N486UA

Service difficulty reports · 108

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 = 'N486UA' 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 CALA2017032100674Battery · failedEMERGENCY LIGHT BATTERY AFT RIGHT FAILED CAPACITY CHECK. REPLACED BATTERY PER MM 33-51-39-0401.Mar 21, 2017 · N486UA · Airbus A320232 · Emergency LightingSDR CALA2017032100673Battery · failedEMERGENCY LIGHT BATTERY AT EMERG RIGHT FAILED CAPACITY CHECK. REPLACED BATTERY AT EMERG RIGHT PER MM 33-51-39-0401.Mar 21, 2017 · N486UA · Airbus A320232 · Emergency LightingSDR CALA2015081194196Coffeemaker · malfunctionedFORWARD GALLEY WORK LIGHT, CB TRIPPED G2, ELEC ODOR NOTICED. NOTE FWD GALLEY WORK LIGHT IS DEACTIVATED & COLLARED BLACK. FOUND ELEC ODOR COMING FROM FWD GALLEY COFFEE MAKER. REPLACED COFFEE MAKER, CHECKED OK.Aug 9, 2015 · N486UA · Airbus A320232 · Buffet/GalleysSDR CALA2014052791147Start Valve · faultyCREW REPORTS DURING NR 2 ENG START APU BLEED PRESS SHOWS ONLY 22 PSI, ENG DID NOT START, CYCLED APU BLEED SWITCH, PRESS RECOVERED TO 30 PSI BUT LATER DROPPED TO 20 PSI. UNABLE TO START ENG WITH START VLV FAULT, RESET A05 & Q4 0 CROSS BLEED START RESULTED IN SMay 23, 2014 · N486UA · Airbus A320232 · Engine Start Valves/ControlsSDR CALA2014052291127Frame · corrodedCORROSION FOUND ON FWD FACE ON FRAME 68 BETWEEN STRINGER 23R & 24R. REMOVED CORROSION AT FWD FACE OF FRAME. PERFORMED REPAIR AT FRAME 68 BETWEEN STRINGER 23R & 24R. REPAIR REQUIRES RE-INSP AT 36294 FC OR 78006 TOTAL FH WHICHEVER COMES FIRST IAW ECRA 5311-01May 21, 2014 · N486UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2014052291126Structure · corrodedAFT CARGO COMPARTMENT SHOW SIGNS OF CORROSION AT STRINGER 42R 6 INCHES AFT OF FRAME 64. PERFORMED LT ANGLE REPAIR AT AFT CARGO COMPARTMENT AT STRINGER 42R AFT OF FRAME 64 IAW SRM 53-00-13 FIG 203 SHEET 3. REPAIR IS A CATEGORY B REPAIR & REQUIRES RE-INSP AT 6May 21, 2014 · N486UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014052291125Structure · corrodedAFT CARGO COMPARTMENT SHOW SIGNS OF CORROSION AT STRINGER 42L BETWEEN FRAME 54 & FRAME 55. PERFORMED LT ANGLE REPAIR AT AFT CARGO COMPARTMENT STRINGER 42L BETWEEN FRAME 54 & FRAME 55 IAW SRM 53-00-13 FIG 205 SHEET 3. REPAIR IS A CATEGORY B REPAIR & REQUIRES May 21, 2014 · N486UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014052291124Structure · corrodedAFT CARGO COMPARTMENT SHOW SIGNS OF CORROSION AT STRINGER 42L JUST AFT OF FRAME 63. PERFORMED LT ANGLE REPAIR AT AFT CARGO COMPARTMENT STRINGER 42L JUST AFT OF FRAME 63 IAW SRM 53-0 0-13 FIG 203 SHEET 3. REPAIR IS A CATEGORY B REPAIR & REQUIRES RE-INSP AT 6May 21, 2014 · N486UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014052291122Skin · corrodedCORROSION AFT CARGO COMPARTMENT JUST AFT RT FRAME 57 UNDER FLOOR STRINGER 38. PERFORMED LT ANGLE REPAIR AT AFT CARGO STRINGER 42L BETWEEN FRAME 58 & FRAME 59 IAW SRM53-00-13 FIG 205 SHEET 3. REPAIR IS A CAT B REPAIR & REQUIRES RE-INSP AT 60000 FC & 75000 