N823UA

Service difficulty reports · 135

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 = 'N823UA' 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 CALA2026100520102Fuel Cap · missingMISSING FUEL CAP UPON ARRIVAL. INSTALLED A FUEL CAP.Oct 3, 2026 · N823UA · Airbus A319131 · Fuel StorageSDR CALA2026091519458Fuel Cap · missingPDA 2 FUELER REPORTING FUEL CAP MISSING REPLACED MISSING FUEL CAP P/N 0727540 PER AMM 28-25-41-00 PARTS USED: 31-2825-9-0001,QTY :1 MFG PN ON - 0727540 MFG SN ON - C260145 M&E SN ON - 00145 M&E PN ON - 31-2825-9-0001 MFG SN OFF - UNABLE TO IDENT MFG PN OFF - Sep 10, 2026 · N823UA · Airbus A319131 · Fuel StorageSDR CALA2026070117517Pressure Blkhd · crackedACCOMPLISHED REPAIR PER ECRA 5330-06129C (AAR REO- L25919 REV IR). NOTE: AAR REO- L25919 REV IR IS INCLUDED WITHIN THIS ECRA AS FIGURES 1-21 FOR REFERENCE. REF AAR N/R 9298232 FOR DETAILS OF WORK ACCOMPLISHED. INITIATING DIP PER PART 1A STEP 5 OF ECRA 5330-061Jun 6, 2026 · N823UA · Airbus A319131 · Fuselage Main, BulkheadSDR CALA2026060816928Stiffener · crackedLEFT FR68 STGR22 HORIZONTAL STIFFENER LOWER RADIUS FLANGE CRACKED. REPAIRED PER ECRA 5341-01572 (REO-L25915 REV IR). NOTE: REO-L25915 REV IR IS INCLUDED IN THIS ECRA AS FIGURES 1-21Jun 6, 2026 · N823UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2026022614080Battery · no testDURING CIDS EMERGENCY LIGHT TEST. PERFORMED BITE OF 13WL IAW 33-51-00-810-802-A, BATTERY FAULT ACTIVATED. R & R THE BATTERY AT 13WL, OPS TEST PASSED IAW TSM 33-51-00-810-802A, AMM33-51-38-000-002.Feb 24, 2026 · N823UA · Airbus A319131 · Emergency LightingSDR CALA2025121812228Light · inoperativeROW 30 IN SEAT EMER LIGHT INOPERATIVE. R & R THE EMERGENCY LIGHT ASSY, OPS CHECKED SATISFACTORY.Dec 15, 2025 · N823UA · Airbus A319131 · Emergency LightingSDR CALA2025022002407Battery · no testCABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - RAN BATTERY TEST, NEED REPLACEMENT FOR ALL 4 LOCATIONS REPLACED WITH NEW EPSU BATTERY PER AMM 51-38-400-001-A. OPS CHECK OK.Feb 19, 2025 · N823UA · Airbus A319131 · Emergency LightingSDR CALA2025010801842Brake Assy · faultedREJECTED TAKE OFF 120KTS REPORTED BY CREW. PERFORM AN INSPECTION OF THE BRAKING SYSTEM REF AMM 05-51-16-200-001-A.. CAPTAIN STATED HE DID NOT EXCEED 100KTS AND SUSPECTED IT TO BE MORE LIKELY 60KTS. DUE TO TIRE FAILURE ACCOMPLISH AMM 05-51-15-200-001-A. ACPDJan 5, 2025 · N823UA · Airbus A319131 · Landing Gear Brake SystemSDR CALA2024060301673Connector · damagedWIRES 5251-7804 AND 5251-5815 DAMAGED FOR CONNECTOR 2743VCA. CJun 1, 2024 · N823UA · Airbus A319131 · Electrical Power System WiringSDR CALA2024022600542Fuel Cap · missingPDA 2 AIRCRAFT CAME IN WITH FUEL CAP MISSING SDR UPDATE FUEL CAP HAS BEEN REPLACED REF LG 7172426. REPLACED MISSING FUEL CAP WITH NEW. PFeb 25, 2024 · N823UA · Airbus A319131 · Fuel StorageSDR CALA2023122003673Engine · failedLOW SPEED ABORT LESS THAN 30 KNOTS. LOUD BANGAND AC VEERED TO RIGHT. ENGINE 2 FAIL ECAM. SEE L/P 6568330 FOR CORRECTIVE ACTION. SCHEDULED PARTS CHANGE"M&E P/N: 31-7200-9-0001 S/N: XXXXXXXXXXXX X. IF S/N FOUND, REMOVE