N894UA

Service difficulty reports · 51

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 = 'N894UA' 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 CALA2026051116140Switch · faultedEMERGENCY LIGHTS ON WITH SWITCH IN ARMED POSITION COCKPIT EMERGENCY LIGHT TOGGLE SWITCH REPLACED IAW ESPM CHAPTER 20 AND OPS CHECK PERFORMED IAW AMM 33-51-00-710-006-A FOUND OK. ACFT OK TO SERVICE.May 7, 2026 · N894UA · Airbus A319132 · Emergency LightingSDR CALA2026050415951Girt Bar · failed inspDURING SLIDE R & R DOOR L2 GIRT BAR FAILED INSPECTION TC 31-2562-9-0001 GIRT BAR SLIDE FUNCTION DOES NOT MOVE FREELY. PHOTO UPDATE PIC UPDATE FOR THE OPERATIONAL CHECK OF THE GIRT BAR TELESCOPING FUNCTION INSTALLED NEW GIRT BAR ON AFT LEFT SLIDE PER AMM 25-62-Apr 30, 2026 · N894UA · Airbus A319132 · Emergency EquipmentSDR CALA2026030414325Light · no discrepancyFA REPORT EMERGENCY EXIT LIGHTS FLICKERED SEVERA L TIMES AS THE DOORS WERE BEING DISARMED ON PACP CABIN EMERGENCY LIGHT TEST ALL DOOR SLIDES AND EPSU TEST NORMAL NO FAULTS FOUND.Mar 2, 2026 · N894UA · Airbus A319132 · Emergency LightingSDR CALA2025121612143Plate · damagedRIGHT FR 66 GUSSET PLATE NR 5 BOTTOM HOLE HAS A OUT OF ROUND INDICATION. AFTER FURTHER EVALUATION, DAMAGE FOUND TO BE IN GUSSET PLATE ONL Y. REMOVED AND REPLACED RH FR66 GUSSET PLATE NR 5 IAW SRM 51-74-11-911-001.Dec 12, 2025 · N894UA · Airbus A319132 · Fuselage Main, StructureSDR CALA2025121212070Pin · corrodedNR 2 ENGINE AFT MOUNT 3EA LOWER INNER PINS ARE CORRODED. REMOVED AND REPLACED NR 2 ENG AFT MAINT LOWER INNER PINS 3EA IAW A 319 AMM 71-22-11-000-010-A AND 71-22-11-400-010-A. T/W TLC 2568 DUE 28/FEB/26.Dec 11, 2025 · N894UA · Airbus A319132 · Engine (Turbine/Turboprop)SDR CALA2025112611484Battery · faultedFWD L EPSU BATTERY FAULT ON FAP. REPLACED FWD L BATTERY IAW AMM 33-51-38-000-002-A. OPS CHECKED NORMAL.Nov 25, 2025 · N894UA · Airbus A319132 · Emergency LightingSDR CALA2025110510922Skin · dentedRAMP REPORTED A DENT UNDER CAPT WINDOW. UPON FURTHER INVESTIGATION FOUND TO BE 2 DENTS. UPPER DENT FOUND TO BE OUT OF LIMITS, DAMAGE IS LOCATED ON STRINGER AND FRAME REF SRM 53-11-11-283-012. ACCOMPLISHED DOUBLER REPAIR IAW ECRA 5311-03412, SRM 53-11-11-283Nov 5, 2025 · N894UA · Airbus A319132 · Fuselage Main, Plate/SkinSDR CALA2025062305789Dau · faultyELEC AC BUSS 1 FAULT FOLL OWED BY NUMEROUS ECAMS EVEN THE SYSTEM S APPEARED NORMAL PFR CONSIDER ADDING TSM 24-50-00-810-806-A FOR TSHOOTING. INLCUDES POSSIBLE CORROLATION OF ELEC AC BUSS 1 FAULT AND SDAC. PER TSM24-50-00-810-806-A, REPLACED SDAC2, REF MM31-55Jun 23, 2025 · N894UA · Airbus A319132 · Electrical Power SystemSDR CALA2024120601428Lamp · inoperativeFOUND EPSU EXT LOAD EMER L FAULT. 