# Service difficulty reports: N834UA

A list on [N834UA](https://openairdocs.org/aircraft/N834UA.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 2 · 95 reports

- [SDR CALA2026071417772](https://openairdocs.org/sdr/CALA2026071417772.md): Battery · faulty · Jul 14, 2026 · N834UA · Airbus A319131 · Emergency Lighting
  > ESPU BATTERY FWD L FAULT MESSAGE DURING EMERGENCY LIGHT OPS CHECK ON CIDS PANEL REMOVED AND REPLACED THE FWD L EPSU BATTERY. IAW AMM 33-51-38. OPS CHECK GOOD.
- [SDR CALA2026031014463](https://openairdocs.org/sdr/CALA2026031014463.md): Power Supply · faulted · Mar 8, 2026 · N834UA · Airbus A319131 · Emergency Lighting
  > ESPU FAULT MESSAGE, ESPU EXT LOAD EMER R. APPEARS DURING EMER LIGHTING TEST. R & R RT CENTER EPSU IAW TASK 33-51-38-000-001-A, FAULT PERSISTED, R & R FOUR EXT EMERGENCY LIGHTS UNDER LT & RT OVERWING EMERGENCY EXIT DOORS REF TASK 33-51-15-000-001-A, OP CK GO
- [SDR CALA2026021113692](https://openairdocs.org/sdr/CALA2026021113692.md): Light · dirty · Feb 9, 2026 · N834UA · Airbus A319131 · Emergency Lighting
  > RIGHT DOOR CEILING EXIT LIGHT INOPERATIVE, DURING INCOMING EMERGENCY LIGHTS OPS CHECK. SUPPORT TASK NSA EMX NR 00002. NO PARTS CHANGED. THE BASE, LENS, AND CONTACTS OF THE R1 DOOR CEILING EXIT LIGHT WERE CLEANED IAW AMM 20-55-10-02. OPS CHECKED GOOD.
- [SDR CALA2026021013662](https://openairdocs.org/sdr/CALA2026021013662.md): Bulb · no test · Feb 9, 2026 · N834UA · Airbus A319131 · Emergency Lighting
  > LT ENTRY EXIT LIGHT INOPERATIVE DURING INCOMING EMERGENCY LIGHTS OPS CHECK. REMOVED AND REINSTALLED BULB AT LT ENTRY EXIT LIGHT IAW AMM 33-51-13-400-001-A, OPS CHECKED GOOD.
- [SDR CALA2026010612690](https://openairdocs.org/sdr/CALA2026010612690.md): Unknown · odor · Jan 5, 2026 · N834UA · Airbus A319131 · Air Distribution System
  > DIRTY SOCK SMELL FL290 EPR 1.19 N1 74 PERCENT N2 83 PERCENT PERFORMED INSPECTION FOR ODOR EVENT REF AMM 05-50-00-810-831-A. TYPE 10 MISC. DETERMEMDED TO BE MOST LICKLEY, CHECKED PACK INLETS AND E & E COMPARTMENTS NO EVIDANCE OF ANY DEFECTS AT THIS TIME. SCENT
- [SDR CALA2025100709752](https://openairdocs.org/sdr/CALA2025100709752.md): Stringer · gouged · Oct 3, 2025 · N834UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > FOUND 2 LARGE SCRATCHES AND DENT ON FUSELAGE JUST AFT OF DOOR 1L.THE GOUGE MEASURES 4.25" BY 2.0" AND GOES ACROSS A STRINGER AND THROUGH TWO RIVET HEADS (AS PICTURED). THE DENT MEASURES.065" DEEP. USING SRM REFERENCE 53-11-11-283-017 BLEND OUT (REWORK) PLUS D
- [SDR CALA2025080107211](https://openairdocs.org/sdr/CALA2025080107211.md): Plate · damaged · Jul 22, 2025 · N834UA · Airbus A319131 · Fuselage Main, Structure
  > FRAME 68, S10 - 16. INNER CAP GUSSET PLATE JOINT, ALL FASTENER HOLES HAVE REJECTABLE INDICATIONS. ACP INITIAL INSPECTION OF THE GUSSET HOLES IAW PART 2 OF THE LATEST REV OF ECRA 5341-01508. ACCOMPLISHED REPAIR IAW RCO-L25500.
