# Service difficulty reports: N818UA

A list on [N818UA](https://openairdocs.org/aircraft/N818UA.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 112 reports

- [SDR CALA2026092519801](https://openairdocs.org/sdr/CALA2026092519801.md): Panel · missing · Sep 21, 2026 · N818UA · Airbus A319131 · Nacelle/Pylon, Main Frame
  > FOUND 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.
- [SDR CALA2026083118996](https://openairdocs.org/sdr/CALA2026083118996.md): Fuel Cap · missing · Aug 27, 2026 · N818UA · Airbus A319131 · Fuel Storage
  > UPON 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.
- [SDR CALA2026061517117](https://openairdocs.org/sdr/CALA2026061517117.md): Light · inoperative · Jun 12, 2026 · N818UA · Airbus A319131 · Emergency Lighting
  > CABIN 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.
- [SDR CALA2026051116104](https://openairdocs.org/sdr/CALA2026051116104.md): A/C Pack · faulted · May 3, 2026 · N818UA · Airbus A319131 · Cabin Cooling System
  > NR 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/
- [SDR CALA2025082508084](https://openairdocs.org/sdr/CALA2025082508084.md): Light · shorted · Aug 23, 2025 · N818UA · Airbus A319131 · Emergency Lighting
  > PROCEDURE - 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/
- [SDR CALA2025082508080](https://openairdocs.org/sdr/CALA2025082508080.md): Light · inoperative · Aug 22, 2025 · N818UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY AISLE LIGHT INOPERATIVE AT ROW 31. R & R EMERGENCY LIGHT ASSY AT ROW 31 IAW AMM 33-51-20. OK FOR SERVICE.
- [SDR CALA2025071406560](https://openairdocs.org/sdr/CALA2025071406560.md): Power Supply · faulted · Jul 11, 2025 · N818UA · Airbus A319131 · Emergency Lighting
  > EPSU EXT LOAD EMER R FAULT. REPLACED 12W EPSU REF AMM 33-51-38-401. OPS CHECKS GOOD.
- [SDR CALA2025051504703](https://openairdocs.org/sdr/CALA2025051504703.md): Bleed Valve · faulted · May 12, 2025 · N818UA · Airbus A319131 · Compressor Bleed Valve
  > ENG 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 PL
- [SDR CALA2025041703948](https://openairdocs.org/sdr/CALA2025041703948.md): Door Frame · corroded · Apr 16, 2025 · N818UA · Airbus A319131 · Fuselage Main, Structure
  > R/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
- [SDR CALA2025041503881](https://openairdocs.org/sdr/CALA2025041503881.md): Frame · cracked · Apr 13, 2025 · N818UA · Airbus A319131 · Fuselage Main, Frame
  > R/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 WI
- [SDR CALA2025041503880](https://openairdocs.org/sdr/CALA2025041503880.md): Frame · cracked · Apr 13, 2025 · N818UA · Airbus A319131 · Fuselage Main, Frame
  > R/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 W
- [SDR CALA2025040703588](https://openairdocs.org/sdr/CALA2025040703588.md): Skin · contaminated · Apr 4, 2025 · N818UA · Airbus A319131 · Elevator, Plate/Skin
  > L/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/
- [SDR CALA2024123001715](https://openairdocs.org/sdr/CALA2024123001715.md): Slide · out of position · Dec 26, 2024 · N818UA · Airbus A319131 · Escape Slide
  > DOOR 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 CHECKLI
- [SDR CALA2024102302713](https://openairdocs.org/sdr/CALA2024102302713.md): Skin · cracked · Oct 19, 2024 · N818UA · Airbus A319131 · Trailing Edge Flaps
  > RT 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.
- [SDR CALA2024081902230](https://openairdocs.org/sdr/CALA2024081902230.md): Fuel Cap · missing · Aug 16, 2024 · N818UA · Airbus A319131 · Fuel Storage
  > PDA 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.
