N805UA

Service difficulty reports · 117

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 = 'N805UA' 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 CALA2025073107122Sensor · unsecureCARGO DOOR OPEN ECAM ON TAXI OUT. FOUND FWD CARGO DOOR CLOSED INDICATION SWITCH ASSY LOOSE, UNABLE TO TIGHTEN DUE TO DAMAGED HARDWARE, CLOSED DOOR AND VERIFIED FWD CARGO DOOR CLOSED AND LATCHED IAW AMM 52-70-00-040-001-A, R & R THE FWD CARGO DOOR PROXIMITY Jul 25, 2025 · N805UA · Airbus A319131 · Door Warning SystemSDR CALA2025011601934Unknown · smokeTOWER REPORTED THATTHEY OBSERVED WHITE SMOKE FROM THE TIRE AREA ON TAKEOFF. PERFORMED A GVI OF THE BRAKING SYSTEM AND TIRE REF AMM 32-40-00-210-801-A & 32-41-00-210-002-A NO DEFECTS NOTED. PERFORMED A WALK AROUND THE AIRCRAFT FOR HYDRAULIC LEAKS NO DEFECTJan 13, 2025 · N805UA · Airbus A319131 · Standard Practices/StructuresSDR CALA2025011401898Battery Pack · no testCABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - AFT LEFT EPSU BATTERY BAD REPLACED BATTERY WITH SERVICEABLE ONE FROM STOCK. OPS CHECK GOOD.PARTS USED:18-3351-3-0001,QTY :1Jan 12, 2025 · N805UA · Airbus A319131 · Emergency LightingSDR CALA2024092700697Pressure Switch · faultyHYD G RSV LO LVL DEBREIFED CREW. #1 EDP WAS SHUT DOWN IMMEDIATLY WHEN LOW PRESSURE INDICATION APPEARED. FLUID LEVEL UPDATE REPLACED LOW LEVEL SWITCH REF TASK 29-11-41-000-003-A. TASK 29-11-41-400-003-A. OPS CHECK GOOD. QTY INDICATOR NORMAL.Sep 25, 2024 · N805UA · Airbus A319131 · Hydraulic Pump (Electric/Engine), MainSDR CALA2024053101650Battery Pack · dischargedEMERGENCY EPSU BATTERY AFT L FAILS OPERATIONAL CHECK. REF TO PEMCO NR 15402.0026 REMOVED AND REPLACED EPSU BATTERY AT 13WL IAW A319 AMM 33-51-38- 000-002-A AND A319 AMM 33-51-38-400-002-A. OPERATIONAL TEST GOOD IAW A319 AMM 33-51-00-710-001-AMay 30, 2024 · N805UA · Airbus A319131 · Lighting SystemSDR CALA2024050601327Window · leakingWATER LEAKING IN COCKPIT MEAR AFT BASE OF FO SIDE WINDOW FAIRHURST, FOUND EXTERIOR SEAL SPLIT IN FWD UPPER CORNER-ALLOWING RAIN TO SEEP IN. ACCOMPLISHED REPAIR PER MT56-003 REV A WITH SILICONE. REPAIR COVERED WITH TAPE. TAPE TO BE RECHECKED EACH FLIGHT AND RMay 2, 2024 · N805UA · Airbus A319131 · Flight Compartment WindowsSDR CALA2024032900905Fuel Cap · missingPDA 2 FUELER REPORTED FUEL CAP MISSING DEFERRING MISSING CAP PER CDL, MX ACTION CW DEFERRED DEFERRED DISPATCH DESK: 28 NAME: JG DATE: 27-MAR-24- OK TO APPLY CDL 28A FOR MISSING FUEL CAP-CAP WAS MISSING ON ARRIVAL. STLOO CONFIRM FUEL CAP WAS LEFT ON TRUCK-NO Mar 27, 2024 · N805UA · Airbus A319131 · Fuel StorageSDR CALA2023090402676Cap · missingPDA2 - EXTERIOR WALK AROUND {A3NB-06-3-6001} - FUEL CAP MISSING AT RIGHT WING CAP, COUPLING R OFF 31-2825-9-0001 7042 ON 0000 CAP, COUPLING R OFF 31-2825-9-0001 7042 ON 31-2825-9-0001 0598 INSTALLED REFUEL DEFUEL COUPLING CAP REF AMM 28-25-41. NO DEFECTS NOTEDAug 26, 2023 · N805UA · Airbus A319131 · Aircraft Fuel Distribution SystemSDR CALA2023082802652Fuel Cap · missingEXTERIOR WALK AROUND {A3NB-06-3-6001} - FUEL CAP MISSING AT RIGHT WING. CAP, COUPLING