N825UA

Service difficulty reports · 70

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 = 'N825UA' 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 CALA2026080918392Fuel Cap · missingFUELER REPORTED AIRCRAFT ARRIVED WITH FUEL COUPLING CAP MISSING. INSTALLED A NEW FUEL COUPLING CAP IAW AMM 28-25-41-400-005-A. NO OTHER DEFECTS NOTEDAug 7, 2026 · N825UA · Airbus A319131 · Fuel StorageSDR CALA2025112511444Skin · dentedDENT ON LOWER AFT CORNER OF DOOR 1L. DENT MEASURES 3" X 1.5" AND IS .015" DEEP. LOCATED AT BOTTOM RT CORNER OF DOOR. 1" UP FROM BOTTOM AND 6" IN FROM AFT EDGE. APPLIED DENT DOT WITH LOG PAGE #. REF. SRM 52-00-00-283-002 FIG 2. REPAIR AT OR BEFORE 200 FC (Nov 22, 2025 · N825UA · Airbus A319131 · Passenger/Crew DoorsSDR CALA2025102710583Battery Pack · no testEMERGENCY BATTERY L DISPLAYED DURING EMERGENCY LIGHTING BITE TEST. REMOVED AND REPLACED EPSU BATTERY IAW AMM 33-51-38. OPS CHECK GOOD.Oct 26, 2025 · N825UA · Airbus A319131 · Emergency LightingSDR CALA2025091608962Bezel · not seated2R DOOR SLIDE ARMINDICATOR BLOCKED BYPACK COVER ON LOWER LOF DOO R AND FLOOR DOOR 2R SLIDE BEZEL FWD LOWER CORNER NOT SEATED PROPERLY OBSRUCTING VIEW OF ARMED INDICATOR DOT ON GIRT BAR. RESEATED SLIDE BEZEL. REF AMM 25-62-44Sep 12, 2025 · N825UA · Airbus A319131 · Emergency EquipmentSDR CALA2025052004842Fitting · wornL/H MLG DOOR ACTUATOR TOP ATTACHMENT FITTING ON KEEL BEAM, HAT B USHING MIGRATED COMPLETELY OUT OF FITTING. COMPLETE ESFR COMPLETE ESFR COMPLETE REMOVED & REPLACED L/H MLG DOOR ACTUATOR UPPER AFT FITTING PER A 319 UAL REPAIR DRAWING R53370501. ISSUE F.May 16, 2025 · N825UA · Airbus A319131 · Fuselage, Door HingeSDR CALA2025032503158Light Sys · malfunctionedEMER EXIT LIGHT REMAIN ILLUMINATED UNTILGEAR IS RETRACTED NORMAL OPERATION INDICATES THE EMERGENCY LIGHTS COME ON AUTOMATICALLY WHEN NO SMOKING SWITCH 190RH IS IN THE ON POSITION. THEY ALSO COME ON, WHEN NO SMOKING SWITCH 190RH IS IN THE AUTO POSITION AND WHENMar 24, 2025 · N825UA · Airbus A319131 · Emergency LightingSDR CALA2025012300177Fuel Cap · missingPDA 2 FUEL CAP MISSING REPORTED BY FUELER REF L/P 3598742 INSTALLED NEW FUEL CAP REF AMM 28-25-41-400-007-A. NOTE: PDA L/P 3601214.Jan 21, 2025 · N825UA · Airbus A319131 · Fuel StorageSDR CALA2025011301882Battery · no testCABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - FWD LH EPSU FOUND BATT FAULT. REPLACED BATTERY PACK OF THE EPSU IAW AMM 33-51-38-400-002-A0. OPS TEST GOOD.Jan 9, 2025 · N825UA · Airbus A319131 · Emergency LightingSDR CALA2023122103699Wheel · damagedLEFT MAIN OUTBOARD WHEEL MISSING A LUG NUT ADDED PICTURE. WHEEL, TIRE, AS OFF 31-3245-9-9001 1996 ON 31-3245-9-9001 2843 WHEEL, TIRE, AS OFF 31-3245-9-9001 1996 ON 0000 #1 MLG WHEEL ASSY CHANGED DUE TO BROKEN TIE BOLT, REF AMM 32-41-11-400-006-A.Dec 17, 2023 · N825UA · Airbus A319131 · Wheel/Ski/FloatSDR CALA2023070702183Fitting · crackedWINDSHIELD LH CONTINUITY FITTING HAS A CRACK INDICATION AT UPPER FLANGE BEGINNING OF RADIUS PER HAECO LCQ N/R 9298605/44605 GEN BY