- [SDR CALA2024072900303](https://openairdocs.org/sdr/CALA2024072900303.md): Seal · leaking · Jul 26, 2024 · N818UA · Airbus A319131 · Emergency Exits
  > CREW 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 PERFORMED
- [SDR CALA2023013100272](https://openairdocs.org/sdr/CALA2023013100272.md): Seal · cracked · Jan 30, 2023 · N818UA · Airbus A319131 · Engine Thrust Reverser
  > PDA 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 WIT
- [SDR CALA2022113003245](https://openairdocs.org/sdr/CALA2022113003245.md): Shear Panel · corroded · Nov 28, 2022 · N818UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT 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.
- [SDR CALA2022111103117](https://openairdocs.org/sdr/CALA2022111103117.md): Skin · cracked · Nov 9, 2022 · N818UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > SUPPORT 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 OU
- [SDR CALA2022110703052](https://openairdocs.org/sdr/CALA2022110703052.md): Door Sill · corroded · Nov 4, 2022 · N818UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL IS CORRODED. R & R R2 DOOR SILL IAW SRM 51-42-11 AND 51-72-11.
- [SDR CALA2022102802978](https://openairdocs.org/sdr/CALA2022102802978.md): Cleat · corroded · Oct 27, 2022 · N818UA · Airbus A319131 · Fuselage Main, Frame
  > FWD 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.
- [SDR CALA2022102702960](https://openairdocs.org/sdr/CALA2022102702960.md): Flange · cracked · Oct 26, 2022 · N818UA · Airbus A319131 · Fuselage Main, Structure
  > SUPPORT 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 892444
- [SDR CALA2022102702959](https://openairdocs.org/sdr/CALA2022102702959.md): Cleat · corroded · Oct 25, 2022 · N818UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > FWD 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 51
- [SDR CALA2022102702955](https://openairdocs.org/sdr/CALA2022102702955.md): Fitting · cracked · Oct 25, 2022 · N818UA · Airbus A319131 · Fuselage Main, Frame
  > FRAME 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 V892444
- [SDR CALA2022102402926](https://openairdocs.org/sdr/CALA2022102402926.md): Fitting · cracked · Oct 23, 2022 · N818UA · Airbus A319131 · Fuselage Main, Structure
  > FLIGHT 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 TH
- [SDR CALA2022102402916](https://openairdocs.org/sdr/CALA2022102402916.md): Door Sill · corroded · Oct 22, 2022 · N818UA · Airbus A319131 · Fuselage Structure (General)
  > L2 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 INSP
- [SDR CALA2022101202793](https://openairdocs.org/sdr/CALA2022101202793.md): Frame · cracked · Oct 11, 2022 · N818UA · Airbus A319131 · Emergency Exits
  > LH 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 V061334
- [SDR CALA2022101002754](https://openairdocs.org/sdr/CALA2022101002754.md): Frame · cracked · Oct 8, 2022 · N818UA · Airbus A319131 · Emergency Exits
  > RH 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 & 002
- [SDR CALA2022052301323](https://openairdocs.org/sdr/CALA2022052301323.md): Panel · missing · May 23, 2022 · N818UA · Airbus A319131 · Flight Control System
  > SMALL 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 PICTURE
- [SDR CALA2022030700602](https://openairdocs.org/sdr/CALA2022030700602.md): Seal · damaged · Mar 7, 2022 · N818UA · Airbus A319131 · Lavatories
  > RAMP 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 M
- [SDR CALA2021062800985](https://openairdocs.org/sdr/CALA2021062800985.md): Fairing · missing · Jun 28, 2021 · N818UA · Airbus A319131 · Trailing Edge Flaps
  > PDA 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.
- [SDR CALA2020120401321](https://openairdocs.org/sdr/CALA2020120401321.md): Battery · inoperative · Dec 3, 2020 · N818UA · Airbus A319131 · Emergency Lighting
  > A3NB-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 CH
- [SDR CALA2018043001204](https://openairdocs.org/sdr/CALA2018043001204.md): Hinge Fitting · worn · Apr 28, 2018 · N818UA · Airbus A319131 · Landing Gear Doors
  > LEFT 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.
- [SDR CALA2018043001203](https://openairdocs.org/sdr/CALA2018043001203.md): Hinge Fitting · worn · Apr 28, 2018 · N818UA · Airbus A319131 · Landing Gear Doors
  > RIGHT 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.
