N441UA

Service difficulty reports · 81

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 = 'N441UA' 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 UALA2011081204254Panel · erodedBELLY PANEL 191BB LE EROSION. APPLIED FILLER TO AREA OF EROSION.Aug 12, 2011 · N441UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR UALA2011071503595Structure · damagedFOUND TWO AREAS ON NR 1 ENG OTBD REVERSER HALF WHERE LIGHTNING EXITED AIRCRAFT. MARKED BY BURN MARKS AND SHREDDED GRAPHITE CLOTH. ALSO NOTED SEVERAL BURNED RIVETS ON REVERSER HALF. SUPPLEMENTAL DATA UPDATE REMOVED TRANSCOWL. FOUND 6 BAD HINGES. REMOVED BLOCKEJul 15, 2011 · N441UA · Airbus A320232 · Engine Thrust ReverserSDR UALA2011070803401Leg Assy · damagedNEED TO REMOVE AND REPLACE NLG LEG ASSY IAW AMM DUE TO IMPACT DAMAGE. REMOVE AND REPLACE NLG LEG ASSY IAW AMM DUE TO IMPACT DAMAGE. REMOVED NLG LEG ASSMBLY. NEED TO INSTALL NEW LEG ASSMBLY. INSTALL SEALANT ON NLG TRUNNION PIN RETAINER BOLT HEAD AND NUT, ANJul 6, 2011 · N441UA · Airbus A320232 · Nose/Tail Landing Gear Strut/AxleSDR UALA2011062403107Skin · damagedDOOR 1L DAMAGED. REMOVED DOOR SKIN PANEL. BACK DRILLED, COUNTERSUNK, AND TRIMMED SKIN PANEL. REPAIRED BENT AREAS. ATTACHED RUB STRIP TO SKIN PANEL. RII INSP ACCOMPLISHED NO DEFECTS. STARTED INSTALLATION OF SKIN PANEL. COMPLETED INSTALLATION OF SKIN PANEL.Jun 24, 2011 · N441UA · Airbus A320232 · Passenger/Crew DoorsSDR UALA2011062303099Nose Cowl · damagedNR 1 NOSE COWL DAMAGED AT 8 O'CLOCK POS. REPLACED NOSE COWL.Jun 22, 2011 · N441UA · Airbus A320232 · Nacelle/Pylon, Main FrameSDR UALA2011060202685Skin · damagedDURING HAIL INSPECTION FOUND UPPER SURFACE LEFT STABILIZER PANEL 334BT HAS 2 DENTS. ONE DENT 11 INCHES FROM INBD EDGE, 6 INCHES FROM TRAILING EDGE. DENT IS .5 INCH DIA BY .018 INCH DEEP. 2ND DENT IS 17 INCH FROM INBD EDGE AND 5.5 INCH FROM TRAILING EDGE. DMay 31, 2011 · N441UA · Airbus A320232 · Horizontal Stabilizer, Plate/SkinSDR UALA2011042502011Lens · missingSLIDE ARMED LENS MISSING LT OVERWING EMER EXIT. REPLACED LENS.Apr 23, 2011 · N441UA · Airbus A320232 · Emergency EquipmentSDR UALA2011042001909Blade · damagedDUE TO FAN BLADE NR 21 WAS DAMAGED, REPLACED. NR 2 ENG S-N V10523 LPC BLADE 21 MOMENT WT 2498.0 AND PERFORMED VIB SURVEY REF MM. PEAK VIB .7 N1 AND .2 N2. OPERATIONAL TEST NORMAL.Apr 19, 2011 · N441UA · Airbus A320232 · Turbine Engine Compressor SectionSDR UALA2010031500853Uplock · malfunctionedNLG ISSUE, RTFL. REPLACED NOSE RETRACT ACTUATOR. CYCLED ALL GEAR THROUGH 2TWO COMPLETE CYCLES AND CYCLED NOSE GEAR AN ADDITIONAL NINE TIMES. ALL INDICATIONS NORMAL IN FLIGHT DECK. REPLACED BOTH LG CIU 1 & 2 IAW MM. REPLACED LANDING GEAR SAFETY VALVE. REPLACEDMar 13, 2010 · N441UA · Airbus A320232 · Landing Gear Retraction/Extension SystemSDR UALA2009042701200Structure · damagedINSTALLED TWO NEW DOUBLERS WITH ZERO TIMED HOLES PER COA407081 REF DRAWING 60N00001. ACP COA 407081.Apr 25, 2009 · N441UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2009031000743Battery · dischargedAFT LT EMERGENCY POWER SUPPLY FAILURE. REPLACED THE EPSU BATTERY UNIT, OPS CHECKED OK.Mar 9, 2009 · N441UA · Airbus A320232 · Emergency LightingSDR 2008UALA06319Skin · damagedFOUND LIGHTNING STRIKE HOLE THROUGH SKIN ABOVE F/O STATIC PORT, REQUIRES PLUG REPAIR. STRINGER HAS DAMAGE WILL REQ REPLACEMENT.Oct 29, 2008 · N441UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2008UALA05547Regulator · leakingCREW OXYGEN SYSTEM LOW. RECORD PRESSURE PRIOR TO SERVICING. FOUND O2 REGULATOR - TRANSMITTER LEAKING AT FILL PORT. REPLACED REGULATOR - TRANSMITTER. FOUND LOOSE B-NUT AT 1ST OBSERVER'S 02 BOX. SECURED LINE. SERVICED O2 TO 1890 PRIOR TO DEPARTURE. Sep 1, 2008 · N441UA · Airbus A320232 · Crew Oxygen SystemSDR 2008UALA03912Frame · dentedFUSELAGE DENT FRAME 30 STRINGER 25R. *S/D* ACCOMPLISHED MAJOR REPAIR AT LCQ. INSTALLED DOUBLER REPAIR PER SRM 53-21-11 FIG 215.Jul 17, 2008 · N441UA · Airbus A320232 · Fuselage Main, FrameSDR 2008UALA03911Skin · dentedFOUND 2 DENTS AT SECTION FR23 AT FLOOR LEVEL ON LEFT SIDE OF AIRCRAFT. *S/D* ACCOMPLISHED MAJOR REPAIR AT IAD. CLEANED AREAS, CHECKED FOR CRACKS, NONE FOUND. TREATED AREAS, PRIMED AREAS, PAINTED AREAS. OK PER SRM 53-00-11.Jul 17, 2008 · N441UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2008UALA03873Frame · corrodedR2 DOOR SILL CORROSION AT FASTENER HOLE FRAME 66. *S/D* ACCOMPLISHED MAJOR REPAIR AT LCQ. INSTALLED REPAIR PER SRM 53-41-14.Jul 14, 2008 · N441UA · Airbus A320232 · Fuselage Main, FrameSDR 2008UALA02997Seal · damagedLANDING GEAR FAILED TO RETRACT. RTFL. FOUND NOSE STRUT SEALS DAMAGED. REPLACED NOSE STRUT SEALS, SERVICED STRUT. NO REPEATS.May 26, 2008 · N441UA · Airbus A320232 · Nose/Tail Landing Gear Strut/AxleSDR 2008UALA02705Blade · failedNR 2 ENGINE STALL. AMBER DECLARED, FLIGHT DIVERTED. ENGINE REPLACED. FOUND HPC 6TH STAGE BLADE FAILURE.May 11, 2008 · N441UA · Airbus A320232 · Turbine Engine Compressor SectionSDR 2008UALA01595Connector · dirtyFLIGHT DIVERTED DUE TO AFT CARGO DOOR INDICATION PROBLEM. POSSIBLE DIRTY CONNECTOR. CLEANED AND SECURED AFT CARGO INDICATION CONNECTOR, ALL FAULTS CLEARED AND NO FURTHER DEFECTS NOTED, OPENED & CLOSED DOOR SEVERAL TIMES WITH NO DEFECTS, AFT CARGO DOOR WARNINMar 21, 2008 · N441UA · Airbus A320232 · Door System WiringSDR 2008UALA00959Oxygen System · low pressureTHE O2 NEEDS SERVICING. SHOWS 1420 PSI. SERVICED CREW O2 LEVEL TO FULL.Feb 21, 2008 · N441UA · Airbus A320232 · Crew Oxygen SystemSDR 2007UALA04769Handle · malfunctionedON DEPARTURE, GEAR HANDLE WAS LOCKED IN DOWN POS FOR APPROX 5 SEC AFTER ACHIEVING POS CLIMB. BROKEN LINK ON UPPER GEAR DOOR CAUSING THE DOOR TO BIND WHEN MOVING TO STOW. REPAIRED BROKEN LINK. SERVICED STRUT ASSY, ACCOMPLISHED GEAR SWINGS, ALL SYSTEMS OPERNov 20, 2007 · N441UA · Airbus A320232 · Landing Gear SelectorSDR 2007UALA01007Line · leakingFLIGHT DIVERTED DUE TO LOSS OF GREEN HYD SYSTEM. A/C TOWED TO GATE. [SUP 06-01-07] FOUND A CRACKED HYDRAULIC LINE LEADING