# N906AX: 1968 Mcdonnell Douglas DC-9-31, registration cancelled 2009-11-18

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 18, 2009
- Status when cancelled: Valid registration
- Airframe: [Mcdonnell Douglas DC-9-31](https://openairdocs.org/model/mcdonnell-douglas-dc-9-31) (registry code 302206A)
- Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs)
- Serial number: 47072
- Year built: 1968
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Standard, transport
- Airworthiness date: June 2, 1982
- Last registry action: November 18, 2009
- Mode S code: AC858C
- Owner when cancelled: [Stewart Industries International LLC](https://openairdocs.org/faa-owner/STEWART%20INDUSTRIES%20INTERNATIONAL%20LLC)
- Location: [Guthrie, OK](https://openairdocs.org/faa-place/OK/Guthrie)
- Owner type: Corporation
- 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/N906AX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=906AX
- Page: https://openairdocs.org/deregistered/N906AX-2009-11-18

From the FAA registry file of October 29, 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-9-31: https://openairdocs.org/model/mcdonnell-douglas-dc-9-31.md

## Service difficulty reports (176, newest 50)

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

- [SDR ABXA080056](https://openairdocs.org/sdr/ABXA080056), Feb 14, 2008: CONTROLLER. DEFECTIVE. ON GROUND AT ALB, NOTED HEAVY ODOR OF BURNING ELECTRICAL EQUIPMENT. AIRED OUT COCKPIT, CLOSED UP AGAIN AND SMELL RETURNED WITHIN TWO MINUTES. FOUND SMELL COMING
- [SDR ABXA070349](https://openairdocs.org/sdr/ABXA070349), Oct 16, 2007: BATTERY PACK. DEFECTIVE. EMERGENCY EVACUATION LIGHTS WOULD NOT TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00-8.
- [SDR ABXA070234](https://openairdocs.org/sdr/ABXA070234), Jun 20, 2007: CUSP WEB. CRACKED. CUSP WEB CRACKED AFT OF FS 313, RIGHT BUTT LINE 56. REPAIRED CUSP WEB AT FS 315 IAW DC9 SRM 53-01.
- [SDR ABXA070233](https://openairdocs.org/sdr/ABXA070233), Jun 19, 2007: ANGLE. CRACKED. SUBFLOOR ANGLE WAS CRACKED FORWARD END LEFT BUTT LINE FS 996. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-2.
- [SDR ABXA070231](https://openairdocs.org/sdr/ABXA070231), Jun 15, 2007: FLOORBEAM. CORRODED. FLOORBEAM AT STA 313, FORWARD SIDE UNDER CUSP WEB HAD CORROSION AROUND NUT PLATE. REPAIRED DAMAGED AREA IAW DC9 SRM K05159.
- [SDR ABXA070228](https://openairdocs.org/sdr/ABXA070228), Jun 13, 2007: CUSP WEB. CORRODED. FRAME FOOT AND CUSP WEB CORRODED -3/3, RIGHT. REPAIRED DAMAGED AREA IAW DC9 SRM 53-01.
- [SDR ABXA070227](https://openairdocs.org/sdr/ABXA070227), Jun 13, 2007: ATTACH FITTING. CORRODED. FRAME FOOT AND CUSP WEB CORRODED. REMOVED AND REPLACED FRAME FITTING AND REMOVED CORROSION FROM CUSP WEB IAW DC9 SRM.
- [SDR ABXA070230](https://openairdocs.org/sdr/ABXA070230), Jun 13, 2007: ATTACH FITTING. CORRODED. FRAME FOOT CORRODED - 832 LEFT. REMOVED AND REPLACED FS 832 LEFT FRAME FOOT IAW DC9 SRM.