- [SDR CALA2018043001202](https://openairdocs.org/sdr/CALA2018043001202.md): Skin · dented · Apr 28, 2018 · N818UA · Airbus A319131 · Leading Edge Devices
  > RIGHT WING NNR 3 SLAT UPPER L/E SKIN DENTED. REPAIRED THE DENT IAW SRM 57- 40-00-300-108.
- [SDR CALA2018043001201](https://openairdocs.org/sdr/CALA2018043001201.md): Skin · dented · Apr 28, 2018 · N818UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > LEFT 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.
- [SDR CALA2017121604481](https://openairdocs.org/sdr/CALA2017121604481.md): Lens · missing · Dec 16, 2017 · N818UA · Airbus A319131 · Emergency Lighting
  > AISLE LIGHT COVER AT ROW 22 MISSING NEVER WAS THERE REPLACED LENS COVER ON EMERGENCY ILLUMINATION LIGHT AT ROW 22 CEILING
- [SDR CALA2015011692989](https://openairdocs.org/sdr/CALA2015011692989.md): Skin Panel · saturated · Jan 13, 2015 · N818UA · Airbus A319131 · Elevator, Plate/Skin
  > RIGHT 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 REI
- [SDR CALA2015011692988](https://openairdocs.org/sdr/CALA2015011692988.md): Skin · saturated · Jan 13, 2015 · N818UA · Airbus A319131 · Elevator, Plate/Skin
  > RIGHT 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,
- [SDR CALA2015011692987](https://openairdocs.org/sdr/CALA2015011692987.md): Skin · saturated · Jan 13, 2015 · N818UA · Airbus A319131 · Elevator, Plate/Skin
  > LEFT 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 EN
- [SDR CALA2015010992914](https://openairdocs.org/sdr/CALA2015010992914.md): Door Sill · corroded · Jan 7, 2015 · N818UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R2 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.
- [SDR CALA2014120292758](https://openairdocs.org/sdr/CALA2014120292758.md): Unknown · odor · Nov 29, 2014 · N818UA · Airbus A319131 · Air Distribution System
  > DURING 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.
- [SDR CALA2014022190406](https://openairdocs.org/sdr/CALA2014022190406.md): Power Supply · inoperative · Feb 20, 2014 · N818UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY 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.
- [SDR CALA2013123094055](https://openairdocs.org/sdr/CALA2013123094055.md): Screw · missing · Dec 29, 2013 · N818UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > CORNER & 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.
- [SDR CALA2013120293336](https://openairdocs.org/sdr/CALA2013120293336.md): Sealant · missing · Dec 1, 2013 · N818UA · Airbus A319131 · Engine Thrust Reverser
  > NR 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.
- [SDR CALA2013120293388](https://openairdocs.org/sdr/CALA2013120293388.md): Connector · corroded · Nov 29, 2013 · N818UA · Airbus A319131 · Landing Gear System Wiring
  > REPEAT 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 U
- [SDR CALA2013103092529](https://openairdocs.org/sdr/CALA2013103092529.md): Switch · damaged · Oct 29, 2013 · N818UA · Airbus A319131 · Weather Radar System
  > WX RADAR SWITCH DAMAGED. REPLACED PANEL GRD CHECKED GOOD BY LAXMM.
- [SDR CALA2013082090592](https://openairdocs.org/sdr/CALA2013082090592.md): Actuator · leaking · Aug 16, 2013 · N818UA · Airbus A319131 · Engine Thrust Reverser
  > MAINTENANCE 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 CHAN
- [SDR UALA2013061204003](https://openairdocs.org/sdr/UALA2013061204003.md): Skin · dented · Jun 10, 2013 · N818UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > DENT IN FUSELAGE, APPROX 2 FEET AFT OF MAIN ENTRY DOOR 1L.
- [SDR UALA2013061204002](https://openairdocs.org/sdr/UALA2013061204002.md): Skin · dented · Jun 10, 2013 · N818UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > DENT FOUND OUT OF LIMITS AT C-CHECK. DENT IS AT FR23 AT STR 23L. REPAIR INSTALLED IAW SRM 53-11-11, FIG 212.

Next page: https://openairdocs.org/aircraft/N818UA/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N818UA/reports

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