33-51-38. TS REF 33-51-00-810-808-A. FOUND LH AFT OVERWING LIGHT INOP. REPLACED LAMPS. OPS CHECK GOOD. EMERGENCY LIGHT TEST PASS. REF AMM SUBTASK 33-51-15-420-050-A.Dec 4, 2024 · N894UA · Airbus A319132 · Emergency LightingSDR CALA2024120403014Fuel Cap · missingPDA2 FUEL CAP MISSING A/C FLEW WITH FUEL CAP MISSING. REPLACING ON CDL FOR ITEM TO BE DDP ACCOMPLISHED REPLACED . CLOSE TO DEPARTURE TIME. DISPATCH DESK: 16 NAME: AW DATE: 30-NOV-24- OK TO CDL TOMC SMITH 28A....Nov 30, 2024 · N894UA · Airbus A319132 · Fuel StorageSDR CALA2024052401578Life Vest · missingSEAT 22E MISSING UNDERSEAT LIFEVEST. REPLACED MISSING PAX SEAT LIFEVEST AT SEAT 22E I.A.W. AMM 25-66-52.May 22, 2024 · N894UA · Airbus A319132 · Life JacketSDR CALA2024041001023Computer · out of toleranceL WING LEAK DISPLAYED ON UPPER ECAM SCREEN. - AIR REF WING LEAK, FOLLOW MT 21-004 INSTRUCTIONS FOR FURTHER TROUBLESHOOTING. INSPECTED LH BLEED DUCT AND SENSING ELEMENTS REF AMM 36-22-16 NO DEFECTS NOTED. CHRONIC LEVEL-1 AIR BLEED MSG IN CRUISE. USE TSM 36-22-0Apr 6, 2024 · N894UA · Airbus A319132 · Navigation SystemSDR CALA2024040800997Coupling · leakingLEFT WING LEAK DISPLAYED ON UPPER ECAM SCREEN. MSG APPEARED AT CRUISE, 39K FEET. PILOT TURNED OFF ENG 1 BLEED PER QRH AND MESSAGE WENT AWAY. UNLOCK TO UPDATE INSPECTED FOR AIR LEAKS IN L WING LOOP AND DUCT SYSTEM. SEARCHED FOR LEAKS FROM APU CHECK VALVE TO WHApr 4, 2024 · N894UA · Airbus A319132 · Pneumatic SystemSDR CALA2024021600435Hose · leakingCREW REPORTS ON APPROACH GREEN SYS LOSS. SYS SECURED PER FLT MAN WILL NEED GRAVITY EXTENSION AND TOW TO GATE LOCKING ITEM FOR FIX CONFIRMATION UNLOCKED FOR SIGN OFF WILL NEED TO ACCOMPLISH AMM 32-00-00-860-003-A TO RETURN GEAR TO FOUND LEFT MLG DOOR ACTUATOR LFeb 14, 2024 · N894UA · Airbus A319132 · Hydraulic System, MainSDR CALA2023033100929Floor Support · corrodedCABIN FLOOR SUPPORT FR16 Y1292 HAS CORROSION. DOT NO. 17-68 () REMOVED AND REPLACED FLOOR SUPPORT P/N: D5311281300251 I.A.W. S .R.M. 51-42-11 SEE ATTACHMENT 44-0008 EMP#: V943415 WORK ACCOMPL ISHED AT ST ENGINEERING OF MOBILE AT BFM ON NR#: 52149Mar 29, 2023 · N894UA · Airbus A319132 · Fuselage Main, StructureSDR CALA2021053100761Fastener · missingPDA 3 REF L-P 6279380 FASTENER MISSING ENG1 OB PYLON 413EL REPLACED FASTENER REF IPC 54-52-11-01A. TOMC NOTIFED.May 31, 2021 · N894UA · Airbus A319132 · Nacelle/Pylon, Main FrameSDR CALA2021051000634Switch · discovered*DECLARED EMERGENCY* LGCIU 1 FAULT DISPLAYED ON UPPER ECAM SCREEN - L-G L/G LGCIU 1 FAULT LGCIU RIGHT AFTER TAKEOFF GEAR HANDLE UP. PICTURE ATTACHED OF SYSTEMS PAGE WAS THE XX SYSTEMS PAGE. NOTE THAT DURING FLIGHT ALL THEY INDICATED ON 32-31-11. ALL OPS CHECKMay 10, 2021 · N894UA · Airbus A319132 · Landing Gear Door Retract SectionSDR CALA2021021200166Power Supply · inoperativeA3NB-33-0004; PRODUCTION REQUEST, 721220, DURING OPERATIONAL CHE CK OF CABIN EMERGENCY LIGHTING THE BATTERY CAPACITY FAILS (EPSU BAT CAP EMER R, AFT L). REF BY PEMCO NR.10481.0021.Feb 11, 2021 · N894UA · Airbus A319132 · Emergency LightingSDR CALA2020072701077Fuel Cap · missingPDA 2 FUEL CAP MISSING ON ARRIVAL INSTALLED FUEL CAP.Jul 25, 2020 · N894UA · Airbus A319132 · Fuel StorageSDR CALA20190821399Bottle · damagedMAIN CABIN DOOR OPENED BY GATE AGENT FROM OUTSIDE THE AIRCRAFT