# Service difficulty reports: N875UA A list on [N875UA](https://openairdocs.org/aircraft/N875UA.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR CALA2026040615073](https://openairdocs.org/sdr/CALA2026040615073.md): Battery Pack · inoperative · Apr 3, 2026 · N875UA · Airbus A319132 · Emergency Lighting > OPERATIONAL CHECK OF THE EMERGENCY POWER SUPPLY UNITS BY BITE-CHECK (PRE EA2500-03960 AND EA2500-08031, REFERENCE EC2500-04561 FOR A/C 871-884, 888-899, 901-950) JOB SET-UP - R BATTERY INOP REMOVED AND REPLACED R FWD EPSU BATTERY REF A319 AMM 33-51-38 OPS CHK - [SDR CALA2025121712192](https://openairdocs.org/sdr/CALA2025121712192.md): Skin · cracked · Dec 16, 2025 · N875UA · Airbus A319132 · Nacelle/Pylon, Plate/Skin > NUMBER 2 PYLON INBD CANTILEVER SKIN HAS VERTICAL CRACK. REPAIRED NR 2 PYLON INBD CANTILEVER SKIN IAW SRM 54-52-12. - [SDR CALA2025100909839](https://openairdocs.org/sdr/CALA2025100909839.md): Wire · broken · Oct 8, 2025 · N875UA · Airbus A319132 · Light System Wiring > SEATS 2B AND 3B EMERGENCY LIGHTS ARE INOPERATIVE. SPLICED BROKEN WIRE BETWEEN SEAT 1A AND 2A. EMERG LIGHT TEST GOOD. IAW AMM 33-51-00-710-001-C1. - [SDR CALA2025100709720](https://openairdocs.org/sdr/CALA2025100709720.md): Slide · out of adjust · Oct 6, 2025 · N875UA · Airbus A319132 · Escape Slide > DOOR 1L, WHEN ARMED GIRT BAR WILL NOT ENGAGE CORRECTLY. REMOVED SLIDE 1L AND REINSTALLED ORIGINAL SLIDE PER AMM 25-62-44-400-007-A. OPS CHECK GOOD. PERFORMED RII INSPECTION OF L1 SLIDE INSTALL PER GMM 09-25-05 RII INSPECTION OK - [SDR CALA2025081207636](https://openairdocs.org/sdr/CALA2025081207636.md): Battery · faulted · Aug 10, 2025 · N875UA · Airbus A319132 · Emergency Lighting > EXIT PATH LIGHTS CAME ON IN FLIGHT. NO FAULTS ON POST FLIGHT OR IN CIDS LAST LEG REPORT. ON EMERGENCY LIGHT SYSTEM BITE TEST FOUND EPSU BATTERY FWD L FAULT. REF TSM 33-51-00-810-802-A, R/R BATTERY AT 10WL EPSU REF AMM 33-51-38, FAULT CLEARED. EMERGENCY LIGHT T - [SDR CALA2025042804301](https://openairdocs.org/sdr/CALA2025042804301.md): Unknown · odor · Apr 28, 2025 · N875UA · Airbus A319132 · Air Distribution System > STRONG ODOR OF BURNING ELECTRICAL IN AFT RIGHT LAV. FA SAID WATER HTR LINE FELT HOT TO TOUCH. ACCOMPLISHED OROR CHECK PER AMM 05-51-10-200-801-A FOUND WATER HEATER IN LAV D HOT TO TOUCH AND SMELL LIKE BURNING. INSPECTED AREA AROUND LAVS AND GALLEY NO OTHER FA - [SDR CALA2025031102699](https://openairdocs.org/sdr/CALA2025031102699.md): Battery · faulted · Mar 10, 2025 · N875UA · Airbus A319132 · Emergency Lighting > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - AFT L EPSU BATT FAULT DURING EMER LIGHT TEST ON PTP PANEL REPLACED EPSU BATT AND OPS CHK GOOD. REF. AMM 33-51-38/401. - [SDR CALA2024062400065](https://openairdocs.org/sdr/CALA2024062400065.md): Eec · unknown · Jun 20, 2024 · N875UA · Airbus A319132 · Fuel Controlling System > ENG 2 STALL, FADEC, SENSOR FAULT, OVRSPD FAULT REF TSM 71-00-00-810-809-A STALL T/S FOR #2 ENG. ACP UP TO 4 B. (2) 4. ACP HIGH POWER TEST, REF AMM 71-00-00-710-013-C, NO MSG REF TSM 71-00-00-810-809-A ITEM 4B(4), POWER TEST WAS SUCCESSFUL, NO MGS. EEC REPLACE - [SDR CALA2024010400028](https://openairdocs.org/sdr/CALA2024010400028.md): Window Frame · cracked · Dec 30, 2023 · N875UA · Airbus A319132 · Fuselage Main, Structure > RH WINDSHIELD FRAME CENTER POST LOWER NODE AREA I/B HOLE CRACKED. GEN BY V06169 ON HAECO LCQ NR 9294349/20349 ACCOMPLISHED SAFETY CUT, BUSHING, AND FASTENER INSTALL IAW ECRA 5310-08253. - [SDR CALA2024010200017](https://openairdocs.org/sdr/CALA2024010200017.md): Fitting · cracked · Dec 20, 2023 · N875UA · Airbus