N814UA

Service difficulty reports · 134

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 = 'N814UA' 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 CALA2026092819854Oil System · lowENG 1 LOW OIL, AFTER ROTATIONIND 4.5 QT AFTER LEVEL OFF 6-8 QT ENGINE 1 FAN COWLS AND THRUST REVERSERS OPENED TO PERFORM VISUAL INSP OF ENGINE. NO LEAKS NOTED. SERVICED ENGINE WITH 9 QUARTS OF OIL AND PERFORMED DRY MOTOR OF ENGINE 1 IAW AMM TASK 71-00-00-710-0Sep 24, 2026 · N814UA · Airbus A319131 · Turbine Engine Oil SystemSDR CALA2026082718946Frame · crackedFRAME 16 RT DOUBLE JOGGLE HOLES NR 1, 6, & C HAD CRACK INDICATIONS DURING ACCOMPLISHMENT OF TC 17-5311-1-2837. INTERIM REPAIR ACCOMPLISHED IAW ECRA 5311-02463, PART 1, ITEM 1. IAW ECRA PART 1 ITEM 2.Jul 25, 2026 · N814UA · Airbus A319131 · Fuselage Main, FrameSDR CALA2026082718944Frame · crackedEA 5341-01231 004, RT SIDE FRAME 68 AT STR 22 INNER CAP & WEB FLANGE IS CRACKED 6.50 INCH LONG. INTERIM REPAIR ACCOMPLISHED IAW PART 1 OF ECRA 5341-01578 WITHOUT DEVIATIONS. ORIGINAL DISCREPANCY UNDER LCQ NR 9292250 AND ECRA 5341-01231. CARRIED TO ACCOMPLISHJul 25, 2026 · N814UA · Airbus A319131 · Fuselage Main, FrameSDR CALA2026081218525Door Frame · damagedLEFT FR 16 DOOR STOP FITTING NR 1, HOLE NR 3, ELONGATED AND PREVIOUS REPAIR AT CROSSBEAM. INTERIM REPAIR ACCOMPLISHED IAW 5311-03459 WITHOUT DEVIATION. ORIGINAL DISCREPANCY UNDER LCQ NR 9292380 AND LP 9532232.Jul 25, 2026 · N814UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2026072618004Door Frame · crackedR2 DOOR FR 68, NR 7 DOOR STOP LOWER INBD HOLE WAS CRACKED, REAMED HOLE IAW SRM 52-41-12, FG 202. NDT INSP IAW 51-10-01 AND NO CRACK NOTED. FABRICATED FREEZE PLUG AND WASHER, INSTALLED IAW 53-41-12. PERFORMED GVI ON R2 DOOR NR 7 DOOR STOP LWR INBD HOLE NO DJul 23, 2026 · N814UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2026083119100Frame · crackedLEFT FRAME 68, STR 22L HORIZONTAL STIFFENER LOWER RADIUS FLANGE CRACKED. INNER FLANGE & HORIZONTAL FLANGE FILLET RADII. ACCOMPLISHED INTERIM REPAIR PER PART 1 OF ECRA 5341-01576 WITHOUT DEVIATIONS.Jul 6, 2026 · N814UA · Airbus A319131 · Fuselage Main, FrameSDR CALA2026083119098Frame · corrodedRIGHT FRAME 66, STR 22-23, HAS 7 HOLES WITH REJECTABLE INDICATIONS. HAD VISIBLE CORROSION SURROUNDING IT ON AFT FACE. REPAIR ACCOMPLISHED IAW PART 1 OF ECRA 5341-01577 WITHOUT DEVIATION.Jul 2, 2026 · N814UA · Airbus A319131 · Fuselage Main, FrameSDR CALA2026063017456Frame · damagedUPON REMOVAL OF R2 DOOR SILL TO FOM FR68 FRAME REPLACEMENT FOUND FR67 FRAME TO HAVE MULITPLE ELONGATED FASTENER HOLES. REMOVED AND REPLACED RT FR67 FRAME IAW SRM 51-44-11 AND 51-42-11.Jun 28, 2026 · N814UA · Airbus A319131 · Fuselage Main, FrameSDR CALA2026063017430Door Sill · corrodedUPON REMOVAL OF R2 DOOR SILL TO FOM FR68 FRAME REPLACEMENT FOUND DOOR SILL TO HAVE CORROSION AND MULTIPLE ELONGATED FASTENER HOL ES. REMOVED AND REPLACED R2 DOOR SILL IAW A319 UAL SRM 51-44-11 AND 51-42-11.Jun 26, 2026 · N814UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2024092600691Packing · damagedY RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN. - HYD RECIEVED ECAM ON T/O AFTER POWER BROUGHT UP DEBRIEFED CREW, PUMPS RUN TIME DID NOT EXCEED 5 MINUTES AFTER RUNNING. PERFORMED INSPECTION OF DPI REF 29-00-00-280-006. NO LOW LEVEL WARNING. UPON INSPECTION FOUNDSep 25, 2024 · N814UA · Airbus A319131 · Hydraulic System, MainSDR CALA2023122803744Fuel Cap · missingFUEL CAP MISSING APPLY CDL 28A INOP STICKER APPLIED IN FLIGHT DECK DISPATCH DESK: 24 NAME: RB DATE: 22-DEC-23- APPROVED CDL FOR MISSING FUEL CAP. INSTALLED NEW FUEL CAP AND NOTICED THE ADJUSTMENT IS NOT CORRECT.(SEE PICTURES). NECESSARY ADJUST THE FUEL CAP AS Dec 23, 2023 · N814UA · Airbus A319131 · Fuel StorageSDR CALA2023092002836Bleed Air Sys · warning messageENG 2 BLEED LEAKECAM...SHUT BLEED OFFPER ECAM PERFORMED LEAK CK / ENGINE RUN ON ENG 2. NO LEAKS NOTED. NO MESSAGES, BITE CK OF BMC SHOWED NO FAULTS. PFR SHOWED NO CURRENT FAULTS. ALL WORK IAW AMM 36-22-16. OK FOR CONTINUED SERVICE. PERFORMED LEAK CK / ENGINE RSep 19, 2023 · N814UA · Airbus A319131 · Engine Bleed Air SystemSDR CALA2023071402243Door Frame · crackedR/H EMERGENCY EXIT FWD FRAME CRACKED PER HAECO LCQ N/R 9294845/ 24845 GEN BY REMOVED AND REPLACED RH EMERGENCY EXIT FWD FRAME IAW UAL SRM 51- 72-11-911-001Jul 13, 2023 · N814UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2023071002201Stringer · corrodedAFT CARGO PIT STRINGER 31R AT FR65 HAS CORROSION JUST FWD OF OUT FLOW VALVE PER HAECO LCQ N/R 9294579/24579 GEN BY V926223Jul 8, 2023 · N814UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2023071002200Door Sill · corrodedR2 DOOR SILL HAS CORROSION AT FR66 AND FR68 PER HAECO LCQ N/R 9294633/24633 GEN BY V061603Jul 8, 2023 · N814UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2023033100956Connector · leakingHYD RESERVOIR FILL CONNECTOR SPINS UNABLE TO ATTACHED SERVICER SERVICEABLE NON-COSMETIC INT DIP ABLE TO SECURE HYD FILL CONNECTION LOCKING PLATE TANGS FOR CONTINUED SERVICING THRU QUICK DISC SERVICE PORT. REQ CARRY APPROVED PER GMM 05-30-06. AT NEXT MAINTENANMar 31, 2023 · N814UA · Airbus A319131 · Hydraulic System, MainSDR CALA2023032700894Reservoir · unknownECAM CAUTION MESSAGE - Y RSVR LO LVL MESSAGE INOP - HYD FOUND YELLOW HYDRAULIC SYSTEM VERY LOW, SERVICED WITH 3 GALLONS RAN YELLOW HYDRAULICS FOR 2+ HOURS WHILE CYCLING FLIGHT MAIN WING FUEL TANKS AND INSPECTED FOR POSSIBLE HYDRAULIC HYDRAULIC FLUID. T/S PER TMar 27, 2023 · N814UA · Airbus A319131 · Hydraulic Power SystemSDR CALA2022090502253Fitting · noneON OR BEFORE AIRCRAFT N814UA (4014) ACCUMULATE 37,170 TOTAL AIRCRAFT FLIGHT CYCLES, PERFORM INSPECTION OF THE LH WINDOW FRAME CONTINUITY FITTING AREA AROUND THE INSTALLED WASHERS PER PART 2 STEP 1 OF THE LATEST REVISION OF EC 5311-02875, THERE AFTER REPEAT INSSep 2, 2022 · N814UA · Airbus A300* · Fuselage Main, FrameSDR CALA2022081002023Skin · damagedDEEP SCRATCH FOUND ON RH SLAT NO.3 INBD TRAILING EDGE SIDE CAUSED BY RUBBING ON 622BT