- [SDR ABXA070229](https://openairdocs.org/sdr/ABXA070229), Jun 13, 2007: SHEAR TIE. CRACKED. SHEAR TIE CRACKED -945 RIGHT, JUST ABOVE LONGERON 16 RIGHT. REMOVED AND REPLACED SHEAR TIE STA 945 IAW DC9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA070224](https://openairdocs.org/sdr/ABXA070224), Jun 12, 2007: MEMBRANE. CRACKED. SUBFLOOR CRACKED AT STA 120 AROUND BUTT LINE 0. REPAIRED SUBFLOOR IAW DC9 SRM.
- [SDR ABXA070226](https://openairdocs.org/sdr/ABXA070226), Jun 12, 2007: ANGLE. CRACKED. AFT PRESSURE BULKHEAD ANGLE AT THRESHOLD WAS CRACKED. REMOVED AND REPLACED ANGLE IAW DC9 SRM 51-30-5.
- [SDR ABXA070225](https://openairdocs.org/sdr/ABXA070225), Jun 11, 2007: FITTING. CRACKED. UPPER SECTION OF AFT PRESSURE BULKHEAD LEFT SIDE HAD A CRACK UNDER HORIZONTAL STIFFENER NR 6. REMOVED AND REPLACED CLIP IAW DC9 SRM 51-30-5 AND 51-30-2.
- [SDR ABXA070223](https://openairdocs.org/sdr/ABXA070223), Jun 11, 2007: ATTACH FITTING. CRACKED. RIGHT WHEEL WELL BULKHEAD TO KEEL ATTACH FITTING CRACKED. REMOVED AND REPLACED ATTACH FITTING IAW DC9 SRM.
- [SDR ABXA070222](https://openairdocs.org/sdr/ABXA070222), Jun 11, 2007: ATTACH ANGLE. CORRODED. ATTACH ANGLE LEFT WHEEL WELL, STA 699, LEFT BUTT LINE 54, ADJACENT TO SLANT PANEL HAD EVIDENCE OF CORROSION. REMOVED AND REPLACED ATTACH ANGLE IAW DC9 SRM 51-30
- [SDR ABXA070221](https://openairdocs.org/sdr/ABXA070221), Jun 8, 2007: FITTING. CRACKED. FLOORBEAM SUPPORT UPPER END FITTING CRACKED, 965 LEFT SIDE. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.
- [SDR ABXA070220](https://openairdocs.org/sdr/ABXA070220), Jun 8, 2007: BULKHEAD. CRACKED. AFT PRESSURE BULKHEAD DOOR CUTOUT AFT LOWER RIGHT CORNER HAD 2 EACH CRACKS. ONE CRACK WAS 2 INCHES AND ONE WAS 1.25 INCH. ONE IN ORIGINAL DOUBLER P/N: 5910130-8
- [SDR ABXA070219](https://openairdocs.org/sdr/ABXA070219), Jun 8, 2007: BULKHEAD. CRACKED. AFT PRESSURE BULKHEAD DOOR CUTOUT AFT LOWER LEFT CORNER HAD 2 EACH CRACKS. ONE CRACK WAS 1.250 INCH AND ONE WAS .75 INCH. ONE IN ORIGINAL DOUBLER P/N: 5910130-8
- [SDR ABXA070232](https://openairdocs.org/sdr/ABXA070232), Jun 5, 2007: FLOORBEAM. CORRODED. FLOORBEAM AT FS 275, RIGHT BUTT LINE 44.5 HAD CORROSION AT GROUNDING STUD. REPAIRED AREA IAW DC9 SRM 53-05.
