N906AX, cancelled Nov 18, 2009

Service difficulty reports · 176

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR ABXA080056Controller · defectiveON 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, REPLACEDFeb 14, 2008 · N906AX · Doug DC931 · Altitude ControllerSDR ABXA070349Battery Pack · defectiveEMERGENCY EVACUATION LIGHTS WOULD NOT TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00-8.Oct 16, 2007 · N906AX · Doug DC931 · Emergency LightingSDR ABXA070234Cusp Web · crackedCUSP WEB CRACKED AFT OF FS 313, RIGHT BUTT LINE 56. REPAIRED CUSP WEB AT FS 315 IAW DC9 SRM 53-01.Jun 20, 2007 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA070233Angle · crackedSUBFLOOR ANGLE WAS CRACKED FORWARD END LEFT BUTT LINE FS 996. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-2.Jun 19, 2007 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA070231Floorbeam · corrodedFLOORBEAM AT STA 313, FORWARD SIDE UNDER CUSP WEB HAD CORROSION AROUND NUT PLATE. REPAIRED DAMAGED AREA IAW DC9 SRM K05159.Jun 15, 2007 · N906AX · Doug DC931 · Fuselage Main, Floor BeamSDR ABXA070228Cusp Web · corrodedFRAME FOOT AND CUSP WEB CORRODED -3/3, RIGHT. REPAIRED DAMAGED AREA IAW DC9 SRM 53-01.Jun 13, 2007 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA070227Attach Fitting · corrodedFRAME FOOT AND CUSP WEB CORRODED. REMOVED AND REPLACED FRAME FITTING AND REMOVED CORROSION FROM CUSP WEB IAW DC9 SRM.Jun 13, 2007 · N906AX · Doug DC931 · Fuselage Main, FrameSDR ABXA070230Attach Fitting · corrodedFRAME FOOT CORRODED - 832 LEFT. REMOVED AND REPLACED FS 832 LEFT FRAME FOOT IAW DC9 SRM.Jun 13, 2007 · N906AX · Doug DC931 · Fuselage Main, FrameSDR ABXA070229Shear Tie · crackedSHEAR 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.Jun 13, 2007 · N906AX · Doug DC931 · Fuselage Internal Mounting StructureSDR ABXA070224Membrane · crackedSUBFLOOR CRACKED AT STA 120 AROUND BUTT LINE 0. REPAIRED SUBFLOOR IAW DC9 SRM.Jun 12, 2007 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA070226Angle · crackedAFT PRESSURE BULKHEAD ANGLE AT THRESHOLD WAS CRACKED. REMOVED AND REPLACED ANGLE IAW DC9 SRM 51-30-5.Jun 12, 2007 · N906AX · Doug DC931 · Fuselage Main, BulkheadSDR ABXA070225Fitting · crackedUPPER 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.Jun 11, 2007 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA070223Attach Fitting · crackedRIGHT WHEEL WELL BULKHEAD TO KEEL ATTACH FITTING CRACKED. REMOVED AND REPLACED ATTACH FITTING IAW DC9 SRM.Jun 11, 2007 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA070222Attach Angle · corrodedATTACH 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.Jun 11, 2007 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA070221Fitting · crackedFLOORBEAM SUPPORT UPPER END FITTING CRACKED, 965 LEFT SIDE. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.Jun 8, 2007 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA070220Bulkhead · crackedAFT 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 Jun 8, 2007 · N906AX · Doug DC931 · Fuselage Main, BulkheadSDR ABXA070219Bulkhead · crackedAFT 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 DRILJun 8, 2007 · N906AX · Doug DC931 · Fuselage Main, BulkheadSDR ABXA070232Floorbeam · corrodedFLOORBEAM AT FS 275, RIGHT BUTT LINE 44.5 HAD CORROSION AT GROUNDING STUD. REPAIRED AREA IAW DC9 SRM 53-05.Jun 5, 2007 · N906AX · Doug DC931 · Fuselage Main, Floor BeamSDR ABXA070025Outflow Valve · frozenDURING 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 Jan 25, 2007 · N906AX · Doug DC931 · Pressure Regulator/Outflow ValveSDR ABXA060155Wire · brokenCREW 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 EVIDMar 30, 2006 · N906AX · Doug DC931 · Ice/Rain Protection System WiringSDR ABXA060088Door · corrodedDURING 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.Feb 19, 2006 · N906AX · Doug DC931 · Landing Gear DoorsSDR ABXA050206Gyro · defectiveDURING 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 FAug 26, 2005 · N906AX · Doug DC931 · Attitude Gyro and Indicating SystemSDR ABXA050134Angle · crackedCRACKED VERTICAL ANGLE BELOW RIGHT BUTT LINE 44 TRACK AT STA 617 FLOORBEAM. REMOVED AND REPLACED ANGLE IAW DC9 SRM 51-30-5.May 18, 2005 · N906AX · Doug DC931 · Fuselage Main, Attach FittingsSDR ABXA050133Frame · crackedRIGHT 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.May 17, 2005 · N906AX · Doug DC931 · Fuselage Main, FrameSDR ABXA050131Support · brokenFLOOR 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.May 16, 2005 