N404UA

Service difficulty reports · 116

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 = 'N404UA' AND registry_match = 'registration'
  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 UALA2012031401668Girt Bar · inoperativeNR 1 RT DOOR OVERWATER SLIDE MR25613-020 CAME WITH INOPERABLE GIRT BAR. TELESCOPING END WOULD NOT RETRACT INTO BAR. REPLACED WITH SERVICABLE. GIRT BAR WAS REPLACED WITH SERVICABLE GIRT BAR ON SLIDE RAFT REPLACEMENT TASK CARD SEQ680 4S2592044.Mar 13, 2012 · N404UA · Airbus A320232 · Emergency EquipmentSDR UALA2012022701169Seat · defectiveCAP SEAT RECLINE INOP DEFECTIVE RATCHETS AND DIFFICULT TO ADJUST. REPLACED SEAT IN REF TO AMM, OPS CHECK NORMAL.Feb 27, 2012 · N404UA · Airbus A320232 · Flight Compartment EquipmentSDR UALA2011102805831Connector · brokenNR 1 CIDS BENCH PLUG BROKEN.Oct 28, 2011 · N404UA · Airbus A320232 · Communications System WiringSDR UALA2011101705588Snubber · faultyR1 DOOR HAS NO SNUBBING ACTION DURING LAST ONE THIRD TO ONE QUARTER OF DOOR TRAVEL IN THE CLOSED DIRECTION. SNUBBER ACTUATOR WAS REPLACED SEPT 12 . REPLACED SNUBBER PER MM. OPS CHECKED NORMAL.Oct 15, 2011 · N404UA · Airbus A320232 · Passenger/Crew DoorsSDR UALA2011072703849Fan Blade · damagedNR 1 ENG FAN BLADE AT 6 O`CLOCK POS HAS A NICK IN IT. DETERMINED DIMENSIONS OF NICK TO BE 1-32 INCH DEEP BY 1-16 INCH LONG IN AREA AT, 5 INCHES FROM BLADE TIP. DRESSED. REPAIRED NICK PER AMM TASK.Jul 27, 2011 · N404UA · Airbus A320232 · Turbine Engine Compressor SectionSDR UALA2011071703609Wire · brokenCABIN EMERGENCY LIGHT TEST FAILED. MESSAGE: EXT LOADS FWD L 33-51-38. JUMPED BOTH LT AND RT SLIDES, NO HELP. HOOKED UP NEW BATTERY AND POWER SUPPLY, NO HELP. TROUBLE SHOT PER WD 33-51-04. FOUND NO GROUND AT FWD RT DOOR SLIDE CONNECTOR 2870VC PIN B TO GROJul 17, 2011 · N404UA · Airbus A320232 · Light System WiringSDR UALA2011042001914Limiter · malfunctionedCREW REPORT: F-CTL SLATS FAULT. CREW REPORTED FLAPS-SLATS FAULT GOING TO FLAPS 1. CFDS SHOWED "27-80-00 SLT 1 SYS JAM - CHECK MECH DRIVE" AND "27-80-00 SLT 2 SYS JAM - CHECK MECHANICAL DRIVE. CREW USED CAPT EMERG AUTHORITY TO CYCLE CB'S B6+B7+Q21 FAULT CLEAApr 20, 2011 · N404UA · Airbus A320232 · Leading Edge Slat Control SystemSDR UALA2011030801130Lanyard · unsecureAFT RT SLIDE RAFT SURVIVAL KIT LANYARD AND RELEASE STRAP FOUND LOOSE. RE-INSTALLED LANYARDS. SLIDE RAFT RESTORED TO TOLERANCE.Mar 8, 2011 · N404UA · Airbus A320232 · Emergency EquipmentSDR UALA2011022500943Wheel · crackedON ARRIVAL FOUND NR 2 WHEEL ASSY CRACKED AND RUBBING ON BRAKE ASSY. NR 2 MLG BRAKE ASSY DAMAGED FROM BROKEN WHEEL ASSY. REMOVED NR 2 WHEEL ASSY. INTERIM INSTALLATION OF TIRE AND WHEEL ASSY FOR ACFT TOWING. REPLACED BRAKE ASSY. FOUND NR 2 MLG TACHOMETER FIFeb 25, 2011 · N404UA · Airbus A320232 · Wheel/Ski/FloatSDR UALA2011013100527Pump · leakingLEFT