N818UA

Service difficulty reports · 112

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 = 'N818UA' 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 CALA2026092519801Panel · missingFOUND NR 1 PYLON SECTION PANEL MISSING, REF IPC 54-57-22-07A, ITEM 90, DETERMINED TO BE CATEGORY 2 50.75 SQ-IN R & R THE PYLON TO NACELLE PROFILE PANEL INBD IAW AMM 54-57-22.Sep 21, 2026 · N818UA · Airbus A319131 · Nacelle/Pylon, Main FrameSDR CALA2026083118996Fuel Cap · missingUPON ARRIVAL AT CLT THE FUEL CAP IS MISSING FROM THE AIRCRAFT. ACFT FLEW FROM DEN TO CLT, BACK TO DEN. UPON ARRIVAL, FUELERS HAD THE CORRECT CAP IN THEIR POSSESION, REINSTALLED CAP IAW AMM 28-25-41-400-007-A.Aug 27, 2026 · N818UA · Airbus A319131 · Fuel StorageSDR CALA2026061517117Light · inoperativeCABIN EMERGENCY LIGHT TEST FAIL ON FAP PANEL. STATUS MESSAGE: EPSU EXT LOAD EMER L ATA 33-51-38 LH AFT EXTERNAL EMERGENCY LIGHT ASSY. FAILED. REPLACED UNIT REF AMM 33-51-15. OPS CHECK GOOD NO DEFECTS NOTED.Jun 12, 2026 · N818UA · Airbus A319131 · Emergency LightingSDR CALA2026051116104A/C Pack · faultedNR 1 PACK BLOWING WARM, RAN FM 2.20.32 CHK LIST PACK HAD ENG EXHAU STOD OR WHEN RUNNING. CREW REPORTED THAT HEY SHUT OFF PACK1 AND THEN SELECTED BACK ON, PACK 1 OPS CHECK GOOD WITH NO FURTHER ODOR. C/W CONDITIONAL INSPECTION REF AMM 05-51-10 VERIFIED BLOWER/May 3, 2026 · N818UA · Airbus A319131 · Cabin Cooling SystemSDR CALA2025082508084Light · shortedPROCEDURE - EPSU EXT LOAD EMER R FAULT ON PTP AFTER EMER SYS TEST EXTERIOR LIGHT FAULT LIGHT ON RIGHT EPSU (PIC INCLUDED) RIGHT OVER WING EXTERIOR LIGHTS NOT WORKING RELAMPED OVERWING EXTERIOR LIGHTS, NO HELP. NO POWER AT PIN B, REINSTALLED LIGHTS ON FARING T/Aug 23, 2025 · N818UA · Airbus A319131 · Emergency LightingSDR CALA2025082508080Light · inoperativeEMERGENCY AISLE LIGHT INOPERATIVE AT ROW 31. R & R EMERGENCY LIGHT ASSY AT ROW 31 IAW AMM 33-51-20. OK FOR SERVICE.Aug 22, 2025 · N818UA · Airbus A319131 · Emergency LightingSDR CALA2025071406560Power Supply · faultedEPSU EXT LOAD EMER R FAULT. REPLACED 12W EPSU REF AMM 33-51-38-401. OPS CHECKS GOOD.Jul 11, 2025 · N818UA · Airbus A319131 · Emergency LightingSDR CALA2025051504703Bleed Valve · faultedENG 2 STALL ON CLIMBOUT. NOTICABLE YAW. ECAM CLEARED ITSELF. NO SHUTDOWNOPENED UP ENGINE NUMBER 2 FOR BOROSCOPE INSPECTION PER TSM 71-00-00-810-809-A STEP D2(A).PLEASE NOTE I ONLY BROKE LOOSE BOROSCOPE PLUGS 3 TO 7 PER THE AMM 72-00-00-200-016-B. BOROSCOPE PLMay 12, 2025 · N818UA · Airbus A319131 · Compressor Bleed ValveSDR CALA2025041703948Door Frame · corrodedR/H FR16 LOWER DOOR CUTOUT