R OFF 31-2825-9-0001 7042 ON 0000 CAP, COUPLING R OFF 31-2825-9-0001 7042 ON 31-2825-9-0001 0598 INSTALLED REFUEL DEFUEL COUPLING CAP REF AMM 28-25-41. NO DEFECTS NOTED.Aug 26, 2023 · N805UA · Airbus A319131 · Aircraft Fuel SystemSDR CALA2023080402420Skin · damagedREFERENCE LP# 5057236 DAMAGE SITES #2-4, AC SUSTAINED GROUND DAMAGE TO FUSELAGE APPROXIMATELY FWD OF FR65 TO AFT OF FR66 & S32L - S35L. AVO10948 ISSUED FOR REPAIR. PARAGRAPH. ENSURE THAT THERE IS NO DAMAGE TO THE ADJACENT WATER ADJACENT STRINGER, FRAME, CLEATSAug 3, 2023 · N805UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2022071501759Skin · damagedDURING A MAINTENANCE HMV-4 CHECK PRODUCTION REPORTED A MILLED DOUBLER ON THE FUSELAGE SKIN AT FR34/STR43 WHILE PERFORMING THE REQUIRED INSPECTION PER UAL EA 5300-02120 REV C OP 001. BETWEEN STGR44 AND STGR42HR PER PART-2 OF THE LATEST REVISION OF ECRA 5321-020Jul 14, 2022 · N805UA · Airbus A300* · Fuselage Floor PanelSDR CALA2022071501757Fitting · damagedWHILE WORKING FLEET CAMPAIGN DIRECTIVE # 5330-05575 FIG 14 HOLE DIAMETER REPORTING RH, HOLES R1,R2,R3,R7,R8,R9,R10,R11,R12,R13,R 14,R15,R16,R17,R18,R19,R20,R21,R72,R73,R75, & R76 WITH DAMAGE AS MARKED ON FIG SHEET R11, R12, R13, R14, R15, R16, R17, R18, R19, RJul 14, 2022 · N805UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2022070801672Door Sill · corrodedCABIN FLOOR STRUCTURE FR66 Y-1162 HAS CORROSION REMOVED CORROSION ON R2 DOOR SILL IAW SRM 51-74-00. FOUND TO BE OUT LIMITS IAW SRM 53-41-24-283 ORIGINAL THICKNESS 0.315" D=0.09 5". DOOR SILL REMOVED AND REPLACED IAW SRM 51-72-11-911-001. EMP : V933866 WC: 3208Jul 8, 2022 · N805UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2022062701593None · corrodedCABIN FLOOR SUPPORT STRUCTURE BTW FR66-FR68, Y-1292, FLOOR BEAM WITH CORROSION,REMOVED CORROSION ON CABIN FLOOR BEAM FR68 Y-1292, MEASURED ORIGINAL THICKNESS .160 D=0.110" L=1.920" W=2.200" FOUND OUT OF LIMITS. FLOOR BEAM REMOVED AND REPLACED STA: ST ENG BFM.Jun 27, 2022 · N805UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2022062401571None · corrodedAFT CABIN L2 DOORWAY, SHAPE SILL HAS CORROSION ON AFT END (NR 32 255). ON REMOVAL OF THE SHAPE SILL, CORROSION WAS FOUND. ON THE TOP FACE OF THE DOOR SILL. CORROSION WAS REMOVED AND FOUND OUT OF LIMITS AND REPLACED SHAPE SILL, DOOR SILL AND CORNER FITTINGSJun 24, 2022 · N805UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2022062401576None · corrodedCABIN FLOOR SUPPORT STRUCTURE, FR65-FR66, Y-1732, BEAM WITH CORROSION (NR 32193) FLOOR BEAM REMOVED IAW SRM 51-72-11-911-001 AND INSTALLED NEW BE AM IAW SRM 51-42-11/001. EMP: V936191 WC: 32193 STA: ST ENG BFM SFR# 1028881Jun 24, 2022 · N805UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2022062401566Skin · dentedDENT RIGHT WING #1 SLAT, INBOARD OF THE ENGINE. BY A PERMANENT STRUCTURAL REPAIR WITHIN 5,000 FC OR 10,000 FH OR 24 MONTHS,WHICHEVER OCCURS FIRST.WORKED PERFORMED BY U163564. SLAT DENT DIMENSIONS L6.75 W3.75 D.190 IN SKIN AREA 3. PERFORMED REPAIR PER SRM 51-73Jun 23, 2022 · N805UA · Airbus A319131 · Wing StructureSDR