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA050132Web · crackedCRACK INSIDE PYLON UNDER PANEL 8206. REPAIRED CRACK IAW DC-9 SRM 54-01.May 16, 2005 · N906AX · Doug DC931 · Nacelle/Pylon Miscellaneous StructureSDR ABXA040201Windshield · crackedFIRST 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 MMJun 3, 2004 · N906AX · Doug DC931 · Flight Compartment WindowsSDR ABXA030395Attach Fitting · crackedINBOARD 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.Sep 27, 2003 · N906AX · Doug DC931 · Wing Miscellaneous StructureSDR ABXA030153Structure · delaminatedDURING 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.May 15, 2003 · N906AX · Doug DC931 · Aileron TabsSDR ABXA030054Solenoid Valve · leakingAIRCRAFT 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 BJan 30, 2003 · N906AX · Doug DC931 · APU Engine Fuel and ControlSDR ABXA010735Door Frame · corrodedAFT 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.Feb 11, 2002 · N906AX · Doug DC931 · Fuselage Main, StructureSDR ABXA010734Spar · crackedLEFT UPPER FORWARD SPAR WAS CRACKED AT THE INBOARD LEADING EDGE ATTACH HOLE. REPAIRED SPAR IAW DC-9 REA D957-43288MR.Feb 10, 2002 · N906AX · Doug DC931 · Wing SparSDR ABXA010733Longeron · crackedLONGERON 4 LEFT AT F.S. 200 WAS CRACKED. REPLACED LONGERON IAW DC-9 SRM 53-02.Feb 8, 2002 · N906AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA010732Fitting · crackedAFT 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.Feb 8, 2002 · N906AX · Doug DC931 · Cargo/Baggage DoorsSDR ABXA010731Fitting · crackedAFT LOWER CARGO DOOR, #4 INTERCOSTAL BEAM, AFT END FITTING CRACKED. REPLACED END FITTING IAW DC-9 SRM 51-30-5 AND 51-30-1.Feb 8, 2002 · N906AX · Doug DC931 · Cargo/Baggage DoorsSDR ABXA010730Intercostal · crackedAFT 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.Feb 8, 2002 · N906AX · Doug DC931 · Cargo/Baggage DoorsSDR ABXA010729Pan · crackedAFT LOWER CARGO DOOR, OUTER PAN BULGED AND CRACKED AROUND BLIND NUT ON LEADING EDGE. REPAIRED AREA IAW DC-9 SERVICE REWORK DWG 5934142.Feb 8, 2002 · N906AX · Doug DC931 · Cargo/Baggage DoorsSDR ABXA010728Tab · delaminatedRIGHT SIDE OF RUDDER TAB DELAMINATED. REPLACED RUDDER CONTROL TAB IAW DC-9 AMM 27-20-02-4-0001.Feb 7, 2002 · N906AX · Doug DC931 · Rudder, Tab StructureSDR ABXA010727Vane · delaminatedINBOARD FIXED VANE WAS DELAMINATED ON LOWER SKIN AT XRS 170. REPLACED FIXED VANE IAW DC-9 SRM 27-51-02-2-0002.Feb 7, 2002 · N906AX · Doug DC931 · Trailing Edge FlapsSDR ABXA010726Panel · delaminatedLEFT 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.Feb 7, 2002 · N906AX · Doug DC931 · Wing, Plate/SkinSDR ABXA010725Support Fitting · crackedTWO 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.Feb 6, 2002 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA000319Skin · delaminatedDURING 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.Jun 16, 2000 · N906AX · Doug DC931 · Landing Gear DoorsSDR ABXA000318Skin · corrodedDURING 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.Jun 16, 2000 · N906AX · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA000317Frame · corrodedDURING 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.Jun 16, 2000 · N906AX · Doug DC931 · Fuselage Main, FrameSDR ABXA000316Longeron · crackedDURING C-CHECK, FOUND LONGERON 24 LEFT CRACKED AT STATION 180. REPLACED LONGERON IAW DC9 SRM 51-30-5.Jun 16, 2000 · N906AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA000315Longeron · crackedDURING C-CHECK, FOUND LONGERON 24 LEFT AT STATION 200 CRACKED. REPLACED LONGERON IAW DC9 SRM 51-30-2.Jun 16, 2000 · N906AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA000314Bracket · crackedDURING C-CHECK, FOUND THE AFT LOWER CARGO COMPARTMENT DOOR JAMB ON LOCKING PIN BRACKET CRACKED. REPLACED BRACKET IAW DC9 SRM 51-30-5.Jun 16, 2000 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA000313Support Fitting · crackedDURING C-CHECK, FOUND THE RT WING OUTBOARD SPOILER OUTBOARD TORSION BAR SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1.Jun 16, 2000 · N906AX · Doug DC931 · SpoilersSDR ABXA000312Longeron · crackedDURING C-CHECK, FOUND LONGERON 16 LT CRACKED AT STATION 965 FUSELAGE FRAME ATTACH POINT. REPLACED LONGERON IAW DC9 SRM 53-02.Jun 16, 2000 · N906AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA000306Longeron · crackedDURING -C- CHECK FOUND LONGERON 16 RT CRACKED AT STATION 965 FRAME ATTACH POINT. REPAIRED LONGERON IAW DC9 SRM 53-02.Jun 16, 2000 · N906AX · Doug DC931 · Fuselage Main, Longeron/Stringer
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