PREVIOUS BLEND REPAIR. (REQUEST PERMA NENT REPAIR INSTRUCTIONS AS PER PART OF EC/RA#5311-01839. REPAIRED RH FRAME 16 AFT WEB FACE AT Z-520 IAW ECRA 5311-03353. WORK ACCOMPLISHED ON HAECO N/R 9290354. ACCOMPLISH A PERMANENT REPAIR Apr 16, 2025 · N818UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2025041503881Frame · crackedR/H FR16 DOUBLE JOGGLE HOLE "A" HAS A CRACK INDICATION AT 9 O'CL OCK IN THE FRAME LAYER. REPAIRED HOLE A R/H FRAME 16 DOUBLE JOGGLE WITH BUSHING AND WASH ER IAW SRM 53-11-12-300-012. FINAL HOLE SIZE REAMED WITH BUSING INSTALLED IS .2175. HFEC ACCOMPLISHED WIApr 13, 2025 · N818UA · Airbus A319131 · Fuselage Main, FrameSDR CALA2025041503880Frame · crackedR/H FR16 DOUBLE JOGGLE HOLE "C" HAS A CRACK INDICATION AT 9 O'CL OCK IN THE FRAME LAYER. REPAIRED HOLE C R/H FRAME 16 DOUBLE JOGGLE WITH BUSHING AND WASH ER IAW SRM 53-11-12-300-012. FINAL HOLE SIZE REAMED WITH BUSING INSTALLED IS .2175. HFEC ACCOMPLISHED WApr 13, 2025 · N818UA · Airbus A319131 · Fuselage Main, FrameSDR CALA2025040703588Skin · contaminatedL/H ELEVATOR HAS LIQUID INGRESS 39.5 IN FROM INBOARD EDGE, 6 IN FROM TRAILING EDGE, 2.5 IN DIAMETER, "REPAIR BEFORE NEXT FLIGHT" PER HAECO LCQ NON ROUTINE 9290380/26380. SEE HAECO NON-ROUTINE 9290380 FOR WORK ACCOMPLISHED. REPAIRED L/H ELEVATOR 39.5 IN FROM I/Apr 4, 2025 · N818UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2024123001715Slide · out of positionDOOR 2L SLIDE PRESSUREGAUGE HAS SHIFTED FORWARD OUT OF VIEW.POS SIBLESLIDE OUT OF POSITION REMOVED DOOR 2L SLIDE REF AMM 25-62-44-000-002-A. UP TO AND INCLUDING STEP 4.A. INSTALLED NEW DOOR SLIDE ASSY AT DOOR 2L REF AMM 25-62-44-400-006-A. RENDER SAFE CHECKLIDec 26, 2024 · N818UA · Airbus A319131 · Escape SlideSDR CALA2024102302713Skin · crackedRT WING I/B FLAP BOTTOM SKIN CRACKED. REPAIRED RT IB FLAP BOTTOM SKIN AND INSTALLED DOUBLER IAW A319 S RM 57-52-00-300-003 A319 SRM 51-77-13-911-020 AND A319 SRM 57-52 -00-300-095 AND UAL EC/RA 5752-02019.Oct 19, 2024 · N818UA · Airbus A319131 · Trailing Edge FlapsSDR CALA2024081902230Fuel Cap · missingPDA 2 REF LOG PAGE 8920951, THE FUELER REPORTED THE FUEL CAP MISSING. CDL 28A ALREADY APPLIED FOR MISSING LANYARD. THE DEFERRAL LOG PAGE WAS UPDATED TO INCLUDE THE CAP.Aug 16, 2024 · N818UA · Airbus A319131 · Fuel StorageSDR CALA2024072900303Seal · leakingCREW REPORTED ABNORMAL WIND NOISE COMING FROM BOTH LEFT EMERGENCY EXITS. PRESSURIZATION NORMAL INSPECTED LH OVERWING FROM OUTSIDE DURING PRESSURIZATION CHECK. FOUND LEAKS FROM TOP RIGHT, TOP LEFT, BOTTOM RIGHT, AND FROM HANDLE. SEE ATTATCHED PICTURES PERFORMEDJul 26, 