CALA2022062401574Seat Track · corrodedCABIN FLOOR SUPPORT STRUCTURE BTW FR66-FR68, Y-1292, FLOOR BEAM WITH CORROSIONJun 22, 2022 · N805UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2022062201551Channel · corrodedAFT CABIN L2 DOORWAY, SHAPE SILL HAS CORROSION ON AFT END (NR 32 255)Jun 21, 2022 · N805UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2022062201550Floor Support · corrodedCABIN FLOOR SUPPORT STRUCTURE, FR65-FR66, Y-1732, BEAM WITH CORR OSION (NR 32193)Jun 21, 2022 · N805UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2022061501516None · corrodedAFT CARGO DOOR CUTOUT LOWER SILL TORQUE BOX UPPER SURFACE CORROD ED AROUND 3EA TIE DOWN FITTINGS BETWEEN FR56-FR58 REMOVED LOWER SILL IAW SRM 51-42-11/001 AND FABRICATED NEW LOWER SILL IAW SRM 57-72-11-911 (2024-T3) 0,125" AND INSTALLED NEW LO WER SILL IAW SRMJun 15, 2022 · N805UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2022061501502Plate · corrodedAFT CARGO DOOR CUTOUT LOWER SILL TORQUE BOX UPPER SURFACE CORROD ED AROUND 3EA TIE DOWN FITTINGS BETWEEN FR56-FR58 REMOVED LOWER SILL IAW SRM 51-42-11/001 AND FABRICATED NEW LOWER SILL IAW SRM 57-72-11-911 (2024-T3) 0,125" AND INSTALLED NEW LO WER SILL IAW SRMJun 14, 2022 · N805UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2022061301495Structure · crackedFWD CARGO COMPARTMENT, FR30-FR34, AFT BULKHEAD, LH SIDE, LOWER S UPPORT STRUCTURE CRACKED. REMOVED PROFILE (PLATE) FWD CARGO FR34 IAW SRM 51-42-11. RECEIVE D NEW PLATE. LOCATED AND DRILLED NEW PLATE IAW SRM 51-44-11/001. INSTALLED NEW PLATE IAW SRM 51-42-11/00Jun 13, 2022 · N805UA · Airbus A319131 · Cargo CompartmentsSDR CALA2022061301494None · corrodedMAIN CABIN FLOOR STRUCTURE FR68, Y-765 HAS CORROSION REMOVED CORROSION AT MAIN CABIN FLOOR STRUCTURE FR68, Y-765 IAW P/N D5347219320000, BATCH 0002756757. EMP: V936054 WC: 32082 STA SMR 51-74-00. FOUND TOBE OUT OF LIMIT AT HARD POINT AREA IAW SRM : ST ENG BFM Jun 13, 2022 · N805UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2022061301488Beam · corrodedCABIN FLOOR STRUCTURE FR66 Y-1162 HAS CORROSION. DETAILS AWAITEDJun 12, 2022 · N805UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2022061301485Plate · damagedRH FR68 AND FR66 INNER CAP JOINT TO THE GUSSET PLATES FROM STRIN GER 10 TO STRINGER 16 HAS DAMAGE INDICATION IN ALL HOLES NOTED. DAMAGE CLASSIFIED AS OUTROUND HOLES AND GOUGES. REAMED TO 0.1865" ALL HOLES AT RH FR66 AND FR68 FROM STR10 TO ST STA: ST ENG BFM R1Jun 10, 2022 · N805UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2022060801471Floor Support · corrodedCABIN FLOOR SUPPORT STRUCTURE BTW FR64-FR70, Y160.5, BEAM WITH C ORROSION REMOVED CORROSION ON CABIN FLOORBEAM AND FOUND WITHIN LIMITS IA W A320 SRM 53-00-14-283-002 L=2" W=1", D=.014" (MAX DEPTH ALLOWE D=.016") AND COUPLINGS REMOVED AND REPLACED IAW A320 SRM Jun 8, 2022 · N805UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2022060801457Support · crackedFWD CARGO COMPARTMENT, FR30-FR34, AFT BULKHEAD, LH SIDE, LOWER SUPPORT STRUCTURE CRACKED.Jun 7, 2022 · N805UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2022060801456Beam · corrodedMAIN CABIN FLOOR STRUCTURE FR68, Y-765 HAS CORROSIONJun 7, 2022 · N805UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2022060201429Floorbeam · corrodedCABIN FLOOR STRUCTURE BEAM BETWEEN FR68/FR69 AND Y160.5 HAS CORR OSION. REMOVED AND INSTALLED FLOORBEAM MAIN CABIN FR68 TO FR70 LH Y160 .5 IAW SRM A319 51-42-11. P/N: D5347219620000 - BATCH NOL 000392 206. EMP: V935976 WC: 32167 STA: ST ENG BFM SFR# 1028737Jun 2, 2022 · N805UA · Airbus A319131 · Fuselage Main, Floor BeamSDR CALA2022060201424Beam · corrodedCABIN FLOOR SUPPORT STRUCTURE BTW FR64-FR70, Y160.5, BEAM WITH C ORROSIONJun 2, 2022 · N805UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2022060101408Beam · corrodedCABIN FLOOR STRUCTURE BEAM BETWEEN FR68/FR69 AND Y160.5 HAS CORROSION.May 31, 2022 · N805UA · Airbus A319131 · Fuselage Main, Floor BeamSDR CALA201812112544Seal · missingENG 2 HAS VISIBLE GAP BETWEEN TOP OF NACELLE & PYLON ABEAM COM P RESSOR SECTION TOP LEFT FOUND THE #2 ENG UPPER AFT C DUCT SEAL MISSING P/N 740-0104-29. REMOVED THE DAMAGED SEAL AND REPLACED WITH NEW. REF AMM 78-32-00Dec 8, 2018 · N805UA · Airbus A319131 · Engine Thrust ReverserSDR CALA2017112404203Battery · faultyCIDS EMERGENCY SYSTEM FAILED THE 2 SERVICE CHECK, BATTERY FAILED FWD LT AND EPSU EMERGENCY L AND EPSU EMER R. REPLACED EPSU BATTERIES AT (10WL), (11WL), AND (12WL) PER MM33- 51-38-400-002, OPS CHECKS GOOD.Nov 24, 2017 · N805UA · Airbus A319131 · Emergency LightingSDR CALA2017060501683Altimeter · stickingSTANDBY ALTIMETER INDICATION ERRONEOUS STBY ALTIMETER NEEDLE STICKS WHILE CLIMBING AND DESCENDING. REPLACED STANDBY ALTIMETER IAW AMM34-21-22-400-001-B. LIGHTING OPERATIONAL TEST PASSED.Jun 5, 2017 · N805UA · Airbus A319131 · Altimeter, Barometric/EncoderSDR CALA2017021300364Proximity Switch · out of adjustDOOR 2R SLIDE ARMING PROX SWITCH 7NW2 WAS FOUND OUT OF TOLERANCE . ADJUSTED THE DOOR 2R SLIDE ARMING PROXIMITY SWITCH 7NW2 WITH REF TO AMM 52-71-00-820-002-A01.Feb 13, 2017 · N805UA · Airbus A319131 · Door Warning SystemSDR CALA2017021300354Oven · faultyAFT GALLEY OVEN R42 POPPED ITS CB AS IT WAS PUT UNDER LOAD FOR REPORTED BURNING SMELL IN CABIN. INSTALLED SERVICEABLE OVEN OPS CHECK GOOD.Feb 13, 2017 · N805UA · Airbus A319131 · Buffet/GalleysSDR CALA2017021200331Oven · defectiveELECTRICAL BURNING SMELL THROUGHOUT CABIN. NO SMOKE PULLED FWD AND AFT GALLEY BREAKERS, APPLY POWER TO GALLEYS. TURNED ONE GALLEY DEVICE AT A TIME. FOUND NO FAULTS OR ODORS IN FORWARD GALLEY. AFT GALLEY DID PRESENT SOME HEAT/OVERHEAT ODORS AT TIMES, NOT ELEFeb 12, 2017 · N805UA · Airbus A319131 · Buffet/GalleysSDR CALA2017021000310Skin · damagedDURING RUDDER INSTALL FOUND SMALL PUNCTURE ON RT SIDE OF RUDDER ABOUT 18 INCHES AFT OF LOWER FWD HOST POINT AND 20 INCHES UP FROM BOTTOM OF RUDDER ALSO A SCRATCH ON UPPER HALF. PERMANENT REPAIR ACCOMPLISHED PER ECRA 5540-01477 AND REO L205285.Feb 10, 2017 · N805UA · Airbus A319131 · Rudder, Plate/SkinSDR CALA2017012300170Battery Pack · faultedEMERGENCY LIGHT SYS TEST FAULTED FOR THE EPSU UNIT AND