N474UA

Service difficulty reports · 113

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 = 'N474UA' 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 CALA2017100203422Lamp · inoperativeRED EMERGENCY LIGHT AT SEAT 21C INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-18. OPS CHECKED GOOD.Oct 2, 2017 · N474UA · Airbus A320232 · Emergency LightingSDR CALA2016111100880Door · not seatedL FWD EMER EXIT DISPLAYED ON UPPER ECAM SCREEN. DOOR REINSTALLED LEFT FWD OW EXIT IAW AMM 52-21-11.Nov 11, 2016 · N474UA · Airbus A320232 · Emergency ExitsSDR CALA2016111100871Slide · unwanted deployLEFT FWD SLIDE INADVERTENTLY DEPLOYED. REPLACED LEFT OVERWING SLIDE ASSY AND INFLATION RESERVOIR IAW AM M 25-62-42 AND 25-62-46. OP CHECKED OK.Nov 11, 2016 · N474UA · Airbus A320232 · Escape SlideSDR CALA2015052693812Door Sill · corrodedAFT CABIN L2 DOOR SILL UPPER SURFACE HAS CORROSION. BLENDED L2 DOOR SILL, REMOVED CORROSION & INSTALLED REPAIR IAW SRM 53-41-14 FIG 201. REPAIR PRINCIPLE 5 REPAIR IS PERMANENT WITH NO SRI REQUIREMENT.May 19, 2015 · N474UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2015052193803Door Sill · corrodedAFT CABIN L2 DOOR SILL UPPER SURFACE HAS CORROSION. BLENDED L2 DOOR SILL, REMOVED CORROSION & INSTALLED REPAIR IAW SRM 53-41-14 FIG 20 1 REPAIR PRINCIPLE 5 REPAIR IS PERMANENT WITH NO SRI REQUIREMENT.May 19, 2015 · N474UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014030390508Unknown · malfunctionedAPU WILL NOT START, SECOND ATTEMPT TO START, NO GOOD. CYCLED APU CONTROL & ECB CB'S NO HELP. OK TO DEFER, APU INOPERATIVE IAW MEL 4910B.Mar 1, 2014 · N474UA · Airbus A320232 · Airborne Auxiliary Power Unit (APU) SystemSDR CALA2013122693919Warning System · activatedAEVC SKIN AIR OUTLET VLV FAULT, FLT DIVERTED.Dec 23, 2013 · N474UA · Airbus A320232 · Cabin Pressure Control SystemSDR CALA2013102392298Clamp · brokenCLAMP ON FIRST CLASS OXYGEN BOTTLE BROKEN.Oct 22, 2013 · N474UA · Airbus A320232 · Portable Oxygen SystemSDR CALA2013102192198Control Valve · faultyPACK 1 & 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. BOTH VLV POSITION INDICATIONS AMBER. - AIR. RT PACK PLACED UNDER MEL LT PACK FUNCTIONED OK. REPLACED FLOW CONTROL VLV IAW AMM, SYSTEM OPERATIONS & LEAKS CHECKED GOOD.Oct 19, 2013 · N474UA · Airbus A320232 · Cabin Cooling SystemSDR CALA2013101592066Sensor · malfunctionedSLAT SYSTEM 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. HAD THIS ECAM TWICE DURING FLT ACCOMPANIED BY SLOW SLAT FLAP RETRACTION AFTER TAKEOFF, ONE TIME IN CRUISE. FAULTS "SLT FLP CSU 51CV OR WIRING TO SLT 2", CSU PCN 482-9083. REPLACED COMMAND SENSOR UNIT IAW MOct 14, 2013 · N474UA · Airbus A320232 · Leading Edge Slat Control SystemSDR CALA2013100491728Seal · out of positionLT WING BODY AFT BODY FAIRING SEAL IS OUT OF PLACE. SEAL IS AFT LT HAND AFT ELEPHANT EAR FAIRING. INTERIM REPAIR WITH HIGH SPEED TAPE MADE.Oct 3, 2013 · N474UA · Airbus A320232 · Aerodynamic FairingsSDR CALA2013092791532Controller · faultyON ENGINE SHUTDOWN GOT BOTH BLOWER & EXTRACT FAN FAULTS. CW MEL 2126V FOR SKIN AIR INLET VALVE. R & R AEVC, OPERATIONS NORMAL. REVERSED DDP NO FAULTS FOUND ACFT OK FOR SRVC REMOVED PLACARD.Sep 27, 2013 · N474UA · Airbus A320232 · Air Distribution SystemSDR CALA2013092591442Generator · faultyAFTER EXTENDING THE RAT, THE AIRCRAFT ESSENTIAL BUS STOPPED WORKING. R & R CSMG IAW A319-320 AMM CH 24-24-51. R & R POWER CONTACTOR 15XE IAW A319-320 AMM CH 24-25-55. AC GENERATION SWITCH CHECKED GOODSep 25, 2013 · N474UA · Airbus A320232 · AC Generator-AlternatorSDR CALA2013092091288Sill · corrodedR2 DOOR SILL CORRODED AT PREVIOUS REPAIR BETWEEN FR 66-68. REINSTALLED REPAIR IAW SRM 53-41-14.Sep 19, 2013 · N474UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2013092091287Stringer · corrodedSTRINGER 43L AT FRAME 34 IS CORRODED. REPLACED FACTORY STRINGER SECTION IAW SRM 51-42-1.Sep 19, 2013 · N474UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2013091891265Skin · corrodedINTERNAL FS SKIN BETWEEN FR34 & 35, STRINGER 41L & 41R HAS CORROSION. FOUND SKIN DAMAGE AROUND FASTENER HOLES.Sep 17, 2013 · N474UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2013091891264Stringer · corrodedSTRINGER 42R AT FRAME 34 IS CORRODED.Sep 17, 2013 · N474UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2013091891263Plate · wornNR 1 PYLON AT RIB 5 LOWER CHAFE PLATE IS WORN. REMOVED PLATE & BLENDED THE AREA. MATERIAL LOSS IS .002\ WITHIN LIMITS IAW SRM 54-51-12, PG 209-210. HFEC INSPECTED BLENDED AREA & FOUND NO CRACKS. REINSTALLED THE PLATE WITH AN EXTENDED WEAR STRIP IAW SRM 54-5Sep 14, 2013 · N474UA · Airbus A320232 · Nacelle/Pylon Miscellaneous StructureSDR CALA2013091891262Skin · dentedDENT FOUND LT SIDE OF FS APPROXIMATELY 2\ AFT OF L1 DOOR. DENT MEASURES 5-8\BY 5-8\BY 0.031\ DEEP. WITHIN LIMITS IAW SRM 53-11-11. HFEC SCANNED INNER & OUTER SURFACE OF DENT, NO CRACKS NOTED.Sep 14, 2013 · N474UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2013081690486Sensor · inoperativeRT WINDOW ANTI-ICE ECAM MESSAGE. PERFORMED TEST IAW TSM 30 -42-00-810-814. PERFORMED CFDS RT SLIDING WINDOW SENSOR BAD.Aug 15, 2013 · N474UA · Airbus A320232 · Windshield/Door Rain/Ice RemovalSDR UALA2013071905076Line · leakingCREW OXYGEN SYSTEM LOW. O2 SYS SERVICED TO1550 PSI. 2 HOURS 40 MINUTES INTO FLT PRESSURE 1370. SUSPECT SYS LEAK, FOUND O2 LINE FROM LT SIDE TEE FITTING LEAKING AT CAPTAIN`S O2 BOX, LINE HAD BADLY CRUSHED WASHER, R & R