N484UA

Service difficulty reports · 91

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 = 'N484UA' 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 CALA2026060116684Fuel Cap · missingFUELER REPORTS CAP IS MISSING REQUESTING CDL FOR MISSING FUEL CAP. CONFIRMED NO LEAKS PRESENT. INSTALLED CAP ASSY REF IPC 28-25-41-02BMay 26, 2026 · N484UA · Airbus A320232 · Fuel StorageSDR CALA2026050515982Power Supply · faultedDURING CABIN EMERGENCY LIGHTING SYS CHECK, SYSTEM OK LIGHT NEVER CAME ON. EPSU UNIT L MESSAGE FOUND AFT LH EPSU UNIT TO BE FAULTY. REPLACED BATTERY PACK AND REPERFORMED CABIN EMERGENCY LIGHT SYSTEM CHECK AT PTP. SYS TEST OK.May 1, 2026 · N484UA · Airbus A320232 · Emergency LightingSDR CALA2025082708164Elec Connector · disconnectedROW 38 ABC ON SEAT EMERGENCY LIGHT INOP FOUND CONNECTOR ON SEAT DISCONNECTED, RECONNECTED & PERFORM EMERGENCY LIGHTING TEST PER AMM 33-51-00-710-804-A, OPS TEST GOODAug 23, 2025 · N484UA · Airbus A320232 · Light System WiringSDR CALA2025072106798Probe · faultedREJECTD T/O 50-60 KIAS DUE TO SPLIT POWER SETTING W/ NO ECAM ITEM UPDATED WITH CURRENT P2T2 SENSOR. ENG #2 REPLACED AT ENG #2 , P2T2 SENSOR PER AMM 73-22-11/401 CONFIG 13 . ALL TEST OK.Jul 18, 2025 · N484UA · Airbus A320232 · Fuel Control/Reciprocating EnginesSDR CALA2025052204910Engine · damagedPDA 2 REF LP #4882215 NO 6 STRUT FAIRING PANEL ASSEMBLY MISSING OUTBOARD SIDE. PANEL, FAIRING, NO. 6 STRUT, ASSEMBLY OF POST SBE72-0435, #2 ENGINE REPLACED DUE TO SHOUD DAMAGE AT 6 O'CLOCK POITION #2 ENGINE REPLACED DUE TO SHOUD DAMAGE AT 6 O'CLOCK POITION RMay 18, 2025 · N484UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR CALA2025042104037Wing · smokeRAMP REPORTS SMOKE COMING FROM WINGS, BURNING SMELL. CONTACTED FIRE DEPARTMENT, NO HEAT SHOWN ON THERMAL IMAGING, NO BURNING SMELL, NO EVIDENCE OF HEAT DAMAGE FOUND. DROPPED FLAP/S SLATS ON GROUND REF AMM 27-50-00, INSPECTED, SMOKE APPEARS TO CONDENSATION WIApr 19, 2025 · N484UA · Airbus A320232 · Wing StructureSDR CALA2025032403112Battery · faultyEPSU BATTERY EMER R INSTALLED SERVICEABLE BATTERY EPSU 12WL REF. AMM 33-51-38-400-002-A. OKAY TO CONTINUE.PARTS USED: 18-3351-3-0001, QTY :1Mar 22, 2025 · N484UA · Airbus A320232 · Emergency LightingSDR CALA2025030702623Light · malfunctionedEMER LIGHTS FLICKERED WITH ASSOC FAULTS PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHT IN REF TO AMM 33-51-00. OPS CHECK NORMAL. COULD NOT DUPLICATE FAULT.Mar 4, 2025 · N484UA · Airbus A320232 · Emergency LightingSDR CALA2024072600285Fuel Cap · missingPDA 2 REFUEL CAP MISSING FROM RIGHT WINGJul 25, 2024 · N484UA · Airbus A320232 · Fuel StorageSDR CALA2024030800667Panel · missingPDA 2 LEFTWING LEADING EDGE PANEL MISSING. ON ARRIVAL FROM SJD, TECH FOUND PANEL 522WB (L/H WING) MISSING WHEN PERFORMING EXTERIOR GVI INSTALLED NEW COVER ASSY ON BLOWOFF PANEL REF IPC 57-41-37.Mar 6, 2024 · N484UA · Airbus A320232 · Wing, Plate/SkinSDR CALA2023050101299Bulb · inoperativeSEAT LAMP RED LIGHT BULB (1EA) INOP AT ROW 21ABC. REMOVED AND REPLACED 1 EPL BULB AT ROW 21ABC