- [SDR ABXA070025](https://openairdocs.org/sdr/ABXA070025), Jan 25, 2007: OUTFLOW VALVE. FROZEN. DURING CLIMB, CABIN WOULD NOT PRESSURIZE, DID ABNORMAL. COULD NOT PRESSURIZE MANUALLY EITHER. CABIN PRESSURE CONTROL WHEEL JAMMED. DUE TO COLD WEATHER, SUSPECT 
- [SDR ABXA060155](https://openairdocs.org/sdr/ABXA060155), Mar 30, 2006: WIRE. BROKEN. CREW REPORTED ELECTRICAL SMELL IN COCKPIT AT ALTITUDE. ODOR DISSIPATED WHEN COCKPIT TEMPERATURE WAS TURNED DOWN. OPERATED LT AND RT AIR CONDITIONING SYSTEMS FOR
- [SDR ABXA060088](https://openairdocs.org/sdr/ABXA060088), Feb 19, 2006: DOOR. CORRODED. DURING LINE INSPECTION OF LEFT MAIN LANDING GEAR OUTBOARD DOOR, FOUND DOOR CORRODED AND SEPARATED FROM HONEYCOMB AT FITTING STRUCTURE. REPLACED DOOR IAW DC9 MM 
- [SDR ABXA050206](https://openairdocs.org/sdr/ABXA050206), Aug 26, 2005: GYRO. DEFECTIVE. DURING CLIMB FROM YYC, CAPTAIN'S ADI HAD NUMEROUS INTERMITTENT GYRO FLAGS AND ADI WAS ERRATIC. IN CRUISE, INTERMITTENT ROLL FLAGS. REMOVED AND REPLACED NR 1 VER
- [SDR ABXA050134](https://openairdocs.org/sdr/ABXA050134), May 18, 2005: ANGLE. CRACKED. CRACKED VERTICAL ANGLE BELOW RIGHT BUTT LINE 44 TRACK AT STA 617 FLOORBEAM. REMOVED AND REPLACED ANGLE IAW DC9 SRM 51-30-5.
- [SDR ABXA050133](https://openairdocs.org/sdr/ABXA050133), May 17, 2005: FRAME. CRACKED. RIGHT CENTER MAIN FRAME AT STA 718 REQUIRES REPLACEMENT PER DC-9 SERVICE BULLETIN 53-100, PAGE 11, ITEM 1E. REMOVED AND REPLACED MAIN FRAME AT STA 718 IAW EA 53
- [SDR ABXA050131](https://openairdocs.org/sdr/ABXA050131), May 16, 2005: SUPPORT. BROKEN. FLOOR TRACK SUPPORT BROKE OFF BETWEEN LONGERON 28 RIGHT, LONGERON 27 RIGHT, AFT OF CARGO DOOR. FABRICATED NEW SUPPORT AND REPAIRED AREA IAW DC-9 SRM 51-30-2.
- [SDR ABXA050132](https://openairdocs.org/sdr/ABXA050132), May 16, 2005: WEB. CRACKED. CRACK INSIDE PYLON UNDER PANEL 8206. REPAIRED CRACK IAW DC-9 SRM 54-01.
- [SDR ABXA040201](https://openairdocs.org/sdr/ABXA040201), Jun 3, 2004: WINDSHIELD. CRACKED. FIRST OFFICER'S WINDSHIELD STARTED TO ARC AT THE LOWER RIGHT CORNER, THEN CRACKED SHORTLY THEREAFTER. AIRCRAFT MADE A DIVERSION TO STL AND MADE AN EMERGENCY LAN
- [SDR ABXA030395](https://openairdocs.org/sdr/ABXA030395), Sep 27, 2003: ATTACH FITTING. CRACKED. INBOARD RIB OF NR 5 SLAT DRIVE LINK HAD AN AFT ATTACH FITTING ATTACHED VERTICALLY TO SPAR AND RIB CRACKED IN 3 PLACES. REPAIRED ATTACH FITTING IAW DC-9 SRM 57-0
- [SDR ABXA030153](https://openairdocs.org/sdr/ABXA030153), May 15, 2003: STRUCTURE. DELAMINATED. DURING A WATCH ITEM INSPECTION, FOUND THE RIGHT AILERON TRIM TAB LOWER SURFACE DELAMINATED 10.6 SQ INCHES AND BEYOND LIMITS IAW DC-9 SRM 51-50-3, PARA 2. REPLAC
- [SDR ABXA030054](https://openairdocs.org/sdr/ABXA030054), Jan 30, 2003: SOLENOID VALVE. LEAKING. AIRCRAFT HAD STRONG JET FUEL ODOR IN COCKPIT AND CABIN AREA. FOUND FUEL SOLENOID VALVE ON APU LEAKING. REMOVED AND REPLACED ALL O-RINGS ON VALVE AND REINSTALLED
- [SDR ABXA010735](https://openairdocs.org/sdr/ABXA010735), Feb 11, 2002: DOOR FRAME. CORRODED. AFT VENTRAL DOOR JAMB AT RBL 0 TO RBL 6, LOWER SECTION, CORRODED AND TWO POPPED RIVETS. REPAIRED AREA IAW DC-9 SRM 51-70-5.
