# Service difficulty reports: N906AX, cancelled Nov 18, 2009

A list on [N906AX, cancelled Nov 18, 2009](https://openairdocs.org/deregistered/N906AX-2009-11-18.md).

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

Page 1 of 4 · 176 reports

- [SDR ABXA080056](https://openairdocs.org/sdr/ABXA080056.md): Controller · defective · Feb 14, 2008 · N906AX · Doug DC931 · Altitude Controller
  > 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 FROM THE AUTO PILOT CONTROLLER. DEFERRED THE AUTO PILOT SYSTEM. CLEARED DEFERRED ITEM, REPLACED
- [SDR ABXA070349](https://openairdocs.org/sdr/ABXA070349.md): Battery Pack · defective · Oct 16, 2007 · N906AX · Doug DC931 · Emergency Lighting
  > 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.md): Cusp Web · cracked · Jun 20, 2007 · N906AX · Doug DC931 · Fuselage Miscellaneous Structure
  > 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.md): Angle · cracked · Jun 19, 2007 · N906AX · Doug DC931 · Fuselage Miscellaneous Structure
  > 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.md): Floorbeam · corroded · Jun 15, 2007 · N906AX · Doug DC931 · Fuselage Main, Floor Beam
  > 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.md): Cusp Web · corroded · Jun 13, 2007 · N906AX · Doug DC931 · Fuselage Miscellaneous Structure
  > FRAME FOOT AND CUSP WEB CORRODED -3/3, RIGHT. REPAIRED DAMAGED AREA IAW DC9 SRM 53-01.
- [SDR ABXA070227](https://openairdocs.org/sdr/ABXA070227.md): Attach Fitting · corroded · Jun 13, 2007 · N906AX · Doug DC931 · Fuselage Main, Frame
  > 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.md): Attach Fitting · corroded · Jun 13, 2007 · N906AX · Doug DC931 · Fuselage Main, Frame
  > FRAME FOOT CORRODED - 832 LEFT. REMOVED AND REPLACED FS 832 LEFT FRAME FOOT IAW DC9 SRM.
- [SDR ABXA070229](https://openairdocs.org/sdr/ABXA070229.md): Shear Tie · cracked · Jun 13, 2007 · N906AX · Doug DC931 · Fuselage Internal Mounting Structure
  > 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.md): Membrane · cracked · Jun 12, 2007 · N906AX · Doug DC931 · Fuselage Miscellaneous Structure
  > SUBFLOOR CRACKED AT STA 120 AROUND BUTT LINE 0. REPAIRED SUBFLOOR IAW DC9 SRM.
- [SDR ABXA070226](https://openairdocs.org/sdr/ABXA070226.md): Angle · cracked · Jun 12, 2007 · N906AX · Doug DC931 · Fuselage Main, Bulkhead
  > 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.md): Fitting · cracked · Jun 11, 2007 · N906AX · Doug DC931 · Fuselage Miscellaneous Structure
  > 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.md): Attach Fitting · cracked · Jun 11, 2007 · N906AX · Doug DC931 · Fuselage Miscellaneous Structure
  > RIGHT WHEEL WELL BULKHEAD TO KEEL ATTACH FITTING CRACKED. REMOVED AND REPLACED ATTACH FITTING IAW DC9 SRM.
- [SDR ABXA070222](https://openairdocs.org/sdr/ABXA070222.md): Attach Angle · corroded · Jun 11, 2007 · N906AX · Doug DC931 · Fuselage Miscellaneous Structure
  > 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 51-30-5.
- [SDR ABXA070221](https://openairdocs.org/sdr/ABXA070221.md): Fitting · cracked · Jun 8, 2007 · N906AX · Doug DC931 · Fuselage Miscellaneous Structure
  > 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.md): Bulkhead · cracked · Jun 8, 2007 · N906AX · Doug DC931 · Fuselage Main, Bulkhead
  > 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: 5910130-85 AND ONE IN LOWER TAB PORTION OF AFT PRESSURE BULKHEAD SKIN P/N: 5910130-5. REPAIRED LOWER LEFT
- [SDR ABXA070219](https://openairdocs.org/sdr/ABXA070219.md): Bulkhead · cracked · Jun 8, 2007 · N906AX · Doug DC931 · Fuselage Main, Bulkhead