V892444 REVISION. ON OR BEFORE 58900 TOTAL FLT CYCLES. PERFORM REPEAT THEREAFTER. INSPECTIONS AT INTERVALS NOT TO EXCEED 8800 FLTJul 5, 2023 · N825UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2023063002096Shear Plate · corrodedAFT CARGO PIT FR59 AT STGR 38R PROFILE PANEL SUPPORTING SHEAR PLATE HAS CORROSION ON FWD END PER HAECO LCQ N/R 9298945/44945 GEN BY V925324Jun 29, 2023 · N825UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2023062602026Stringer · corrodedFWD CARGO PIT R/H FR30 BETWEEN STRINGERS 41R-42R HAS CORROSION ON CLEAT PER HAECO LCQ NON ROUTINE 9298726/44726 GENERATED BY V91 9150 RMV AND RPL AND INSTALLED NEW CLEAT PO#1134829.4 D5323072020002 AT FWD CARGO R/H FR30 BETWEER STRG 5.41R-42R IAW A319 SRM 51-4Jun 25, 2023 · N825UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2023062602014Doubler · corrodedFWD CARGO PIT R/H BETWEEN FR30-34 AND BETWEEN STRINGERS 43R-44 HAS CORROSION ON SKIN DOUBLER PER HAECO LCQ N/R 9298727/44727 GEN BY V919150 RMVD AND FABRICATED AND INSTALLED DOUBLER AT FWD CARGO FR30-FR34 BETWEEN STRINGER 43R-44 IAW A319 SRM 53-21-11-08-A DWG Jun 24, 2023 · N825UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2023061601876Unknown · corrodedUPON REMOVAL OF GIRT BAR FITTING BASE PLATE TO APPLY REPAIR TO L 2 DOOR SILL FOUND CORROSION AT FR66 PER NR9298903/44903 GEN BY V 080280 RMVD AND RPLD L2 DOOR SILL IAW SRM 51-72-11-911-001 APPLIED TOPC OAT IAW SRM 51-75-12-911-002 BY MECH V928628 INSP BY V0779Jun 15, 2023 · N825UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2023061601875Unknown · corrodedUPON REMOVAL OF GIRT BAR FITTING BASE PLATE TO APPLY REPAIR TO R 2 DOOR SILL FOUND CORROSION AT FR66 PER NR9298904/44904 GEN BY V 080280 REMOVED AND REPLACED R2 DOOR SILL IAW SRM 51-72-11 BY MECH V0397 46 INSP BY N078625Jun 15, 2023 · N825UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2023061201814Door · corrodedAFT CARGO PIT DOOR THRESHOLD HAS SEVERAL AREAS OF SURFACE CORROS ION PER HAECO LCQ N/R 9298567/44567 GEN BY V925324 RMVD AND RPLD AFT CARGO PIT DOOR THRESHOLD IAW SRM 51-74-00 AND 53-41-49-283-003 MECH V925324 INSP BY V061704Jun 9, 2023 · N825UA · Airbus A319131 · Cargo/Baggage DoorsSDR CALA2023042401237Bypass Valve · failedAIR PACK 2 REG FAULT...FLIGHT DECK TEMP UNCONTROLLABLE...AT 84 DEGREES AND CLIMBING. POST FLIGHT REPORT INFO REMOVED RIGHT PACK PANEL 192FB FOR TROUBLESHOOTING ACCESS. REPLACED PACK 2 TURBINE BYPASS VALVE (30HH) REF AMM 21-63-00-720-001-A. VERIFIED ALL ZONE TEApr 24, 2023 · N825UA · Airbus A319131 · Cabin Temperature Control SystemSDR CALA2021101401877Fuel Cap · missingPDA 3 UNDERWING FUEL CAP MISSING C/W DDP PER MEL PLACED ON C/W DDP PER MEL DISPATCH DESK: 37 NAME: JO DATE: 10-OCT-21- OK TO CDL NEED FUEL CAP M/E 31-2825-9-0001 INSTALLED FUEL CAP REF. IPC 28-11-43Oct 14, 2021 · N825UA · Airbus A319131 · Aircraft Fuel SystemSDR CALA2020020800371Window Frame · crackedDURING C-2 CHECK AT AAR DLH "REFNON-ROUTINE 9622631" FOUND WINDS HIELD CENTER POST LOWER ATTACHMENT INTERNAL R/H