AND REPLACE. IF THE PART REPLACED REQUI RESDec 13, 2023 · N823UA · Airbus A319131 · Engine (Turbine/Turboprop)SDR CALA2023091102751Window Post · crackedRIGHT HAND WINDSHIELD SIDE POST UPPER ATTACHMENT AT FR4, OTBD FWD HOLE ON HORIZ HAS A CRACK INDICATION IN TOP LAYER, OTBD DIRECT ION, FR 4, INBD HOLE ON VERT FLANGE HAS A CRACK INDICATION IN FWD LAYER, 12 O''CLOCK DIRECTION PER NR 9296608/36608 AND NR 929660 9Sep 8, 2023 · N823UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2023091102749Flange · crackedRH FR 68 STR 22 LOWER FLANGE CRACKED ABOUT .500 LONG. GEN BY V08 0280 ON HAECO LCQ NR 9296667/36667 "ACCOMPLISH INITIAL INSPS ON THE RH FR68 REPAIR PART AT 5341-01407 ON OR BEFORE THE AC REACHES 51879FC''S. 19700FC''S THEREAFTER." FR68 STGR22RH PER PT 2A OF THSep 8, 2023 · N823UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2023090402697Stringer · corrodedMAIN CABIN UNDERFLOOR FR 69-70 CORROSION ON STRINGER 43L. GEN BY V061708 ON HAECO LCQ NR 9296748 REPAIRED SECTION OF STGR 43LH BTW FR 69-70 IAW A319 SRM 53-47-13 -300-004 ACMP BY MECH V925324 INSP BY V061704Sep 3, 2023 · N823UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2023082802654Skin · dentedLOWER FUSELAGE EXTERNAL SKIN HAS 2 EA SMALL DENTS AT FR26 FR27 STR 42L STR 43L PER HAECO LCQ N/R 9296868/36868 DIM.1.5"X .875" AND RPR DBLR IAW SRM 53-21-11-300-076. REQUIRES EMBODIMENT IAW SRI 53-21-11-205-060 TABLE 1. THIS IS A CAT B INSP AT 60,000 FC/ 120,0Aug 26, 2023 · N823UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2023082102588Threshold · corrodedAFT CARGO THRESHOLD PLATE HAS CORROSION @FR57 (A3NB-05-3-6023) GENERATED AT HAECO LCQ PER NR 9296480 (36480) BY MECH V061603. REMOVED AND REPLACED AFT CARGO TORSION BOX COVER UPPER SURFACE IAW A319 SRM 51-42-11 PER MECH V942327 INSP V061704Aug 19, 2023 · N823UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2023082102584Web · corrodedFWD CARGO DOOR WEB HAS 2 SPOTS OF CORROSION BETWEEN FRAMES 27-28 . PER HAECO LCQ NR 9296265/36265 REMOVED AND REPALCED FWD CARGO DOOR WEB & REAPPLIED SURFACE PROT ECTION & FITTINGS IAW A310 SRM 51-72-11-911-001, 51-42-11-001, 5 1-44-11-001, 51-21-11-001, 51-23Aug 18, 2023 · N823UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2023081802561Fitting · crackedLH CONTINUITY FITTING CRACKED, PERFORMED REPAIR BY REPLACING THE LH CONTINUITY FITTING AND REAP PLYING SURFACE PROTECTION IAW ECRA 5310-08193 CAT A REPAIR NO RE INSP REQ.Aug 17, 2023 · N823UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2023081402499Door Sill · corrodedR2 DOOR SILL CORROSION AROUND FASTENER HOLE AT FR66 PER NR929674 6/36746 GEN BY V061708 REPAIRED R-2 DOOR SILL FWD SPLICE AREA AT FR66 IAW A319 SRM 53-4 1-14-300-001 FIG 001.Aug 12, 2023 · N823UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2023080902460Intercostal · crackedLH O/W EMER HATCH FWD AND AFT INTERCOSTALS ARE CRACKED PER HAECO LCQ N/R 9296777/36777 GEN BY N078625 REMOVED AND REPLACED FWD AND AFT INTERCOSTALS AT LH OW EMER. DOO R HATCH IAW A319 SRM 52-21-00-04-A, 51-42-11/001. PERFORMED BY V 080280.Aug 8, 2023 · N823UA · Airbus A319131 · Emergency ExitsSDR CALA2023080902459Intercostal · crackedRH O/W EMER HATCH FWD AND AFT I/B INTERCOSTALS ARE CRACKED PER HAECO LCQ N/R 9296778/36778. REMOVED AND REPLACED FWD AND AFT INTERCOSTALS AT RH OW EMER. DOOR HATCH IAW A319 SRM 52-21-00-04-A, 51-42-11/001.Aug 8, 2023 · N823UA · Airbus A319131 · Emergency ExitsSDR CALA2023080402421Fitting · crackedEA 5330-04821 REVISION L (AD2015-02-14) HFEC SURFACE INSP OF LH KEEL BEAM MLG DOOR FWD HINGE FITTING FOUND A 125 INCH CRACK IN T HE FWD LUG RUNNING HORIZONTALLY FROM EDGE AFT CRACK IS MARKED IN RED AND IDENTIFIED WITH DOT CH1 IN CLOSE PROXIMITY PER HAECO LCQ NAug 2, 2023 · N823UA · Airbus A319131 · Landing Gear DoorsSDR CALA2023073102376Plate · corrodedMAIN CABIN FR70 CORROSION AROUND FASTENER HOLE ON LH LATERAL SHEAR PLATE PER HAECO LCQ N/R 9296749/36749 GEN BY V061708Jul 29, 2023 · N823UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2023062602013Transmitter · failedOIL PRESSURE BELOW 80 PSI DISPLAYED ON UPPER ECAM SC REEN. - ENG 1 REPLACED #1 ENG OIL PRESS TRANSMITTER REF AMM79-33-15-400-010-A. OPS CHECK NORMAL. AC OKAY FOR CONT SERVICE. PARTS USED: 31-7931-3-0005,QTY :1Jun 24, 2023 · N823UA · Airbus A319131 · Engine Oil System (Airframe Furnished)SDR CALA2023060701782Nut · missingFOUND TIRE NO 3 MISSING LUG NUT ON PREFLIGHTINSPECTION REPLACED #3 MLG TIRE REF MM32-41-11.Jun 6, 2023 · N823UA · Airbus A319131 · Wheel/Ski/FloatSDR 2023FA0000022Shaft · damagedHPC REAR SHAFT,GALLING LOC.2 IAW SUBTASK 72-41-13-220-189 NOT PERMITTED. LLP TO BE RETIRED WITH 12843 CYCLES SINCE NEW (LIFE LIMIT WAS 20000 CYCLES)Jan 6, 2023 · N823UA · Airbus A319131 · Turbine Engine Compressor SectionSDR 2022FA0000774Turbine Wheel · crackedCRACKED IN AREA A1 OVER REPAIR VRS4018 LIMITS (SUBTASK 72-50-00-230-071). MINIMUM REMAINING KNIFE EDGE HEIGHT LESS THAN 0.0177 IN. (0.45 MM) (SUBTASK 72-50-00-350-061). NON REPAIRABLE. LIFE LIMITED PART TO BE SCRAPPED WITH 12843 CYCLES (LIFE LIMIT 20000 CYCLESDec 23, 2022 · N823UA · Airbus A319131 · Turbine SectionSDR CALA2022052501336Avionics Unit · faultySKIN VALVE FAULT DISPLAYED ON UPPER ECAM SCREEN. - V ENT NO MESSAGES PRESENT ON ARRIVAL TO GATE. POST FLT REPORT SHOWS MULTIPLE MSGS FOR SKIN VENT, EXTRACT, AND INLET VALVES. AEVC TEST OKAY, ALL VALVES OPERATE NORMAL. RPL AEVC COMPUTER DUE TO SUSPECTED CONTROMay 25, 2022 · N823UA · Airbus A319131 · Cabin Pressure Control SystemSDR CALA2022052501347Fuel Cap · missingTHIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL REPORT SUBMITTED ON 5/25/22.FUEL CAP MISSING. PLACED ON CDL. PLACED FUEL CAP ON CDL CREATED PDA. REPLACED FUEL COUPLING CAP.May 22, 2022 · N823UA · Airbus A300* · Aircraft Fuel SystemSDR CALA2021082501428Hydraulic System · lowGREEN HYD LEVEL LOW BLUE HYD LEVEL HIYELLOW HYD LEVEL LOW SERVICED HYD SYSTEM GREEN AND. YELLOW, AND BLUE SYSTEM IS WITHIN LIMIT REF MAINTENACE TIP SECTION 1A AND REF MT 29-004 , LEAK CK OK.Aug 24, 2021 · N823UA · Airbus A319131 · Hydraulic System, MainSDR CALA2021081301327Pump · failedY RSVR OVHT DISPLAYED ON UPPER ECAM SCREEN. - HYD LEVELING AT FL360 REMOVED AND REPLACED YELLOW ELECTRIC PUMP REF AMM 29-13-51,AND CHECK VALVE 3083GM REF AMM 29-24-21. OPS AND LEAK CHECK GOOD.. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1969534 SN OFF 1058 PUMAug 13, 2021 · N823UA · Airbus A319131 · Hydraulic Pump (Electric/Engine), MainSDR CALA2019092801652Actuator · faultyNOSE LANDING GEAR NOT CLOSED, ECAM RECYCLE, NO HELP. PER CREW DEBRIEF: NLG DOORS NEVER LOCKED IN UP POSITION, AMBER INDICATION ALWAYS ON. POST FLIGHT REPORT FLT PHSE 5 L/G DOORS NOT CLOSED. WITH ASSOCIATED NLG DOOR UPLOCK MSG (2534GM,2531GM) PICKED UP BY BOTH Sep 26, 2019 · N823UA · Airbus A319131 · Landing Gear Door ActuatorSDR CALA2019081091331Pressure Panel · crackedROTO PROBE INSPECTION SHOWS CRACK INDICATION IN PRESSURE PANEL FR 35-36. L/H SIDE HOLE # 16 REPAIRED HOLE 16 IN PRESSURE PANEL BETWEEN FR35-36 LH SIDE IAW ECRA 5331-02423 ACCOMPLISH INITAL INSPECTION REQUIREMENTS AT LH PRESSURE PANEL FR35-36Aug 7, 2019 · N823UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2019080901330Pressure Panel · crackedAD 2018-06-04 EA 5330-05126 OP 002...A-20 NO DOT ROTO PROBE INSPECTION SHOWS CRACK INDIACTION IN PRESSURE PANEL FR35-36. L/H SIDE. HOLES 3,4,AND 16. CONTACT ENGINEERING FOR REPAIR INSTRUCT IONS AND REPAIR BEFORE NEXT FLIGHT. REPAIRED PRESSURE PANEL BETWEEN FR3Aug 7, 2019 · N823UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2019080431294Power Supply · no testREMOVE AND REPLACE THE CABIN EMERGENCY LIGHT POWE R SUPPLY. CHANGED DUE TO A FAILED BIT E TEST. REMOVED AND REPLACED THE CABIN EMERGENCY LIGHT POWER SUPPLY.Aug 1, 2019 · N823UA · Airbus A319131 · Emergency LightingSDR CALA2019080301293Battery · no testTHE EMERGENCY LIGHT TEST AT THE PTP FAILS WITH TH E MESSAGE EPSU BATTERY FWD. REMOVED AND REPLACED FWD LT BATTERY OF THE EPSU IAW AMM 33- 51-38-400-002-A.Aug 1, 2019 · N823UA · Airbus A319131 · Emergency LightingSDR CALA2019080431292Battery Pack · no test(SUPPORT TASK) THE EMERGENCY LIGHT TEST AT THE PTP FAILS WITH TH E MESSAGE ''EPSU BATTERY EMER R? ATA 33-51-38. REFER TO AAR N/R: 9620608. REMOVED AND REPLACED RH BATTERY OF THE EPSU IAW A319 AMM 33-51-3 8-000-002-A AND 31-51-38-400-002-A. OPS CHECK COMPLIED WAug 1, 2019 · N823UA · Airbus A319131 · Emergency LightingSDR CALA2017100203366Seal · leakingACRID, ELECTRICAL ODOR IN COCKPIT AND 1ST CLASS. NOTICABLE AT LOW DIFF PRESSURES. CHECKED AFT, FWD,AND BOTH SIDE E & E AREAS, NO SMOKE ODOR. PERFORMED AVEC TEST IAW AMM 21-26-00, NO FAULTS FOUND, PERFORMED BCL 1 AND 2 BITE TEST IAW AMM 24-38-00, NO FUALTSOct 2, 2017 · N823UA · Airbus A319131 · Drag Control ActuatorSDR CALA2017073102461Fitting · crackedLEFT WINDSHIELD SIDE POST UPPER ATTACHMENT, INTERNAL SIDE, HOLE 3 IS CRACKED AT 9:00 POSITION SIDE POST LAYER. ACCOMPLISHED A REPAIR IAW ECRA 5310-07169.Jul 31, 2017 · N823UA · Airbus A319131 · Fuselage Main, Attach FittingsSDR CALA2017072802398Torque Box · corrodedAFT CARGO COMP TORSION BOX HAS SEVERAL WEB SPOTS OF CORROSION FROM FRAME 55R TO FRAME 59R. REMOVED AND REPLACED AFT CARGO TORSION BOX WEB IAW SRM 51-7 2-911-002.Jul 27, 2017 · N823UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2017072802395Access