- [SDR CALA2025080107210](https://openairdocs.org/sdr/CALA2025080107210.md): Frame · corroded · Jul 22, 2025 · N834UA · Airbus A319131 · Fuselage Main, Frame
  > LEFT FR 66, S10 - 16L INNER CAP GUSSET PLATE JOINT, ALL FASTENER ATTACH HOLES HAVE INDICATIONS. INTERIM REPAIR FOR FR 66 HAS BEEN ACCOMPLISHED IAW PART 1 OF ECRA 5341-01508 WITHOUT DEVIATIONS. ACCOMPLISHED REPAIR IAW REO-L25500REV1R WITH NO DEVIATIONS.
- [SDR CALA2025071706660](https://openairdocs.org/sdr/CALA2025071706660.md): Door Sill · corroded · Jul 16, 2025 · N834UA · Airbus A319131 · Fuselage Main, Structure
  > CABIN R2 ENTRY FLOOR HAS CORROSION AROUND FWD AND AFT GIRT BAR F ITTING A3NB-53-3-6222 PER HAECO LCQ NON ROUTINE 9290675/40675. REMOVED AND REPLACED R2 DOOR SILL IAW A319 SRM 51-42-11.
- [SDR CALA2025071706659](https://openairdocs.org/sdr/CALA2025071706659.md): Bracket · corroded · Jul 16, 2025 · N834UA · Airbus A319131 · Fuselage Main, Attach Fittings
  > RH AFT WATER DRAIN FR69 HAS CORROSION ON TIP. REMOVED AND REPLACED LH AFT WATER DRAIN FR 69 IAW A319 SRM 51-72 -11.
- [SDR CALA2025071706655](https://openairdocs.org/sdr/CALA2025071706655.md): Frame · gouged · Jul 11, 2025 · N834UA · Airbus A319131 · Fuselage Main, Frame
  > FWD PRESSURE BULKHEAD FRAME 1 FWD FACE UPPER DOUBLER RBL 7 HAS A GOUGE. REMOVED AND REPLACED FWD PRESSURE BULKHEAD FRAME 1 FWD SPLICE I AW A319 SRM 51-42-11.
- [SDR CALA2025071606613](https://openairdocs.org/sdr/CALA2025071606613.md): Skin · contaminated · Jul 9, 2025 · N834UA · Airbus A319131 · Elevator, Plate/Skin
  > LEFT ELEVATOR UPPER SURFACE HAS INDICATION OF WATER INGRESS 27 IN FROM IB EDGE, 23 IN FROM AFT EDGE AND 2 IN IN DIAMETER. REPAIRED LT ELEVATOR UPPER SURFACE IAW SRM 55-20-00-20 0-006-A AND SRM 55-21-11-300-005.
- [SDR CALA2025063006066](https://openairdocs.org/sdr/CALA2025063006066.md): Skin · corroded · Jun 27, 2025 · N834UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > AFT LAVATORY VENTILATION OUTLET INTERNAL STRUCTURE SKIN HAS CORROSION BETWEEN FR 69-70 AND STR 31 & 32 PER HAECO LCQ N/R 9290435/40435 GEN BY V937268 REMOVED AND REPLACED INTERNAL STRUCTURE SKIN (DOUBLER) AT AFT LAV VENTILATION OUTLET FR69-70, STG 31R - 32R IA
- [SDR CALA2025071706648](https://openairdocs.org/sdr/CALA2025071706648.md): Shear Plate · corroded · Jun 25, 2025 · N834UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > LEFT SHEAR PLATE SUPPORT (FR.69-70) CORRODED. REMOVED AND REPLACED LT SHEAR PLATE SUPPORT FR69-70 IAW SRM 51-42-11.