2024 · N818UA · Airbus A319131 · Emergency ExitsSDR CALA2023013100272Seal · crackedPDA 2 #1 ENG INBD T-R TO PYLON FLEX SEAL CRACKED & PARTIALLY MISSING .... SECOND FROM AFT IS PARTIALLY MISSING AND THIRD FROM AFT IS CRACKED -- SEE PHOTO APPLIED. PER STEP 3 ISSUE DIP TO INSPECT PER PART 2A EZCH FLIGHT CYCLE AND PERMENANT REPAIR PER PART 3 WITJan 30, 2023 · N818UA · Airbus A319131 · Engine Thrust ReverserSDR CALA2022113003245Shear Panel · corrodedAFT CABIN SHEAR PLATE LH SIDE IS CORRODED. PER HAECO LCQ NON-ROU TINE 9294440/44440. REMOVED AND REPLACED NEW SHEAR PLATE ON AFT CABIN L/H SIDE FR69 TO FR70 IAW SRM 51-72-11-911-001 AND TOP COATED FASTENERS I AW A319 SRM 51-23-11-001.Nov 28, 2022 · N818UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2022111103117Skin · crackedSUPPORT TASK: SURVERYED THE FASTENERS AT LH FR35, BETWEEN STRG 2 8 AND STRG 31, A PREVIOUS REPAIR IS SUSPECTED AS FASTENERS ARE A BOVE NOMINAL SIZE. FR35 STR30 LH HAS 3 CRACK INDICATIONS IN HOLE #2 IN FWD SKIN AND AFT SKIN LAYER @3 AND 9 OCLOCK AS SEEN FROM OUNov 9, 2022 · N818UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2022110703052Door Sill · corrodedR2 DOOR SILL IS CORRODED. R & R R2 DOOR SILL IAW SRM 51-42-11 AND 51-72-11.Nov 4, 2022 · N818UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2022102802978Cleat · corrodedFWD CARGO PIT R/H FR27 BETWEEN STRINGERS 41R-42R HAS CORROSION A T CLEAT DOT M093. PER HAECO LCQ NON-ROUTINE 9294244/44244 GENERA TED BY V919150. SPEC: A3NB-53-3-6105. REMOVED AND REPLACED CLEAT FWD CARGO R/H FR27 BETWEEN STRINGERS 41R-42R P/N 5323052620017 P.Oct 27, 2022 · N818UA · Airbus A319131 · Fuselage Main, FrameSDR CALA2022102702960Flange · crackedSUPPORT TASK: FRAME 68 STR 22 RH FLANGE HAS CRACK ABOVE DOOR STO P BOLT #3 PER HAECO LCQ NON-ROUTINE 9294158/44158 GENERATED BY V 892444Oct 26, 2022 · N818UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2022102702959Cleat · corrodedFWD CARGO PIT R/H FR27 BETWEEN STRINGER 42R-43R HAS CORROSION AT CLEAT (A3NB-53-3-6105) GENERATED BY V919150 AT HAECO LCQ PER NR 9294246 (44246) REMOVED AND REPLACED CLEAT FWD CARGO PIT R/H FR27 BETWEEN STRING ERS 42R-43R WITH P/N 5323039820101 IAW A319 SRM 51Oct 25, 2022 · N818UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2022102702955Fitting · crackedFRAME 68 STR 22 LH HAS CRACK IND. IN FLANGE AT RADIUS ABOVE DOOR STOP BOLT #3 PER HAECO LCQ NON ROUTINE 9294160/44160 GENERATED BY V892444Oct 25, 2022 · N818UA · Airbus A319131 · Fuselage Main, FrameSDR CALA2022102402926Fitting · crackedFLIGHT DECK WINDSHIELD CONTINUITY FITTINGS LH AND RH HAVE CRACK