A319132 · Fuselage Miscellaneous Structure > FLIGHT DECK WINDSHIELD L/H CONTINUITY FITTING HAS A CRACK INDICA TION. LOWER NODE PER PART 2 OF THE LATEST REVISION OF ECRA5310-08253 CYCLES. PERFORM REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED ON OR BEFORE THE AIRCRAFT REACHES 38,201 TOTAL AIRCRAFT FLIGHT - [SDR CALA2022050901190](https://openairdocs.org/sdr/CALA2022050901190.md): None · none · May 9, 2022 · N875UA · Boeing 737 · Rate of Climb Indicator > REJECTED TAKEOFFNO AIRSPEED INDICTNFO INSTRUMENTS FOUND INSECT DEBRIS MUD DAUBER NEST IN FOS PITOT PROBE, CLEARED SYSTEM, NITROGEN FLUSH. IAW AMM34-10-00. PERFORMED SYSTEM TEST IAW AMM34-13-00 INCLUDING LEAK,OP CHECK AND AIRSPEED TEST. NO DEFECTS NOTED SYST - [SDR CALA2022040800935](https://openairdocs.org/sdr/CALA2022040800935.md): None · missing · Apr 5, 2022 · N875UA · Airbus A300* · Aircraft Fuel System > THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER CALA2022040800935 SUBMITTED ON 04/08/22.UEL CAP MISSING FUEL CAP WAS NOT MISSING, LANYARD ASSY BROKEN, REPLACED LANYARD ASSY. - [SDR CALA2022021400370](https://openairdocs.org/sdr/CALA2022021400370.md): Battery · inoperative · Feb 12, 2022 · N875UA · Airbus A319132 · Emergency Lighting > FWD LEFT ESPU BATTERY FAULT (10WLA) REPLACE BATTERY REPLACED FWD EPSU BATTERY L1 DOOR IAW AMM 33-51- 38 AND OPS TEST GOOD IAW AMM 33-51-00. ACCOMPLISHED BY EMP#V9339 55 AT BFM ST AEROSPACE MOBILE. NR#0021991 - [SDR CALA2020022400477](https://openairdocs.org/sdr/CALA2020022400477.md): Beam · corroded · Feb 19, 2020 · N875UA · Airbus A319132 · Cargo/Baggage Doors > FWD CGO DOOR FR26-FR26A BEAM 4-5 INTERNAL EXISTING REPAIR DOUBLER FND CORROSION REF NON-ROUTINE NO.9400513 - REF TASK CAED LOG:3491882, NRC NO.GGL0617. FWD CARGO DOOR FR26-FR26 BEAM 4-5 INTERNAL EXISTING REPAIR DOUBL ER REPAIRED PER ECRA 5231-01130. PLACING O - [SDR CALA2020022400476](https://openairdocs.org/sdr/CALA2020022400476.md): Door Sill · corroded · Feb 19, 2020 · N875UA · Airbus A319132 · Fuselage Miscellaneous Structure > AFT CGO COMPT DOORSILLL PLATE UPPER SURFACE FOUND CORROSION REF NON-ROUTINE NO.9499535. AFT CARGO DOOR SILL PLATE REPLACED PER SRM 51-42-11 & DWG D53477 154. REF HAECO N/R GGL3777 FOR DETAILS OF WORK ACCOMPLISHED. - [SDR CALA2020022400474](https://openairdocs.org/sdr/CALA2020022400474.md): Door Sill · corroded · Feb 19, 2020 · N875UA · Airbus A319132 · Fuselage Miscellaneous Structure > AFT WET AREA R2 DOOR SILL FOUND CORROSION(FR68) REF NON-ROUTINE NO.9499871. AFT WET AREA R2 DOOR SILL REPLACED PER SRM 51-42-11 & DWG D53480 505. REF HAECO N/R GGL5277 FOR DETAILS OF WORK ACCOMPLISHED. - [SDR CALA2020022400475](https://openairdocs.org/sdr/CALA2020022400475.md): Door Sill · corroded · Feb 19, 2020 · N875UA · Airbus A319132 · Fuselage Miscellaneous Structure > AFT WET AREA L2 DOOR SILL FR68 FOUND CORROSION REF NON-ROUTINE NO.9499861. SPEC NO.A3NB-53-3-6187. L2 DOOR SILL REPLACED PER SRM 51-42-11 AND DWG D53480076. REF HAECO N/R GGL5186 FOR DETAILS OF WORK ACCOMPLISHED. - [SDR CALA2020022400463](https://openairdocs.org/sdr/CALA2020022400463.md): Skin · dented · Feb 17, 2020 · N875UA · Airbus A319132 · Fuselage Main, Plate/Skin > REAR FUSELAGE UPPER EXTERNAL SURFACE FOUND 1EA DENT MARK AT FR82 -83 STRINGER 2R-3R REF NON-ROUTINE NO.9400060 - ORIGINATED BY EMP V916780,SPEC NO.A3NB-05-3-6062. REAR FUSE UPPER EXT SURFACE AT FR82-FR83 STR 2R-3R REPAIRED PER SRM 53-51-11-300-010. THIS IS A C ## 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 = 'N875UA' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N875UA/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.