N875UA

Service difficulty reports · 18

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 = 'N875UA' 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 CALA2026040615073Battery Pack · inoperativeOPERATIONAL 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 CHKApr 3, 2026 · N875UA · Airbus A319132 · Emergency LightingSDR CALA2025121712192Skin · crackedNUMBER 2 PYLON INBD CANTILEVER SKIN HAS VERTICAL CRACK. REPAIRED NR 2 PYLON INBD CANTILEVER SKIN IAW SRM 54-52-12.Dec 16, 2025 · N875UA · Airbus A319132 · Nacelle/Pylon, Plate/SkinSDR CALA2025100909839Wire · brokenSEATS 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.Oct 8, 2025 · N875UA · Airbus A319132 · Light System WiringSDR CALA2025100709720Slide · out of adjustDOOR 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 OKOct 6, 2025 · N875UA · Airbus A319132 · Escape SlideSDR CALA2025081207636Battery · faultedEXIT 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 TAug 10, 2025 · N875UA · Airbus A319132 · Emergency LightingSDR CALA2025042804301Unknown · odorSTRONG 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 FAApr 28, 2025 · N875UA · Airbus A319132 · Air Distribution SystemSDR CALA2025031102699Battery · faultedOPERATIONAL 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.Mar 10, 2025 · N875UA · Airbus A319132 · Emergency LightingSDR CALA2024062400065Eec · unknownENG 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 REPLACEJun 20, 2024 · N875UA · Airbus A319132 · Fuel Controlling SystemSDR CALA2024010400028Window Frame · crackedRH 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.Dec 30, 2023 · N875UA · Airbus A319132 · Fuselage Main, StructureSDR CALA2024010200017Fitting · crackedFLIGHT 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 FLIGHTDec 20, 2023 · N875UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2022050901190None · noneREJECTED 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 SYSTMay 9, 2022 · N875UA · Boeing 737 · Rate of Climb IndicatorSDR CALA2022040800935None · missingTHIS 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.Apr 5, 2022 · N875UA · Airbus A300* · Aircraft Fuel SystemSDR CALA2022021400370Battery · inoperativeFWD 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#0021991Feb 12, 2022 · N875UA · Airbus A319132 · Emergency LightingSDR CALA2020022400477Beam · corrodedFWD 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 OFeb 19, 2020 · N875UA · Airbus A319132 · Cargo/Baggage DoorsSDR CALA2020022400476Door Sill · corrodedAFT 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.Feb 19, 2020 · N875UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2020022400474Door Sill · corrodedAFT 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.Feb 19, 2020 · N875UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2020022400475Door Sill · corrodedAFT 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.Feb 19, 2020 · N875UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2020022400463Skin · dentedREAR 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 CFeb 17, 2020 · N875UA · Airbus A319132 · Fuselage Main, Plate/Skin
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