- [SDR CALA2025062505874](https://openairdocs.org/sdr/CALA2025062505874.md): Shear Plate · corroded · Jun 20, 2025 · N834UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > CABIN FLOOR LH SHEAR PLATE AT FR 69-70 HAS CORROSION AND MISSING RIVETS AT Y1292 A3NB-53-3-6222. R & R L/H SHEAR PLATE AT FR 69-70 IAW SRM A319 51-42-11.
- [SDR CALA2025062305817](https://openairdocs.org/sdr/CALA2025062305817.md): Profile · cracked · Jun 20, 2025 · N834UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > BULK CARGO FR60 STR 38L PROFILE PANEL IS CRACKED. REMOVED AND REPLACED DAMAGED PROFILE PANEL IN AFT CC, BULK CC AT FR 60 STR 38L IAW A319 SRM 57-42-11/001.
- [SDR CALA2025062305809](https://openairdocs.org/sdr/CALA2025062305809.md): Seat Track · corroded · Jun 19, 2025 · N834UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN -Y1292 SEAT TRACK STA 37 TO 40 HAS CORROSION (A3NB-53 -3-6339) PER HAECO LCQ NON ROUTINE 9290808/40808 REMOVED AND REPLACED SEAT TRACK -Y1292 AT FR 37-FR 40 IAW SRM 51-42-11. REMOVED CORROSION ON SEAT TRACK -Y1292 FOUND TO BE OUT OF LIMITS REMOVED S
- [SDR CALA2025061705623](https://openairdocs.org/sdr/CALA2025061705623.md): Door Frame · cracked · Jun 14, 2025 · N834UA · Airbus A319131 · Fuselage Main, Structure
  > RIGHT O/W ESCAPE HATCH AFT VERTICAL FRAME APPEARS TO BE CRACKED. REMOVED AND REPLACED RH OW ESCAPE HATCH AFT VERTICAL FRAME IAW A 320/319 SRM 51-72-11-911-002, SRM 51-42-11.
- [SDR CALA2025061705622](https://openairdocs.org/sdr/CALA2025061705622.md): Door Frame · cracked · Jun 14, 2025 · N834UA · Airbus A319131 · Fuselage Main, Structure
  > LEFT O/W ESCAPE HATCH FWD VERTICAL FRAME APPEARS TO BE CRACKED. REMOVED AND REPLACED LH OW ESCAPE HATCH FWD VERTICAL FRAME IAW A 3208319 51-72-11-911.
- [SDR CALA2025061705621](https://openairdocs.org/sdr/CALA2025061705621.md): Angle · cracked · Jun 14, 2025 · N834UA · Airbus A319131 · Emergency Exits
  > L/H O/W ESCAPE HATCH AFT VERTICAL FRAME APPEARS TO BE CRACKED. REMOVED AND REPLACED LH OW ESCAPE HATCH AFT VERTICAL FRAME IAW A 320/319 SRM 51-72-11-911.
- [SDR CALA2025061705620](https://openairdocs.org/sdr/CALA2025061705620.md): Skin · cracked · Jun 14, 2025 · N834UA · Airbus A319131 · Emergency Exits
  > R/H EMERGENCY HATCH CRACK IN SKIN AT FASTENER APROX 6 INCHES FROM TOP OF L/H LOAD TRANSMITTING PER HAECO LCQ N/R 9290553/ 40553. REMOVED AND REPLACED RH EMERGENCY HATCH FWD VERTICAL FRAME IAW A SRM 51-72-11-911.