WINDSHIELD FRAME HAS CRACK INDICATION IN UPPER RADIUS OF CUTOUT EMINATING OUT OF UPPER BOLT HOLE. ACCOMPLISHED INTERIM REPAIR PER PART 1 OF ECRA 53Feb 4, 2020 · N825UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2020020800370Window Frame · crackedDURING C-2 CHECK AT AAR DLH "REF NON-ROUTINE 9622630" FOUND WINDSHIELD CENTER POST LOWER ATTACHMENT INTERNAL LH WINDSHIELD FRAME HAS CRACK INDICATION IN UPPER RADIUS OF CUTOUT EMINATING OUT OF UPPER BOLT HOLE. ACCOMPLISHED PART 1 OF ECRA 5311-02243. NEED TO ACFeb 4, 2020 · N825UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2019041200567Control Unit · inoperativeWR ANT. WEATHER RADAR INOP. PFR HIT ON ANTENNA R&R RADAR ANTENNA UNIT IAW AMM 34-41-11, OPS TEST WOULD NOT TILT +10 DEGREES PER OPS TEST. R&R RADAR CONTROL UNIT IAW AMM 34-41-12, OPS TEST AND BITE TEST OF RADAR SYSTEMS PASSED. OK FOR SERVICE. ROTABLE PARTS CHAApr 11, 2019 · N825UA · Airbus A319131 · Weather Radar SystemSDR CALA2016112500970Battery Pack · faultedFWD EPSU FAULT LIGHT DURING TEST REPLACED EMERGENCY BATTERY PER AMM 33-51-38. NOW OKNov 25, 2016 · N825UA · Airbus A319131 · Lighting SystemSDR CALA2015111794834Skin · unknownLEFT ELEVATOR, UPPER SKIN HAS 19 TRAPPED WATER INDICATIONS. ALL REPAIRS ACCOMPLISHED IAW SRM 55-21-11 & ECRA 5520-01470 ECRA PART 2. REQUIRES 1ST INSPECTION AT 60000C OR 120000T WHICHEVER COMES 1ST.Nov 12, 2015 · N825UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2015111794833Skin · unknownRIGHT ELEVATOR, UPPER SKIN HAS 10 TRAPPED WATER INDICATIONS. ALL REPAIRS ACCOMPLISHED IAW SRM 55-21-11 & ECRA 5520-01470 ECRA PART 2. REQUIRES 1ST INSPECTION AT 60000C OR 120000T WHICHEVER COMES 1ST.Nov 12, 2015 · N825UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2015111794818Stringer · corrodedSTRINGER 31R, BETWEEN FRAMES 65 & 66, JUST BELOW OUTFLOW VLV HAS EXFOLIATED CORROSION. R & R STRINGER 31R, BETWEEN FRAMES 65 & 66 IAW SRM 51-42-11.Nov 10, 2015 · N825UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2015111794812Door Sill · corrodedR2 DOOR SILL CORRODED UNDER FWD & AFT GIRT BAR FITTINGS. R & R R2 DOOR SILL IAW SRM 51-42-11 PG 25 & 51-72-11 PG 1.Nov 9, 2015 · N825UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2015101294584Unknown · malfunctionedCABIN ALTITUDE ROSE TO 11000 FEET AT FL 330. CPC 1 & 2 SHOWS NO FAULTS. REPLACED CPC 1 & 2 PRECAUTIONARY & DISCUSSED ACTION WITH TOMC, IAW AMM 21-31-34-000 & 21-31-34-401. BITE TESTED GOOD, NO FAULTS PRESENT.Oct 12, 2015 · N825UA · Airbus A319131 · Cabin Pressure Control SystemSDR CALA2015101494587Unknown · malfunctionedCABIN PRESS STARTED TO CLIMB ON INITIAL DESCENT. CABIN ALT ROSE TO 11000 FEET AT FL 330. DECLARED EMER, DONNED O2 MASKS CPC 1 & 2 SHOWED NO FAULTS. REPLACED CPC 1 & 2 PRECAUTIONARY. BITE TESTED GOOD, NO FAULTS PRESENT.Oct 11, 2015 · N825UA · Airbus A319131 · Cabin Pressure Control SystemSDR CALA2014123092870Oxygen Mask · unwanted deployO2 MASKS DROPPED ROW 32ABC. INSPECTED PAX O2 PANEL IAW MT 35-003, NO DAMAGE NOTED. REPACKED O2 COMPARTMENT & SECURED