  > 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: 5910130-87 AND ONE IN ORIGINAL DOUBLER P/N: 5910130-85. ALSO AFT PRESSURE BULKHEAD SKIN LOWER TAB HAD DRIL
- [SDR ABXA070232](https://openairdocs.org/sdr/ABXA070232.md): Floorbeam · corroded · Jun 5, 2007 · N906AX · Doug DC931 · Fuselage Main, Floor Beam
  > 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.md): Outflow Valve · frozen · Jan 25, 2007 · N906AX · Doug DC931 · Pressure Regulator/Outflow Valve
  > DURING CLIMB, CABIN WOULD NOT PRESSURIZE, DID ABNORMAL. COULD NOT PRESSURIZE MANUALLY EITHER. CABIN PRESSURE CONTROL WHEEL JAMMED. DUE TO COLD WEATHER, SUSPECT OUTFLOW VALVE FROZEN. HEATED AND LUBRICATED VALVE. PRESSURIZED AIRCRAFT ON GROUND, OPS CHECKED
- [SDR ABXA060155](https://openairdocs.org/sdr/ABXA060155.md): Wire · broken · Mar 30, 2006 · N906AX · Doug DC931 · Ice/Rain Protection System Wiring
  > CREW REPORTED ELECTRICAL SMELL IN COCKPIT AT ALTITUDE. ODOR DISSIPATED WHEN COCKPIT TEMPERATURE WAS TURNED DOWN. OPERATED LT AND RT AIR CONDITIONING SYSTEMS FOR 20 MINUTES EACH AT NEAR MAXIMUM DUCT TEMPERATURES. NO FAULTS NOTED. FOUND BROKEN WIRE WITH EVID
- [SDR ABXA060088](https://openairdocs.org/sdr/ABXA060088.md): Door · corroded · Feb 19, 2006 · N906AX · Doug DC931 · Landing Gear Doors
  > 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 32-10-00.
- [SDR ABXA050206](https://openairdocs.org/sdr/ABXA050206.md): Gyro · defective · Aug 26, 2005 · N906AX · Doug DC931 · Attitude Gyro and Indicating System
  > 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 VERTICAL GYRO IAW DC-9 AMM 37-27-01-4. SYSTEM OPS CHECKED GOOD. (CACTUS CALL OUT OF YYC ENROUTE TO F
- [SDR ABXA050134](https://openairdocs.org/sdr/ABXA050134.md): Angle · cracked · May 18, 2005 · N906AX · Doug DC931 · Fuselage Main, Attach Fittings
  > 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.md): Frame · cracked · May 17, 2005 · N906AX · Doug DC931 · Fuselage Main, Frame
  > 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 53400324-001-2.
- [SDR ABXA050131](https://openairdocs.org/sdr/ABXA050131.md): Support · broken · May 16, 2005 · N906AX · Doug DC931 · Fuselage Miscellaneous Structure
  > 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.md): Web · cracked · May 16, 2005 · N906AX · Doug DC931 · Nacelle/Pylon Miscellaneous Structure
  > CRACK INSIDE PYLON UNDER PANEL 8206. REPAIRED CRACK IAW DC-9 SRM 54-01.
- [SDR ABXA040201](https://openairdocs.org/sdr/ABXA040201.md): Windshield · cracked · Jun 3, 2004 · N906AX · Doug DC931 · Flight Compartment Windows
  > 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 LANDING. REPLACED RIGHT WINDSHIELD IAW DC-9 MM 56-10-02-2-0004. REPLACED TEMP CONTROLLER IAW DC-9 MM
- [SDR ABXA030395](https://openairdocs.org/sdr/ABXA030395.md): Attach Fitting · cracked · Sep 27, 2003 · N906AX · Doug DC931 · Wing Miscellaneous Structure
  > 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 57-09.
- [SDR ABXA030153](https://openairdocs.org/sdr/ABXA030153.md): Structure · delaminated · May 15, 2003 · N906AX · Doug DC931 · Aileron Tabs
  > 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. REPLACED RIGHT AILERON TRIM TAB IAW DC-9 MM 27-10-05-2-0001.
- [SDR ABXA030054](https://openairdocs.org/sdr/ABXA030054.md): Solenoid Valve · leaking · Jan 30, 2003 · N906AX · Doug DC931 · APU Engine Fuel and Control
  > 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. LEAK CHECKED GOOD IAW DC-9 MM 49-30-03-2-003. REPLACED LT COALESCAR BAG AS PRECAUTIONARY. FOUND B