FH SMay 21, 2014 · N486UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2014052291111Stringer · corrodedAFT CARGO BAY SHOWS SIGNS OF CORROSION ON STRINGER 42R, 9 INCHES AFT OF FRAME 63. PERFORMED ANGLE REPAIR IAW SRM 53-00-13 FIG 203 SHEET 3 REPAIR IS A CAT B.May 19, 2014 · N486UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2014051991062Connector · unknownCEILING EMERGENCY LIGHT AT ROW 1 INOPERATIVE. TROUBLESHOOTING CEILING EMERGENCY LIGHT AT ROW 1 FOUND CONNECTOR & OPERATION CHECKED CEILING EMERGENCY LIGHT IAW AMM 33-51-11-400-001-A OPERATIONS CHECKED NORMAL.May 17, 2014 · N486UA · Airbus A320232 · Light System WiringSDR CALA2014051691032Structure · corrodedAFT CARGO COMPARTMENT SHOWS SIGNS OF CORROSION AT STRINGER 42L BETWEEN FRAME 58 & FRAME 59. PERFORMED LT ANGLE REPAIR AT AFT CARGO STRINGER 42L BETWEEN FRAME 58 & FRAME 59. THIS IS A CAT B REPAIR & REQUIRES INSPECTION AT 60000C AFTER REPAIR EMBODIMENT SUBSEQMay 15, 2014 · N486UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014051691031Structure · corrodedCORROSION AFT CARGO COMPARTMENT JUST AFT RT FRAME 57 UNDER FLOOR STRINGER 38. PERFORMED LT ANGLE REPAIR AT AFT CARGO STRINGER 42L BETWEEN FRAME 58 & FRAME 59 IAW SRM 53-00-13 FIG 202 SHEET 3. REPAIR IS A CAT B REPAIR & REQUIRES INSPECTION AT 60000 FC & 75000May 15, 2014 · N486UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014051391014Skin · damagedLEFT ELEV UPPER SURFACE HAS 6 FINDINGS FROM THERMOGRAPHY. LOCATIONS ARE 48 FROM INBD END & 20 FROM TE, 56 FROM INBD END & 21.5 FROM TE, 58 FROM INBD END & 14.25 FROM TE, 99.38 FROM OTBD END & 18 FROM TE, 53.5 FROM OTBD END & 6.5 FROM TE, 17 FROM LE & 6.5 FROMMay 10, 2014 · N486UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2014050990994Skin · damagedRIGHT ELEV HAS 4 FINDINGS FROM THERMOGRAPHY INSPECTION. 3 ARE ON UPPER SURFACE & 1 ON LWR SURFACE. UPPER SURFACE, 23.5 INCHES FROM INBD END & 8.5 INCHES FROM TE, 66.50 INCHES FROM OTBD END & 13 INCHES FROM TE, 18 INCHES FROM LE & 7.5 INCHES FROM TE & 1 LOWERMay 7, 2014 · N486UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2014050990993Skin · damagedLEFT ELEV UPPER SURFACE HAS 6 FINDINGS FROM THERMOGRAPHY. LOCATIONS ARE 48 INCHES FROM INBD END & 20 INCHES FROM TE, 56 INCHES FROM INBD END & 21.5 INCHES FROM TE, 58 INCHES FROM INBD END & 14.25 INCHES FROM TE, 99.38 INCHES FROM OTBD END & 18 INCHES FROM TE May 7, 2014 · N486UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2014012890257Epr System · faultedEPR MODE FAULT ENG 1 REFER TO TSM CHAPTER 77 ECAM & UAL A320 MEL CARD 73 120. ENG 1 EPR MODE FAULT DURING CLB. BOTH ENGS PUT INTO N1 MODE IAW CHECKLIST. NOTE ACFT HEALTH MONITORING ALSO SHOWS P2T2 SENS-HC -EEC1.Jan 24, 2014 · N486UA · Airbus A320232 · Engine Pressure Ratio (EPR)SDR CALA2013121293627Sense Line · crackedON INBD SIDE OF NR 1 ENG FOUND CRACKED LINE FOR 4.9 AIR SENSING, REPLACED LINE.Dec 11, 2013 · N486UA · Airbus A320232 · Fuel Controlling SystemSDR CALA2013112093102Fitting · crackedDOOR 2L HAS 4 INCH CRACK AT LOWER AFT INTERNAL FRAME CORNER FITTING.Nov 18, 2013 · N486UA · Airbus A320232 · Passenger/Crew DoorsSDR CALA2013110592648Relay · failedFLT CTL SEC 1 FAULT ECAM RAN CHECK LIST WOULD NOT RESET. LND DIST REQ LESS THAN 4000 FT. REPLACED RELAY 41CE1, RERACKED SEC1 & OPERATIONS CHECKED IAW MM. TESTED NORMAL, NO FURTHER FAULTS, OPERATIONS NORMAL.Nov 3, 2013 · N486UA · Airbus A320232 · Flight Control SystemSDR CALA2013102992492Skin Panel · delaminatedBELLY PANEL 191BB SHOWS LE DELAMINATION. INSTALLED TAPE IAW SRM 51-77-12 & PLACED ON CF.Oct 28, 2013 · N486UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2013100891867Valve · faultedNR 2 ENGINE HP VALVE FAULT DISPLAYED ON UPPER ECAM SCREEN. REPLACED NR 2 ENGINE HP VALVE IAW MM, OPS CHECKED GOOD.Oct 7, 2013 · N486UA · Airbus A320232 · Pneumatic Distribution SystemSDR CALA2013092791534Servo · faultedELEVATOR SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN. ITEM ROLLED FORWARD. REPLACED ENTIRE ELEVATOR SERVO, PCN 644-9014. REPLACED LT BLUE SYS ELEVATOR SERVO IAW MM & RIGGED IAW MM 27-34-00. OPERATIONS CHECKED GOOD.Sep 26, 2013 · N486UA · Airbus A320232 · Elevator Control SystemSDR UALA2013071504917Element · brokenMX STATUS MESSAGE AIR BLEED DISPLAYED ON THE LOWER ECAM SCREEN. FAULTED LT WING LOOP A. TROUBLESHOT IAW TSM 36-22-00 TO STEP 4A, 2. FOUND LOOP A RESISTANCE TO BE 2.1 MEG FROM BMC 1. TROUBLESHOT IAW AMM 36-22-16. PFR & BMC1 BITE SHOWS FAULT LT WING LOOP "AJul 15, 2013 · N486UA · Airbus A320232 · Fire DetectionSDR UALA2013070504688Cids · malfunctionedEMERGENCY CALL GOES OFF WITHOUT CREW INTERACTION. REPLACED CIDS 2 DIRECTOR.Jul 2, 2013 · N486UA · Airbus A320232 · Audio Integrating SystemSDR UALA2013050203075Slide · faultyREPLACE NR 1R EVAC SLIDE. SLIDE AT DOOR 1R WAS MR25823, DASH OFF 2258. REPLACED SLIDE ASSY AS PER MM 25-62-44, OPS CHECKED GOOD. EMERGENCY LIGHT CONNECTOR ATTACHED AND ROUTED, NORMAL ECAM WARNINGS, EMERGENCY LIGHT TESTED OK. ACCOMPLISHED INSPECTION OF SLIDApr 30, 2013 · N486UA · Airbus A320232 · Escape SlideSDR UALA2013012400412Windshield · faultyL1 WINDOW HAS A FLAW BOTTOM 2 INCHES DISTORT VIEW. CONFIRMED BY BOTH PILOTS. MAINT TEXT: AFTER DE-BRIEF THE CREW THEY STATED IT DOES OBSTRUCT VIEW AND IS DISTORTED. INSTALLED L1 WINDOW PER AMM.Jan 24, 2013 · N486UA · Airbus A320232 · Flight Compartment WindowsSDR UALA2013011100185Wheel · vibrationNOSE WHEEL SHIMMY ON LANDING SLOWING THRU 80-70 KNOTS. REMOVED AND REPLACED LEFT AND RIGHT NOSE WHEELS.Jan 10, 2013 · N486UA · Airbus A320232 · Wheel/Ski/FloatSDR UALA2013011100193Controller · failedCAPTAIN'S WINDSHIELD HEAT IS INOPERATIVE. REPLACED NR 1 WHC PER MM 30-42-34. L WINDSHIELD OPS CHECKED NORMAL. RECONFIGURE LT WINDSHIELD CONNECTOR TO READ SPARE SENSOR PER TSM 30-42-00-810-801-A. FURTHER REFERENCE MT30-003. COMPLETED NR 1 WINDOW INSTALLATION.Jan 10, 2013 · N486UA · Airbus A320232 · Windshield/Door Rain/Ice RemovalSDR UALA2013010900135Controller · inoperativeLEFT WINDSHIELD