PANEL DOOR. MANUAL MASK RELEASE OPERATIONAL CHECK IAW AMM 35-23-00- 710-001 WITHIN 3 DAYS.Dec 21, 2014 · N825UA · Airbus A319131 · Passenger Oxygen SystemSDR CALA2014122392863Oxygen Mask · unwanted deployO2 MASKS DROPPED ROW 32ABC. INSPECTED PAX O2 PANEL IAW MT 35-003, NO DAMAGE NOTED. REPACKED O2 COMPARTMENT & SECURED PANEL DOOR. MANUAL MASK RELEASE OPERATIONAL CHECK IAW AMM 35-23-00- 710-001 WITHIN 3 DAYS.Dec 21, 2014 · N825UA · Airbus A319131 · Passenger Oxygen SystemSDR CALA2013082690734Grill · crackedNR 1 ENGINE NOSE COWL EXHAUST GRILL IS CRACKED, MARKED. REMOVED NR 1 ENGINE NOSE COWL EXHAUST GRILL & SENT TO SHOP. WELD REPAIRED ACCOMPLISHED IAW 71-11-11-200-011-A 13. INSTALLED PANEL AFTER WELD REPAIR.Aug 23, 2013 · N825UA · Airbus A319131 · Engine Cowling SystemSDR CALA2013082390702Power Supply · inoperativeDURING EMERGENCY LIGHT SYS CHECK, THE " EPSU INT LOAD FWD L" MESSAGE SHOWS. REPLACED FWD LT EPSU, 10WL IAW AMM 33-51-38-000-001-A, 33-51-38-400-001-A. ACCOMPLISHED CIDS RESET. TESTED OK.Aug 23, 2013 · N825UA · Airbus A319131 · Emergency LightingSDR UALA2013061404107Fitting · gougedNR 1 FEC, SMALL GOUGES IN THE FWD MOUNTING SPIGOT FITTING. ACCOMPLISHED BLENDING IAW 54-51-18, PG.103Jun 13, 2013 · N825UA · Airbus A319131 · Nacelle/Pylon, Main FrameSDR UALA2013061704165Gearbox · leakingHAND SIZED PUDDLE OF OIL UNDER ENG 1 AFT OF DRAIN MAST. OIL ON BOTTOM OF ENGINE. OPERATED ENGINE FOUND OIL LEAKING OUT OF LIMITS FROM TOP OF ANGLE GEARBOX IAW TSM 79-00-00-810-838-A, IF UNABLE TO CORRECT SOURCE OF EXTERNAL OIL LEAK, REPLACE ENGINE. REPLACED NJun 11, 2013 · N825UA · Airbus A319131 · Turbine Engine Accessory DriveSDR UALA2013060303849Windshield · faultyANTI-ICE RT WINDSHIELD EICAS. (REPEAT GRIPE) DEFERED IAW MEL 30-42 PTS IAW MM 30-42-00-710-001A AND WSM 30-42-02 SENSOR TEST OK SUSPECT WINDSHIELD AT FAULT IN FLT NEEDS NEW WINDSHIELD, PCN (110- 3206). REPLACED WINDSHIELD IAW MM.Jun 3, 2013 · N825UA · Airbus A319131 · Flight Compartment WindowsSDR UALA2013060303848Controller · faultyR WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN. ANTI ICE. REPLACED WHC IAW AMM, OPS CHECK OK.May 31, 2013 · N825UA · Airbus A319131 · Windshield/Door Rain/Ice RemovalSDR UALA2013053103811Wire Harness · failedRIGHT WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN. ANTI-ICE INSTALLED HARNESS 9F21895-501 TO SWAP TO SPARE SENSOR FOR RT WINDSHIELD.May 30, 2013 · N825UA · Airbus A319131 · Ice/Rain Protection System WiringSDR UALA2013012100346Shunt · corrodedFOUND SHUNT 3PB2 CORRODED BETWEEN CONTACTS. REPLACED SHUNT 3PB2. BCL TEST OKAY.Jan 20, 2013 · N825UA · Airbus A319131 · DC Indicating SystemSDR UALA2013011700300Sdac · failedELEC BCL2 FAULT ECAM. TROUBLESHOT PER TSM 24-38-00-810- 833 WITH NO DEFECTS. REMOVED AND REPLACED SDAC2 IAW AMM 31-55-34, OPS CHECKED NORMAL.Jan 15, 2013 · N825UA · Airbus A319131 · Electrical Power SystemSDR UALA2013010200006Interface Unit · faultyWHILE ENROUTE GOT LGCIU 1 FAULT. NO AIRBORNE RESET AVAIL. GPWS AND REVERSER INOP. RETURNED TO