N892UA

Service difficulty reports · 35

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 = 'N892UA' 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 CALA2025102210413Fuel Cap · missingAC ARRIVED IN ORD WITH FUEL CAP ASSY MISSING .Oct 21, 2025 · N892UA · Airbus A319132 · Fuel StorageSDR CALA2025101309936Door · no discrepancyREMOVED RIGHT EMERGENCY EXIT HATCH SEAT 21F REF AMM 52-21-11 REPLACED EMERGENCY EXIT HATCH SEAL AT DOOR 21F REF AMM 52-21-18-960-003-A, NO DEFECTS FOUND. REINSTALLED HATCH AT 21F REF AMM 52-21-11-400-001-A, NO DEFECTS NOTED. PERFORMED CABIN PRESSURIZATION REF Oct 12, 2025 · N892UA · Airbus A319132 · Emergency ExitsSDR CALA2025092209081Battery Pack · no testPROCEDURE - EPSU FWD BATTERY FAULT FOUND ON EMERGENCY LIGHTING CHECK. R & R FWD EPSU BATTERY ABOVE FWD ENTRY DOOR. REF: AMM TASK 33-51-38-000-002-A & TASK 33-51-38-400-002-A. OP CHECK GOOD, NO MORE FAULTS SHOWING ON TEST.Sep 20, 2025 · N892UA · Airbus A319132 · Emergency LightingSDR CALA2025090908662Oxygen Panel · unsecure2R OXYGEN MASK AT FA STATION AFT FALLING DOWN, MASK STILL IN COMARTMENT, SECURED PANEL AT 2R O2 AT FA STATION. MASK DID NOT FALL OUT, PANEL WAS NOT SEATED PROPERLY. REF AMM 35-20-00Sep 5, 2025 · N892UA · Airbus A319132 · Passenger Oxygen SystemSDR CALA2025082708186Tape · unsecureFA REPORTS ABNORMALLY LO UD WHISTLE FROM RIGHT OV ERWING EXIT. SECURED LOOSE TAPE ON RIGHT WING.Aug 24, 2025 · N892UA · Airbus A319132 · Wing StructureSDR CALA2025021702338Warning Message · false activationAFT CARGO DOOR OPEN INDICATION ON CLIMB. CRW REPORTED NORMAL INDICATIONS RETURNED AFTER LANDING. ACCOMPLISHED OPERATIONAL CHECK OF AFT CARGO DOOR PER AMM TASK 52-32-00-710-001-A NO DEFECTS NOTED. CHECKED SENSOR 32WV AND CONNECTOR FOR DEFECTS NONE NOTED.Feb 17, 2025 · N892UA · Airbus A319132 · Door Warning SystemSDR CALA2025021100332Scuff Plate · worn#1 PYLON BOTTOM SCUFF PLATE AFT OF AFT ENGINE MOUNT HAS WEAR PER HAECO LCQ N/R 9294185/42185. RMVD AND RPLD SCUFF PLATE AFT OF AFT ENGINE MOUNT ON #1 PYLON IAW A319 SRM 54-51-12-300-003 THIS REPAIR REQ SRI EVERY 4900FC 1200FH FROM EMBODIMENT SUBSEQUENT INSP AFeb 8, 2025 · N892UA · Airbus A319132 · Nacelle/Pylon, Plate/SkinSDR CALA2025020200262Angle · crackedLH SIDE VERTICAL WING TO BODY STRUCTURE BRACKET IS CRACKED PER HAECO LCQ N/R 9294125/42125 GEN BY V918855Jan 31, 2025 · N892UA · Airbus A319132 · Aerodynamic FairingsSDR CALA2025010601780Power Supply · faultedRIGHT EMERGENCY POWER SUPPLY BATTERY 12WL REQUIRES REPLACEMENT. REPLACED POWER SUPPLY AND BATTERY REF AMM 33-51-38. TESTED NORMAL.PARTS USED: 18-3351-3-0001,QTY :1 31-3350-9-9001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1835569 SN OFF 8208 IPC REFEREJan 3, 2025 · N892UA · Airbus A319132 · Emergency LightingSDR CALA2025010300022Power Supply · no testAFT LEFT 13WL EMERGENCY POWER SUPPLY