N451UA

Service difficulty reports · 97

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 = 'N451UA' 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 UALA2013041102458Switch · brokenF/O OXYGEN TEST SWITCH BROKEN. ADJUSTED AND SECURED SWITCH, OPS CHECKED OKAY.Apr 11, 2013 · N451UA · Airbus A320232 · Crew Oxygen SystemSDR UALA2012111206507Stowage Box · faultyF/O O2 MASK MICROPHONE INOPERATIVE. SWAPPED F/O AND 2ND OBS O2 BOX F/O O2 MASK MICROPHONE OPS CHECKED GOOD.Nov 10, 2012 · N451UA · Airbus A320232 · Audio Integrating SystemSDR UALA2012101205815Oxygen Bottle · low pressureCREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. CONFIRMED PRESS DOWN TO APPROX 980 PSI. REMOVED AND SERVICED CREW BOTTLE PER AMM. OPS AND LEAK CHECKS GOOD. SAFETIED VALVE OPEN AFTER BOTTLE RE-INSTALLED.Oct 10, 2012 · N451UA · Airbus A320232 · Crew Oxygen SystemSDR UALA2012081304435Oxygen Bottle · low pressureFIRST CLASS O2 BOTTLE GAUGE SHOWS LOW PRESSURE. REPLACED O2 BOTTLE.Aug 11, 2012 · N451UA · Airbus A320232 · Portable Oxygen SystemSDR UALA2012071203773Computer · faultyON TAKEOFF, CLIMB-OUT HAD TO USE EXCESSIVE FORWARD STICK INPUT TO KEEP PITCH FROM INCREASING. REPLACED ELAC 2. REPLACED ELAC 2 AS PER MM, CHECKED GOOD PER MM. ACFT IS FULL LAND III CAPABLE.Jul 12, 2012 · N451UA · Airbus A320232 · Flight Control SystemSDR UALA2012052903011Pitot Line · obstructedTAKEOFF ABORTED ABOUT 90 KTS DUE TO FIRST OFFICERS AIRSPEED INOPERATIVE. AUTOBRAKES ACTIVATED. REPLACED ADM 19FP2 PER MM. SYSTEM RETURNED TO NORMAL. REPLACED FIRST OFFICERS PITOT TUBE DUE TO OBSTRUCTION. LEAK CHECK AND HEAT CHECKS GOOD.May 29, 2012 · N451UA · Airbus A320232 · Pitot/Static SystemSDR UALA2012050302615Microphone · inoperativeCAPTAIN'S HAND MICROPHONE INOPERATIVE, SWAPPED THE CAPTAIN'S MICROPHONE WITH THE FIRST OBS'S MICROPHONE. INSTALLLED NEW MICROPHONE.May 1, 2012 · N451UA · Airbus A320232 · Audio Integrating SystemSDR UALA2012050202593Microphone · inoperativeCAPTAIN'S HAND MICROPHONE INOPERATIVE. SWAPPED THE CAPT'S MICROPHONE WITH THE FIRST OBS'S MICROPHON.May 1, 2012 · N451UA · Airbus A320232 · Audio Integrating SystemSDR UALA2012022301092Cover · crackedRUDDER PEDALS JAMMED DURING FLARE. INORDINATE FORCE REQ'D TO MOVE PEDALS. UNSAFE FOR FLIGHT. RUDDER PEDAL ADJUSTMENT FOOTREST IS LOOSE AND PUSHES PEDALS AT TIMES. FIRST OFFICERS RUDDER PEDALS WILL NOT ADJUST. RUDDER PEDAL ADJ IS NOT AFFECTED, COVER BETWEENFeb 23, 2012 · N451UA · Airbus A320232 · Rudder Control SystemSDR UALA2011080804150Oxygen Mask · leakingF/O OXYGEN MASK DOES NOT SELF TEST PROPERLY. FAILS THE LEAK TEST. REPLACED F/O'S O2 MASK ASSY PER AMM.Aug 6, 2011 · N451UA · Airbus A320232 · Crew Oxygen SystemSDR UALA2011062203078Skin · damagedAFT-FUSELAGEDAMAGE. FAIRINGS 198BB & 198GB DAMAGED ALONG WITH THREE INNER SUPPORT RIBS.Jun 22, 2011 · N451UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR UALA2011032901503Trim System · malfunctionedACCOMPLISHING AN OPERATIONAL TEST OF TRIMMABLE HORIZONTAL STABILIZER. TEST FAILS STEP 7 OF AMM. THS ACTUATOR NEVER STOPS. ON THE LEFT AND RIGHT THS ACTUATOR CONTROL SHAFT THE LOCKWIRE AND CAPS ARE