N939AX, cancelled Jul 20, 2017

Service difficulty reports · 106

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 = 'N939AX' AND deregistration_id = 'N939AX-2017-07-20'
  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 ABXA080083Relay · defectiveCENTER PRIMARY TRIM CIRCUIT BREAKER TRIPPED DURING TRIM SETTING. FOUND UP TRIM RELAY BURNT AT TERMINALS A1 & A2. REPLACED NOSE UP PRIMARY TRIM RELAY AND TERMINALS A1 & A2. OPS CHECK GOOD IAW DC9 AMM 27-40-04-5-0002.Feb 26, 2008 · N939AX · Doug DC932 · Stabilizer Control SystemSDR ABXA070105Floorbeam · crackedFLOORBEAM CRACKED TO LIGHTENING HOLE APPROXIMATELY STA 175, BUTT LINE 0. REPAIRED AREA IAW REA D953-55576MR.Apr 2, 2007 · N939AX · Doug DC932 · Fuselage Main, Floor BeamSDR ABXA070103Frame · crackedAFT RIGHT MAIN FRAME HAD CRACK AT FORWARD AND AFT FLANGES, MUST BE REPLACED PER NEA 53400102-002-30. REMOVED AND REPLACED RIGHT MAIN FRAME IAW DC9 EA 53400326-001-2. CRACK LENGTHS WERE 1" AND 1 1/4".Mar 16, 2007 · N939AX · Doug DC932 · Fuselage Main, FrameSDR ABXA070100Attach Angle · corrodedUPPER SURFACE OF PYLON BULKHEAD TO FLOORBEAM ATTACH ANGLE AT STA 965 CORRODED FROM RIGHT BUTT LINE 55, RIGHT BUTT LINE 36. FABRICATED AND INSTALLED NEW PYLON BULKHEAD TO FLOORBEAM ATTACH ANGLE IAW DAC DWG 9912243.Mar 15, 2007 · N939AX · Doug DC932 · Fuselage Main, Attach FittingsSDR ABXA070099Bulkhead · crackedRIGHT PYLON BULKHEAD AT STA 965 HAD CRACKED ATTACH FITTING AT RIGHT BUTT LINE 32. REMOVED AND REPLACED FITTING IAW DAC DWG 9912243.Mar 15, 2007 · N939AX · Doug DC932 · Nacelle/Pylon, Bulkhead/FirewallSDR ABXA070094Shear Tie · crackedSHEAR TIE CRACKED AT FS 945, BETWEEN LONGERON 15 RIGHT AND LONGERON 16 RIGHT. REMOVED AND REPLACED SHEAR TIE IAW DC9 SRM 51-30-2, 51-30-5 AND 51-30-1.Mar 15, 2007 · N939AX · Doug DC932 · Fuselage Internal Mounting StructureSDR ABXA070102Bulkhead · crackedAFT PRESSURE BULKHEAD LOWER DOOR CORNER HAD A CRACK IN SKIN. THE REPAIR INSTALLED DID NOT MATCH ANY CONFIGURATION OF DWG J060088 IN NUMBER, PLACEMENT AND MATERIAL OF DOUBLERS. REMOVED PREVIOUS REPAIR. NO CRACKS FOUND. REPAIRED LOWER DOOR CORNER IAW SERVICEMar 15, 2007 · N939AX · Doug DC932 · Fuselage Main, BulkheadSDR ABXA070096Frame · corrodedLOWER POCKETS IN MAIN FRAME IN LEFT WHEEL WELL HAD CORROSION AROUND LOWER VERTICAL ATTACH BOLTS. CLEANED, TREATED CORROSION AROUND LOWER VERTICAL ATTACH BOLT ON LEFT MAIN FRAME 718 AIW DC9 SRM.Mar 14, 2007 · N939AX · Doug DC932 · Fuselage Main, FrameSDR ABXA070093Bulkhead · crackedAFT PRESSURE BULKHEAD LEFT UPPER DOOR CORNER HAD 2 CRACKS THAT NEEDED TO BE STOP DRILLED. REMOVED OUTSIDE DOUBLER, STOP DRILLED CRACKS IAW SRO J060088. REINSTALLED DOUBLER IAW SRO J060088 AND DC9 SRM 51-30-5. CRACK LENGTHS WERE 7/8", 3/4" AND 1".Mar 13, 2007 · N939AX · Doug DC932 · Fuselage Main, BulkheadSDR ABXA070092Rib · crackedLEFT WING XRS 164, RIB FITTING CRACKED. REMOVED AND REPLACED RIB AT LEFT WING XRS 164 IAW DC9 SRM.Mar 13, 2007 · N939AX · Doug DC932 · Wing, Rib/BulkheadSDR ABXA070068Power Supply · dischargedCOCKPIT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY SUPPLY POWER PACK IAW DC9 MM 33-53-00.Mar 5, 2007 · N939AX · Doug DC932 · Emergency