WING FUEL TANK PUMP HOUSING AREA IS WET WITH FUEL WIPED DOWN AREA AND 15 MINS LATER AREA IS WET AGAIN. FUEL STAINS APPEAR TO BE STREAMING AFT ALONG WIRE COVER AFT DURING FLIGHT. FOUND FUEL PUMP 25QA LEAKING. BEGAN REMOVAL IAW MM. CIRCUIT BREAKERS HAVE Jan 28, 2011 · N404UA · Airbus A320232 · Engine Fuel PumpSDR UALA2011012400396Lanyard · misinstalledDOOR 2L SLIDE LANYARDS NOT INSTALLED CORRECTLY. WHITE LANYARD IS ROUTED THROUGH TRIGGER. YELLOW LANYARD IS NOT ROUTED THROUGH TRIGGER. OPENED GIRT AND ROUTED BOTH LANYARDS IAW FIG 410 OF MM. CLOSED GIRT, CHECKED ARM DISARM ACTION. VERIFIED CORRECT LANYARJan 23, 2011 · N404UA · Airbus A320232 · Escape SlideSDR UALA2010101903869Hook · out of adjustDOOR 2 RT - INTERIOR HANDLE CAN BE MOVED TO THE CLOSED POSITION WITH DOOR STILL OPEN. SUSPECT HANDLE INTERLOCK MECHANISM NOT FUNCTIONING AS DESIGNED. REMOVED UPPER DOOR LINING. FOUND THE HOOKS HAVE SLIPPED ON THEIR ADJUSTMENT SERRATIONS. (THEY ARE MOUNTED OOct 18, 2010 · N404UA · Airbus A320232 · Passenger/Crew DoorsSDR UALA2010090703303Proximity Switch · faultedRT AFT SLIDE INDICATION INOP ON DOOR-OXY SYS ECAM PAGE - DOOR-OXY. SLIDE ARMED INDICATION INTERMITTENT. REPLACED 7WN2 PROX SW AND TESTED IAW MM. CHECKED GOOD ON TEST. ACCOMPLISHED RII INSP AS REQUIRED. OPS CHECK NORMAL.Sep 4, 2010 · N404UA · Airbus A320232 · Escape SlideSDR UALA2010071902581Stringer · corrodedSTRINGER JUST BELOW THE CABIN OUTFLOW VALVE IS CORRODED. REPAIR IAW SRM 51-42-11,ON WU P7018X,AND SRM 51-75-12.Jul 18, 2010 · N404UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR UALA2010061102042Unknown · odorAFTER DMC 3 FAULT AT CRUISE CREW AND PAX EXP ACRID SMELL. ACCOMPLISHED TSM 24-00-00- 201 PAGES 25 AND 26. FOUND NO IRREGULARITES DURING OPS OR SNIFF CHECK TO DMC3. FOUND NO TRIPPED C-B'S, ECAM MESSAGES AND NO CIDS OR DEU PROBLEMS. CHECKED ALL E&E COMPARTMENJun 10, 2010 · N404UA · Airbus A320232 · Air Distribution SystemSDR UALA2010042601367Valve · faultyMLG DOOR IS STUCK IN THE DOWN POSITION LT SIDE. DOOR IS STUCK DUE TO FAULTY VALVE. REPLACED BYPASS VALVE AND OP CHECKS ARE OK.Apr 24, 2010 · N404UA · Airbus A320232 · Landing Gear Door Retract SectionSDR UALA2010032300988Handle · not seatedDOOR FWD CARGO LT ILLUM, RTFL. FOUND FWD CARGO DOOR HANDLE JUST OFF DETENT POSITION, BUT DOOR STILL IN LOCKED POSITION. OPERATED DOOR HANDLE SEVERAL TIMES, LOCKS PROPERLY. CHECKS GOOD. NO HISTORY. ACFT OK FOR SVC.Mar 23, 2010 · N404UA · Airbus A320232 · Cargo/Baggage DoorsSDR UALA2010012100254Smoke Detector · false indicationAVIONICS SMOKE MSG, RTFL. CYCLED D5, D6, Y17, C06, T18. CHECKED PFR NO FAULTS ON SYS, CHECKED AVIONICS BAY NO SMOKE PRES ENT RAN CFDS TEST OF ECAM1 REF TSM 26-15-00-810-803. MSG CLEARE D AND NOT PRESENT AT THIS TIME SUSPECT HIGH HUMIDITY IN AVIONICS BAY. Jan 20, 2010 · N404UA · Airbus A320232 · Smoke