REQUIRES REPLACEMENT. REMOVED AND REPLACED POWER SUPPLY PER REF AMM 33-51-38. OPS CHECK GOOD.Jan 3, 2025 · N892UA · Airbus A319132 · Emergency LightingSDR CALA2025010601797Power Supply · not reportedAFT LEFT 13WL EMERGENCY POWER SUPPLY REQUIRES REPLACEMENT PART INFO UPDATED REMOVED AND REPLACED POWER SUPPLY PER REF AMM 33-51-38 OPS CHECK GOODJan 2, 2025 · N892UA · Airbus A319132 · Emergency LightingSDR CALA2024120201380Hydraulic Line · leakingCREW REPORTED LOST YELLOW HYDRAULIC SYSTEM. YELLOW HYD QTY SHOWING ZERO ON HYD PAGE REF LP 3046594 FOR WORK PERFORMED Y HYD RSVR LO LVL COMPLETE FLUID LOSS OPENING AND COLLARING C/BS FOR YELLOW PUMP AND CARGO DOORS. AB03 AB06 AND T12 BREAKERS OPENED. FOUND HYDDec 2, 2024 · N892UA · Airbus A319132 · Hydraulic System, MainSDR CALA2024073100337Cids · faultedCIDS RESET INFLIGHT FOLLOWED 319 SYS RESET IN FM OPS NOW NORMAL RAN CIDS BITE CHECK THROUGH BOTH FA PANEL AND MCDU REFER AMM 23-73-00-740-005-A ALL TEST OK NO C/B TRIPPED DUE TO HISTORY RAN CIDS FUNC TEST OPS REFER AMM 23-73-00-720-006-A CHECK GOOD NO FAULT NOJul 28, 2024 · N892UA · Airbus A319132 · Communications SystemSDR CALA2024050601328Fuel Cap · missingPDA 2 CAP, COUPLING REFUEL UNDER WING - REPORTED MISSING BY FUEL VENDOR. FUEL CAP IS ON AIRCRAFT FUEL CAP LANYARD IS BROKEN,REPLACED FUEL CAP LANDARD. SEE PHOTOSMay 3, 2024 · N892UA · Airbus A319132 · Fuel StorageSDR CALA2024042601244Pump · faultedHYD G RSVR OVHTIN CLIMB. FOLLOWED ECAM SLIGHTLY DECREASED AND FAULT LIGHT EXTINGUISHED BUT ECAM MESSAGE ALONG WITH OVERHEAT WARNING ON HYDROLIC PAGE ON LOWER ECAM WITH REMAINED. ABOUT 15 MINUTES BEFORE TOUCHDOWN, THEY TURNED LEFT FAULT INDICATIONS ON ENG 1 PUMApr 23, 2024 · N892UA · Airbus A319132 · Hydraulic Pump (Electric/Engine), MainSDR CALA2024042401214Transducer · overheatedG RSVR OVHT DISPLAYED ON UPPER ECAM SCREEN. - HYD RAN ECAM PROC..OVHT WENT OUT AFTR 10 MINS RECOVERD GRN HYD SYS.. OPS NRML CONSISTENTLY. PERFORMED #2 ENG DRY MOTOR, GREEN INDICATION FLUCTUATED BETWEEN 2450-2700 PSI AND YELLOW PRESSURE MAINTAINED AROUND 2900 PApr 21, 2024 · N892UA · Airbus A319132 · Hydraulic System, MainSDR CALA2024040300969Repair · inadequateCONVERT TEMPORARY REPAIR TO PERMANENT REPAIR AT RH SIDE SKIN PAN EL BETWEEN FR2-3 FWD OF RH REF LOG PAGE 7270995 AND ECRA 5330-07 208 PER HAECO LCQ NR 9298002/22002. CONVERSION FROM TEMPORARY TO PERMANENT SKIN REPAIR NOT POSSIBLE D53118296 RH LATERAL SKIN PNL Apr 2, 2024 · N892UA · Airbus A319132 · Fuselage Main, Plate/SkinSDR CALA2024040300968Stiffener · crackedUPON INSTALL OF R/H LATERAL SKIN PANEL FOUND SKIN STIFFENER AT L OWER LAP JOINT FR1-2 TO HAVE CRACK AT AFT END. REMOVED AND INSTALLED NEW R/H LATERAL SKIN PANEL SKIN STIFFENER AT LOWER LAP JOINT FR1-2 AS PER A319 SRM 51-42-11.Apr 2, 2024 · N892UA · Airbus A319132 · Fuselage Main, StructureSDR