LightingSDR ABXA070001Unknown · malfunctionedAIRCRAFT LOST PRESSURIZATION AT 6500 FT IN DESCENT TO ILN, BOTH PACKS ON. CHECKED TAIL COMPARTMENT FOR LOOSE AND BLOWN DUCTS. NO DEFECTS FOUND. PERFORMED ADJ/TEST OF CABIN PRESSURE CONTROL WITH PNEUMATIC SOURCE IAW DC9 MM 21-32-00-2-0101. SYSTEM OPERATES NDec 28, 2006 · N939AX · Doug DC932 · Cabin Pressure Control SystemSDR ABXA070002Control Panel · defectiveNR 2 COM FREQUENCY SELECTOR WAS REPORTED AS INOPERATIVE BY CREW. ELECTED TO REROUTE FLIGHT 122 ICT TO ILN, OVERFLEW SGF. ON L/P 033705-049/2, NR 2 COM FREQUENCY SELECTOR OCCASIONALLY DIALED WRONG FREQUENCY. VOLUME AND SELECTOR KNOBS WHEN WIGGLED SHORTED OUTDec 27, 2006 · N939AX · Doug DC932 · Audio Integrating SystemSDR ABXA040202Skin · crackedDURING LINE MAINTENANCE, FOUND FUSELAGE SKIN CRACKED AND BULGED AT STA 759, LONGERON 29 RIGHT. REPAIRED SKIN IAW DC-9 SRM 53-04, FIG 12B.Jun 7, 2004 · N939AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA040203Skin · crackedDURING LINE MAINTENANCE, FOUND FUSELAGE SKIN CRACKED AND CORRODED AT STA 917 AND LONGERON 28 RIGHT. REPAIRED SKIN IAW REA D953-49934MR.Jun 7, 2004 · N939AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA030344Fitting · corrodedFLAP HINGE STUDS AT FLAP FITTING STA. 267 HEAVILY CORRODED. REPLACED FLAP HINGE IAW DC-9 MM 57-40-01-2-0001.Aug 21, 2003 · N939AX · Doug DC932 · Trailing Edge FlapsSDR ABXA030343Intercostal · crackedCABIN FLOORBEAM INTERCOSTAL BETWEEN STA. 256 AND 275, BUTT LINE O, CRACKED FORWARD END. REPLACED INTERCOSTAL IAW DC-9 SSRM K05159.Aug 20, 2003 · N939AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA010816Rod · out of adjustCAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. FOUND UPPER HOOK NOT CLEARING TO ALLOW WINDOW TO OPEN. ADJUSTED UPPER ROD WINDOW IAW DC-9 MM, OPS CHECKED GOOD.Apr 4, 2002 · N939AX · Doug DC932 · Flight Compartment WindowsSDR ABXA010661Fitting · crackedAFT LOWER CARGO DOOR #2 BEAM, AFT END FITTING WAS CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2, 51-30-1, 51-20-0.Dec 14, 2001 · N939AX · Doug DC932 · DoorsSDR ABXA010660Skin · canningFUSELAGE EXTERIOR SKIN WAS OIL CANNING UNDER THE NR 2 PYLON, FORWARD OF STATION 965 IN TWO BAYS. REPAIRED IAW DC-9 SRM 53-04.Dec 12, 2001 · N939AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA010595Track · dirtyCAPTAIN'S CLEAR VIEW WINDOW WAS STUCK CLOSED. OPENED WINDOW AND CLEANED THE TRACK. OPS CHECKED GOOD IAW DC-9 MM.Nov 27, 2001 · N939AX · Doug DC932 · Flight Compartment WindowsSDR ABXA010532Battery · dischargedTHE EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES IAW DC-9 MM 33-53-00. THE EMERGENCY LIGHT BATTERY PACK WAS DEFERRED FOR REPLACEMENT. THE EMERGENCY LIGHT BATTERY PACK WAS REPLACED.Oct 8, 2001 · N939AX · Doug DC932 · Emergency LightingSDR ABXA010052Wire · damagedTHE LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED INTERMITTANTLY. THE FLIGHT RETURNED TO ILN TO COMPLETE REPAIRS. MAINTENANCE INSPECTED AND REPAIRED A WIRE FOR CONNECTOR P1-130 PIN NR 4. LANDING GEAR OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS Feb 13, 2001 · N939AX · Doug DC932 · Landing Gear System WiringSDR ABXA0100014Window · seizedCREW WAS UNABLE TO OPERATE CAPTAINS CLEARVIEW WINDOW. THE AIRCRAFT RETURNED TO BLOCKS. MAINTENANCE INSPECTED AND LUBRICATED THE CAPTAINS CLEAR VIEW WINDOW IAW DC-9 MM. OPS CHECKED GOOD.Jan 17, 2001 · N939AX · Doug DC932 · Flight Compartment WindowsSDR ABXA000248Window · out of adjCAPTAIN''S CLEARVIEW WINDOW (EMERGENCY EXIT) WOULD NOT OPEN. ADJUSTED CAM FOLLOWER VERTICAL AND EXTENSION ADJUSTMENTS.May 9, 2000 · N939AX · Doug DC932 · Flight Compartment WindowsSDR ABXA000252Fitting · corrodedDURING D-CHECK, FOUND CENTER TANK TO SLANT PANEL FITTING CORRODED. REPLACED FITTING IAW DC9 SRM 51-10-4.Apr 26, 2000 · N939AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA000249Tank · corrodedDURING D-CHECK, FOUND AFT EDGE OF UPPER CENTER TANK PLATING CORRODED AT STATION XCW 20. REPAIRED IAW ABX REA D957-36744.Apr 26, 2000 · N939AX · Doug DC932 · Wing, Center BoxSDR ABXA000247Doubler · corrodedDURING D-CHECK, FOUND INTERNAL DOUBLER CORRODED AT STATION 579 AND LONGERON 30. REPLACED DOUBLER IAW DC9 SRM 51-30-2.Apr 26, 2000 · N939AX · Doug DC932 · Fuselage Main, StructureSDR ABXA000237Fitting · crackedDURING D-CHECK, FOUND SLANT PANEL OUTBOARD FITTING, STATION 699 CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1.Apr 26, 2000 · N939AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA000250Fitting · crackedDURING D-CHECK, FOUND PYLON SUPPORT BULKHEAD FITTING CORRODED AT STATION 965 LEFT. REPLACED SUPPORT FITTING IAW DC9 SRM 51-30-5.Apr 21, 2000 · N939AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA000240Fitting · corrodedDURING D-CHECK, FOUND NR 1 SLAT TRACK FITTING CORRODED. REPLACED FITTING IAW DC9 SRM 51-30-2.Apr 13, 2000 · N939AX · Doug DC932 · Leading Edge DevicesSDR ABXA000261Cap · corrodedDURING ''D'' CHECK, FOUND TEE CAP CORRODED AT STA 604 BETWEEN LONGERON 29L AND 30. REPAIRED TEE CAP IAW DC9 SRM 53-03.Apr 12, 2000 · N939AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA000246Fitting · crackedDURING D-CHECK, FOUND LONGERON 29 RIGHT END FITTING AT STATION 604 CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5.Apr 12, 2000 · N939AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA000242Fitting · crackedDURING D-CHECK, FOUND LONGERON 30 SPLICE FITTING CRACKED AT STATION 602. REPLACEDFITTING IAW DC9 SRM 51-10-2.Apr 11, 2000 · N939AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA000245Rib · crackedDURING D-CHECK, FOUND RIGHT HORIZONTAL STABILIZER OUTBOARD RIB CRACKED. REPLACED RIB IAW DC9 SRM 51-30-1.Apr 10, 2000 · N939AX · Doug DC932 · Horizontal Stabilizer, Spar/RibSDR ABXA000263Floorbeam · corrodedDURING ''''D'''' CHECK, FOUND FLOORBEAM CORRODED AT STA 313 AND LBL 40. REPAIRED FLOORBEAM IAW DC9 SRM 53-05.Apr 8, 2000 · N939AX · Doug DC932 · Fuselage Main, Floor BeamSDR ABXA000265Gusset · corrodedDURING ''D'' CHECK, FOUND CORROSION ON GUSSET PLATES AT STATION 965, LONGERON 19R. REPLACED GUSSETS IAW DC9 SRM 51-30-5.Apr 6, 2000 · N939AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA000264Splice · corrodedDURING ''D'' CHECK, FOUND SEAT TRACK SPLICE CORRODED ON LOWER SIDE, STATION 395, RBL 8. REPLACED SPLICE IAW DC9 SRM 51-30-1.Apr 6, 2000 · N939AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA000251Intercostal · corrodedDURING D-CHECK, FOUND INTERCOSTAL WEB CORRODED AT STATION 945 - 965 AND LONGERON 19 RIGHT. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-5.Apr 6, 2000 · N939AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA000239Doubler · corrodedDURING D-CHECK, FOUND CORROSION ON DOUBLER, STATION 1087 AND LONGERON 1 LEFT. REPLACED DOUBLER IAW DC9 SRM 51-30-2.Apr 6, 2000 · N939AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA000241Intercostal · corrodedDURING D-CHECK, FOUND CORRODED INTERCOSTAL BETWEEN STATION 218 AND 237 AT LONGERON 28 LEFT. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2.Apr 5, 2000 · N939AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA000238Angle · corrodedDURING D-CHECK, FOUND NOSE WHEEL WELL UPPER PRESSURE PANEL STIFFENER CORRODED. REPLACEDPRESSURE PANEL STIFFENER IAW DC9 SRM.Apr 4, 2000 · N939AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA000262Angle · crackedDURING D-CHECK INSPECTION, FOUND LEFT VERTICAL STAB TO FUSELAGE ATTACH ANGLE CRACKED AT STATION 1109. REPAIRED ANGLE IAW ABX REA D953-36544-MR.Apr 3, 2000 · N939AX · Doug DC932 · Vertical StabilizerSDR ABXA000244Fitting · corrodedRIGHT OUTBOARD SLAT IDLER TRACK FITTING HAD HEAVY CORROSION/EXFOLIATION AT 3 MOUNT HOLES. REPLACED RIGHT NR 1 LEADING EDGE SLAT.Mar 31, 2000 · N939AX · Doug DC932 · Leading Edge DevicesSDR ABXA000243Web · crackedLEFT CUSP WEB CRACKED AT STATION 596 AND RBL 44. REPLACED CUSP WEB IAW DC9 SRM51-30-2.Mar 31, 2000 · N939AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9900022Control Valve · iced upON APPROACH, LANDING GEAR HANDLE WAS 'FROZEN' IN THE UP POSITION. ACCOMPLISHED DC9 ABNORMAL PROCEDURES. EMERGENCY GEAR EXTENSION, RESULTED IN UNEVENTFUL LANDING. REMOVED ICE FROM LANDING GEAR CONTROL VALVE CABLES, RESET EMERGENCY EXTENSION CONTROLS. CYCLEDJan 13, 1999 · N939AX · Doug DC932 · Landing Gear Retraction/Extension SystemSDR ABXA9800835Tee · corrodedILN - DUIRNG C-CHECK, FOUND CUSP TEE ANGLES AT LONGERON 18R AND STA 946 - STA 980 CORRODED ON LOWER SIDE. REPAIRED IAW DC9 SRM 53-05. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X)Sep 17, 1998 · N939AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9800834Web · corrodedILN - DURING C-CHECK, FOUND CUSP WEB CORRODED AT STA 965 BETWEEN RBL 44 ND RBL 54.5, IN LIGHTENING HOLE AREA BETWEEN STA 945 - STA 965. REPAIRED CUSP WEB IAW ABX REA D953-24862-MR. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X)Sep 17, 1998 · N939AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9800833Fitting · crackedILN - DURING C-CHECK, FOUND LOWER LEFT VENTRAL DOOR STOP SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-2 AND SRM 51-30-5. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X)Sep 17, 1998 · N939AX · Doug DC932 · Passenger/Crew DoorsSDR ABXA9800832Frame · corrodedILN - DURING C-CHECK, FOUND FUSELAGE FRAME AT STA 180 AND LONGERONS 22R- 27R CORRODED. REPAIRED FRAME IAW DC9 SRM 53-03. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X)Sep 17, 1998 · N939AX · Doug DC932 · Fuselage Main, Frame
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