- [SDR CALA2025060205175](https://openairdocs.org/sdr/CALA2025060205175.md): Shear Plate · corroded · Jun 1, 2025 · N834UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > CABIN FLOOR RH SHEAR PLATE LOWER AND UPPER SURFACES AT FR 69-70 HAS CORROSION. REMOVED CORROSION ON RH SHEAR PLATE IAW A320 SRM 51-74-00. SHEAR PLATE DOES NOT HAVE ALLOWABLE DAMAGE LIMITS PER SRM. REMOVED AND REPLACED RH SHEAR PLATE IAW A320 SRM 51-42-11. WP
- [SDR CALA2025032803275](https://openairdocs.org/sdr/CALA2025032803275.md): Power Supply · no test · Mar 27, 2025 · N834UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY POWER SUPPLY UNIT FAILED OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT IAW AMM TASK 33-51-38-000-001-A0 & TASK 33-51-38-400-001-A. PERFORMED CABIN EMERGENCY LIGHTS TEST. OPS CHECK GOOD.PARTS USED: 31-33
- [SDR CALA2025021402330](https://openairdocs.org/sdr/CALA2025021402330.md): Fan · failed · Feb 10, 2025 · N834UA · Airbus A319131 · Air Distribution Fan
  > VERY STRONG BURNING SMEL L AFTER LANDING SIMILAR TO PAPER OR PLA STIC. NO VISIBLE SMOKE OR ECAMS. ODOR WAS ONLY IN THE COCKPIT EVERYTHING OPERATED NORMALLY. CAME 1 MINUTE AFTER LANDING AVNCS VENT BLOWER FAN BREAKER POPED (AD10) APPLIED MEL 2126AC. DDP COMPLIED
- [SDR CALA2025020602223](https://openairdocs.org/sdr/CALA2025020602223.md): Power Supply · discharged · Feb 4, 2025 · N834UA · Airbus A319131 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - EPSU UNIT AFT L 33-51-38 RPLCD EPSU AND NEW BATT, NO HELP. SLAVED IN NEW EPSU AND NEW BATT, NO HELP, RESULTS IN NO COMM AT CIDS PANEL TEST. PLEASE VERIFY PROPER EPSU PART NUMBER IS CURRENTLY INSTLD
- [SDR CALA2024102802743](https://openairdocs.org/sdr/CALA2024102802743.md): Slat · damaged · Oct 24, 2024 · N834UA · Airbus A319131 · Leading Edge Devices
  > BIRDSTRIKE ON CLIMBOUT AROUND 8000FT. DAMAGE TO LEFT SLAT. ATTACHING PPU INFO FOR SLAT REMOVAL. UPDATE PERFORMED REMOVAL OF THE NO. 4 SLAT UP TO AND INCLUDING STEP REMOVAL OF THE NO. 4 SLAT FROM 4.A.(1)(A)1 UPTO COMPLETION AS INSPECTED LEFT HAND SIDE SLAT #4
- [SDR CALA2024051301447](https://openairdocs.org/sdr/CALA2024051301447.md): Fuel Cap · missing · May 7, 2024 · N834UA · Airbus A319131 · Fuel Storage
  > PDA 2 FUEL CAP FOUND MISSING ONM ARR FROM ATL CONTACTING ATL TO FOLLOW UP IF LEFT BEHIND ITEM CLOSED WILL UPDATE AS NEEDED
- [SDR CALA2023122003692](https://openairdocs.org/sdr/CALA2023122003692.md): Skin · contaminated · Dec 17, 2023 · N834UA · Airbus A319131 · Elevator, Plate/Skin
  > R/H ELEVATOR HAS LIQUID INGRESS AT 29 INCHES FROM INBOARD EDGE 9.5 INCHES FROM TRAILING EDGE 2IN DIAMETER. REPAIRED RH ELEVATOR UPPER SKIN 29 IN FROM IB EDGE 9.5 IN FROM T /E 2IN DIA ZONE 1 IAW A319 SRM 55-21-11-300-005 CAT A REPAIR PN D5528000301500 SN 208
- [SDR CALA2023122003690](https://openairdocs.org/sdr/CALA2023122003690.md): Skin · contaminated · Dec 17, 2023 · N834UA · Airbus A319131 · Elevator, Plate/Skin
  > R/H ELEVATOR HAS LIQUID INGRESS AT 12 INCHESFROM INBOARD EDGE 17I NCHES FROM TRAILING EDGE 2 INCHES IN DIAMETER. REPAIRED RH ELEVATOR 12IN FROM I/B 17IN FROM T/E UPPER SKIN 2IN DIA ZONE 1 IAW A319 SRM 55-21-11-300-005 CAT A REPAIR PN D552800 0301500.