REMOVED. PARTS IN COCKPIT. STILL COULDN'T GET EITHER LT NOMar 28, 2011 · N451UA · Airbus A320232 · Stabilizer Control SystemSDR UALA2011021400766Unknown · vibrationLATERAL MOD VIBRATION FELT IN AFT GALLEY DURING CLIMB. PERFORMED RUDDER, AND ELEVATOR T/E FREE PLAY CHECK DUE TO VIBE REPORTING FORM DATA. 2 LEGS IN A ROW HAVE AFT FUSELAGE VIBE. PERFORMED ELEVATOR SERVO CONTROLS AND HINGE BEARING CONDITION CHECK AND RUDDEFeb 12, 2011 · N451UA · Airbus A320232 · Flight Control SystemSDR UALA2011011700252Control Unit · faultySMOKE LAV AND CARGO DET FAULT ECAM. SYS FAULT RESET UNSUCCESSFUL. REPLACED SMOKE DETECTION CONTROL UNIT, TESTED OK.Jan 15, 2011 · N451UA · Airbus A320232 · Smoke DetectionSDR UALA2010111504205Light · odorCAPTS MAP LIGHT EMITTED ELECTRICAL SMOKE ODOR BEFORE BURNING OUT. CHECKED CB Z5: NOT TRIPPED (ASM 33 -12-00), PERFORMED GENERAL VISUAL INSPECTION OF MAP LIGHT, NO HAZARDS EVIDENT. REPLACED LIGHT ASSY, CHECKS OK NOW.Nov 13, 2010 · N451UA · Airbus A320232 · Flight Compartment LightingSDR UALA2010050701556Power Supply · inoperativeEPSU INT LOAD FWD L' ON PTP. REPLACED EMERGENCY POWER SUPPLY UNIT 10W. OP CHECKS GOOD.May 7, 2010 · N451UA · Airbus A320232 · Emergency LightingSDR UALA2009071302022Panel · faultyEMERGENCY EVACUATION COMMAND IS INTERMITTENT FROM THE AFT ATTENDANT'S PANEL. REMOVED & REPLACED AFT ATTENDANT'S PANEL. ACP OPS CHECK ON BASE NON-ROUTINE K5481G. ALL CHECKS OKAY.Jul 10, 2009 · N451UA · Airbus A320232 · Interphone/Passenger Announcement (PA) SystemSDR UALA2009071001997Connector · defectiveEMERGENCY EXIT LIGHT ROW SIX IS INOPERATIVE. REMOVED & REPLACED EMERGENCY EXIT LIGHT ASSY LENS P/N BC5-0533-003 & SOCKET CONNECTOR P/N 3416402. OPS CHECKED GOOD.Jul 9, 2009 · N451UA · Airbus A320232 · Light System WiringSDR 2008UALA05546Floorbeam · corrodedBEAM 255 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. REMOVED BEAM. BEGAN INSTALLING FLOORBEAM 255 IN A/C. COMPLETED INSTALLATION OF FLOORBEAM 255. INSPECTED INSTALLATION OF BEAM 255 FOR SAFETY AND SECURITY.Aug 31, 2008 · N451UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA05532Floorbeam · corrodedFLOORBEAM 250 CORRODED (MARKED). ALSO HAS 8 EA SHEARED FASTENERS ON OUTBOARD SIDE OF BEAM (MARKED). MAJOR REPAIR ACCOMPLISHED. BEAM REMOVED, TRANSFERRED FASTENER HOLES TO NEW BEAM. BEGAN INSTALLING FLOORBEAM 250 IN AC. COMPLETED INSTALLATION OF FLOORBEAM Aug 29, 2008 · N451UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA05531Sill · corrodedDOOR SILL 2R HAS CORROSION (MARKED). DOOR SILL 2R HAS CORROSION (MARKED). MAJOR REPAIR ACCOMPLISHED. REMOVED DOOR SILL. PICKED UP HOLES IN NEW SILL PAN. STARTED INSTALLING HI-LOKS THRU EXTERNAL SKIN COMMON TO DOOR 2R SILL BEAM ONLY. CONTINUED INSTALLING FAug 29, 2008 · N451UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA05502Floorbeam · corrodedFLOORBEAM 225 CORRODED AROUND FWD NUT PLATE HOLE (MARKED). MAJOR REPAIR ACCOMPLISHED: REMOVED BEAM, DRILLED BEAM AND ATTACH ANGLES. INSTALLED FLOORBEAM 225 IN A/C.Aug 27, 2008 · N451UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA05485Floorbeam · corrodedFLOORBEAM 245 CORRODED (MARKED). MAJOR