HEAT INOPERATIVE AT UPPER ECAM SCREEN. ACCOMPLISHED TBS 30-42-00-81 0-801-A. SWAPPED WHC 1 WITH WHC 2. CONFIRMED WHC (3DG1) FAULTY. INSTALLED WHC'S TO THE ORIGINAL POSITION. REPLACED NR 1 WHC PER MM 30-42-34. LEFT WINDSHIELD OPS CHECKED NJan 7, 2013 · N486UA · Airbus A320232 · Windshield/Door Rain/Ice RemovalSDR UALA2013010700090Sensor · failedCAPTAIN'S WINDSHIELD HEAT IS INOP. PFR SHOWS LEFT WINDSHIELD SENSOR FAILED. INSTALLED JUMPER HARNESS, WINDOW HEAT NOW OK.Jan 5, 2013 · N486UA · Airbus A320232 · Ice/Rain Protection SystemSDR UALA2012111306530Seal · looseHIGHER THAN NORMAL WIND NOISE CAPT L3 WINDOW. SAMC TEXT: PERFORM REPAIR PER AMM 56-11-12-300-002-A, USE PCN 841-0098 (B 1-6TH SEALANT), AIRBUS MATERIAL 09-045. GPM REF 6-0- 00-028, PG 49. USE HEAT GUN TO ACCELERATE CURE TIME. REPAIRED L3 WINDOW WEATHER SEANov 12, 2012 · N486UA · Airbus A320232 · Flight Compartment WindowsSDR UALA2012081304402Battery · inoperativeEMERGENCY LIGHT TEST, 'EPCS L FWD' DISPLAYED. REPLACED BATTERY 10WL AND TESTED OKAY.Aug 10, 2012 · N486UA · Airbus A320232 · Emergency LightingSDR UALA2012081004345Visor · damagedCAPTAINS SUN VISOR DEFECTIVE, FELL OUT OF SOCKET ON FIRST MOVEMENT. REINSTALLED CAPTAINS SUN VISOR INTO THE SOCKET AND SECURED. OPS CHECKED GOOD.Aug 8, 2012 · N486UA · Airbus A320232 · Flight Compartment EquipmentSDR UALA2012070903696Valve · leakingLARGE HYDRAULIC LEAK COMING FROM AFT WING TO BODY FAIRINGS LT AND RT AND CENTER. ALSO COMING FROM GEAR DOORS. LOCATED LEAK CLEAN AREA. REPLACED YELLOW SYSTEM PRIORITY VALVE. SERVICED YELLOW SYSTEM TO HALF FULL FOR ACCOMPLISHING LEAK CHECK.Jul 7, 2012 · N486UA · Airbus A320232 · Hydraulic System, MainSDR UALA2012061503297Fan · faultyBURNING ODOR IN COCKPIT AMBER FAN INDICATION ON COND PAGE. WHEN ODOR OCCURRED HAD LEFT FAN AMBER INDICATOR ON COND PAGE. RAN PACKS TO DISSIPATE SMELL. TURNED FAN SWITCH BACK ON AND NO FURTHER ELECRICAL ODOR. REPLACED LEFT CIRCULATION FAN. NO FAULT OR ECAJun 12, 2012 · N486UA · Airbus A320232 · Air Distribution FanSDR UALA2012061103181Transmitter · failedCAPTAIN NOSE TILLER BINDS AND STICKS IN POSITION WITHOUT RECENTERING. REPLACED TRANSMITTER UNIT ASSY IAW MM 32-51-11, OPS GOOD.Jun 6, 2012 · N486UA · Airbus A320232 · Landing Gear Steering SystemSDR UALA2012040602145Tail Cone · crackedNR 1 EXHAUST TAIL CONE HAS A CRACK AT 10 O'CLOCK POSITION APPROX 6 INCHES LONG. FOUND CRACK TO BE 4.5 INCH LONG, STOP DRILLED CRACK.Apr 5, 2012 · N486UA · Airbus A320232 · Engine Collector/Tailpipe/NozzleSDR UALA2011121906977Battery · dischargedEPSU BAT R MESSAGE FOUND DURING EEL TEST. REPLACED RT OVERWING EPSU BATTERY.Dec 17, 2011 · N486UA · Airbus A320232 · Emergency LightingSDR UALA2011082204486Rub Strip · damagedLT WING OUTBOARD AFT FLAP METAL RUBSTRIP TORN & PEELING OFF ON TOP AFT INNER SECTION OF FLAP, OUTBOARD OF NR 1 ENG. 1' X 2' SECTION. ACP INTERIM REPAIR WITH METAL SPEED TAPE. REFERENCE MT 57-003 TO USE B AND 1-6TH SEALANT TO REINSTALL STRIP. RUBSTRIP PCN 11Aug 20, 2011 · N486UA · Airbus A320232 · Trailing Edge FlapsSDR UALA2011062703141Actuator · malfunctionedLEFT GREEN ELEVATOR POSITION TRANSDUCER 34 CE1 TRANSDUCER FAULT. ELAC 2 PITCH FAULT DISPLAYED AFTER ENG START. PFR FAULTING POS TRANSDUCER 34CE 1. SWAPPED TO SPARE TRANSDUCER ON ELEVATOR SERVO CONTROL. ACCOMPLISHED SUCCESFUL EFCS TEST AND AUTOLAND TEST. REJun 26, 2011 · N486UA · Airbus A320232 · Elevator Control SystemSDR UALA2011040401615Insulation · damagedAFT CARGO DOOR ECAM, RTFL. CURRENT LEG REPORT IS FAULTING AFT CARGO DOOR SAFETY MECH PROX SENSOR 32WV TGT POS. VISUAL INSPECTION OF MECHANICAL SHOWS NO IRREGS. DEFFERED PER MEL. FOUND INSULATION DAMAGED ON HARNESS TO SENSOR 32WV, DOESNT APPEAR TO HAVE ANY Apr 2, 2011 · N486UA · Airbus A320232 · Door System WiringSDR UALA2011032101361Transducer · faultyNR 2 ENG VIBRATION, RTFL. PERFORMED TRANSIENT ACOUSTIC PROPAGATION TEST OF NR 2 ENG LP COMPRESSOR FAN BLADES PER AMM. ALL BLADES FOUND WITHIN LIMITS. NR 2 ENGINE, REMOVED INLET CONE AND FAIRING FOR INSPECTION OF BLADE RETAINING RING. CHECKED TORQUE OF BLADMar 21, 2011 · N486UA · Airbus A320232 · Engine Vibration AnalyzerSDR UALA2011022500950Tiller · obstructedCAPTAIN'S NOSE WHEEL STEERING HANDWHEEL INOPERATIVE. CAPTAIN'S TILLER STIFF AND BINDING. SLOW TO CENTER. REPOSITIONED COCKPIT INTERIOR PANEL FOR PROPER CLEARANCE WITH CAPTAIN'S TILLER KNOB.Feb 24, 2011 · N486UA · Airbus A320232 · Steering UnitSDR UALA2010030800792Connector · damagedEPSU INT LOAD AFT LT FAULT ON CIDS TEST. TROUBLESHOOTING NARROWED FAULT DOWN TO FAILED EMERGENCY LIGHT CONNECTOR WHICH WAS GROUNDING OUT INSIDE SEB HOLDING COMPARTMENT UNDER ROW 27ABC. NEED NEW WIRE HARNESS, PROTECTED EXPOSED END & STOWED INSIDE NOTED COMPARMar 7, 2010 · N486UA · Airbus A320232 · Light System WiringSDR UALA2009070801966Engine · hung startENG 1 HUNG START TWICE WITH START FAULT USING AUTO AND MANUAL START, APU DUCT PRESS NORMAL, GOT GOOD N2 INDICATION BUT NO N1.Jul 7, 2009 · N486UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR UALA2008112506664Battery Pack · inoperativeFWD BATTERY PACK INOP ON PSU 10WL. REPLACED BATTERY PACK, CHECKED OK.Nov 24, 2008 · N486UA · Airbus A320232 · Emergency LightingSDR UALA2008112406641Light · missingSEAT 4A IS MISSING ONE OF TWO SEAT MOUNTED ELECTROLUMINESCENT. RELAMPED 4A, OPS CHECK OKAY.Nov 24, 2008 · N486UA · Airbus A320232 · Emergency LightingSDR UALA2008112406631Wire Harness · shortedEMERGENCY LIGHTS FAIL TEST. SHOWS EPSU INT LOAD EMER L. FOUND SHORT O GROUND CONNECTOR 11WL SOCKET "T" REF AWM 33-51-04, CHASING WIRES. FOUND HARNESS SHORTED AT SEAT 22. REPLACED LIGHT ASSY, CHECKED OK.Nov 23, 2008 · N486UA · Airbus A320232 · Light System WiringSDR 2008UALA01026Control Unit · defectiveF-CTL ELEV SERVO FAULT ECAM AFTER T/O. EXCESSIVE PLAY IN ROD END CONNECTOR(S). REPLACED LT BLUE ELEVATOR SERVO CONTROL UNIT (34CE3), TESTS GOOD.Feb 24, 2008 · N486UA · Airbus A320232 · Elevator Control System
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