DENVER. REPLACED LGCIU 1, OP CKS GOOD.Jan 2, 2013 · N825UA · Airbus A319131 · Landing Gear Retraction/Extension SystemSDR UALA2011111406198Computer · faultyFLIGHT CONTROL BUMPING. AFTER 90 MINUTES AT CRUISE FL360 HAD LOW AMPLITUDE BUMPS FELT IN COCKPIT, OBSERVED BOTH AILERONS PULSE UP ONE INCH SIMULTANEOUSLY. WITH ELAC1 OR ELAC2 OFF, THE BUMPING STOPPED. SIMILAR BUMP NOTED WHEN SWITCHING ELAC1 OFF. NOTED BY MNov 12, 2011 · N825UA · Airbus A319131 · Aileron Control SystemSDR UALA2011111006143Computer · faultyELAC-2 ISSUES, FLIGHT DIVERTED. NR 2 ELAC REF MM. PERFORMED OPERATIONAL TEST OF ELAC. PERFORMED EFCS 1&2, NO FAULTS FOUND. PERFORMED AFS TEST REF MM, TEST PASSED ON GND. KNOWN GOOD ELAC1 AND 2 DUE TO CONTINUING ELAC 1 AND 2 FAULTS WITH MULTIPLE SEPARATE REPLACNov 10, 2011 · N825UA · Airbus A319131 · Elevator Control SystemSDR UALA2011110305951Computer · faultyELAC 1 FAULT. REPLACED ELAC 2 PER MM. OPERATIONAL CHKS OKAY.Nov 3, 2011 · N825UA · Airbus A319131 · Elevator Control SystemSDR UALA2011101105526Seat · bindingF/O SEAT FORWARD AFT IS BINDING USING MANUAL CONTROLS. REPLACED F/O'S SEAT PER MM.Oct 10, 2011 · N825UA · Airbus A319131 · Flight Compartment EquipmentSDR UALA2011081504309Outflow Valve · faultyAVIONICS PROBLEM, FLIGHT DIVERTED. AVIONICS VENT SKIN VLV FAULT AFTER T/O. FOLLOWED FLT MAN BOTH BLOWER AND EXTRACT VLV TO OVERRIDE, NOW INLET VLV SHOWS CLOSED BUT EXTRACT SHOWS FULL OPEN. SAMC TEXT: EXTRACT VLV SHOULD SHOW CLOSED IN THIS CONFIGURATION SUSAug 14, 2011 · N825UA · Airbus A319131 · Pressure Regulator/Outflow ValveSDR UALA2011071403570Wedge · damagedLEFT OUTBD TRAILING EDGE FLAP, TRAILING EDGE WEDGE HAS NUMEROUS HAIL-DAMAGE DENTS APPROXIMATELY ONE-SIXTEENTH OF AN INCH DEEP.Jul 14, 2011 · N825UA · Airbus A319131 · Trailing Edge FlapsSDR UALA2011060802806Thrust Reverser · delaminatedFOUND DELAMINATION ON ENG CORE SIDE OF THE NR 1 LEFT SIDE THRUST REV HALF OUTER METAL PLY IS PEELING UP. AREA OF DAMAGE IS 128 SQ INCHES AND IS WITHIN CF LIMITS, TO BE RE-CHECKED ONCE DAILY. DL8304 CREATED TO MONITOR. REPAIRED DAMAGE AREA PER MT.Jun 7, 2011 · N825UA · Airbus A319131 · Engine Thrust ReverserSDR UALA2011060602755Light · disconnectedEMERGENCY LIGHT ROWS 6C AND 10C DO NOT TURN ON. RECONNECTED EMERGENCY LIGHTS ROWS 6C AND 10C, TESTED ALL NORMAL.Jun 6, 2011 · N825UA · Airbus A319131 · Emergency LightingSDR UALA2010122004617Control Unit · faultyLT CTR TANK PUMP LOW PRESS MSG, FLT DIVERTED. R & R FUEL LEVEL SENSING CONTROL UNIT. CYC RIGHT CTR FUEL PUMP CB INSP CONNECTOR AT FUEL PUMP AND CONTACTOR 36QA. MOVED 5000LBS OF FUEL WITH THE RIGHT CTR PUMP. REPLACED RELAY 45QA, LEFT CTR PUMP OPERATES NORMDec 20, 2010 · N825UA · Airbus A319131 · Fuel Indicating SystemSDR UALA2010071302499Power Supply · failedEMERGENCY EXIT LIGHTS ARE LIT IN BACK GALLEY IN FLIGHT. EMERGENCY LIGHT TEST FAILED OVERWING POWER SUPPLY UNIT 12WL. REPLACED UNIT, OPS CHECKS OKAY.Jul 13, 2010 · N825UA · Airbus A319131 · Emergency Lighting
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