REPAIR ACCOMPLISHED. REMOVED BEAM. TRANSFERRED ATTACHING PARTS AND IS READY FOR FIT INTO AC. BEAM INSTALLED. INSPECTED THE INSTALLATION OF BEAM 245 FOR SECURITY AND FOUND SECURE.Aug 26, 2008 · N451UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA05475Shear Plate · corrodedRIGHT SHEAR PLATE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVED RT SHEAR PLATE. INSTALLED NEW RT SHEAR PLATE.Aug 26, 2008 · N451UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA05484Sill · corrodedDOOR 2L SILL IS CORRODED (MARKED).Aug 26, 2008 · N451UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA05474Floorbeam · corrodedFLOORBEAM 235 CORRODED (MARKED). MAJOR REPAIR ACCOMPLISHED. INSTALLED TIE DOWN FITTINGS FOR LAV AND GALLEY MODULES ONTO NEW FLOORBEAM 235. FITTED BEAM 235 TO ACFT (PICKED UP HOLES) AND FITTED 2EA. NEW SPLICES AT FWD END OF BEAM 235. INSTALLED FLOORBEAM 23Aug 25, 2008 · N451UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA05448Floorbeam · corrodedFLOOR BEAM 205 IS CORRODED (MARKED). *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVED FLOORBEAM 205. REMOVED ANGLES, WORKING ON BENCH. INSTALLED GALLEY ATTACH POINTS, DRILLED NEW SPLICE ANGLES. INSTALLED NEW SPLICE ANGLES.Aug 24, 2008 · N451UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA05447Floorbeam · corrodedFLOORBEAM 200 IS CORRODED (MARKED). MAJOR REPAIR ACCOMPLISHED. REMOVED FLOORBEAM 200. REMOVED ANGLES ATTACHED TO BEAM 165, DRILLED SPLICE ANGLES FOR BEAM 200 TO 205. COMPLETED INSTALLATION. Aug 24, 2008 · N451UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA05446Floorbeam · corrodedFLOORBEAM 165 CORRODED (MARKED). MAJOR REPAIR ACCOMPLISHED. REMOVED FLOORBEAM 165. REMOVED ANGLES. TRANSFERRED BRACKETS AND ATTACHED BEAM 165 AND 200 WITH SPLICE ANGLES WORKING ON BENCH. COMPLETED INSTALLATION.Aug 24, 2008 · N451UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA05445Floorbeam · corrodedFLOORBEAM 210 IS CORRODED (MARKED). MAJOR REPAIR ACCOMPLISHED. REMOVED FLOORBEAM 210. TRANSFERRED ATTACH BRACKETS AND STARTED ATTACHING TO BEAM 175. BEAMS 210 AND 175 ARE TOGETHER AND NEED THE FWD END DRILLED TO BRACKETS IN A/C. PICKED UP REMAINING HOLESAug 24, 2008 · N451UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA05444Floorbeam · corrodedFLOORBEAM 175 IS CORRODED (MARKED). MAJOR REPAIR ACCOMPLISHED. REMOVED FLOORBEAM 175. TRANSFERRED CABLE ATTACH BRACKETS AND STARTED ASSEMBLY WITH BEAM 210. BEAM 175 AND 210 ARE TOGETHER AND NEED FWD END OF BEAM PUT INTO AC AND DRILL FWD ATTACH HOLES. PICAug 24, 2008 · N451UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA02695Light · inoperativeSEAT 8A EMERGENCY LIGHT INOP.May 8, 2008 · N451UA · Airbus A320232 · Emergency LightingSDR 2008UALA01354Oxygen System · lowTHE O2 NEEDS SERVICING SHOWS 1420. SERVICED CREW O2 TO FULL, NO LEAKS NOTED AT TIME OF SERVICE.Mar 12, 2008 · N451UA · Airbus A320232 · Crew Oxygen SystemSDR 2008UALA00594Power Supply · failedL MID CABIN EPSU FAILED TEST. FOUND EPSU FAILED. REPLACED EPSU, ALL TESTS NORMAL.Feb 3, 2008 · N451UA · Airbus A320232 · Emergency LightingSDR 2008UALA00229Power Supply · dischargedEMERGENCY