- [SDR CALA2023020100296](https://openairdocs.org/sdr/CALA2023020100296.md): Seal · missing · Feb 1, 2023 · N834UA · Airbus A319131 · Nose/Tail Landing Gear
  > PDA 3 FOUND ON WALK AROUND: AT NOSE GEAR LEG DOOR. RIGHT PLATE (SEAL) IS MISSING INSTALLED NEW PLATE (SEAL) ON RIGHT SIDE OF NOSE GEAR LEG DOOR
- [SDR CALA2022111703171](https://openairdocs.org/sdr/CALA2022111703171.md): Fuel Cap · missing · Nov 17, 2022 · N834UA · Airbus A319131 · Fuel Storage
  > RIGHT WING REFUEL CAP MISSING REFUEL/DEFUEL COUPLING CAP MISSING NO LEAKS NOTED FUEL CAP. INSTALLED FUEL CAP. FOUND MISSING FUEL CAP..
- [SDR CALA2022110703074](https://openairdocs.org/sdr/CALA2022110703074.md): Fastener · missing · Nov 7, 2022 · N834UA · Airbus A319131 · Fuselage Structure (General)
  > MISSING FASTENERS, INSTALLED NEW FASTENERS.
- [SDR CALA2022093002579](https://openairdocs.org/sdr/CALA2022093002579.md): None · none · Sep 30, 2022 · N834UA · Airbus A300* · Fuselage Internal Mounting Structure
  > AFT PIT, THRESHOLD METAL STICKING UP EF5300010-1 REF. ECRA 5322-01050 REV. H AND INITIATED A DIP TO REPAIR WITHIN 7 CALENDAR DAYS. REINSPECT TAPE PER PART 2 DAILY AND TO PERFORM PART 3 PERMANENT COMPLIED WITH PART 1C INTERIM REPAIR, TRIMMED AND TAPED THRESHOLD
- [SDR CALA2021102001933](https://openairdocs.org/sdr/CALA2021102001933.md): None · missing · Oct 20, 2021 · N834UA · Airbus A319131 · Steering Unit
  > PDA 3 NLG ELECTRICAL BOX BYPASS LEVER SPRING CLAMPS AND ATTACHING HARDWARE COMPLETELY MISSING -- SEE PHOTO PHOTO ADDED. PARTS IPC 32-51-12-01E THREADS ARE STRIPPED FOR ATTACH HARDWARE-- NEEDS ELECT BOX ASSLY R AND R NOSE WHEEL STEERING ELECTRICAL BOX REF AMM
- [SDR CALA2019111601976](https://openairdocs.org/sdr/CALA2019111601976.md): Panel · damaged · Nov 13, 2019 · N834UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > RH FR35 STRINGER 30 HAS REJECTABLE DAMAGE ON HOLE NUMBER 3 ON NR 9290222 PER HAECO LCQ REPAIRED #3 HOLE RH FR35 AT STR 30 IAW ECRA 5331-02503. CREATE A DTA DIP TO READ ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF ECR A 5331-02503 ON OR BEFORE 09MAY2020. PLANNI
- [SDR CALA2019111601969](https://openairdocs.org/sdr/CALA2019111601969.md): Skin · dented · Nov 11, 2019 · N834UA · Airbus A319131 · Electrical/Electronic Compartment Doors
  > FWD E&E DOOR HAS DENT ON OUTER SKIN THAT EXTENDS TO STIFFENER SU PPORT TASK PER HAECO LCQ NR 9290655 GENERATED BY V080285 REMOVED AND REPLACED E&E DOOR SKIN/FABRICATED N/R 29186 IAW A319 SRM 51-42-11-801, TREATED, PRIMED AND TOP COAT SKIN DOOR E&E IA W A319 SR
- [SDR CALA2019110981930](https://openairdocs.org/sdr/CALA2019110981930.md): Fitting · loose · Nov 6, 2019 · N834UA · Airbus A319131 · Fuselage Main, Attach Fittings
  > L/H KEEL BEAM AFT ACTUATOR FITTING NEEDS TO BE REPLACED DUE TO O VERSIZED HOLES PER HAECO LCQ NON ROUTINE 9290787 GENERATED BY V9 01091 REMOVED, REPLACED AND INSTALLED L/H KEEL BEAM AFT ACTUATOR FITTI NG IAW A319 SRM 51-42-11-801, A319 SRM 51-44-11-801, AND SB