IAW A320 AMM 33-51-18-00/400-002-A OPS CHECK GOOD PER STS N0031. R & R 1 EPL BULB AT ROW 21ABC IAW A 320 AMM 33-51-18-000/400-002-A. OPS CHECK GOODApr 29, 2023 · N484UA · Airbus A320232 · Emergency LightingSDR CALA2023050101298Bulb · inoperativeSEAT LAMP RED LIGHTBULB (EA) INOP AT ROW 22ABC. REMOVED & REPLACED AFT CARGO COMPARTMENT SKID PLATES IAW A320 EC RA 5322-01050. R & R 1 EPL BULB AT ROW 22ABC IAW A320 AMM 33-51-18-000-400-002-A. OPS CHECK GOOD.Apr 29, 2023 · N484UA · Airbus A320232 · Passenger Compartment LightingSDR CALA2022060201421Check Valve · crackedECAM CAUTION MESSAGE - G RSVR LO LVL MESSAGE INOP - HYD FOUND CRACKED CHECK VALVE ON PTU HP MANIFOLD REF IPC 29-11-15-02 ITEM 150.REPLACED CHECK VALVE PER AIPC 29-11-15-02. LEAK CHECK GOODJun 2, 2022 · N484UA · Airbus A320232 · Hydraulic Power Accumulator, MainSDR CALA2022022800524Hydraulic System · depletedYELLOW SYSTEM ALMOST DEPLETED. LARGE LEAK NOTICED BEHIND RIGHT GEAR WELL. WAS ABLE TO CLOSE CARGO DOORS MANUALLY BY HAND PUMP. FOUND WEEPING B-NUT ON AUTOMATIC SELECTOR VALVE, TORQUED IN REFERENCE TO AMM 32-42-13 (FIG 31-42-13-991-00100-B ITEM 17). SERVICING AFeb 28, 2022 · N484UA · Airbus A320232 · Hydraulic Pump (Electric/Engine), MainSDR CALA2022010700058Stringer · crackedLH SIDE FRAME 68 AT STR22 INNER CAP AND WEB FLANGEIS CRACKED. CR ACK ABOVE THE LOWER MOUNT HOLES OF THE #1 DOOR STOP, AFT SIDE, I N AND ABOVE RADIOUS. CRACK APPROX 2.25" WITH ENDS MARKED IN BLAC K. L23516 REV IR IS INCLUDED AS APPENDIX A FOR REFERENCE. ACCOMPLJan 6, 2022 · N484UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2022010700057Stringer · crackedL/H FR35 STR30L HOLE #3 HAS CRACK INDIACTIONS AT THE 2:00. 3:00, AND 4:00 POSITIONS. REF HAECO N/R 9294150 FOR REFERENCE. #3 FINIAL HOLE SIZE .199". ACCOMPLISH INITIAL INS THE LATEST OF THE REVISION OF ECRA 5331-02825 ON OR BEFORE 59,68 HOURS, WHICHEVER COMES Jan 6, 2022 · N484UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2022010700056Frame · crackedL/H FR35 STR 30 HOLES #2 HAS CRACK INDACTIONS AT THE 5:00, 6:00, AND 11:00 POSITIONS CONTACT ENGINEERING FOR REPAIR INSTRUCTION BEFORE NEXT FLIGHT. FOR A REFERENCE FOR #2 HOLE. FINIAL HOLE SIZE .250". ACCOMPLISH OF THE REVISION OF ECRA 5331-02825 ON OR BEFORE Jan 6, 2022 · N484UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022010700055Door Frame · crackedL2 DOOR FRAME 68 DOOR STOP FITTING #1 LOWER INBOARD HOLE IS CRAC KED IN THE FRAME WEB AT 5:00 AND 10:00 POSITION. REO-L23516 REV IR IS INCLUDED AS APPENDIX A FOR REFERENCE.#3 HOL REPAIR ON THE FR68 DOOR STOP #1 AND STR 22 FLANGE PER PART 3 OF E START DIA .269"Jan 6, 2022 · N484UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2022010700037Frame · crackedLH SIDE FRAME 68 AT STR 22 INNER CAP AND WEB FLANGE IS CRACKED. CRACK LOCATED ABOVE THE LOWER MOUNT HOLES OF THE #1 DOOR STOP, A FT SIDE, IN AND ABOVE RADIUS. CRACK APPROX 2.25" WITH ENDS MARKE D IN BLACK. L2 DOOR DRAME 68 DOOR STOP FITTING #1 LOWER I/B HOLE IJan 5, 2022 · N484UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022010700036Frame · crackedL/H FR35 STR30L HOLE #2 HAS CRACK AT THE 5:00, 6:00, AND 11:00 P OSITIONS. HOLE #3 HAS CRACK INDICATIONS AT 2:00, 3:00, AND 4:00. #1 HAS CRACK INDICATIONS AT 5:30 AND 6:30 POSITIONS. PER HAECO LCQ NR 9294149/22149, 9294150/22150, 9294148/22148. GENERATED BY V0Jan 5, 2022 · N484UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2021122902464Fitting · corrodedMAIN CABIN L2 DOOR SILL AFT CORNER FITTING HAS CORROSION (A3NB-5 3-3-6222) GENERATED BY:N078592 AT HAECO LCQ PER NON ROUTINE 929 273 (22273) REMOVED AND REPLACED CORNER FITTING FR68 L/H DOOR SILL. IAW A320 SRM 51-42-11/001 PARA 2B,F PERFORMED BY:V061630 INSPECDec 28, 2021 · N484UA · Airbus A300* · Fuselage Structure (General)SDR CALA2021122902463Door Sill · corrodedMAIN CABIN L2 DOOR SILL FWD GIRT BAR MOUNT POINT HAS 2 AREAS OF CORROSION. (A3NB-53-3-6222) GENERATED BY N078592 AT HAECO LCQ PE R NR 9294271 (22271) REMOVED AND REPLACED L-2 DOOR SILL IAW A320 SRM 51-42-11/001. PE RFORMED BY V061630 INSP BY N078570.Dec 28, 2021 · N484UA · Airbus A300* · DoorsSDR CALA2021121702379Stringer · corrodedFWD CARGO LWR SILL WEB PLATE FR26 TO FR28 UPPER SURFACE HAS SEV ERAL AREAS OF CORROSION (A3NB-53-3-6105) GENERATED BY N078592 AT HAECO LCQ PER NON ROUTINE 9294405 (22405) REMOVED CORRODED FWD CARGO SILL WEB PLATE AND INSTALLED NEW WEB PLATE IAW A320 SRM 51-42-Dec 15, 2021 · N484UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2021121702378Stringer · corrodedAFT CARGO PIT STRINGER 41RT BETWEEN FRAME 61-62 HAS CORROSION O N VERTICAL FLANGE (SUPPORT TASK) GENERATED BY V052030 AT HAECO L CQ PER NR 9294337 (22337) REMOVED AND REPLACED STRINGER 41RT AFT CARGO. IAW A320 SRM 51-72 -11. PERFORMED BY V052030 INSP BY V06133Dec 15, 2021 · N484UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2021121702377Stringer · corrodedAFT CARGO PIT STRINGER 42 LEFT HAS CORROSION AT FRAME 57LT AND F R59 LEFT (SUPPORT TASK) GENERATED BY V052030 @HAECO LCQ PER NR 9 294340 (22340) REMOVED AND REPLACED STRINGER 42L IN AFT CARGO. IAW A320 SRM 51- 72-11. PERFORMED BY V052030 INSP BY V061334Dec 15, 2021 · N484UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2021121702376Stringer · corrodedAFT CARGO PIT BETWEEN FR63-64 STRINGER 42R HAS CORROSION SPOTS O N UPPER SURFACE GENERATED BY V919150 AT HAECO LCQ PER NR # 9294507 (22507) REMOVED CORRODED STRINGER 42R AT FR63-64 AND INSTALLED NEW STRIN GER IAW A320 SRM 51-42-11 PERFORMED BY V913406 INSP BYDec 15, 2021 · N484UA · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2021121202342Fitting · corrodedMAIN CABIN R2 DOOR SILL HAS (2EA) AREAS OF CORROSION ON UPPER SU RFACE CENTER SHAPE SILL ONLY. GENERATED BY N078592 PER HAECO LCQ NR 9294286/22286 REMOVED AND REPLACED R-2 DOOR SILL SHAPE SILL IAW A320 SRM 51-42 -11/001 PARA 6 DOT REMOVED KC50 BY MECH V061630 Dec 10, 2021 · N484UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2021121202341Fitting · corrodedR2 DOOR SILL FWD CORNER FITTING HAS CORROSION. GENERATED BY N078 592 PER HAECO LCQ NR 9294287. REMOVED AND REPLACED CORNER FITTING AT R2 DOOR SILL