AFT EPSU BATTERY. REPLACED BATTERY PACK, TEST PASSED. IAW MM 33 51 38 000 002A,Jan 23, 2017 · N805UA · Airbus A319131 · Emergency LightingSDR CALA2016083095699Connector · damagedEMERGENCY LIGHTS AT SEATS 11C, 29C DO NOT ILLUMINATE WHEN POWER OFF 11C OK, REPINNED SEAT 29C CONNECTOR, OPS CHECKED GOODAug 27, 2016 · N805UA · Airbus A319131 · Emergency LightingSDR CALA2016082695687Lamp · inoperativeEMERGENCY LIGHTS AT SEATS 11C, 29C DO NOT ILLUMINATE WHEN POWER IS OFF. REPLACED THE LAMPS, TESTED OK.Aug 24, 2016 · N805UA · Airbus A319131 · Emergency LightingSDR CALA2016080995610Wire Harness · not reportedNOSE WHEEL STEERING FAULT ECAM MESSAGE. EMERGENCY DECLARED AND LANDED OK. REPLACED NOSE GEAR HARNESS 2M, OPS CHECKED OK IAW MM 32-21-43-400-003-AAug 8, 2016 · N805UA · Airbus A319131 · Landing Gear System WiringSDR CALA2016060895439Connector · dirtyTWO ECAMS UPON AUTO BRAKE ARM WHEEL, NOSE WHEEL STEERING FAULT & BRAKES SYS 1 FAULT. EMER DECLARED TO ENSURE LONG RNWY. PFR FAULTED BSCU STEERING FDBK SENSORS, 3GC - 4GC. CLEANED CONNECTOR ON SERVO CTL NOSE WHEEL STEERING, 6GC, & ALL FAULTS WENT AWAY IAW TSJun 7, 2016 · N805UA · Airbus A319131 · Landing Gear System WiringSDR CALA2015111794820Flap · malfunctionedFLAPS LOCKED AT POSITION 2, WING TIP BRAKES ENGAGED AT 190 KTS, RESET WTB FLAPS IAW AMM 27-50-00-869-006. PREFORMED OPERATIONS FLAP TEST IAW AMM 27-54-00-710-001, TESTED OK. ALSO CFDS SFCC 1 & 2 BITE TESTED OK IAW AMM 27-51-00. FLAPS WTB FAULT MSG CLEARED.Nov 10, 2015 · N805UA · Airbus A319131 · Trailing Edge Flap Control SystemSDR CALA2015021293136Connector · not seatedEMERGENCY LIGHT TEST FAILED WITH MSG EPSU INTERNAL LOAD EMER RT IAW TSM 33-51-00-810-807A. RESEAT CONNECTOR 12WL. GND OPERATIONS TESTED AMM 33-51-58 & NO DEFECTS NOTED.Feb 8, 2015 · N805UA · Airbus A319131 · Light System WiringSDR CALA2014062091305Warning System · false activationCOMPRESSOR VANE DISPLAYED ON UPPER ECAM SCREEN, ENG PARAMETERS NORMAL. OCCURRED DURING CLIMB OUT WAS JUST MOMENTARY. THEN REOCCURRED DURING TAXI-IN & REMAINED DISPLAYED. WORKED WITH LOCAL MAINTENANCE & FOUND FAULT ACRONYM B25TK IN FADEC. TROUBLESHOOTING ONJun 17, 2014 · N805UA · Airbus A319131 · Bleed Air Indicating SystemSDR CALA2014010790066Light · inoperativeDOOR 1L SLIDE LIGHTS INOPERATIVE IAW TSM 33-51-00 -810-808-A.Jan 6, 2014 · N805UA · Airbus A319131 · Emergency LightingSDR CALA2014010290019Starter · malfunctionedSTART FAULT DISPLAYED ON UPPER ECAM SCREEN ENG 2. ENG 2 START FAULT LO START AIR PRESS, CHECK BLD AIR SUPPLY NR 2, ITEM ROLLED FWD. NORMAL AIR PRESS BUT NO ROTATION. MX ATTEMPTED STICK START, REPORTED AIR BLEED LEAK UNDER COWL. REPLACED THE ENG NR 2 STARTDec 31, 2013 · N805UA · Airbus A319131 · Engine StarterSDR CALA2013111292851Actuator · faultyELAC 2 INOPERATIVE. ECAM F CTL ELAC 2 PITCH FAULT RESET TWICE CAME BACK AFTER 1 MIN EACH TIME. IAW TSM 27-93-00-810-836-A REPLACED PITCH TRIM ACTUATOR IAW AMM 27-44-57-000-001-A & GROUND CHECKED NORMAL.Nov 10, 2013 · N805UA · Airbus A319131 · Stabilizer Actuator
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