PROTRODING SCREW HEAD. REQUIRES FURTHER EVALUATION. LTPR NR# 5001173902-0010. CREATED DMG REF GMM 06-35-05. THIS IS A CAT "A" RPR WITH NO REINSPECTION REQUIRED. PERFORMED REPAug 9, 2022 · N814UA · Airbus A319131 · Wing, Control Surface Attach FittingsSDR CALA2021031500321Pipe · leaking*EMERGENCY DECLARED* HYD Y RSVR LO LVL ECAM AT CRUISE. LOST YELLOW SYSTEM AND ACCUMULATOR. PYLON LEAKING,PART. # D2901010201200,TUBING REMOVED NEED TO BE INSTALLED. INSPECTED HYDRAULIC LEAK AT #2 ENGINE AND FOUND TUBING IN THE LOCKED FOR POSITIVE FIX. CONTACT Mar 15, 2021 · N814UA · Airbus A319131 · Hydraulic System, MainSDR CALA2020123001413Landing Gear · malfunctionedAFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT. GEAR DOORS OPERATED NOR MALLY UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. INSPECT NLG FOR ANY OBVIOUS DEFECTS AND REPORT TO TOMC LOCKED FOR GEAR DOWN FERRY.Dec 29, 2020 · N814UA · Airbus A319131 · Landing Gear Retraction/Extension SystemSDR CALA2020080901090Battery Pack · dischargedBATTERY PACK FOR 13WL WILL NOT PASS CAPACITY CHECK. REMOVED AND REPLACED THE BATTERY PACK 13WL AND OP CHECKED GOOD IAW AMM 33-51-38-000-002-A & 33-51-38-400-002-A.Aug 5, 2020 · N814UA · Airbus A319131 · Emergency LightingSDR CALA2020020800345Pressure Deck · crackedREF EA 5330-05216 REV A STEP 3.2 #4 HOLE IS CRACK ON THE ALUMINUM PRESSURE DECK PANEL ONLY. REPAIRED #4 HOLE ON PRESSURE DECK PANEL REF. EC/RA#: 5331-02602. ACCOMPLISH INITIAL INSPECTION REQUIREMENTS PER PART 2 OF EC/RA 5331-02602 ON OR BEFORE THE AIRCRAFT REAFeb 5, 2020 · N814UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2019071501207Pedestal · inoperativeWX RADAR INOP.WR ANT AND WR R/T MSGON BOTH NDS WXR R/T PN ON : 066-50008-0409 SN ON: 10041 SN OFF: 10065 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1365535 SN OFF 0065 TRANSCEIVER, WX OFF 31-2311-9-0001 0065 ON 31-2311-9-0001 8041 REMOVED AND REPLACED WEATHERJul 15, 2019 · N814UA · Airbus A319131 · Weather Radar SystemSDR CALA2019011300073Selector · faultyHAD AUTOBRAKE FAULT ECAM. WHICH SHOWED NORM BRAKES INOP WHICH I S NAGAINST MEL. INTERVIEWED CREW: FLIGHT CREW STATED THAT ECAM MESSAGE CAME ON DURING CRUISE AND THEN WENT AWAY. MESSAGE RETURNED AGAIN DURING LANDING/ROLL OUT. ALSO, THERE IS A NOTICEABLEJan 10, 2019 · N814UA · Airbus A319131 · Landing Gear Brake SystemSDR CALA2018081701808Transmitter · failedBRAKES SYS NR 1 FAULTED. RESET THE NOSE WHEEL STEERING ONCE, MESSAGE STILL DISPLAYED. RAN BSCU SYSTEM TESTS. FAULTS ON BSCU 1 BRAKE PEDAL TRANSMITTER 9GG. REPLACED THE BRAKE PEDDAL TRANSMITTER IAW MM 32-42-47. BITE TESTED BSCU 1 AND 2. NO FAULTS.Aug 15, 2018 · N814UA · Airbus A319131 · Landing Gear Brake SystemSDR CALA2018071001581Fitting · corrodedL2 DOOR AFT LOWER CORNER FITTING HAS CORROSION. REMOVED AND REPLACED L2 DOOR AFT LOWER CORNER FITTING IAW SRM 51-42-11-001.Jun 25, 2018 · N814UA · Airbus A319131 · Passenger/Crew DoorsSDR CALA2018041601167Power Supply · no testCABIN EMERGENCY LIGHTS FAILED TO TEST, EPSU REMOVED & REPLACED IAW AMM 33-50-00, OPS CHECKED GOOD.Apr 16, 2018 · N814UA · Airbus A319131 · Emergency LightingSDR CALA2017122904664Battery Pack · inoperativeFOUND SEVERAL EMERGENCY LIGHTS NOT WORKING, REPLACED L1 AND LEFT EMERGENCY DOOR BATTERY PACKS. SYSTEM OPS NORMAL.Dec 29, 2017 · N814UA · Airbus A319131 · Emergency LightingSDR CALA2017032500720Altimeter · faultySTANDBY ALTIMETER INDICATION ERRONEOUS AT FL370 STBY ALT READS FL358. ACCOMPLISHED FUNCTIONAL TEST REF AMM34-21-00. STBY ALT NEEDLE STICKS. REPLACED STBY ALTIMETER REF AMM34-21-22 OPS CHECKS NORMAL.Mar 25, 2017 · N814UA · Airbus A319131 · Altimeter, Barometric/EncoderSDR CALA2016110295889Skin · crackedLT FUSE SKIN AT FR35 STR 30L HAS A CRACK INDICATION ON HOLE MARKED 2. INTERIM REPAIR ACP IAW EC RA5330-05813 PART 1.Oct 30, 2016 · N814UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2016110295888Skin · crackedRT FUSE SKIN AT FR35 STR 30R HAS A CRACK INDICATION ON HOLE MARKED 2. INTERIM RPR ACP IAW ECRA 5330-05813 PART 1.Oct 30, 2016 · N814UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2016103195877Fitting · corrodedR1 DOOR SILL FWD GIRT BAR FITTING AREA CORROSION AROUND FWD OUTBD, AFT INBD, & AFT OUTBD HOLE AT FR20 STR23. REMOVED CORROSION BY SPOT FACING ALL 3 HOLES ON FR20 .017 .025 .020 MATERIAL REMOVED & FOUND TO BE IN LIMITS IAW A319 SRM53-11-14 FIG 108 PARA 7B FABOct 24, 2016 · N814UA · Airbus A319131 · Fuselage Main, Attach FittingsSDR CALA2016102495851Threshold · corrodedFWD CARGO THRESHOLD WEB HAS CORROSION AND FOUND OUT OF LIMITS. REMOVED AND REPLACED IAW SRM 53-21-13 PG 101-104.Oct 24, 2016 · N814UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2016101995833Door Sill · corrodedL2 DOOR CUTOUT FWD LOWER CORNER HAS CORROSION. REMOVED AND REPLACED L2 DOOR SILL IAW SRM 51-42-11.Oct 18, 2016 · N814UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2016101995818Door Sill · corrodedL2 DOOR SILL FR68 HAS CORROSION AROUND THE LAST TWO NUT PLATE HOLES AFT END AT DOOR SILL. REMOVED CORROSION AND FABBED REPAIR DOUBLER AND INSTALLED IAW SRM 53-41-14 PARA 5A FIG201 REPAIR PRINCIPLE 5.Oct 17, 2016 · N814UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2016101395796Shear Plate · corrodedFR 70 STR 23 RT, AFT CORNER LOWER PANEL HAS CORROSION ON PLATE. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-72-11.Oct 10, 2016 · N814UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2016101395795Door Sill · corrodedAFT CARGO DOOR SILL CORROSION NUMEROUS AREAS BETWEEN FR59 & FR56. REMOVED AND REPLACED AFT CARGO SILL IAW SRM 51-42-11.Oct 10, 2016 · N814UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2016101395794Structure · corrodedAFT PIT THRESHOLD CONNECTION HAS CORROSION. REMOVED AND REPLACED AFT PIT THRESHOLD SHEET CONNECTION IAW 51-42-11.Oct 10, 2016 · N814UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2016101395793Plate · corrodedAFT CARGO BAY SUPPORT PLATE JUST INBD OF DOOR SILL CORRODED AROUND FWD-TIE DOWN AT FR56. REMOVED AND REPLACED WITH NEW THRESHOLD PLATE