WITH SLIDE ARMED. SLIDE PACK. CREW REPORT- DOOR WAS ACTUALLY OPENED BY LEAD FLIGHT ATTENDANT, NOT THE GATE AGENT. R & R FWD LEFT EVAC SLIDE AND RAFT ASSY PER AMM 25-62-44. SERVICED DOOR ASST BOTTLEAug 19, 2019 · N894UA · Airbus A319132 · Escape SlideSDR CALA2019030800361Skin · dentedPERFORM PERMANENT REPAIR FUSELAGE SKIN AT FR 62 STR 28L PER EC/ RA 5330-06289 SUPPORT TASK PER LCQ NR 9298279. PERFORMED PERMANENT DOUBLER REPAIR PER EC/RA 5330-06289 PART 3 ALTERNATELY ACCOMPLISHED PER SRM 53-00-11-300-043 TABLE 08 FIG. 01 CUT OUT DIM 2.1"L XMar 5, 2019 · N894UA · Airbus A319132 · Fuselage Main, Plate/SkinSDR CALA2019030100333Angle · crackedLT EMERGENCY EXIT HATCH FORWARD FRAME UPPER SEGMENT #1 8TH FASTENER FROM TOP IS CRACKED. 0.040" LONG LOWER SEGMENT #1 FASTENER HOLE 14TH = 0.270", 16TH = 0.260", 17TH = 0.150", 18TH = 0.150" TOTAL = 1.23" A3NB-52-3-6096 PER LCQ NR 9298289 REMOVED AND REPLACED Feb 28, 2019 · N894UA · Airbus A319132 · Emergency ExitsSDR CALA2019030100332Angle · crackedRT EMERGENCY EXIT HATCH FORWARD FRAME LOWER SEGMENT #1 FASTENER HOLE IS CRACKED 16TH = 0.38" A3NB-52-3-6096 PER LCQ NR 929 8291 REMOVED AND REPLACED EMERGENCY EXIT HATCH LOWER SEGMENT IAW SRM 51-72-11-911-001.Feb 28, 2019 · N894UA · Airbus A319132 · Emergency ExitsSDR CALA2019030100331Angle · crackedRT EMERGENCY EXIT HATCH AFT FRAME LOWER SEGMENT #1 FASTENER HOLE IS CRACKED 13TH = 0.210", 14TH = 0.340", 15TH = 0.260", 16TH = 0.290", 17TH = 0.145" TOTAL = 1.245" A3NB-52-3-6096 PER LCQ NR 9298292 REMOVED AND REPLACED RT EMERGENCY EXIT HATCH AFT FROM LOWER SFeb 28, 2019 · N894UA · Airbus A319132 · Emergency ExitsSDR CALA2019030100330Angle · crackedLT EMERGENCY EXIT HATCH AFT FRAME LOWER SEGMENT #1 FASTENER HOLE IS CRACKED 16TH = 0.350", 17TH = 0.150", 18TH = 0.150" TOTAL = 0.7" A3NB-52-3-6096 PER LCQ NR 9298290 3 REMOVED AND REPLACED LT EMERGENCY EXIT HATCH AFT FRAME LOWER SEGMENT IAW SRM 51-72-11-911-0Feb 28, 2019 · N894UA · Airbus A319132 · Emergency ExitsSDR CALA2019030100307Gusset · damagedRT INNER CAP JOINT-GUSSETS FRAME 68 STRINGER 12 2ND HOLE FROM TO P, #2, HAS REJECTABLE INDICATIONS A3NB-53-4-6355 AD 2015-05-02 P ER LCQ NR 9298204 UPON FURTHER EVALUATION OF GUSSET HOLES 1EA HOLE @FR68 STR 12R G OUND TO BE DAMAGED REAMED HOLE TO @ DIA OF 0.21Feb 27, 2019 · N894UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2018122402643Battery Pack · faultyCIDS FAULT EMERGENCY EQUIPMENT "EPSU UNIT FWD L ATA 33-51-38" TRIED EPSU NO HELP SUSPECT BATTERY,NIS DEN,PART ON AOG. REMOVED PANEL FOR ACCESS IAW AMM 25-23-42 PANEL IN G1 AREA, BATTERY PN 3214-31 M&E 18-3351-3-0001 ON ORDER. REPLACED FWD L AND OVERWING L BATTDec 24, 2018 · N894UA · Airbus A319132 · Emergency LightingSDR CALA2017091503206Power Supply · malfunctionedCABIN EMERGENCY LIGHTS, OPS CHECK FAILED. FAULTED EPSU BATTERY EMERGENCY LIGHT RESET SYS, OPS CHECKED OK IAW AMM 33-51-38,Sep 15, 2017 · N894UA · Airbus A319132 · Emergency LightingSDR CALA2017090103017Flashlight · inoperativeAFT FLIGHT ATTENDENT, SEAT 