- [SDR ABXA010735](https://openairdocs.org/sdr/ABXA010735.md): Door Frame · corroded · Feb 11, 2002 · N906AX · Doug DC931 · Fuselage Main, Structure
  > 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.md): Spar · cracked · Feb 10, 2002 · N906AX · Doug DC931 · Wing Spar
  > 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.md): Longeron · cracked · Feb 8, 2002 · N906AX · Doug DC931 · Fuselage Main, Longeron/Stringer
  > LONGERON 4 LEFT AT F.S. 200 WAS CRACKED. REPLACED LONGERON IAW DC-9 SRM 53-02.
- [SDR ABXA010732](https://openairdocs.org/sdr/ABXA010732.md): Fitting · cracked · Feb 8, 2002 · N906AX · Doug DC931 · Cargo/Baggage Doors
  > 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.md): Fitting · cracked · Feb 8, 2002 · N906AX · Doug DC931 · Cargo/Baggage Doors
  > 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.md): Intercostal · cracked · Feb 8, 2002 · N906AX · Doug DC931 · Cargo/Baggage Doors
  > 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.md): Pan · cracked · Feb 8, 2002 · N906AX · Doug DC931 · Cargo/Baggage Doors
  > 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.md): Tab · delaminated · Feb 7, 2002 · N906AX · Doug DC931 · Rudder, Tab Structure
  > 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.md): Vane · delaminated · Feb 7, 2002 · N906AX · Doug DC931 · Trailing Edge Flaps
  > 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.md): Panel · delaminated · Feb 7, 2002 · N906AX · Doug DC931 · Wing, Plate/Skin
  > 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.md): Support Fitting · cracked · Feb 6, 2002 · N906AX · Doug DC931 · Fuselage Miscellaneous Structure
  > 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.md): Skin · delaminated · Jun 16, 2000 · N906AX · Doug DC931 · Landing Gear Doors
  > 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 OHM 32-10-6 AND DC9 MM 32-12-01.
- [SDR ABXA000318](https://openairdocs.org/sdr/ABXA000318.md): Skin · corroded · Jun 16, 2000 · N906AX · Doug DC931 · Fuselage Main, Plate/Skin
  > 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.md): Frame · corroded · Jun 16, 2000 · N906AX · Doug DC931 · Fuselage Main, Frame
  > 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. K05159.
- [SDR ABXA000316](https://openairdocs.org/sdr/ABXA000316.md): Longeron · cracked · Jun 16, 2000 · N906AX · Doug DC931 · Fuselage Main, Longeron/Stringer
  > 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.md): Longeron · cracked · Jun 16, 2000 · N906AX · Doug DC931 · Fuselage Main, Longeron/Stringer
  > 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.md): Bracket · cracked · Jun 16, 2000 · N906AX · Doug DC931 · Fuselage Miscellaneous Structure
  > 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.md): Support Fitting · cracked · Jun 16, 2000 · N906AX · Doug DC931 · Spoilers
  > 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.md): Longeron · cracked · Jun 16, 2000 · N906AX · Doug DC931 · Fuselage Main, Longeron/Stringer
  > 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.md): Longeron · cracked · Jun 16, 2000 · N906AX · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING -C- CHECK FOUND LONGERON 16 RT CRACKED AT STATION 965 FRAME ATTACH POINT. REPAIRED LONGERON IAW DC9 SRM 53-02.

Next page: https://openairdocs.org/deregistered/N906AX-2009-11-18/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N906AX' AND deregistration_id = 'N906AX-2009-11-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N906AX-2009-11-18/reports

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