Door · bentTHS ACCESS DOOR IS BENT, FOUND TO BE OUT OF LIMITS IAW SRM 51-41-23-283-002, REV 118. REMOVED AND REPLACED THE ACCESS DOOR IAW SRM 51-72-11-911-001, REV 118, AND AMM 52-41-16-400-0 01Jul 26, 2017 · N823UA · Airbus A319131 · DoorsSDR CALA2017072802394Plate · corrodedDURING AFT CARGO BILGE AREA CLEANING, FOUND CORROSION ON FRAME 68, STRINGERS 43L - 43R REENFORCING PLATE. REMOVED AND REPLACED THE PLATE IAW SRM 51-42-11, 51-74-00, 51-73-11, 51-44-11, DRAWING 11304 AND SRM 51-72-11.Jul 26, 2017 · N823UA · Airbus A319131 · Fuselage Main, FrameSDR CALA2017072102288Fitting · corrodedDISCOVERED CORROSION ON THE AFT CARGO DOOR CUT OUT FWD CORNER FITTING. DURING REMOVAL OF MIN OR SCRIBE MARKS ON THRESHOLD STRUCTURE, BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-73-11-001, REV 118, INSTALLED A NEW FITTING IAW SRM 51-72-11 -911Jul 18, 2017 · N823UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2017081402666Shear Tie · corrodedAFT CARGO SHEAR TIE IS CORRODED AT STRINGERS 41L - 42L. BLENDED CORROSION ON AFT CARGO SHEAR TIE AND FOUND TO BE OUT OF LIMITS IAW SRM 51-73-00. FABRICATED NEW SHEAR TIE IAW DRAWING 53476518 AND INSTALLED IAW SRM 51-42-11.Jul 14, 2017 · N823UA · Airbus A319131 · Fuselage Internal Mounting StructureSDR CALA2017081402665Door Sill · crackedL2 DOOR SILL AT LOWER ANGLE FRAME 68 IS CRACKED. REMOVED AND REPLACED L2 DOOR SILL FRAMES 66 - 68 IAW SRM 51-72-11, AND SRM 51-42-11, REV 118.Jul 14, 2017 · N823UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2017071402198Support Fitting · crackedAFT CABIN SUPPORT FITTING FOR BEAM Y1162 IS CRACKED AT FR 68 REMOVED CRACKED AFT CABIN SUPPORT FITTING FOR BEAM Y1162 FR-68, RECEIVED NEW SUPPORT FITTING AND INSTALLED FITTING IAW SRM 51-72-11, AND 51-42-11, REV 118.Jul 13, 2017 · N823UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2017071402197Fitting · out of positionL2 SILL FWD CORNER FITTING HAS INTERFERENCE WITH LWR NO.6 DOOR STOP. REMOVED AND REPLACED FWD LOWER L-2 CORNER FITTING IAW RFTS OPS 6 0039 NR 41, IAW SRM 51-72-11-912-001, 51-44-11-001, 51-75-12-0 01, 51-21-11-001, REV 118, 51-75-12-001, AND 53-41-79.Jul 13, 2017 · N823UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2017071402196Angle · damagedFRAME 67 HAS ONE OUT OF ROUND HOLE AT ATTACHMENT TO THE L2 DOOR SILL REMOVED THE OLD CLEAT AND INSTALLED IAW SRM 51-72-11-119-001, AND 51-42- 11-001, REV. 118.Jul 13, 2017 · N823UA · Airbus A319131 · Fuselage Main, Attach FittingsSDR CALA2017071402195Hinge Fitting · out of positionRIGHT ELEVATOR NR 6 HINGE FITTING HAS A LARGE GAP ON INBOARD SIDE BETWEEN HINGE ARM. REMOVED AND REPLACED WITH A NEW RT ELEVATOR HINGE FITTING IAW SRM 51-42-11 AND SRM 51-2211.Jul 13, 2017 · N823UA · Airbus A319131 · Elevator StructureSDR CALA2017071002127Angle · damagedR2 DOOR SILL ATTACH ANGLE AT FRAME 67 HAS SEVERAL ELONGATED HOLES. FABRICATED A NEW ATTACH ANGLE IAW DWG D53480076000, AND INSTALLED IAW SRM 51-42-11-001, REV 118, AND GMM 07-35-05.Jul 10, 2017 · N823UA · Airbus A319131 · Fuselage Miscellaneous Structure
Back to N823UA