2L, EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED THE FLASHLIGHT.Sep 1, 2017 · N894UA · Airbus A319132 · Emergency EquipmentSDR CALA2017071002141Wire · burnedELECTRICAL.ODOR.FROM CAPTAIN`S ACARS PRINTER. PULLED THE CIRCUIT BREAKER. FOUND WIRE INSULATION HAD BURNED INSIDE PRINTER. REPLACED THE PRINTER.Jul 10, 2017 · N894UA · Airbus A319132 · Electrical Power System WiringSDR CALA2017061601842Floor Support · corrodedCABIN FLOOR SUPPORT FRAMES 65 - 66, Y1730, HAD SURFACE CORROSION AROUND NUTPLATES JUST FWD OF R2 DOOR SILL. REPAIRED THE AREA IAW SRM 53-41-14-300-001.Jun 16, 2017 · N894UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2017061601838Door Sill · corrodedAFT CARGO BAY SILL PLATE CORRODED AT FRAME 58. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-42-11-001, PARAGRAPGH D, E, AND F, FIGURE 110.Jun 15, 2017 · N894UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2017061601835Crossbeam · corrodedFORWARD CARGO BAY FRAME 28 CROSSBEAM ATTACH ANGLE CORRODED STRINGER 44. CORROSION BEYOND LIMITS. REMOVED AND REPLACED IAW SRM 51-72-11-911-001, PG 2,3Jun 14, 2017 · N894UA · Airbus A319132 · Fuselage Main, StructureSDR CALA2017061201802Fitting · corrodedAFT CARGO DOOR SILL SUPPORT FITTING BETWEEN FRAMES 55A - 56 HAS CORROSION AROUND FASTENER HOLE. REMOVED AND REPLACED DOOR SILL SUPPORT IAW SRM 54-24-11-001, PARA F.Jun 12, 2017 · N894UA · Airbus A319132 · Fuselage Main, Attach FittingsSDR CALA2017061201801Fitting · corrodedAFT CARGO DOOR SILL SUPPORT FITTING JUST AFT OF FRAME 57 HAS CORROSION AROUND FASTENER HOLE. REMOVED AND REPLACED AFT CARGO DOOR SILL SUPPORT IAW SRM 51-40-11-001, PARAGRAPH F.Jun 12, 2017 · N894UA · Airbus A319132 · Fuselage Main, Attach FittingsSDR CALA2017061201798Door Sill · corrodedFWD CARGO DOOR SILL FRAMES 24- 29 HAS CORROSION. REMOVED AND REPLACED THE FWD CARGO DOOR SILL IAW SRM 51-72-11- 911-001, PAR 2.3Jun 11, 2017 · N894UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2017061201797Web · corrodedFWD CARGO DOOR THRESHOLD HAS CORROSION IN SEVERAL AREAS. REMOVED & REPLACED THE THRESHOLD WEB IAW SRM 51-72-11 -911-001, PARA 2, & 3Jun 11, 2017 · N894UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2017061201796Fitting · corrodedFITTING AT FRAME 58, STRINGER 41R CORRODED AT FASTENER HOLE. REMOVED & REPLACED THE FITTING IAW SRM 51-42-11-001, PARAGRAPH F.Jun 11, 2017 · N894UA · Airbus A319132 · Fuselage Main, Attach FittingsSDR CALA2017061101794Skin · dentedRIGHT FWD FUSELAGE SKIN DENTED, FRAME 8, STRINGER 24R. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-11-283-002, FIG 10102. PERFORMED A DOUBLER REPAIR IAW SRM 53-00-11-300-029.Jun 11, 2017 · N894UA · Airbus A319132 · Fuselage Main, Plate/SkinSDR CALA2017060901747Stringer · corrodedCORROSION ON STR 39L 6" AFT OF FRAME 28 . EVALUATED CORROSION & FOUND NOT TO BE WITHIN LIMITS IAW SRM 51-21-13-283-001 FIG 10102. FABRICATED REPAIR PARTS IAW SRM 53-00-13-300-001. INSTALLED REPAIR PARTS IAW SRM 51-42-11-001 PARA F & PARA