TO THE THRUST REVERSER MANUAL ACTUATION CONTROL VALVE IN THE NR 1 ENGINE PYLON. MANUFACTURED AND INSTALLED A NEW LINE. REPLACED HP AND Apr 1, 2007 · N441UA · Airbus A320232 · Hydraulic System, MainSDR 2007UALA00420Wire Harness · misroutedDOOR 1R MED EVACUATION SLIDE ELECTRICAL HARNESS IS INCORRECTLY ROUTED. [SUP 05-16-07] REINSTALLED ELECTRICAL HARNESS CORRECTLY. SLIDE IS ORIGINAL EQUIPMENT FROM WHEN AIRCRAFT WAS DELIVERED AND THERE IS NO EVIDENCE OF THE SLIDE EVER BEING SERVICED TO THE EXTEFeb 12, 2007 · N441UA · Airbus A320232 · Equipment/Furnishings WiringSDR 2005UALA01177Blade · wornENGINE 2 STALL DISPLAYED ON UPPER ECAM SCREEN DURING CLIMB OR CRUISE ACCELERATION. ENGINE NOT SHUTDOWN. STALL DISPLAYED ON UPPER ECAM SCREEN AFTER POWER REDUCTION FROM T/O POWER. ENGINE NOT SHUT DOWN. TROUBLESHOOTING BORESCOPE INSPECTION REVEALED OUT-OF-LIOct 22, 2005 · N441UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2005UALA00952Floor Support · corrodedCORROSION AT AFT GALLEY FLOOR SUPPORT 66-70.Sep 8, 2005 · N441UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2005UALA00565Hose · brokenTHE HOSE WAS FOUND BROKEN BY ASPIRATOR DURING THE UNPACKING PROCESS. DURING UNPACKING OF THE SLIDE IN THE SHOP, THE HOSE WAS FOUND BROKEN FROM PLATE. THE PROBABLE CAUSE IS KINKED ROUTING OF THE HOSE DURING THE PREVIOUS PACKING OF THE ASSEMBLY. THE CONTINUESJun 13, 2005 · N441UA · Airbus A320232 · Escape SlideSDR 2005UALA00267Idg · shutdownAPU AUTO SHUTDOWN WITH THE NR 2 IDG DEFERRED. REPLACED PRECAUTIONARY PER SFOLM THE APU OIL PRESS SWITCH, OIL SUMP TEMP SENSOR, OIL LEVEL SENSOR, AND ECB. RAN APU ON GROUND FOR ONE HOUR WITH ELEC AND PNEU LOADS NO AUTO SHUTDOWNS. APU HAD 2 PREVIOUS GRND ASD. Mar 26, 2005 · N441UA · Airbus A320232 · Airborne Auxiliary Power Unit (APU) SystemSDR 2004UALA00546Check Valve · inoperativeRETURN TO FIELD UNDER AMBER ALERT DUE TO LOSS OF YELLOW HYDRAULICS. YELLOW HYDRAULIC SYSTEM PUMP CHECK VALVE FAILED. REPLACED CHECK VALVE.Jun 6, 2004 · N441UA · Airbus A320232 · Hydraulic System, MainSDR 2002UALA00132Carbon Seal · leakingNR 1 ENGINE HAD INFLIGHT SHUTDOWN DUE TO LOSS OF OIL QUANTITY AND DECREASE IN OIL PRESSURE. AFTER SHUTDOWN ENGINE WINDMILLED FOR 35 MINUTES, OIL TEMPERATURE 110-115, OIL PRESSURE 9.5 PSI AND OIL QUANTITY ZERO. INTERFACE BETWEEN FUEL PUMP AND MAIN ENGINE GEARJan 21, 2002 · N441UA · Airbus A320232 · Turbine Engine Accessory DriveSDR 99UAL900127Power Supply · inopEMERGENCY LIGHT TEST FAILS WITH EPSU INT LOAD R MESSAGE. *S/D* INTERNAL LOAD FAULT WAS DETECTED AT THE EMERGENCY POWER SUPPLY UNIT (12WL). THE EMERGENCY POWER SUPPLY UNIT AND ITS BATTERY WERE THEN REPLACED.Feb 21, 1999 · N441UA · Airbus A320232 · Emergency LightingSDR 98UAL900005Torque Links · disconnectedNLG TORQUE LINKS DISCONNECTED UPON LANDING. NLG TIRES ROTATED 180 DEGREES DURING A SLOW LEFT TURN FOLLOWING LANDING ROLL-OUT.Jan 8, 1998 · N441UA · Airbus A320232 · Nose/Tail Landing Gear
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