AT AFT CARGO LOWER DOOR FROM FR55.5 TO FR59 IAW SRM 51-42-11.Oct 10, 2016 · N814UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2016101395800Support Frame · corrodedRT WW SHEAR PLATE SUPPORT FRAME BETWEEN FR69-FR90 FOUND TO HAVE CORROSION. REMOVED AND REPLACED RT SHEAR PLATE SUPPORT FRAME IAW SRM 51-72-11.Oct 8, 2016 · N814UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2015091894368Computer · malfunctionedCENTER FUEL TANK PUMPS WILL NOT TURN ON AFTER FLAP SLAT RETRACTION. CYCLING OF AUTO FUEL FEED PB SWITCH FROM AUTO TO MANUAL, NO HELP. UNABLE TO MOVE FUEL OUT OF CTR FUEL TANK. NO INFLIGHT RESET AVAILABLE, ACFT DIVERTING, BOTH CTR TANK GFIS & FQIC WERE REPLASep 15, 2015 · N814UA · Airbus A319131 · Fuel Indicating SystemSDR CALA2015062494020Hydraulic System · lowCREW REPORT, HYD GREEN ENG 1 PUMP LO PSI WITH HYD GREEN RSVR LO LEVEL. FLIGHT CREW SHUTDOWN GREEN SYS BEFORE QTY EMPTIED IAW QRH. SERVICED GREEN HYD SYS, CHECKED FOR HYD LEAKS. PERFORMED FLIGHT CONTROL CHECK, NO LEAKS NOTED. NO LEAKS NOTED ON ACFT ON FUSELJun 22, 2015 · N814UA · Airbus A319131 · Hydraulic System, MainSDR CALA2015062294004Fluid · lowCREW REPORT, HYD GREEN ENG 1 PUMP LO PSI WITH HYD GREEN RSVR LO LEVEL. FLIGHT CREW SHUTDOWN GREEN SYS BEFORE QTY EMPTIED IAW QRH. SERVICED GREEN HYD SYS & CHECKED FOR HYD LEAKS. PERFORMED FLIGHT CONTROL CHECK, NO LEAKS NOTED. NO LEAKS NOTED ON ACFT ON FUSEJun 22, 2015 · N814UA · Airbus A319131 · Hydraulic System, MainSDR CALA2015051993800Sensor · corrodedCREW RETURNED TO THE FIELD DUE TO MLG NOT RETRACTING WHEN SELECTED UP. AHM IS FAULTING THE LT GEAR EXTEND PROX SENSOR 21GA. REPLACED 21GA SENSOR DUE TO CORROSION. REPLACED LT MLG MAIN GEAR HARNESS CONNECTOR INSIDE J BOX. REPLACED LT 1M HARNESS, LT 2M ENHANMay 15, 2015 · N814UA · Airbus A319131 · Landing Gear Position and WarningSDR CALA2015021293119Door Sill · corrodedR2 DOOR SILL HAS CORROSION AT FRAME 66. REPLACED R2 DOOR SILL IAW SRM 51-44-11 & 51-42-11.Feb 11, 2015 · N814UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2015021293146Door Frame · crackedRIGHT NR 2 DOOR FRAME 68, NR 7 DOOR STOP, LOWER INBD HOLE HAS CRACK INDICATION. REAMED HOLE IAW SRM 52-41-12 FG 202, NDT INSPECTION IAW 51-10-01 & NO CRACK NOTED. FABRICATED FREEZE PLUG & WASHER & INSTALLED IAW 53-41-12.Feb 9, 2015 · N814UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2015021293145Door Sill · corrodedSHAPE SILL ON R2 DOOR SILL IS CORRODED. R & R DOOR SILL IAW SRM 53-41-14 FIG 101.Feb 9, 2015 · N814UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2015021293144Fitting · corrodedR2 DOOR CUT OUT AFT CORNER FITTING AT FRAME 68 IS CORRODED. REMOVED & REPLACED FITTING IAW SRM 53-41-14 FIG 101.Feb 9, 2015 · N814UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2015021293143Fitting · corrodedFRAME 66 R2 DOOR FWD CORNER FITTING CORRODED. R & R CORNER FITTING IAW SRM 53-41-14 FIG 101.Feb 9, 2015 · N814UA · Airbus A319131 · Fuselage Miscellaneous Structure
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