E.Jun 6, 2017 · N894UA · Airbus A319132 · Fuselage Main, Longeron/StringerSDR CALA2017060501673Support · corrodedFWD CARGO DOOR SILL SUPPORT NR 4 HAS CORRODED HOLES. REMOVED & REPLACED THE SUPPORT IAW SRM 51-42-11-001, PARA 4B. ALL STEPS ON THIS TASK HAVE BEEN FOUND T O BE IN C/W CURRENT SRM REV 118Jun 5, 2017 · N894UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2017060501672Support · corrodedFWD CARGO DOOR SILL SUPPORT NR 5 HAS CORRODED HOLES. REMOVED & REPLACED THE SUPPORT IAW SRM 51-42-11-001, PARA 4B. ALL STEPS ON TASK FOUND TO BE IN C/W CURRENT SRM REV 118Jun 5, 2017 · N894UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2017060501676Door Sill · corrodedFWD CARGO DOOR SILL SUPPORT NR 3 HAS CORRODED HOLES. REMOVED & REPLACED FWD CARGO DOOR SUPPORT IAW SRM 51-4 2-11-001 PARA 4B. ALL STEPS ON TASK FOUND TO BE IN C/W CURRENT S RM REV 118Jun 5, 2017 · N894UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2017060501675Door Sill · corrodedFWD CARGO DOOR SILL SUPPORT NR 6 HAS CORRODED HOLES. REMOVED & REPLACED FWD CARGO NR 6 DOOR SUPPORT IAW SRM 51-4 2-11-001 PARA 5B. ALL STEPS ON THIS TASK IS IN C/W CURRENT SRM R EV 118Jun 5, 2017 · N894UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2017052601561Stringer · corrodedCORROSION FOUND AROUND FASTENER HOLE ON STRINGER 41R, 10 INCHES AFT OF FRAME 58 AND 6 INCHES AFT OF FRAME 56. REPAIRED THE STRINGER IAW DRAWING R534-70620 ISSUE B AND TD 80302950/010/2017.May 23, 2017 · N894UA · Airbus A319132 · Fuselage Main, Longeron/StringerSDR CALA2017081402658Threshold · damaged46 HOLES ARE OUT OF ROUND IN AFT CARGO THRESHOLD STRUCTURE FROM FRAMES 55 - 59. REPAIRED DISCREPANT HOLES IAW SRM 51-44-11 & ECRA 5340-0177 8.May 21, 2017 · N894UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2017052201526Fitting · corrodedAFT CARGO DOOR CUTOUT HAS CORROSION AT FR59 ON CORNER SEALING ASSEMBLY. REMOVED CORNER SEAL ASSY. REPLACED CORNER SEAL ASSY IAW SRM 51-72-11-91 1-001, 51-42-11. TOP COATED IAW SRM 51-23-11.May 21, 2017 · N894UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2017052101509Frame · corrodedAFT CARGO FR59 HAS CORROSION AT STR38R. REPAIRED AFT CARGO FR59 IAW TS 80290673-010/2017 NR A AND ECRA 5340-01775. ACP PERM REPAIR FR59 BETWEEN S37R AND S43R PER PART 3 OF ECRA 5340-01775 ON OR BEFORE 12OCTOBER2017.May 20, 2017 · N894UA · Airbus A319132 · Fuselage Main, FrameSDR CALA2017042801157Door Sill · corrodedAFT CABIN FLOOR STRUCTURE R2 DOOR SILL FR66-68 CORROSION. REMOVED AND REPLACED AFT CABIN FLOOR STRUCTURE R2 DOOR SILL FR66 -68 IAW SRM 51-72-11, 53-41-14, 51-42-.Apr 25, 2017 · N894UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2017081402649Door Sill · corrodedAFT CABIN FLOOR STRUCTURE L2 DOOR SILL FR66-68 CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14. REMOVED AND REPLACED THE DOOR SILL IAW SRM 53-41-14, 51-42 -11, AND 51-49-00.Apr 24, 2017 · N894UA · Airbus A319132 · Fuselage Miscellaneous Structure
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