), Jul 26, 2000: PAN. CRACKED. LEFT MAIN LANDING GEAR DOOR WAS CRACKED IN UPPER FORWARD DOOR PAN. REPLACED PAN IAW DC9 SRM 53-30-2. - [SDR ABXA000376](https://openairdocs.org/sdr/ABXA000376), Jul 26, 2000: PAN. CRACKED. RIGHT MAIN LANDING GEAR DOOR HAD CRACK IN UPPER PAN. REPLACED RIGHT MAIN GEAR DOOR IAW DC9 SRM 51-30-2. - [SDR ABXA000383](https://openairdocs.org/sdr/ABXA000383), Jul 19, 2000: FITTING. CRACKED. HORIZONTAL STABILIZER BOX SECTION FITTING CRACKED AT PANEL NR 3902. REPLACED FITTING IAW DC9 SRM. - [SDR ABXA000385](https://openairdocs.org/sdr/ABXA000385), Jul 18, 2000: DOUBLER. CRACKED. FORWARD LOWER CARGO DOOR LOWER INNER PAN ANGLE DOUBLER CRACKED. REPLACED ANGLE IAW DC9 SSRM DWG K05159. - [SDR ABXA000374](https://openairdocs.org/sdr/ABXA000374), Jul 13, 2000: STRUCTURE. CORRODED. RIGHT ELEVATOR CENTER SECTION HAD INTERIOR STRUCTURE CORROSION. REPLACED RIGHT ELEVATORIAW DC9 SRM 51-10-1. - [SDR ABXA000384](https://openairdocs.org/sdr/ABXA000384), Jul 11, 2000: FITTING. CRACKED. AFT LOWER CARGO DOOR UPPER AFT INTERCOSTAL TEE FITTING CRACKED AT UPPER AFT DOOR STOP. REPLACED TEE-FITTING. - [SDR ABXA000379](https://openairdocs.org/sdr/ABXA000379), Jul 11, 2000: WEB. CRACKED. LEFT WING TRAILING EDGE WEB, FORWARD OF AILERON, CRACKED APPROXIMATELY TWO INCHES FROM OUTBOARD EDGE. - [SDR ABXA000375](https://openairdocs.org/sdr/ABXA000375), Jul 11, 2000: PAN. CRACKED. FORWARD LOWER CARGO DOOR OUTER PAN WAS CRACKED AT DOOR STOPS NR 1, 12, 13 AND 14. REPLACED DOOR IAW DC9 SRM. - [SDR ABXA000387](https://openairdocs.org/sdr/ABXA000387), Jul 10, 2000: SKIN. CRACKED. AFT CARGO COMPARTMENT DOOR SKIN CRACKED. REPAIRED DOOR IAW DC9 SRM 52-01. - [SDR ABXA9801200](https://openairdocs.org/sdr/ABXA9801200), Dec 28, 1998: CLIP. CRACKED. DURING C-CHECK, FOUND STATION 996 RIGHT FUSELAGE FRAME ATTACH FOOT CLIP CRACKED. REPLACED CLIP IAW DC9 SRM 51-30-5. - [SDR ABXA9801199](https://openairdocs.org/sdr/ABXA9801199), Dec 28, 1998: SHEAR TIE. CRACKED. DURING C-CHECK, FOUND CRACKED SHEAR TIE AT STATION 980, BELOW LONGERON 14 LEFT. REPLACED SHEAR TIE IAW DC9 SRM 51-30-2 AND 51-30-5. - [SDR ABXA9801198](https://openairdocs.org/sdr/ABXA9801198), Dec 28, 1998: CLIP. CRACKED. DURING C-CHECK, FOUND CRACKED SHEAR CLIP AT RIGHT WING STATION XRS 69.00 AT AFT BOTTOM. REPLACED SHEAR CLIP IAW DC9 SRM 51-10-04. - [SDR ABXA9801194](https://openairdocs.org/sdr/ABXA9801194), Dec 28, 1998: FRAME. CRACKED. DURING C-CHECK, FOUND LEFT FUSELAGE MAIN FRAME AT STATION 718 CRACKED. REPLACED MAIN FRAME IAW DC9 SRM 51-2-0. - [SDR ABXA9801204](https://openairdocs.org/sdr/ABXA9801204), Dec 22, 1998: FRAME. CRACKED. DURING C-CHECK, FOUND FUSELAGE FRAME AT STATION 699 CRACKED AT LONGERON 16 RIGHT. REPLACED MAIN FRAME IAW DC9 SRM 53-13-1. - [SDR ABXA9801203](https://openairdocs.org/sdr/ABXA9801203), Dec 22, 1998: FLOORBEAM. CORRODED. DURING C-CHECK, FOUND STATION 218 FLOORBEAM CORRODED AT BL 22 RIGHT. REPAIRED IAW ABX REA D953-25916. - [SDR ABXA9801202](https://openairdocs.org/sdr/ABXA9801202), Dec 