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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CALA2026060116684Fuel Cap · missingFUELER REPORTS CAP IS MISSING REQUESTING CDL FOR MISSING FUEL CAP. CONFIRMED NO LEAKS PRESENT. INSTALLED CAP ASSY REF IPC 28-25-41-02BSDR 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.SDR 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 GOODSDR 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.SDR 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 RSDR 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 WISDR 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 :1SDR 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.SDR CALA2024072600285Fuel Cap · missingPDA 2 REFUEL CAP MISSING FROM RIGHT WINGSDR 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.SDR 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 GOODSDR 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.SDR 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 GOODSDR 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 ASDR 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. ACCOMPLSDR 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 SDR 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 SDR 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"SDR 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 ISDR 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 V0SDR 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 INSPECSDR 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.SDR 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-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 V06133SDR 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 V061334SDR 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 BYSDR 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 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 V919150SDR 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 51-75SDR 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 SDR 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 INTERCOSDR 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 V06SDR 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 V913406SDR CALA2020012000216Fuel Cap · missingFUEL CAP MISSING. INSTALLED A NEW CAP.SDR 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 -001SDR 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 SDR CALA2019041200562Fuel Cap · missingFUEL CAP MISSING .SDR CALA2017120104286Battery · faultyEPSU BATT EMERGENCY L FAILED SYS TEST. RPL EPSU BATT EMERGENCY L. OPS CHK OK.SDR 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.SDR CALA2017082502897Cradle · brokenREAR EMERGENCY FLASHLIGHT HOUSING BROKEN AT 2L JUMPSEAT. REPLACED BROKEN HOUSINGSDR CALA2016081195626Battery Pack · no testEMERGENCY LIGHT TEST FAILED WITH EPSU BATTERY FWD LEFT FAULT. REPLACED EPSU BATTERY, OPS CHECKED NORMAL.SDR CALA2016040495250Fluid · lowYELLOW HYD SYS ECAM MSG, ZERO INDICATION. SERVICED YELLOW HYD QTY AS REQUIRED, NO LEAKS NOTED.SDR 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.SDR 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.SDR CALA2014060991250Aileron · malfunctionedRIGHT AILERON DEFLECTED DOWN 2 - 3 SCALE WITH ASSOCIATED ROLL OBSERVED.SDR 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.SDR CALA2014041490821Adapter · corrodedLEFT WING MANUAL REFUELING ADAPTER APERTURE HAS PITTING CORROSION RIB 19 - RIB 20. BLENDED CORROSION & MEASURED THE AREA.SDR CALA2014041490820Adapter · corrodedRIGHT WING MANUAL REFUELING ADAPTER APERTURE HAS PITTING CORROSION RIB 19 - RIB 20. BLENDED THE AREA & MEASURED REMAINING THICKNESS.SDR 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 - FRAMESDR 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. AP
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