# Service difficulty reports: N882UA A list on [N882UA](https://openairdocs.org/aircraft/N882UA.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR CALA2026081118474](https://openairdocs.org/sdr/CALA2026081118474.md): Light · broken · Aug 10, 2026 · N882UA · Airbus A319132 · Emergency Lighting > SEAT 3 EMERGENCY PATH LIGHTS INOPERATIVE. FOUND SEAT 3A WITH BOTH EMERGENCY LIGHTS BROKEN. REPLACED SEAT 3B FWD & AFT EMERGENCY LIGHT ASSEMBLIES IAW AMM 33-51-18. OPS NORMAL, OK TO CONTINUE. - [SDR CALA2026042915817](https://openairdocs.org/sdr/CALA2026042915817.md): Light · no discrepancy · Apr 28, 2026 · N882UA · Airbus A319132 · Emergency Lighting > EXTERNAL EMERGENCY LIGHTS INOP ON WING TO BODY PANELS 191DT AND 192DT ACCORDING TO AMM TASK 33-51-00-720-001-B, (CHECK OF THE DOOR POWER SWITCH POWER SUPPLY FROM THE EMERGENCY LIGHT SYSTEM AND OF THE DOOR SWITCH OPERATION FOR THE EXTERIOR LIGHTS), OPEATIONAL T - [SDR CALA2026042215609](https://openairdocs.org/sdr/CALA2026042215609.md): Wire · broken · Apr 14, 2026 · N882UA · Airbus A319132 · Light System Wiring > IASLE EMERGENCY LIGHTS AT ROW 3ABC INOP FOUND BROKEN WIRE UNDER SEAT TRACK COVER FWD OF ROW 2AB IN WIRE HARNESS 9002WL1 CREATED WIRE SPLICE UNDER SEAT TRACK COVER FWD OF ROW 2AB PER ESPM 20-43-11-01. WIRE IS LOCATED IN WIRE HARNESS 9002WL1 REF AWM 33-51-06 PAG - [SDR CALA2025031002648](https://openairdocs.org/sdr/CALA2025031002648.md): Smoke Detector · no discrepancy · Mar 8, 2025 · N882UA · Airbus A319132 · Smoke Detection > LAVATORY SMOKE WARNING. CLRD ON ITS OWN. SUSPECT PAX WAS VAPING IN LAV E BASED ON SMELL. INSPECTED LAV FOR TAMPERING. NO SIGNS. PERFORMED OPS TEST OF DETECTION SYSTEM. OPS CHECK GOOD AT THIS TIME. REF AMM 26-17-00-710-001-A - [SDR CALA2024100902609](https://openairdocs.org/sdr/CALA2024100902609.md): Skin · damaged · Oct 6, 2024 · N882UA · Airbus A319132 · Elevator, Plate/Skin > L/H ELEVATOR UPPER I/B SKIN HAS A PUNCTURE, 26IN FROME I/B END, 26IN FROME TRAILING EDGE, 1IN IN DIAMETER. "REPAIR PRIOR TO NEXT FLIGHT". HAECO LCQ NR 9290356 / 20356 REPAIRED L/H ELEVATOR UPPER SKIN 26 IN FROM I/B END 26 IN FROM T /E 1 IN DIA ZONE A IAW A319 - [SDR CALA2024100702572](https://openairdocs.org/sdr/CALA2024100702572.md): Skin · no discrepancy · Oct 4, 2024 · N882UA · Airbus A319132 · Fuselage Main, Plate/Skin > REMOVE UPPER FUSELAGE SKIN FR1-3 TO F.O.M. (CONTINUITY FITTING R EPLACEMENT). REMOVED AND REINSTALLED FUSELAGE UPPER SKIN TO FOM CONTINUITY FI TTING REPLACEMENT AT FR1-FR3 IAW A319 SRM 51-72-11-911-001. - [SDR CALA2024100702571](https://openairdocs.org/sdr/CALA2024100702571.md): Fitting · cracked · Oct 4, 2024 · N882UA · Airbus A319132 · Fuselage Main, Structure > FLIGHT DECK, WINDSHIELD CONTINUITY FTG HAS CRACK INDICATION APPR OX.400 INCH OUT FROM CTR POST ON HORIZONTAL LEG ON LH AND RH SI DE. "CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLI GHT". RECEIVED FINAL RFTS #4 OPS 60006 WITH INSTRUCTION TO ACCOM - [SDR CALA2024041501061](https://openairdocs.org/sdr/CALA2024041501061.md): Plate · missing · Apr 12, 2024 · N882UA · Airbus A319132 · Fuselage Structure (General) > PDA RIGHT SIDE PROTECTIVE PLATE (NOSE WHEEL SPIN BRAKE) WAS FOUND MISSING FROM ACFT ON ARRIVAL WHILE TROUBLESHOOTING LP 7631557 SDR COMPLETED. INSTALLED PROTECTIVE PLATE. REF AMM 32-42-52-960-001-A. - [SDR CALA2023081102479](https://openairdocs.org/sdr/CALA2023081102479.md): Fuel Cap · missing · Aug 4, 2023 · N882UA · Airbus A319132 · Aircraft Fuel System > PDA 2 FUEL CAP MISSING UPON ARRIVAL COUPLING SEAL INTACT, NO FUEL LEAK. OK TO CDL REPLACED FUEL CAP W/SERVICEABLE CAP. REMOVED