LIGHTS FAILS TEST. FAULTS EPSU UNIT LEFT. EPSU FAILURE. REPLACED EPSU, OPS CHECKED NORMAL.Jan 12, 2008 · N451UA · Airbus A320232 · Emergency LightingSDR 2007UALA04801Power Supply · dischargedEMERGENCY LIGHT TEST FAIL RIGHT SIDE POWER SUPPLY. FOUND EPSU FAILURE. REPLACED RT EPSU, NO REPEATS.Nov 22, 2007 · N451UA · Airbus A320232 · Emergency LightingSDR 2007UALA04415Light · inoperativeSEAT 26C EMERGENCY LIGHT INOP: MISSING LENS & LIGHT ASSY DAMAGED. REPLACED LIGHT ASSY, OPS CHECK OK.Oct 28, 2007 · N451UA · Airbus A320232 · Emergency LightingSDR 2007UALA03743Oxygen System · reads lowCREW OXYGEN SYSTEM LOW. RECORD PRESSURE PRIOR TO SERVICING.Sep 14, 2007 · N451UA · Airbus A320232 · Crew Oxygen SystemSDR 2007UALA02677Hose · brokenCAPTAIN`S O2 MASK WEB WILL NOT INFLATE INNER HOSE BROKEN. INNER HOSE BROKEN ON CAPTAINS O2 MASK. REPLACED MASK ASSY.Jul 17, 2007 · N451UA · Airbus A320232 · Crew Oxygen SystemSDR 2007UALA02337Unknown · odorSMELL THRU OUT A-C. UNKNOWN SMELL. PAX EYES AND NOSES BURNING.Jun 29, 2007 · N451UA · Airbus A320232 · Air Distribution SystemSDR 2006UALA01755Battery · failedCABIN EMERGENCY LIGHT TEST PANEL, MSG DISPLAYED (EPSU COMM AFT L, ATA 33-51-38) WHILE TRYING TO ACCOMPLISH EMERGENCY LIGHT TEST. REPLACED AFT EPSU BATTERY, OPS CHECKS GOOD.Sep 10, 2006 · N451UA · Airbus A320232 · Emergency LightingSDR 2006UALA00512Valve · odorBURNED RUBBER ODOR IN CABIN REPORTED BY CREW. AFT TRIM AIR VALVE NOT OPERATING PROPERLY. REPLACED THE TRIM AIR VALVE.Mar 16, 2006 · N451UA · Airbus A320232 · Air Distribution SystemSDR 2005UALA00590Tape · separatedHINGE TAPE ON FLOOR RAMP IS SEPARATED. ADHESIVE FAILURE, RESULTED IN TAPE SEPARATION DURING THE PRESSURIZATION OF THE ASSEMBLY. UNIT WAS SENT TO OEM FOR REPAIR/DISPOSITION.Jun 24, 2005 · N451UA · Airbus A320232 · Escape SlideSDR 2004UALA00766Pump · inoperativeLEFT TANK PUMP NR 2 ECAM, NR 1 PUMP WAS PREVIOUSLY DEFERRED. THE LEFT WING TANK NR 2 FUEL BOOST PUMP WAS INOPERATIVE. REPLACED LEFT WING TANK FUEL NR 2 FUEL BOOST PUMP. OPERATIONS CHECK NORMAL.Aug 14, 2004 · N451UA · Airbus A320232 · Fuel Boost PumpSDR 2001UALA01196AileronRH AILERON ASSEMBLY UPPER SKIN DAMAGE BY HAIL RESULTING IN A DENT 1 INCH IN DIAMETER ON THE UPPER SKIN, .5 INCHES FROM THE INBOARD EDGE AND 5 INCHES FROM THE TRAILING EDGE. THERE IS ALSO A CRACK AT THE BOTTOM OF THE DENT MEASURING .5 INCHES LONG. ACCOMPLISHEJun 20, 2001 · N451UA · Airbus A320232 · AileronsSDR 99UAL900615Blower · failedA LOUD NOISE WAS HEARD UNDER FLIGHT DECK AND F/A SMELLED ELECTRICAL ODOR. PROBLEM WAS POSIBLE AVIONICS COOLING SYSTEM. AFTER OVERRIDING SYSTEM, SMELL DISSIPATED AND NOISE STOPPED. ALL SYSTEMS REPORTING NORMAL. FLIGHT CONTINUED TO DESTINATION. *S/D* THE ANov 29, 1999 · N451UA · Airbus A320232 · Air Distribution FanSDR 98UAL900482Gear · failedDIVERTED TO ONT WITH NR 2 ENGINE SHUTDOWN DUE TO OIL PRESSURE INDICATION. *S/D* OIL PUMP DRIVE GEAR FAILED CAUSING LOSS OF OIL PRESSURE. GEAR FAILED FROM A MANUFACTURING DEFECT. CONSIDERED ISOLATED CASE.Sep 30, 1998 · N451UA · Airbus A320232 · Turbine Engine Oil System
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