# Service difficulty reports: N876UA A list on [N876UA](https://openairdocs.org/aircraft/N876UA.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR CALA2025102310445](https://openairdocs.org/sdr/CALA2025102310445.md): Power Supply · no test · Oct 22, 2025 · N876UA · Airbus A319132 · Emergency Lighting > EMERGENCY BATTERY W/C 18-3351-1-0003 FAILED. REQUIRES 13WL POWER SUPPLY AND BATTERY. REMOVED AND REPLACED 13WL EPSU AND BATTERY PER AMM 33-51-38, ALSO REPLACED BATTERY 11WL PER 33-51-38, OPS TEST OF ALL EMERGENCY LIGHTS TEST OK FROM THE FAP. VISUAL OF ALL EME - [SDR CALA2025101309938](https://openairdocs.org/sdr/CALA2025101309938.md): Cover · detached · Oct 10, 2025 · N876UA · Airbus A319132 · Escape Slide > DOOR 2R SLIDE COVER DETACHED. SECURED DECORATIVE COVER IAW AMM 25-62-00-400-801-A. - [SDR CALA2025031102695](https://openairdocs.org/sdr/CALA2025031102695.md): Wire · broken · Mar 8, 2025 · N876UA · Airbus A319132 · Light System Wiring > FOUND EMERGENCY EXIT PATH LIGHTING AT SEATS 2B & 3B INOP DURING OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} FOUND BROKEN WIRE AT SEAT ROW 2 UNDER SEAT TRACK COVER. SPLICE REPAIRED BROKEN WIRE. OPS CHK GOOD. REF. ESPM 20-53-20 AND AMM 33-51-00. - [SDR CALA2023112703470](https://openairdocs.org/sdr/CALA2023112703470.md): Unknown · unknown · Nov 26, 2023 · N876UA · Airbus A319132 · Landing Gear System > ECAMS BRAKES AUTO BRK FAULT BRAKE RELEASED UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PERFORM RESET AND BITE TEST OF BCSU 1 AND 2 REF AMM 32-46-00 UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOM - [SDR CALA2023081802568](https://openairdocs.org/sdr/CALA2023081802568.md): Outflow Valve · unknown · Aug 16, 2023 · N876UA · Airbus A319132 · Pressure Regulator/Outflow Valve > SYS 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. - CAB PR TIME THIS ACFT HAD TO DO AN AIR RETURN FOR CABIN PRESSURIZATION PROBLEM. SPOKE WITH CREW. THEY STATED ISSUE HAPPENED AT APROX 8500 FT. RAN BOTH CPC 1 AND CPC 2 TEST ON MCDU WITH NO FAULTS FOUND. RAN COULD NO - [SDR CALA2023081602540](https://openairdocs.org/sdr/CALA2023081602540.md): Controller · faulty · Aug 14, 2023 · N876UA · Airbus A319132 · Cabin Pressure Controller > CABIN DEPRESSURIZED THR 290 ABOUT 10 MINUTES AFT ER SYSTEM 1 FAULTED. REPLACED BOTH CPC1 AND CPC2 REF MM21-31-34-400-001-A. TROUBLESHOT USING THE FOLLOWING TSM''S, TSM 21-31-00-810-816-A, TSM 21-31-00-810-806-A, TSM 21-31-00-810-803-A, TSM 31-51-00-810-931-A A - [SDR CALA2023071902282](https://openairdocs.org/sdr/CALA2023071902282.md): Line · leaking · Jul 17, 2023 · N876UA · Airbus A319132 · Hydraulic System, Main > FLIGHT CREW REPORTED LOSE OF GREEN HYD SYSTEM FLUID, THEN STATED HYD LEVEL APPEARS TO BE EMPTY. LANDING GEAR MANUALLY EXTENDED BY CREW ON APPROCH. HYD RES GREEN WAS NOT EMPTY ON ARRIVAL. FOUND LEAK AT LH GEAR DOOR MAIN ACTUATOR, B PORT FLEX LINE, M&E 03-2900-3 - [SDR CALA2022120703331](https://openairdocs.org/sdr/CALA2022120703331.md): Actuator · failed · Dec 7, 2022 · N876UA · Airbus A319132 · Turbine Engine Compressor Section > COMPRESSOR VANE DISPLAYED ON UPPER ECAM SCREEN. ENGINE PARAMETERS NORMAL. - ENG 1 ENG 1 COMPRESSOR VANE PARAMETERS NORMAL ACCOMPLISHED POWER ASSURANCE RUN.ACOMPLISHED AMM TASK 75-32-41-00-010-A UP TO STEP E. TEST FAILED MESSAGE CAME BACK ENG1 COMPRESSOR VANE - [SDR CALA2022110903095](https://openairdocs.org/sdr/CALA2022110903095.md): Warning Message · false activation · Nov 9, 2022 · N876UA · Airbus A319132 · Door Warning System > CREW REPORTED A LOW SPEED REJ TAKEOFF LESS THAN 20KTS DUE TO DOOR AFT CARGO ECAM MSG APPEARED JUST AT POWER SETTING. FAULT CLEARED AFTER ACFT RETURNED TO GATE CREW REPORTED LESS THAN 20KTS REJ TAKEOFF. FAULT WAS ALREADY CLEARED AT ARRIVAL TO GATE. RAMP CYCLED - [SDR CALA2022071301724](https://openairdocs.org/sdr/CALA2022071301724.md): Fuel Cap · missing · Jul 13, 2022 · N876UA · Airbus A319132 · Aircraft Fuel System > PDA 2 RAMP REPORTED FUEL CAP MISSING INSTALLED NEW FUEL CAP AS REQUIRED. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1821356 SN OFF 2066 CAP, COUPLING R OFF 31-2825-9-0001 2066 ON 31-2825-9-0001 0940 - [SDR CALA2019090201469](https://openairdocs.org/sdr/CALA2019090201469.md): Stringer · corroded · Aug 29, 2019 · N876UA · Airbus A319132 · Fuselage Main, Longeron/Stringer > BULK CGO REAR FR65-66 STR 31R STRINGER FND CORROSION. REF NON-ROUTINE NR 9482737. SPEC NR A3NB-05-3- 6022. BULK CGO FR65-66 STR 31R STRINGER REPAIRED AS PER ECRA 5341-01183 REV -. - [SDR CALA2019083001449](https://openairdocs.org/sdr/CALA2019083001449.md): Battery · discharged · Aug 26, 2019 · N876UA · Airbus A319132 · Emergency Lighting > 13WL BATTERY CAPACITY LOW P/N 3214-31, REPLACED 13WL EPSU BATTERY PACK C/OUT OPERATIONAL TEST FOUND THE RESULT NORMAL IAW AMM 33-51-38-000/4 00-002A REV 102 & AMM 33-51-00-710-001C1 REV102. - [SDR CALA2019083001448](https://openairdocs.org/sdr/CALA2019083001448.md): Battery · discharged · Aug 26, 2019 · N876UA · Airbus A319132 · Emergency Lighting > 10WL BATTERY CAPACITY LOW P/N:3214-31, PERFORMED BY EMP V903217,REPLACED 10WL EPSU BATTERY PACK & C/OUT OPERATIONAL TEST FND THE RESULT NORMAL AS PER AMM 33-51-38-000/ 400-002A & AMM 33-51-00-710-001C1 REV102. - [SDR CALA2019082301414](https://openairdocs.org/sdr/CALA2019082301414.md): Stringer · failed · Aug 21, 2019 · N876UA · Airbus A319132 · Fuselage Main, Longeron/Stringer > AFT CGO FR59 S32L STRINGER FOUND CORROSION. STRINGER REPAIRED AS PER SRM 53-00-13-3 00-001 REV 128. - [SDR CALA2019082301406](https://openairdocs.org/sdr/CALA2019082301406.md): Fitting · corroded · Aug 20, 2019 · N876UA · Airbus A319132 · Emergency Equipment > L2 DOOR LOWER DOOR SILL AT CORNER AROUND GIRT BAR FITTING FOUND CORROSION. GIRT BAR FITTING REMOVED AND REPLACED AS PER SRM51-42-11 REV.128(UAL) AND SRM51-44-11 REV.128(UAL) AND PER DWGD53480505 ISSUE:CE. - [SDR CALA2019081601370](https://openairdocs.org/sdr/CALA2019081601370.md): Floor Support · corroded · Aug 15, 2019 · N876UA · Airbus A319132 · Fuselage Miscellaneous Structure > FWD CGO FR27 STR39-41 R/H FLR SUPPORT WEB FOUND CORRODED. THE FLOOR SUPPORT WEB REPLACED AS PER SRM 51-72-11 REV.128 AND INSTALLED AS PER SRM 51-42-11 REV. 128,DWG D53231685 ISSUE H. - [SDR CALA2019081601369](https://openairdocs.org/sdr/CALA2019081601369.md): Floor Support · corroded · Aug 14, 2019 · N876UA · Airbus A319132 · Fuselage Miscellaneous Structure > FWD CGO FR30 Y=-3 FLR SUPPORT LOWER FND CORROSION. REF NON-ROUTI NE NO.9482305 - ORIGINATED BY EMP V902716 SPEC NO.A3NB-05-3-6013. PERFORMED BY EMP V905768 FWD CGO FR30 Y=3 FLR SUPPORT REMOVED AN D REPLACED AS PER SRM 51-42-11 REV 128 AND SRM 51-44-11 REV 128 ## 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 = 'N876UA' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N876UA/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.