CALA2024040300963Repair · inadequateCONVERT TEMPORARY REPAIR TO PERMANENT REPAIR AT RH SIDE SKIN PAN EL BETWEEN FR2-3 FWD OF RH CONVERSION FROM TEMPORARY TO PERMANENT SKIN REPAIR NOT POSSIBLE D53118296 RH LATERAL SKIN PNL FROM FR 1 - FR 12 PN D531100752010 3 STEP 6 OF ECRA INSTRUCTS TO CLOSE DIPApr 2, 2024 · N892UA · Airbus A319132 · Fuselage Main, Plate/SkinSDR CALA2023031700770Unknown · corrodedAFT CARGO PIT L/H FR64 BETWEEN STRINGERS 43L-44 HAS CORROSION ON SKIN DOUBLER (A3NB-53-4-6179). GENERATED BY V919150 AT HAECO LC Q PER NR 9298610 (20610). 5341-01376. WORK ACCOMPLISHED BY LCQ EMP V932428. ACCOMPLISH PER PART 2 OF LATEST REVISION OF EC/RA 5341-Mar 15, 2023 · N892UA · Airbus A319132 · Fuselage Main, Plate/SkinSDR CALA2023031300708Stop · crackedFR 68 RH DOOR STOP #1 LOWER IB HOLE HAS CRACK INDICATION IN FRAM E LAYER 6 O''CLOCK DIRECTION 100% SCREEN HEIGHT PER HAECO LCQ N/R 9298588/20588 REAMED FREEZE PLUG TO .2820" PER SRM 53-41-12-300-011. REAMED 5340-01734 STEP 9. PER SRI 53-41-12-205-010 INSPECTIMar 10, 2023 · N892UA · Airbus A319132 · Fuselage Main, StructureSDR CALA2023031000684Stop · crackedFR 68 RH DOOR STOP #1 LOWER IB HOLE HAS CRACK INDICATION IN FRAM E LAYER 6 O''CLOCK DIRECTION 100% SCREEN HEIGHT PER HAECO LCQ N/R 9298588/20588 REAMED FREEZE PLUG TO .2820" PER SRM 53-41-12-300-011. REAMED 5340-01734 STEP 9. PER SRI 53-41-12-205-010 INSPECTIMar 10, 2023 · N892UA · Airbus A319132 · Fuselage Main, StructureSDR CALA2023022700557Nut Plate · corrodedFR68 LH FWD FACE AT NUT PLATE HOLE HAS CORROSION PER HAECO LCQ N R 9298794/20794 GENERATED BY V061680 SPEC: A3NB-53-3-6222. = .030", REM''ING MTL = .068", MAX ALLOWABLE REM''ING MTL = .050", HFEC AND ROTO INSPECTED AREA AND NUT PLATE HOLE IAW 51-10-08 REPAIR FFeb 25, 2023 · N892UA · Airbus A319132 · Fuselage Main, FrameSDR CALA2023022700551Plate · corrodedAFT WET AREA L2 DOOR SILL PLATE AFT CORNER HAS CORROSION FR68-68 PER HAECO LCQ NR 9298668/20668 GENERATED BY V926223 SPEC: A3NB-5 3-3-6222 RMVD AND RPLD AFT WET AREA L2 DOOR SILL IAW UAL SRM 51-72-11 BY MECH V061742 INSP BY V061334Feb 24, 2023 · N892UA · Airbus A319132 · Fuselage Main, Floor BeamSDR CALA2023022700550Door Sill · corrodedFWD CARGO DOOR SILL HAS CORROSION SPOTS ON UPPER SURFACE GENERAT ED AT HAECO LCQ PER NR 9298573 (20573) BY V919150. {A3NB-53-3-61 05} REMOVED AND REPLACED FWD CARGO DOOR SILL IAW A319 SRM 51-42-11-0 01. TREATED, PRIMED, AND TOP COAT AREA IAW A319 SRM 51-23-11-Feb 24, 2023 · N892UA · Airbus A319132 · Fuselage Main, Plate/SkinSDR CALA2023022400527Plate · corrodedAFT WET AREA R-2 DOOR SILL PLATE HAS CORROSION FWD END FR 66-68 PER HAECO LCQ NR 9298673/20673 GENERATED BY V926223 SPEC: A3NB-5 3-3-6222. REPAIRED R-2 DOOR SILL PLATE IAW 53-41-14-300-001 ADD EMP:V940814 REPAIRED R-2 DOOR SILL PLATE IAW 53-41-14-300-001Feb 22, 2023 · N892UA · Airbus A319132 · Fuselage Main, Floor BeamSDR CALA2023022400526None · crackedR/H OVERWING EMERGENCY EXIT HAS CRACK AT INNER BOTTOM ANGLE-WEB PER HAECO LCQ NR 9298411/20411 SPEC: A3NB-05-3-6168. GENERATED B Y V919150. REMOVED AND REPLACED R/H OVERWING EMERGENCY EXIT INNER, BOTTOM ANGLE-WEB IAW SRM 51-42-11 AND DWG# 0522-79010 ADD EMP:V9Feb 22, 2023 · N892UA · Airbus A319132 · Fuselage Main, Plate/SkinSDR CALA2023021600446None · corrodedFWD CARGO PIT R/H FR26 BETWEEN STRINGERS 41R-42R CLEAT HAS CORROSION DOT M067. PER HAECO LCQ NONROUTINE 9298576/20576. GENERATED BY V919150. SPEC: A3NB-53-3-6105. FOUND CLEAT CORRODED AT FR26 BETWEEN STRINGERS 41R-42R TO BE OUT IAW A319 SRM 51-44-11/001A AND IFeb 15, 2023 · N892UA · Airbus A319132 · Fuselage Main, Plate/SkinSDR CALA2023020100282Intercostal · noneAD RELATED TASK (2022-02-11) RH FR16 DOOR STOP #7 INBD LOWER HOL E, #3. HAS A CRACK INDICATION IN THE INTERCOSTAL LAYER AT 6 O;CL OCK POSITION, REPAIRE BEFORE NEXT FLIGHT PER HAECO LCQ NR 929845 2/20452 GENERATED BY V061671. REMOVED AND REPLACED FR16 R/H #7 INJan 31, 2023 · N892UA · Airbus A319132 · Fuselage Main, FrameSDR CALA2019021700256Angle · crackedRH EMERGENCY EXIT HATCH FORWARD LOWER SEGMENT 1 IS CRACKED 16TH FASTENER FROM TOP = .110" LONG A3NB-52-3-6096 PER HAECO LCQ NR 9 296229 GENERATED BY V061633 REMOVED AND REPLACED DISCREPENT FRAME ANGLE ON R/H EMERGENCY EXI T HATCH AT FWD LOWER SEGMENT IAW A319 Feb 14, 2019 · N892UA · Airbus A319132 · Emergency ExitsSDR CALA2019021700255Angle · crackedLH EMERGENCY EXIT HATCH FORWARD LOWER SEGMENT 1 IS CRACKED 15TH, 16TH AND 17TH FASTENER FROM TOP = .5" LONG AND AFT LOWER SEGMEN T 1 IS CRACKED AT 17TH FASTENER FROM TOP = .0250" LONG A3NB-52-3 -6096 PER HAECO LCQ NR 9296228 GENERATED BY V061633 REMOVED AND REFeb 14, 2019 · N892UA · Airbus A319132 · Emergency ExitsSDR CALA2017032700739Threshold · crackedAFT PIT THRESHOLD CRACKED AT FASTENER HOLE BETWEEN FR57-FR58. REMOVED AND REPLACED THRESHOLD PLATE IAW SRM 51-42-11.Mar 27, 2017 · N892UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2017032700738Plate · corrodedCORROSION IN AFT CARGO DOORWAY AT FS 58 AROUND TIE DOWN. REMOVED AND REPLACED WEB SEAT PLATE AND SPLICER PLATE IAW SRM 51-42-11.Mar 27, 2017 · N892UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2017032600729Floor Support · corrodedAFT CARGO FLOOR SUPPORT AT FR59 H AS ELONGATED HOLE & CORROSION. REMOVED DAMAGE & REPLACED FLOOR SUPPORT AREA AT FR59 IAW TD18027 8508/006/2017 NR A.Mar 26, 2017 · N892UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2017032500725Structure · corrodedCORROSION AT R2 DOOR SILL AREA FR 65-66. REPAIRED CORROSION ON R2 DOOR SILL AREA FR65-66 IAW A319 SRM 53- 41-14 FIG 201 & PARA 5A.Mar 25, 2017 · N892UA · Airbus A319132 · Fuselage Miscellaneous Structure
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