LINE, SERVICED O2 TO 1900 PSI AND O2 HEJul 18, 2013 · N474UA · Airbus A320232 · Crew Oxygen SystemSDR UALA2013071504916Contactor · faultyBCL 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. ELEC. CREW COMMENTS: IN CRUISE ECAM. ELEC BCL 1 FAULT. ACCOMPLISH CHRONIC REVIEW. REF TSM 24-38-00-810-806- A THE BAT LINE CONTACTOR FAILED. R & R BAT LINE CONTACTOR BCL-1 REF AMM, OPS CHECKS NORMAL.Jul 12, 2013 · N474UA · Airbus A320232 · DC Generating SystemSDR UALA2013062504402Fire Detector · false indicationAPU EMERGENCY SHUTDOWN, APU FIRE LIGHT ON. NO SMOKE NOTED FROM OUTSIDE. NO SMOKE SEEN BY FLIGHT CREW. ACCOMPLISHED BITE TEST OF FIRE DETECTION AND APU EBU IAW AMM 26-13-00-710 AND 49-00-00-710 . NO FAULTS NOTED. RAN APU ALL OPS CHECKED OK.Jun 22, 2013 · N474UA · Airbus A320232 · Fire DetectionSDR UALA2013061804218Unknown · odorF/A SMELLED SMOKE IN AFT GALLEY COMING FROM AIR VENT OVER GALLEY TABLE, NO OVEN IN BACK. THERE WAS NO VISIBLE SMOKE REPORTED BY FA. APPEARS TO HAVE EMANATED FROM COFFEEMAKERS, BURNED COFFEE ODOR. PULLED COFFEEMAKERS OUT AND INSPECTED, NO DEFECTS NOTED. CLEANJun 16, 2013 · N474UA · Airbus A320232 · Air Distribution SystemSDR UALA2013051403348Fire Detector · faultyFIRE LOOP A FAULT DISPLAYED ON UPPER ECAM SCREEN, ENG 1. REPLACED NR 1 FDIU REF MM 26-12-34 SYS CHECKS NORMAL WHILE AT THE GATE.May 11, 2013 · N474UA · Airbus A320232 · Fire DetectionSDR UALA2013043003008Display · inoperativeLOWER ECAM SCREEN WENT BLANK NO DASH LINE ON LANDING. REPLACED ECAM DU REF MM, OPS CHECK GOOD.Apr 28, 2013 · N474UA · Airbus A320232 · Central DisplaySDR UALA2013030501322Battery Pack · faultyFORWARD F/A PANEL EMERGENCY LIGHT TEST FAULT. EPSU BATTERY EMERGENCY RT AND EPSU BATTERY EMERGENCY LT. REPLACED BATTERY PACK.Mar 5, 2013 · N474UA · Airbus A320232 · Emergency LightingSDR UALA2013021300864Seal · damagedAIRFRAME VIBRATION WITH FLAPS FULL NOT EXISTENT AT FLAPS THREE. FREE MOVEMENT AT TRAILING EDGE OF FLAPS, SPHERICAL BEARING. FOUND RIGHT WING TO FUSELAGE FAIRING SEAL SEVERLY DAMAGED. REPLACED SEAL PER AMM. DIAGNOSED PER TSM 27-54-00. NO OTHER DEFECTS WERE FOFeb 13, 2013 · N474UA · Airbus A320232 · Aerodynamic FairingsSDR UALA2012092005322Fastener · poppedFASTENER POPPED NEAR LEFT PACK OUTFLOW. RE-SECURED FASTENER.Sep 18, 2012 · N474UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2012091105102Unknown · malfunctionedF/O'S WINDSHIELD HEAT IS INOP. SLIDING WINDOW INOP. FAULTING SLIDING WINDOW SENSOR, WORK WITH MT 30-003. OPBLM PARTS: 565-2103 9F21895-501 (HARNESS). CYCLED WINDOW HEAT CBS, FAULT CLEARED WITH NORMAL INDICATIONS. NO FURTHER MAINTENANCE ACTION NEEDED PER OSep 9, 2012 · N474UA · Airbus A320232 · Windshield/Door Rain/Ice RemovalSDR UALA2012082204691Valve · faultyGEAR DOORS STUCK, RTFL. REF TSM32-31-00-810-807-A. REPLACED VALVE AS PER AMM, OPERATIONAL COMPLETE.Aug 22, 2012 · N474UA · Airbus A320232 · Landing Gear Door Retract SectionSDR UALA2012071203772Skin · scratchedSCRATCH ON L2 DOOR SKIN 11.25 INCH BELOW DOOR HANDLE CUT OUT, 14 INCHES AFT OF LEADING EDGE OF DOOR. SCRATCH IS VERTICAL AND 1.75 INCHES LONG. SCRATCH IS 2.25 INCHES AFT OF NEAREST RIVETS. REWORKED SCRATCH PER SRM. ALODINED AND PRIMED AREA. WITHIN LIMITS Jul 10, 2012 · N474UA · Airbus A320232 · Passenger/Crew DoorsSDR UALA2012061403259Transmitter · faultyCREW REPORT: NR 1 ENGINE OIL QTY FLUCUTATING 3.5 TO 7.5 TO 13.0 STABILIZING AT 6.0 MAINT CHECKED OIL TANK NR 1 ENGINE PER MEL 7931A, NO OIL ADDED. REPLACED NR 1 ENG OIL QTY TRANSMITTER PER MM, OP CHECKED OKAY.Jun 14, 2012 · N474UA · Airbus A320232 · Engine Oil QuantitySDR UALA2012060803137Actuator · faultyAPU WILL NOT START. APU DOORS WILL NOT OPEN TO ALLOW APU START. REPLACED APU DOOR ACTUATOR, OPS CHECKED GOOD.Jun 8, 2012 · N474UA · Airbus A320232 · APU Core EngineSDR UALA2012042302436Switch · stickingRADIO TRIGGER SWITCH ON F/O SIDE STICK SOMETIMES STICKS IN TRANSMIT POSITION. REPLACED FIRST OFFICER'S PUSH TO TALK SWITCH ON THE SIDE STICK.Apr 21, 2012 · N474UA · Airbus A320232 · Communications SystemSDR UALA2011122207069Module · faultedLOST NOSE WHEEL STEERING A 2ND TIME. REPLACED BSCU NO HELP, CFDS FAULTS 6GC STEERING ELECTRO HYD MODULE, PARTS ON HAND. WILL RPL TERMINAL WORKING.Dec 21, 2011 · N474UA · Airbus A320232 · Landing Gear Steering SystemSDR UALA2011111506261Tab · bentCREW REPORT: PIECE OF FLAT METAL PROTRUDING FROM BOTTOM OF RIGHT ENGINE AFT OF BOTTOM LATCH. NR 1 LATCH TAP FOR LATCH OPEN IND BENT. STRAIGHTENED TAB. VERIFIED T-R HALVES SHUT PER MM. FAN COWLS SECURED CLOSED PER MM.Nov 14, 2011 · N474UA · Airbus A320232 · Engine Thrust ReverserSDR UALA2011101705598Latch · failedCOCKPIT CENTER JUMPSEAT WILL NOT LOCK IN STOWED POSITION. RELATCHED JUMPSEAT LATCH, LOCKS NORMAL IN STOWED POSITION.Oct 15, 2011 · N474UA · Airbus A320232 · Flight Compartment EquipmentSDR UALA2011072503807Drain Valve · leakingLEFT OUTER FUEL H20 DRAIN DRIPPING. REPLACED LEFT WING OUTER FUEL DRAIN VALVE 21QM IAW AMM.Jul 22, 2011 · N474UA · Airbus A320232 · Fuel StorageSDR UALA2011040401590Coffeemaker · faultyELEC SMELL IN GALLEY, FLIGHT DIVERTED. INVESTIGATED AFT GALLEY, FOUND NO EVIDENCE OF FIRE DAMAGE RELATED TO OVENS, ELECTRICAL PANELS, LIGHT PANELS AND LIGHT FIXTURES. DID FIND EVIDENCE OF ELECTRICAL ARCING BEHIND COFFEEMAKERS IN AFT GALLEY. ELECTRICALLY ISOApr 3, 2011 · N474UA · Airbus A320232 · Buffet/GalleysSDR UALA2010110304086Windshield · faultyLEFT WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN. ANTI