- [SDR ABXA010734](https://openairdocs.org/sdr/ABXA010734), Feb 10, 2002: SPAR. CRACKED. LEFT UPPER FORWARD SPAR WAS CRACKED AT THE INBOARD LEADING EDGE ATTACH HOLE. REPAIRED SPAR IAW DC-9 REA D957-43288MR.
- [SDR ABXA010733](https://openairdocs.org/sdr/ABXA010733), Feb 8, 2002: LONGERON. CRACKED. LONGERON 4 LEFT AT F.S. 200 WAS CRACKED. REPLACED LONGERON IAW DC-9 SRM 53-02.
- [SDR ABXA010732](https://openairdocs.org/sdr/ABXA010732), Feb 8, 2002: FITTING. CRACKED. AFT LOWER CARGO DOOR, NR 3 INTERCOSTAL BEAM FORWARD END FITTING ANGLE CRACKED. REPLACED ANGLE IAW DC-9 SRM 51-30-1 AND 51-30-5.
- [SDR ABXA010731](https://openairdocs.org/sdr/ABXA010731), Feb 8, 2002: FITTING. CRACKED. AFT LOWER CARGO DOOR, #4 INTERCOSTAL BEAM, AFT END FITTING CRACKED. REPLACED END FITTING IAW DC-9 SRM 51-30-5 AND 51-30-1.
- [SDR ABXA010730](https://openairdocs.org/sdr/ABXA010730), Feb 8, 2002: INTERCOSTAL. CRACKED. AFT LOWER CARGO DOOR, TEMPORARY REPAIR (STOP DRILL) ON INTERCOSTAL ON AFT SIDE OF LOWER DOOR STOP FITTING. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-1.
- [SDR ABXA010729](https://openairdocs.org/sdr/ABXA010729), Feb 8, 2002: PAN. CRACKED. AFT LOWER CARGO DOOR, OUTER PAN BULGED AND CRACKED AROUND BLIND NUT ON LEADING EDGE. REPAIRED AREA IAW DC-9 SERVICE REWORK DWG 5934142.
- [SDR ABXA010728](https://openairdocs.org/sdr/ABXA010728), Feb 7, 2002: TAB. DELAMINATED. RIGHT SIDE OF RUDDER TAB DELAMINATED. REPLACED RUDDER CONTROL TAB IAW DC-9 AMM 27-20-02-4-0001.
- [SDR ABXA010727](https://openairdocs.org/sdr/ABXA010727), Feb 7, 2002: VANE. DELAMINATED. INBOARD FIXED VANE WAS DELAMINATED ON LOWER SKIN AT XRS 170. REPLACED FIXED VANE IAW DC-9 SRM 27-51-02-2-0002.
- [SDR ABXA010726](https://openairdocs.org/sdr/ABXA010726), Feb 7, 2002: PANEL. DELAMINATED. LEFT WING, LOWER INBOARD BONDED PANEL HAD AREA OF DELAMINATION. REPLACED PANEL IAW DC-9 SRM 51-30-2 AND 51-30-1. SEAM SEALED PANEL IAW DC-9 SRM 51-20-6.
- [SDR ABXA010725](https://openairdocs.org/sdr/ABXA010725), Feb 6, 2002: SUPPORT FITTING. CRACKED. TWO VERTICAL SUPPORTS CRACKED, EACH SIDE OF THE RUDDER TORQUE TUBE AREA. REPLACED THE VERTICAL SUPPORT BRACKETS, RIGHT AND LEFT SIDE IAW DC-9 SRM 51-30-5.