- [SDR CALA2019110501915](https://openairdocs.org/sdr/CALA2019110501915.md): Hinge Fitting · damaged · Nov 1, 2019 · N834UA · Airbus A319131 · Fuselage, Door Hinge
  > L/H KEEL BEAM LOWER FWD HINGE FITTING NEEDS TO BE REPLACED DUE O VERSIZED HOLES PER HAECO LCQ NON ROUTINE 9290786 GENERATED REMOVED,REPLACED AND INSTALLED LH KEEL BEAM LOWER FWD HINGE FITT ING IAW SRM 51-44-11-801,SRM 51-72-12-911-002 BY MECH IN SP BY AT HAECO
- [SDR CALA2019110501914](https://openairdocs.org/sdr/CALA2019110501914.md): Shear Plate · corroded · Nov 1, 2019 · N834UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CABIN RH SHEAR PLATE AT FR68+6" CORRODED A3NB-05-3-6029 PER HAECO LCQ NON ROUTINE 9290847 GENERATED REMOVED & REPLACED RH AFT CABIN SHEAR PLATE AT FR68 IAW A319 SRM 51-72-11-911-001 CATEGORY A REPAIR AT HAECO LCQ ON HANGAR NR 92 90847 PERFORMED BY MECH RII
- [SDR CALA2019110501913](https://openairdocs.org/sdr/CALA2019110501913.md): Stop Fitting · cracked · Nov 1, 2019 · N834UA · Airbus A319131 · Fuselage Main, Structure
  > AT FR16 L1 DOOR CUTOUT STOP FTG #7 HOLES 1 THRU 4 HAVE REJECTABL E CRACK/DAMAGE INDICATIONS AD 2018-25-02 RELATED TASK PER HAECO LCQ NON ROUTINE 9290834 GENERATED REMOVED AND REPLACED L1 FR16 NO.7 DOOR STOP INTERCOSTAL FITTING IAW SRM 51-42-11-801 AND 51-77-11
- [SDR CALA2019110501912](https://openairdocs.org/sdr/CALA2019110501912.md): Stop Fitting · cracked · Nov 1, 2019 · N834UA · Airbus A319131 · Fuselage Main, Structure
  > AT FR16 R1 DOOR CUTOUT STOP FTG #7 HOLES 1 THRU 4 HAVE REJECTABL LE CRACK/DAMAGE INDICATIONS AD2018-25-02 PER HAECO LCQ NON ROUTI NE 9290833 GENERATED REMOVED & REPLACED R1 FR16 NO. 7 DOOR STOP INTERCOSTAL FITTING I AW A319 SRM 51-42-11-801 CATEGORY A REPAIR A
- [SDR CALA2019110101864](https://openairdocs.org/sdr/CALA2019110101864.md): Door Sill · corroded · Oct 29, 2019 · N834UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT PIT DOOR SILL HAS MANY CORROSION SPOTS PER HAECO LCQ NON ROU TINE 9290736 GENERATED REMOVED AND REPLACED AFT CARGO DOOR SILL IAW A319 SRM 51-72-11-9 11-001
- [SDR CALA2019110101863](https://openairdocs.org/sdr/CALA2019110101863.md): Door Sill · corroded · Oct 28, 2019 · N834UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA R2 DOOR SILL CORRODED AT FR66 AND FR68 A3NB-0 5-3-6056 PER HAECO LCQ NON ROUTINE CARD 9290404 REMOVED AND REPLACED 1EA CORRODED R2 DOOR SILL IN THE AFT CABIN WET AREA IAW AIRBUS A319 SRM 51-72-11-911-001
- [SDR CALA2019102311787](https://openairdocs.org/sdr/CALA2019102311787.md): Web · corroded · Oct 18, 2019 · N834UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT PIT WEB BOX MANY CORROSION SPOTS PER HAECO LCQ NON ROUTINE 9 290735. REMOVED AND REPLACED AFT CARGO WEB BOX IAW A319 SRM 51-72-11-911 -001.