INDICATIONS "CONTACT ENGINEERING FOR REPAIR INSTRCUTIONS BEFORE NEXT FLIGHT" GENERATED AT HAECO LCQ PER NR 9294615 (44615) BY V8 92444 SUPPORT TASK ACCOMPLISHED A CATEGORY A PERMANENT REPAIR ON THOct 23, 2022 · N818UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2022102402916Door Sill · corrodedL2 DOOR SILL PLATE IS CORRODED. PER HAECO LCQ NON-ROUTINE 929444 1/44441 GENERATED BY V892442 SPEC: A3NB-53-3-6357. REPAIRED (2) DOOR SILL PLATE AT FR68 IAW A319 SRM 53-41-14-300-0 01 FIGURE 001 REPAIRED TOPCOAT IAW SRM 51-75-12-911-002 PERFORME D V928628 INSPOct 22, 2022 · N818UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2022101202793Frame · crackedLH EMERGENCY EXIT LH FRAME HAS EVIDENCE OF CRACK PER NR9294643/4 4643 GEN BY V935513 RMVD DAMAGED SEGMENT/FRAME ON LH SIDE OF LH EMERGENCY EXIT AND R EPLACED WITH A NEW FRAME IAW SRM 51-72-11-911-001 BY MECH V07484 6 INSP BY V061334Oct 11, 2022 · N818UA · Airbus A319131 · Emergency ExitsSDR CALA2022101002754Frame · crackedRH EMERGENCY EXIT LH AND RH FRAME HAS EVIDENCE OF CRACK. PER HAE CO LCQ NR 9294644/ 44644 REMOVED DAMAGED RH & LH FRAMES & REPLACED WITH NEW FRAMES IAW A3 19 SRM 51-72-11-911-001 & 002Oct 8, 2022 · N818UA · Airbus A319131 · Emergency ExitsSDR CALA2022052301323Panel · missingSMALL 2 INCH ROUND ACCESS PANEL MISSING FROMINBOARD SIDE OF OUTER MOST FLP/TRK FRNG RT SIDE REQUESTING CDL 27A. APPLIED SPEED TAPE TO HOLE. COMPLIED WITH CDL 27AD. ADD EMP:U113818 DISPATCH DESK: 06 NAME: AN DATE: 18-MAY-22- OK TO CDL UPDATED NR WITH PICTUREMay 23, 2022 · N818UA · Airbus A319131 · Flight Control SystemSDR CALA2022030700602Seal · damagedRAMP REPORTS FWD LAVATORY RIGHT SHROUD ACCESS PANEL PUSHED IN . SECURED INTERIM AS REQUIRED AND DEFERRED IAW NEF 2522NC, DDP C/W STICKER APPLIED. VARGAS TOMC DEFERRED DIRECTLY BY TOMC SHROUD SEAL IS DAMAGED REPORTED BY RAMP UPDATED MAA CODE FIX USING VENDOR MMar 7, 2022 · N818UA · Airbus A319131 · LavatoriesSDR CALA2021062800985Fairing · missingPDA 3 REF LOGPAGE #6550149 4 FLAP TRACK FAIRING PIVOT COVERS WERE FOUND MISSING ON ARRIVAL MEX. LOGPAGE #6550149 DEFERED PER CDL 27AD. IAH AND IAD HAVE BEEN INFORMED AND ARE CHECKING LOCALLY FOR POSSIBLE REMOVAL ISSUES THAT OCCURED AND NOT REINSTALLED.Jun 28, 2021 · N818UA · Airbus A319131 · Trailing Edge FlapsSDR CALA2020120401321Battery · inoperativeA3NB-33-3-6012 MAIN CABIN EMERGENCY LIGHT SYSTEM FAILS EPSU BATTERY FWD L33-51-38. (SDR) REF TO PEMCO/AIRBORNE NR 10261.0031. REMOVED AND REPLACED EPSU BATTERY PACK (10WL) (AERO DESIGN,INC), IAW A319 AMM 33-51-38-000-002-A, 33-51-38-400-002-A. OPERATIONS CHDec 3, 2020 · N818UA · Airbus A319131 · Emergency LightingSDR CALA2018043001204Hinge Fitting · wornLEFT MLG DOOR HINGE FITTING FORWARD LUG, FORWARD FACE, IS WORN AROUND THE BORE. REMOVED AND REPLACED THE MLG DOOR HINGE FITTING IAW SRM 51-4 2-11-001, PARA 2F, AND 51-44-11-001, TABLES 00108 AND 00116.Apr 28, 2018 · N818UA · Airbus A319131 · Landing Gear DoorsSDR CALA2018043001203Hinge Fitting · wornRIGHT MLG DOOR HINGE FITTING FORWARD LUG, FORWARD FACE, IS WORN AROUND THE BORE. REMOVED & REPLACED THE RT MLG DOOR HINGE FITTING IAW SRM 51-42 -11, PARA 2.F.Apr 28, 2018 · N818UA · Airbus A319131 · Landing Gear DoorsSDR CALA2018043001202Skin · dentedRIGHT WING NNR 3 SLAT UPPER L/E SKIN DENTED. REPAIRED THE DENT IAW SRM 57- 40-00-300-108.Apr 28, 2018 · N818UA · Airbus A319131 · Leading Edge DevicesSDR CALA2018043001201Skin · dentedLEFT LOWER FUSELAGE SKIN HAS A DENT AT FRAME 27, BETWEEN STRINGERS 38L - 39L. INSTALLED A REPAIR DOUBLER IAW SRM 53-00-11-300-043, FIG 20145, AND SRI53-00-205-017.Apr 28, 2018 · N818UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2017121604481Lens · missingAISLE LIGHT COVER AT ROW 22 MISSING NEVER WAS THERE REPLACED LENS COVER ON EMERGENCY ILLUMINATION LIGHT AT ROW 22 CEILINGDec 16, 2017 · N818UA · Airbus A319131 · Emergency LightingSDR CALA2015011692989Skin Panel · saturatedRIGHT ELEVATOR LOWER SKIN PANEL HAS 2 TRAPPED WATER INDICATIONS 124" FROM INBD END 5" FROM TE 3 X 4" DIA, 139" FROM INBD END 4.5" FROM TE 3 X 3.5" DIA. MOISTURE PRESENT. REPAIRED IAW SRM 55-21-11 PARA 5E FIG 205. SRI 55-21-11-2-002-00 TABLE 203 REQUIRES REIJan 13, 2015 · N818UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2015011692988Skin · saturatedRIGHT ELEVATOR UPPER PANEL HAS 5 TRAPPED WATER INDICATIONS 54" FROM INBD END 5" FROM TE 4" DIA, 125" FROM INBD END 5" FROM TE 4" DIA, 168" FROM INBD END 4.5" FROM TE 2.5" DIA, 176" FROM INBD END 4.5" FROM TE 3" DIA, 189" FROM INBD END 4" FROM TE 3 X 3.5" DIA, Jan 13, 2015 · N818UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2015011692987Skin · saturatedLEFT ELEVATOR HAS 1 TRAPPED WATER INDICATION THE LOWER SKIN 88" FROM INBD END & 4.5" FROM TE 3" DIA. & 7" ON UPPER SKIN 39" FROM INBD END 4.5" FROM TE 2.5" DIA 88" FROM INBD END 6" FROM TE 3.5 X 4" DIA, 94" FROM INBD END 5" FROM TE 2.5 DIA, 101.5" FROM INBD ENJan 13, 2015 · N818UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2015010992914Door Sill · corrodedR2 DOOR SILL HAS CORROSION ON AFT INBD FLANGE NUTPLATE HOLE. REPAIRED DOOR SILL AT INBD FLANGE IAW SRM 53-41-14 FIG 201 SHEET 3 REPAIR PRINCIPLE 4.Jan 7, 2015 · N818UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014120292758Unknown · odorDURING FLIGHT, ACFT HAS A SMELL SIMILAR TO PLASTIC MELTING IN OVEN. SEEMS TO WORSEN WITH POWER INCREASE. PERFORMED NR 2 ENG WASH. REPLACED LT & RT RECIRCULATION FILTERS. PERFORMED HIGH POWER ENG RUN TO BURN OUT SMELL IAW JRH-2-40-35. NO ODOR AT THIS TIME.Nov 29, 2014 · N818UA · Airbus A319131 · Air Distribution SystemSDR CALA2014022190406Power Supply · inoperativeEMERGENCY LIGHT TEST FAILED ON 2 SERVICE. REPLACED RT OVERWING EPSU WL 12 & LT OVERWING EPSU BATTERY IAW MM33-51-38. ACCOMPLISHED OPERATIONAL TEST OF THE EMERGENCY LIGHTS IAW MM33- 51-00, OPERATIONS CHECKED GOOD.Feb 20, 2014 · N818UA · Airbus A319131 · Emergency LightingSDR CALA2013123094055Screw · missingCORNER & CORNER 1 SCREWS MISSING AT AFT INBD EDGE OF BELLY PNL JUST AFT OF ROT BCN. PLACED ON DEFERRAL NEEDS NUT PLATE PANEL 192KB INBD SIDE IAW 53-35-00-200-002A. ONLY ONE SCREW REMAINS MISSING WHICH IS INBD CTR, ALL OTHERS REPLACED.Dec 29, 2013 · N818UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2013120293336Sealant · missingNR 2 ENG THRUST REVERSER C DUCT SEAL, SEALANT, MISSING ON LT & RT HALF, IAW AMM MT78- 016 FOR DISPOSITION. REPAIRED SEAL ON CNA IAW MT 78-001.Dec 1, 2013 · N818UA · Airbus A319131 · Engine Thrust ReverserSDR CALA2013120293388Connector · corrodedREPEAT LOG ON TAXI OUT, MULTIPLE ECAM MESSAGES RELATED TO RT MLG SENSOR 22GA. PHYSICAL INSPECTION OF SENSOR 22GA ON RT GEAR, NO OBVIOUS DEFECTS IAW PFR MESSAGE 32-31-73, 22GA TARGET POSITION SOURCE LGCIU 2, IAW TSM 32-31-00-810-842-A. MESSAGE DID NOT OCCUR UNov 29, 2013 · N818UA · Airbus A319131 · Landing Gear System WiringSDR CALA2013103092529Switch · damagedWX RADAR SWITCH DAMAGED. REPLACED PANEL GRD CHECKED GOOD BY LAXMM.Oct 29, 2013 · N818UA · Airbus A319131 · Weather Radar SystemSDR CALA2013082090592Actuator · leakingMAINTENANCE WALKAROUND FOUND HYD FLUID LEAKING FROM NR 1 ENGINE LOWER AFT FAN COWLING. FOUND UPPER OUTBOARD ACTUATOR LEAKING. DEACT ENGINE THRUST REVERSER SYSTEM FOR FLIGHT REF MM. STOWED AND LOCKED, NO LEAKS. FOUND THRUST REVERSER ACTUATOR LEAKING AND CHANAug 16, 2013 · N818UA · Airbus A319131 · Engine Thrust ReverserSDR UALA2013061204003Skin · dentedDENT IN FUSELAGE, APPROX 2 FEET AFT OF MAIN ENTRY DOOR 1L.Jun 10, 2013 · N818UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR UALA2013061204002Skin · dentedDENT FOUND OUT OF LIMITS AT C-CHECK. DENT IS AT FR23 AT STR 23L. REPAIR INSTALLED IAW SRM 53-11-11, FIG 212.Jun 10, 2013 · N818UA · Airbus A319131 · Fuselage Main, Plate/Skin
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