- [SDR ABXA000319](https://openairdocs.org/sdr/ABXA000319), Jun 16, 2000: SKIN. DELAMINATED. DURING C-CHECK, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR DELAMINATED 40 SQ INCHES ON INTERIOR SIDE AND 36 SQ INCHES ON EXTERIOR SIDE. REPLACED DOOR IAW DC9 O
- [SDR ABXA000318](https://openairdocs.org/sdr/ABXA000318), Jun 16, 2000: SKIN. CORRODED. DURING C-CHECK, FOUND THE FUSELAGE INTERIOR SKIN AT THE LEFT ALTERNATE STATIC PORT CORRODED BEYOND LIMITS AT FS 342. REPAIRED SKIN IAW DC9 SRM 53-04.
- [SDR ABXA000317](https://openairdocs.org/sdr/ABXA000317), Jun 16, 2000: FRAME. CORRODED. DURING C CHECK FOUND FRAME AT STATION 218 AND LONGERON 23 LEFT CORRODED ON LOWER LEG. REMOVED CORROSION IAW DC9 SRM 51-10-3 AND REPAIRED IAW ABX SSRM DWG. K0515
- [SDR ABXA000316](https://openairdocs.org/sdr/ABXA000316), Jun 16, 2000: LONGERON. CRACKED. DURING C-CHECK, FOUND LONGERON 24 LEFT CRACKED AT STATION 180. REPLACED LONGERON IAW DC9 SRM 51-30-5.
- [SDR ABXA000315](https://openairdocs.org/sdr/ABXA000315), Jun 16, 2000: LONGERON. CRACKED. DURING C-CHECK, FOUND LONGERON 24 LEFT AT STATION 200 CRACKED. REPLACED LONGERON IAW DC9 SRM 51-30-2.
- [SDR ABXA000314](https://openairdocs.org/sdr/ABXA000314), Jun 16, 2000: BRACKET. CRACKED. DURING C-CHECK, FOUND THE AFT LOWER CARGO COMPARTMENT DOOR JAMB ON LOCKING PIN BRACKET CRACKED. REPLACED BRACKET IAW DC9 SRM 51-30-5.
- [SDR ABXA000313](https://openairdocs.org/sdr/ABXA000313), Jun 16, 2000: SUPPORT FITTING. CRACKED. DURING C-CHECK, FOUND THE RT WING OUTBOARD SPOILER OUTBOARD TORSION BAR SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1.
- [SDR ABXA000312](https://openairdocs.org/sdr/ABXA000312), Jun 16, 2000: LONGERON. CRACKED. DURING C-CHECK, FOUND LONGERON 16 LT CRACKED AT STATION 965 FUSELAGE FRAME ATTACH POINT. REPLACED LONGERON IAW DC9 SRM 53-02.
- [SDR ABXA000306](https://openairdocs.org/sdr/ABXA000306), Jun 16, 2000: LONGERON. CRACKED. DURING -C- CHECK FOUND LONGERON 16 RT CRACKED AT STATION 965 FRAME ATTACH POINT. REPAIRED LONGERON IAW DC9 SRM 53-02.

All 176: https://openairdocs.org/deregistered/N906AX-2009-11-18/reports.md

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20020101000279I](https://openairdocs.org/incident/20020101000279I), Jan 1, 2002: Doug DC931 (N906AX), Minneapolis, MN. (-23) Aircraft departed msp and returned for landing following inability to pressurize aircraft. Captain's emergency access panel was found dislodged--likely…
- [Incident 19851121066999I](https://openairdocs.org/incident/19851121066999I), Nov 21, 1985: Doug DC931 (N906AX), Omaha, NE. Toxic fumes in aircraft with crew using oxygen. Cargo marked tools contained plastic pipe cement and was leaking.

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