- [SDR CALA2019102311781](https://openairdocs.org/sdr/CALA2019102311781.md): Fitting · corroded · Oct 17, 2019 · N834UA · Airbus A319131 · Service Doors
  > EVIDENCE OF CORROSION AT R-2 DOOR LWR CORNER FITTING PER HAECO L CQ NR LP 9290776 REMOVED AND REPLACED 2EA CORRODED R2 DOOR FWD AND AFT CORNER FIT TINGS IAW AIRBUS A319 SRM 51-72-11-911-001
- [SDR CALA2019101801767](https://openairdocs.org/sdr/CALA2019101801767.md): Shear Plate · corroded · Oct 16, 2019 · N834UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA LH SHEAR PLATE CORRODED FR69-70 MULTIPLE AREA S A3NB-05-3-6056 PER LCQ NON ROUTINE 9290389 GENERATED BY V061629 REMOVED AND REPLACED AFT CABIN WET AREA L/H SHEAR PLATE LOCATED AT FR69-70 IAW A319 SRM 51-72-11-911-001.
- [SDR CALA2019101801766](https://openairdocs.org/sdr/CALA2019101801766.md): Shear Plate · corroded · Oct 16, 2019 · N834UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA RH SHEAR PLATE CORRODED FR69-70 MULTIPLE AREA S A3NB-05-3-6056 PER HAECO LCQ NON ROUTINE 9290402 GENERATED BY V061629 REMOVED AND REPLACED RH SHEAR PLATE FR69-70 IAW A319 SRM 51-42-1 1-801 AND 51-72-11-801.
- [SDR CALA2019101401746](https://openairdocs.org/sdr/CALA2019101401746.md): Door Sill · corroded · Oct 10, 2019 · N834UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > EVIDENCE OF CORROSION L-2 DOOR FASTENER HOLES FR68 UNDER GIRT PL ATE A3NB-53-3-6299 PER HAECO LCQ NON ROUTINE 9290778. REMOVED AND REPLACED 1EA CORRODED L2 DOOR SILL FROM THE L2 DOOR CUT OUT IN THE AFT CABIN IAW AIRBUS A319 SRM 51-72-11-911-001 CA T A REPAIR.
- [SDR CALA2017102703826](https://openairdocs.org/sdr/CALA2017102703826.md): Light · malfunctioned · Oct 27, 2017 · N834UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHT OPS CHECK FAILED, MESSAGE EPSU BATTERY FWD L CAME UP. RESET THE SYSTEM IAW AMM 23-73-00 OPS GOOD
- [SDR CALA2016123001199](https://openairdocs.org/sdr/CALA2016123001199.md): Connector · loose · Dec 30, 2016 · N834UA · Airbus A319131 · Light System Wiring
  > EPSU INT LOAD FWD LEFT FAULT WHEN PERFORMING EMERGENCY LIGHTS TEST RESEATED BATTERY PACK AND RESEATED CONNECTOR ON POWER SUPPLY,RET ESATED SYSTEM AND CHECKS OKAY.

Next page: https://openairdocs.org/aircraft/N834UA/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 = 'N834UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N834UA/reports

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