22, 1998: FITTING. CRACKED. DURING C-CHECK, FOUND CRACKED FLOOR SUPPORT FITTING AT STATION 945 INBOARD OF LONGERON 27 RIGHT. REPLACED FITTING IAW DC9 SRM 51-30-5. - [SDR ABXA9801197](https://openairdocs.org/sdr/ABXA9801197), Dec 22, 1998: LONGERON. CRACKED. DURING C-CHECK, FOUND CRACK IN LONGERON 16 RIGHT AT STATION 965. REPAIRED IAW DC9 SRM 53-02-0. - [SDR ABXA9801196](https://openairdocs.org/sdr/ABXA9801196), Dec 22, 1998: FITTING. CRACKED. DURING C-CHECK, FOUND CRACKED FLOOR SUPPORT FITTING AT STATION 945, BETWEEN 27 AND 28 LEFT. REPLACED FITTING IAW DC9 SRM 51-30-5. - [SDR ABXA9801195](https://openairdocs.org/sdr/ABXA9801195), Dec 22, 1998: WEB. CRACKED. DURING C-CHECK, FOUND LEFT CUSP WEB AT STATION 890 CRACKED. REPLACED CUSP WEB IAW DC9 SRM 51-30-2. - [SDR ABXA9701573](https://openairdocs.org/sdr/ABXA9701573), Oct 8, 1997: BATTERY. DISCHARGED. COCKPIT EMERGENCY LIGHTS WERE DIM. REPLACED EMERGENCY LIGHT BATTERIES IAW DC9 MM 33-53-0. OPS CHECKED GOOD. - [SDR ABXA9701257](https://openairdocs.org/sdr/ABXA9701257), Jul 15, 1997: BATTERY. DISCHARGED. DURING TEST, EMERGENCY LIGHTS WERE VERY DIM. REPLACED BATTERY. - [SDR ABXA9700438](https://openairdocs.org/sdr/ABXA9700438), Mar 28, 1997: BRACKET. CORRODED. DURING C-CHECK, THE LEFT AILERON PULLEY BRACKET IN THE LEFT WHEEL WELL WAS CORRODED. THE PULLEY BRACKET WAS REPLACED. - [SDR ABXA9700480](https://openairdocs.org/sdr/ABXA9700480), Mar 25, 1997: VANE. DELAMINATED. DURING C-CHECK, FOUND FLAP CENTER VANE DELAMINATED. REPLACED VANE IAW DC9 MM. - [SDR ABXA9700442](https://openairdocs.org/sdr/ABXA9700442), Mar 25, 1997: FRAME. CRACKED. DURING C-CHECK, THE FUSELAGE MAIN FRAME AT STATION 658 LEFT WAS FOUND CRACKED. REPAIRED MAIN FRAME IAW REA D953-18858-MR. - [SDR ABXA9700437](https://openairdocs.org/sdr/ABXA9700437), Mar 25, 1997: ANGLE. CRACKED. DURING C-CHECK, THE CENTER WING FLOOR SUPPORT ANGLE AT STA 658 LBL 44 WAS FOUND CRACKED. REPLACED ANGLE. - [SDR ABXA9700436](https://openairdocs.org/sdr/ABXA9700436), Mar 25, 1997: ANGLE. CRACKED. DURING C-CHECK, FOUND CENTER WING FLOOR SUPPORT ANGLE, STA 650 CRACKED. REPLACED ANGLE IAW DC9 SRM. - [SDR ABXA9700994](https://openairdocs.org/sdr/ABXA9700994), Mar 24, 1997: VANE. DELAMINATED. LEFT HAND FLAP, CENTER, FIXED VANE DELAMINTED ON TOP. REPAIRED 3 DELAMINATED AREA ON UPPER SURFACE IAW DC9 SRM. - [SDR ABXA9700439](https://openairdocs.org/sdr/ABXA9700439), Mar 24, 1997: FITTING. CORRODED. DURING C-CHECK, FOUND CENTER FLAP HINGE ATTACH FORWARD FITTING CORRODED. REPLACED FITTING IAW DC9 MM. - [SDR ABXA9700435](https://openairdocs.org/sdr/ABXA9700435), Mar 24, 1997: PAN. CRACKED. DURING C-CHECK, FOUND LANDING GEAR INBOARD DOOR FORWARD PAN CRACKED. REPLACED PAN IAW DC9 SRM. All 88: https://openairdocs.org/deregistered/N907AX-2009-08-28/reports.md ## Other aircraft with N907AX - [Registered now](https://openairdocs.org/aircraft/N907AX): Cort J Neuman APEX, S/N 1, built 2022 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.