IAW A320 SRM 51-42-11/001 PARA 6 B,F DOT REMOVED KC51 BY MECH V061630 INSP BY V919150Dec 10, 2021 · N484UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2021120602247Plate · corrodedCARGO PIT IB TORSION BOX COVER SHEET HAS CORROSION AROUND TIE DO WN FITTINGS PER NR9294383/22383 GEN BY V052030. RMVD AFT CARGO PIT INBD TORSION BOX COVER SHEET AND INSTALLED NE W TORSION BOX COVER SHEET IAW SRM 53-41-49-283-004. APPLIED TOP COAT IAW SRM 51-75Dec 4, 2021 · N484UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2021120102212Intercostal · crackedLEFT FR 16 DOOR STOP FITTING #7, INBD UPPER HOLE HAS A CRACK IND ICATION AT 5 O''CLOCK POSITION AT FRAME TO INTERCOSTAL LAYER. (AD 2019-20-10). GENERATE BY V061671 AT HAECO LCQ PER NR 9294263 (2 2263) REMOVED AND REPLACED L/H FRAME 16 DOOR STOP #7 INTERCOSTAL Nov 30, 2021 · N484UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2021120102211Intercostal · crackedAD 2019-20-10; RIGHT FR 16 DOOR STOP FITTING #7, INBD LOWER HOLE HAS A CRACK INDICATION AT 7 O''CLOCK POSITION AT FRAME TOTO INTE RCOSTAL LAYER GENERATED BY V061671 ON HAECO LCQ NR 9294264 (2226 4) REMOVED AND REPLACED R/H FRAME 16 DOOR STOP FITTING #7 INTERCONov 30, 2021 · N484UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2021112202143None · corrodedFWD CARGO FR32 STR44 HAS CORROSION ON FWD FACE OF SHEAR TIE (A3N B-53-3-6105). GENERATED BY N078592 AT HAECO LCQ PER NR 9294415 ( 22415). REMOVED AND REPLACED FWD CARGO SHEAR TIE AT FR32 STR44 IAW A320 SRM 51-72-11-911-001. PERFORMED BY V061765 AND INSP BY V06Nov 19, 2021 · N484UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2021112202139Angle · corrodedMAIN CABIN R2 DOOR SILL FR68 HAS CORROSION AT FASTENER HOLE (A3N B-53-3-6222)GENERATED BY N078592 AT HAECO LCQ PER NR 9294284 (22 284) PERFORMED MAIN CABIN R2 DOOR SILL REPAIR AT FRAME 68 IAW A320 SR M 53-41-14-300-001, REPAIR PRINCIPLE #5.PERFORMED BY V913406Nov 18, 2021 · N484UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2020012000216Fuel Cap · missingFUEL CAP MISSING. INSTALLED A NEW CAP.Jan 20, 2020 · N484UA · Airbus A320232 · Fuel StorageSDR CALA2019061400944Shear Panel · corrodedAFT WET AREA LEFT LATERAL SHEAR PLATE HAS A CORROSION AROUND FASTENER HOLES BETWEEN FR69 AND FR70 STA Y1732 REMOVED AND REPLACED SHEAR PLATE AT AFT WET AREA LEFT LATERAL BETWEEN FR69 AND FR70 Y1732 IAW A320 SRM 51-42-11 & 51-72-11-911 -001Jun 13, 2019 · N484UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2019061400943Shear Plate · corrodedAFT WET AREA RIGHT LATERAL SHEAR PLATE HAS CORROSION AROUND FAST ENER HOLES BETWEEN FR 69 AND FR 70 STA -Y1732 DATA WAS TRANSCRIBED FROM PAPER DOCUMENT :AAR N/R 9593890 WORK REMOVED AND REPLACED AFT WET AREA RIGHT LATERAL SHEAR PLATE BETW EEN FR 69 AND FR 70 Jun 13, 2019 · N484UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2019041200562Fuel Cap · missingFUEL CAP MISSING .Apr 9, 2019 · N484UA · Airbus A320232 · Fuel StorageSDR CALA2017120104286Battery · faultyEPSU BATT EMERGENCY L FAILED SYS TEST. RPL EPSU BATT EMERGENCY L. OPS CHK OK.Dec 1, 2017 · N484UA · Airbus A320232 · Emergency LightingSDR CALA2017111204047Battery · dischargedEMERGENCY LIGHTING POWER SUPPLY BATT FAIL. R&R BATT. OP-CHECK GOOD. AMM 33-51-000-002-A, AMM 33-51-38-400-002-A.Nov 12, 2017 · N484UA · Airbus A320232 · Lighting SystemSDR CALA2017082502897Cradle · brokenREAR EMERGENCY FLASHLIGHT HOUSING BROKEN AT 2L JUMPSEAT. REPLACED BROKEN HOUSINGAug 25, 2017 · N484UA · Airbus A320232 · Emergency EquipmentSDR CALA2016081195626Battery Pack · no testEMERGENCY LIGHT TEST FAILED WITH EPSU BATTERY FWD LEFT FAULT. REPLACED EPSU BATTERY, OPS CHECKED NORMAL.Jun 26, 2016 · N484UA · Airbus A320232 · Emergency LightingSDR CALA2016040495250Fluid · lowYELLOW HYD SYS ECAM MSG, ZERO INDICATION. SERVICED YELLOW HYD QTY AS REQUIRED, NO LEAKS NOTED.Mar 31, 2016 · N484UA · Airbus A320232 · Hydraulic System, MainSDR CALA2015120894866Stringer · corrodedCORROSION ON STRINGER 31R AT C65 FRAME IN AREA AFT OF AFT CARGO COMPARTMENT UNDER OUTFLOW VLV, LOWER FWD CORNER. R & R STRINGER 31R, FRAME 64 - 67 IAW SRM 51-42-11 PAR 7.Dec 2, 2015 · N484UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2015092194380Battery · dischargedREFERENCE 2 SERVICE, EMER LIGHTS FAIL TEST. R & R LT FWD EPSU BATTERY, BATTERY ONLY, IAW AMM 33-51-38-000-002A & 33-51-38-400-002A. OPERATIONS CHECKED OK.Sep 20, 2015 · N484UA · Airbus A320232 · Emergency LightingSDR CALA2014060991250Aileron · malfunctionedRIGHT AILERON DEFLECTED DOWN 2 - 3 SCALE WITH ASSOCIATED ROLL OBSERVED.Jun 9, 2014 · N484UA · Airbus A320232 · Aileron Control SystemSDR CALA2014050690961Unknown · faultyO2 SERVICED TO FULL IN DENVER, SHOWED 1500 AT DULLES. NOW SHOWING 1360 IN FLT. BOTTLE PRE-SERVICE READING WAS 1600 PSI, SERVICE TO 2000 PSI. COCKPIT INDICATION SHOWED 1900 PSI. CREW WILL MONITOR PRESS INFLIGHT.May 5, 2014 · N484UA · Airbus A320232 · Crew Oxygen SystemSDR CALA2014041490821Adapter · corrodedLEFT WING MANUAL REFUELING ADAPTER APERTURE HAS PITTING CORROSION RIB 19 - RIB 20. BLENDED CORROSION & MEASURED THE AREA.Apr 13, 2014 · N484UA · Airbus A320232 · Fuel StorageSDR CALA2014041490820Adapter · corrodedRIGHT WING MANUAL REFUELING ADAPTER APERTURE HAS PITTING CORROSION RIB 19 - RIB 20. BLENDED THE AREA & MEASURED REMAINING THICKNESS.Apr 13, 2014 · N484UA · Airbus A320232 · Fuel StorageSDR CALA2014041490819Stringer · corrodedFRAME 63 - FRAME 64 & STRINGER 42L HAS CORROSION IN AFT CARGO COMPARTMENT. BLENDED CORROSION & FOUND THE AREA BEYOND LIMITS IAW SRM 51-72-11 PG 11. CUT OUT CORRODED AREA OF STRINGER & INSTALLED STRINGER REPAIR & SPLICE ON STRINGER 42L FROM FRAME 62.5 - FRAMEApr 13, 2014 · N484UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2014040890782Skin · saturatedRIGHT ELEVATOR UPPER SKIN SURFACE HAS A WATER INGRESS INDICATION 39 INCHES FROM INBD END, 3 INCHES FROM TE, 3.5 INCHES DIAMETER. REPAIRED RT ELEVATOR UPPER SKIN AT LOCATION NOTED. DRILLED WITNESS HOLES & FOUND WATER. CUT OUT, SANDED AREA & REMOVED WATER. APApr 5, 2014 · N484UA · Airbus A320232 · Elevator, Plate/Skin
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