DetectionSDR UALA2009121603899Bellcrank · frozenDOOR 1L HARD TO ARM. LINER REMOVED. ISOLATED CABLE FROM SYSTEM. STILL HAVE SOME BINDING. FOUND FROZEN BELLCRANK AND SPACER FROZEN TO BOLT. (BELLCRANK ASSY AND ROD ASSY ARE DISCONNECTED AND GIVEN TO HNGR SMC.. WITH BELLCRANK DISCONNECTED DOOR ARMS NORMALLY). REDec 16, 2009 · N404UA · Airbus A320232 · Passenger/Crew DoorsSDR UALA2009111803594Lanyard · out of positionDOOR 1R LANYARD NOT VISIBLE ON SLIDE PACK. MAYBE MISSING OR DAMAGED BEYOND SVC LIMITS, A-C CANNOT OPERATE ON EXTENDED OVERWATER. FOUND LANYARD TWISTED AND OUT OF POSITION, REPOSITIONED AND SECURED MOORING LINE AND SURVIVAL KIT LANYARD.Nov 15, 2009 · N404UA · Airbus A320232 · Escape SlideSDR UALA2009111803593Lanyard · out of positionLANYARD MISSING FROM SLIDE PACK DOOR 2R: MAYBE MISSING OR DAMAGED BEYOND SVC LIMITS, A-C CANNOT OPERATED ON EXTENDED OVERWATER. FOUND LANYARD TWISTED AND OUT OF POSITION, REPOSITIONED AND ROUTED MOORING LINE AND SURVIVAL KIT LANYARD.Nov 15, 2009 · N404UA · Airbus A320232 · Escape SlideSDR UALA2009080302317Slide · faultyL1 DOOR SLIDE LOWER SUPPORT BRACKET BROKEN. REPLACED & INSPECTED SLIDE. MANAGEMENT INSPECTED INSTALLATION AND CONFIRMED WITH AMT THAT PROPER PROCEDURES WERE FOLLOWED.Aug 2, 2009 · N404UA · Airbus A320232 · Escape SlideSDR UALA2009080302316Feeder Cable · damagedAFT MOST EEL FEEDER CABLE BROKEN AT SEAT TRACK. REPAIRED CABLE, OP CHECK EMERGENCY LIGHTS.Aug 2, 2009 · N404UA · Airbus A320232 · Light System WiringSDR UALA2009031000653Actuator · out of rigA/C FLIES WITH LT WING DOWN, WITH 1.5 UNITS LT RUDDER TRIM REQUIRED. WHILE TROUBLESHOOTNG FOUND RT OUTBOARD B AIL ACTUATOR BUSHINGS AND ROD ENDS OUT OF RIG. BOTH BLUE AND GREEN RT AIL SERVO ACT WERE REPLACED.Feb 25, 2009 · N404UA · Airbus A320232 · Aileron Control SystemSDR UALA2009022500653Actuator · wornA/C FLIES WITH LT WING DOWN WITH 1.5 UNITS LT RUDDER TRIM REQUIRED. WHILE TROUBLESHOOTNG FOUND RT OTBOARD B AIL ACTUATOR BUSHINGS AND ROD ENDS. BOTH BLUE AND GREEN RT AIL SERVO ACT WERE REPLACED.Feb 25, 2009 · N404UA · Airbus A320232 · Aileron Control SystemSDR 2008UALA06497Structure · crackedRT TRAY (AFT OF DOOR 2R) IS CRACKED AND MARKED. FABRICATED TRAY FROM 2024T3.063 THICK. INSTALLED TRAY.Nov 11, 2008 · N404UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA06482Beam · corrodedRT BEAM LABELED - Y1292 HAS CORROSION AT FR66 AND IS MARKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED BEAM TO AIRCRAFT. NEEDS SUPPORTS BETWEEN FR64 - FR65 INSTALLED.Nov 11, 2008 · N404UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA06474Beam · corrodedBEAM 205 HAS CORROSION AT FRAME 68. MAJOR REPAIR ACCOMPLISHED. REMOVED BEAM. REMOVED BRACKETS AND TRANSFER DRILLED ONTO NEW BEAM. CONNECTED BEAM 205 TO BEAM 200. READY TO INSTALL IN AC. INSTALLED BEAM.Nov 11, 2008 · N404UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA06473Structure · corrodedRT SHEAR TRAY HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. TRAY REPLACED. Nov 11, 2008 · N404UA · Airbus A320232 · Passenger/Crew DoorsSDR 2008UALA06472Sill · corrodedDOOR 2R SILL PLATE HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. REPLACED DOOR 2R SILL PLATE.Nov 11, 2008 · N404UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA06470Threshold · corrodedRT DOOR 2R THRESHOLD CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. STARTED REMOVING FASTENERS. REMOVED DOOR SILL AND STARTED TO MFG NEW SILL. INSTALLING FASTENERS. CONTINUED INSTALLING FASTENERS AND MFG NEW FWD SPLICE ANGLES. INSTALLING FASTENERS, SNov 9, 2008 · N404UA · Airbus A320232 · Passenger/Crew DoorsSDR 2008UALA06430Support · corrodedRT AFT SHEAR PLATE SUPPORT HAS CORROSION ON BOTTOM SIDE. SUPPORT NEEDS REPLACED. MAJOR REPAIR ACCOMPLISHED. REPLACED RT AFT SHEAR PLATE SUPPORT.Nov 8, 2008 · N404UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA06429Shear Plate · corrodedRIGHT AFT SHEAR PLATE CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. REPLACED RT AFT SHEAR PLATE.Nov 8, 2008 · N404UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA06425Shear Plate · crackedLT TRAY AFT OF DOOR 2L CRACKED AND MARKED. MAJOR REPAIR ACCOMPLISHED. FINISHED DRILLING NEW SHEAR PLATE AND STARTED INSTALLING. INSTALLED REMAINING FASTENERS LT TRAY AFT OF DOOR 2L. ACCOMPLISHED INSPECTION OF FASTENER INSTALLATION.Nov 7, 2008 · N404UA · Airbus A320232 · Passenger/Crew DoorsSDR 2008UALA06406Beam · corrodedBEAM 200 HAS CORROSION AT FRAME 67. MAJOR REPAIR ACCOMPLISHED. REMOVED BEAM. REMOVED BRACKETS AND TRANSFER DRILLED ONTO NEW BEAM. CONNECTED BEAM 200 TO BEAM 205. READY TO INSTALL IN ACFT. INSTALLED BEAM 200 TO ACFT.Nov 7, 2008 · N404UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA06375Floorbeam · corrodedBEAM 235 HAS CORROSION AT AFT END OF FRAME 68. REMOVED FASTENERS BEAM STILL NEEDS REMOVED. REMOVED BEAM 235. NEW BEAM IS ON BENCH AND IS DRILLED OUT, MOUNTS ARE HELD IN PLACE. PLACED SEALANT AND HARDWARE BY BEAM. REPLACED BEAM.Nov 5, 2008 · N404UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA03792Smoke Detector · faultyLAVATORY DETECTOR FAULT DISPLAYED ON UPPER ECAM SCREEN. FOUND SMOKE DETECTOR MALFUNCTIONED. REPLACED SMOKE DETECTOR, SYS OPS CHECKED NORMALLY.Jul 8, 2008 · N404UA · Airbus A320232 · Smoke DetectionSDR 2008UALA03522Charger · faultyEMERG LIGHT TEST FAILED AFTER SLIDE CHANGE..."L EMERG BATT" FAULT. WEAK BATTERY, REPLACED LEFT OVERWING BATTERY & CHARGER. TEST OK.Jun 22, 2008 · N404UA · Airbus A320232 · Emergency LightingSDR 2008UALA02459Relay · failedAPU FIRE EXTINGUISHING CIRCUIT CHECK FAILS. FOUND FLIGHT GROUND RELAY 43WF FAILING. FLIGHT GROUND RELAY 43WF REPLACED, OPS TESTED SYSTEM NORMAL.Apr 25, 2008 · N404UA · Airbus A320232 · Fire Bottle, PortableSDR 2008UALA01769Computer · faultedF-CTL ELAC 2 FAULT ON UPPER ECAM. PERFORMED RESET AND RECURRED. ELAC INTERMITTANT, BAD MPS BOARD INTERNAL. REPLACED ELAC 2, ALL TESTS NORMAL.Mar 28, 2008 · N404UA · Airbus A320232 · Flight Control SystemSDR 2008UALA01688Window Frame · dentedDENT 12 INCH BELOW F/O WINDOW FRAME 5.5 INCH HIGH 4.5 INCH WIDTH 0.1 DEEP. 12 INCHES ABOVE CF9026. SUPPLEMENTAL DATA UPDATE ACCOMPLISHED MAJOR REPAIR IN SFO.Mar 25, 2008 · N404UA · Airbus A320232 · Fuselage Main, StructureSDR 2008UALA00462Light · inoperativeSEAT MOUNTED FLOOR PROXIMITY EMERGENCY ESCAPE LIGHT OUT AT SEAT 24C. REPLACED LIGHT ASSY.Jan 27, 2008 · N404UA · Airbus A320232 · Emergency LightingSDR 2007UALA03420Light · inoperativeAISLE EMERGENCY LIGHT PATH HAS LIGHTS OUT AT ROW 18, 19, 21. FOUND LAMPS FAULTY. RELAMPED EMERGENCY LIGHTS AT ROW 18,19,21.Aug 25, 2007 · N404UA · Airbus A320232 · Emergency LightingSDR 2007UALA03419Light · brokenAISLE EMERGENCY LIGHT PATH HAS LIGHT BROKEN AT SEAT 17. UNKNOWN DAMAGE TO LIGHT ASSY. REPLACED LIGHT ASSY AT SEAT 17.Aug 25, 2007 · N404UA · Airbus A320232 · Emergency LightingSDR 2007UALA00799Wire · shortedCABIN EMERGENCY LIGHTING DOES NOT TEST OK. SEAT FOUND MOUNTED ON TOP OF POWER (RED) WIRE, CAUSING SHORT. RESPLICED ALL THREE SEATS TO POWER AND GROUND WIRE FROM WALL CONNECTOR. ROUTED PROPERLY AND SECURED. ALL LIGHTS TEST NORMAL. EMER LIGHT TEST AT ATTNDT PAMar 17, 2007 · N404UA · Airbus A320232 · Light System WiringSDR 2007UALA00422A/C Pack · overheatedPACK 2 OVERHEAT DISPLAYED ON UPPER ECAM SCREEN. AIR CREW COMMENTS: FLIGHT ATTENDANT OBSERVED VERY FAINT SMOKE IN BACK AS WELL AS ODOR. [SUP 05-16-07] DETERMINED THAT AIR CYCLE MACHINE IN PACK 2 HAD SEIZED DUE TO FAILED BEARINGS.Feb 12, 2007 · N404UA · Airbus A320232 · Cabin Cooling SystemSDR 2007UALA00434Slide · faultyFOUND AT PTP PANEL TEST LEFT INTER EXTERNAL FAULTS. [SUP 05-16-07] REPLACED THE LT OVERWING SLIDE ASSEMBLY. AT OVERHAUL, DETERMINED THAT THE PACK BOARD WAS FAULTY.Feb 9, 2007 · N404UA · Airbus A320232 · Escape SlideSDR 2006UALA02196Cover · dislodgedSLIDE COVER AT 2L COMES OFF. REPLACED 2 LEFT SLIDE RAFT.Nov 15, 2006 · N404UA · Airbus A320232 · Escape SlideSDR 2006UALA02085Valve · unserviceableLOW BOTTLE PRESSURE. SHOP FINDINGS: LEAKING AROUND FILL VALVE O-RING. REPLACED FILTER VALVE AND FILL VALVE O-RING.Oct 27, 2006 · N404UA · Airbus A320232 · Escape SlideSDR 2006UALA00138Skin · damagedPUNCTURE TO FUSELAGE SKIN FOUND ON LT SIDE BETWEEN BODY STATION 11100 TO 12167. APPROX FRAME 27 TO FR 29. DAMAGE ENCOMPASSES A 40 INCHES LONG HORIZONTAL INDENTATION, 21.5 INCH LONG X 15 PUNCTURE. DAMAGE IS ALONG SKIN LAP. MAJOR REPAIR DOUBLER INSTALLED IN AJan 26, 2006 · N404UA · Airbus A320232 · Fuselage Main, Plate/Skin
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