ICE. WINDSHIELD FOUND FAULTY. WINDSHIELD REPLACED. OKAY FOR SERVICE.Nov 3, 2010 · N474UA · Airbus A320232 · Flight Compartment WindowsSDR UALA2010050301467Rod End · out of limitsVIBRATION-NOISE ENCOUNTERED IN FLIGHT NEED TO COMPLETE VIBRATION REPORTING CHECKLIST AND DEBRIEF MX ON ARRIVAL TO DESTINATION. VIBRATION FELT DURING CLIMB THROUGH FL270-360. SUSPECT RIGGING OR DOORS NOT ENGINE RELATED. ACP INTEGRITY CHECKS ON ELEVATOR AND RUDMay 2, 2010 · N474UA · Airbus A320232 · Rudder Control SystemSDR UALA2009101503239Connector · looseEMERGENCY LIGHT TEST MESSAGE *ESPU INT LOAD FWD L*. ACCOMPLISHED TROUBLESHOOTING AND FOUND LOOSE CONNECTOR AT LEFT OVERWING BATTERY CHARGER. RE-SECURED AND OPS TEST NORMAL.Oct 15, 2009 · N474UA · Airbus A320232 · Light System WiringSDR UALA2009101503240Light · inoperativeLEFT EXTERIOR OVERWING AFT EMERGENCY LIGHT INOP. REPLACED BULB AND ACCOMPLISHED LIGHT TEST. WORKS NORMAL.Oct 14, 2009 · N474UA · Airbus A320232 · Emergency LightingSDR UALA2009080302301Battery Pack · faultyAFTER LT OVERWING SLIDE CHANGE EMERGENCY LIGHT TEST SHOWS, EPSU BATTERY AFT L, REPAIR AS NECESSARY. REPLACED BATTERY PACK. GROUND CHECK AS NORMAL.Jul 31, 2009 · N474UA · Airbus A320232 · Emergency LightingSDR UALA2009011300147Slide · unserviceableDURING INTERIOR INSP, FOUND L1 DOOR SLIDE TO BE OUT OF LIMITS. REMOVED 1L SLIDE AND PINED PLACED IN SHOP. PUT ATTACHING HARDWARE BACK INTO ATTACHING HOLES IN ORDER NOT TO LOOSE THE BOLTS. GIRT BAR IS STILL ATTACHED TO SLIDE. INSTALLED LAST BOLT INTO THE SLIDEJan 13, 2009 · N474UA · Airbus A320232 · Escape SlideSDR UALA2008122407000Slide · low pressureTHE 1L SLIDE PRESSURE LOW. COLD SOAKED DOOR WAS OPEN FOR OVER 1 HR. OP PER MM 25-62-00 PG 603 (NOTE A).Dec 24, 2008 · N474UA · Airbus A320232 · Escape SlideSDR UALA2008120906800Slide · disconnectedFWD RT CABIN DOOR SLIDE PACK ASSY CONNECTOR BETWEEN CABLE LOOP ASSY AND COVER RELEASE CABLE WAS FOUND DISCONNECTED. SLIDE REPLACED DUE TO CRACKED MOUNTING LUG.Dec 9, 2008 · N474UA · Airbus A320232 · Escape SlideSDR UALA2008120906801Wire · pinchedBOTH OVERWING EXIT LIGHTS WILL NOT ILLUMINATE AND RT EPSU FAILED BITE TEST. FOUND EMERGENCY LIGHT WIRE PINCH UNDER SEAT TRACK ROW 10 LEFT. REMOVED WIRE AND REPAIRED DAMAGE WIRE, OPERATIONAL CHECKS OF LEFT AND RIGHT OVERWING LIGHTS CHECKS OK, ALSO NO FURTHER Dec 9, 2008 · N474UA · Airbus A320232 · Light System WiringSDR UALA2008120906799Connector · disconnectedLT AFT CABIN DOOR SLIDE CONNECTOR BETWEEN CABLE LOOP ASSY AND COVER RELEASE CABLE WAS FOUND DISCONNECTED. CABLE LOOP ASSY & COVER RELEASE CABLE CONNECTED.Dec 8, 2008 · N474UA · Airbus A320232 · Equipment/Furnishings Wiring
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