PLACARD. OK FOR SERVICE. AMM REF 28-25-41. - [SDR CALA2023052201587](https://openairdocs.org/sdr/CALA2023052201587.md): Battery · inoperative · May 20, 2023 · N882UA · Airbus A319132 · Emergency Lighting > DURING OPC OF CABIN EMERGENCY LIGHTNING BATTERY CAPACITY NOTED THAT EPSU BATTERY 13WL FAILED. REPLACEMENT IS REQUIRED. LTPR NR# 5001232433-0010. BATTERY REPLACED PER AMM 33-51-38 - [SDR CALA2023052201586](https://openairdocs.org/sdr/CALA2023052201586.md): Battery · inoperative · May 20, 2023 · N882UA · Airbus A319132 · Emergency Lighting > DURING OPC OF CABIN EMERGENCY LIGHTNING BATTERY CAPACITY NOTED THAT EPSU BATTERY 11WL FAILED. REPLACEMENT IS REQUIRED. LTPR NR# 5001232433-0010. - [SDR CALA2023052201585](https://openairdocs.org/sdr/CALA2023052201585.md): Battery · inoperative · May 20, 2023 · N882UA · Airbus A319132 · Emergency Lighting > DURING OPC OF CABIN EMERGENCY LIGHTNING BATTERY CAPACITY NOTED THAT EPSU BATTERY 12WL FAILED. REPLACEMENT IS REQUIRED. LTPR NR# 5001232433-0010. BATTERY REPLACED PER AMM 33-51-38 - [SDR CALA2023052201584](https://openairdocs.org/sdr/CALA2023052201584.md): Battery · inoperative · May 20, 2023 · N882UA · Airbus A319132 · Emergency Lighting > DURING OPC OF CABIN EMERGENCY LIGHTNING BATTERY CAPACITY NOTED THAT EPSU BATTERY 10WL FAILED. REPLACEMENT IS REQUIRED. LTPR NR# 5001232430-0010. - [SDR CALA2023022200519](https://openairdocs.org/sdr/CALA2023022200519.md): Brake · none · Feb 21, 2023 · N882UA · Airbus A319132 · Brake > REJECTED TAKEOFF VIA TOWER REQUEST. AUTOBRAKES ACTUATED, RIGHT BRAKE TEMP REACHED 375 DEGREES TEMP. CREW REPORTS LOW SPEED REJ, APPROXIMATELY 75KNOTS WITH NO BRAKE LOCKING. TEMPS COOLED. - [SDR CALA2022102802986](https://openairdocs.org/sdr/CALA2022102802986.md): Transmitter · warning message · Oct 28, 2022 · N882UA · Airbus A319132 · Hydraulic Quantity Sensor > G RSVR LOW LEVEL ECAMAT FL310 AVAIL ON BOTH CONNECTORS. DUE TO HISTORY, ALSO RECOMMEND REPLACING THE GREEN SYS QUAN. TRANSMITTER. PHOTO -- POST FLIGHT REPORT T/S REF TSM 29-11-00-810-803-A. FOUND GREEN SYSTEM LOW LEVEL INSTALLED NEW CANNON PLUG CONNECTOR 1000G - [SDR CALA2021042600530](https://openairdocs.org/sdr/CALA2021042600530.md): Support Beam · corroded · Apr 23, 2021 · N882UA · Airbus A319132 · Fuselage Miscellaneous Structure > R2 DOOR SILL PANEL SUPPORT BEAM FOUND CORROSION AT FR68 REFER HAECO NON-ROUTINE LP 9428470 - ORIGINATED BY EMP V906558 SPEC NO AENB-53-3-6187 PERFORM BY EMP V905768 R2 DOOR SILL PANEL SUPPORT BEAM REPLACED AS PER SRM 51-72-11 REV 135,INSTALLED AS PER SRM 51-42 - [SDR CALA2021041900489](https://openairdocs.org/sdr/CALA2021041900489.md): Door Frame · cracked · Apr 16, 2021 · N882UA · Airbus A319132 · Fuselage Main, Structure > FR68 LH AFT DOOR NO.1 STOP FITTING FOUND 1EA HOLE CRACKED AT FRA ME REFER HAECO NON-ROUTINE LP 9435136 - ORIGINATED BY EMP V90649 8 EA5340-01724 REV C OP002 STEP 3.1 CABIN AFT DOOR FR68 L/H #1 STOP FTG AT FRAME WEB REPAIRED AS PER SRM 53-41-12-300-010 REV 135. - [SDR CALA2021031900339](https://openairdocs.org/sdr/CALA2021031900339.md): Frame · corroded · Mar 18, 2021 · N882UA · Airbus A319132 · Fuselage Main, Frame > AFT CGO FR59 STR38L-39L FRAME UPPER SURFACE FND CORROSION.REFER NON-ROUTINE LP 9430052,ORIGINATED BY EMP V902716.SPEC NO.A3NB-53 -4-6179. PERFORMED BY EMP V902716,AFTER CARGO FR59 STR38L-STR39L FRAME REPLACED AS PER SRM 51-72-11 REV.135,INSTALLED AS PER SRM 51 ## 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 = 'N882UA' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N882UA/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.