N475UA

Service difficulty reports · 125

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 = 'N475UA' 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 CALA2022012700253Frame · crackedA3NB-53-3-6132 RH FWD EMREGENCY EXIT DOOR RH I/B BEAM FRAME CRAC KED DOT 42-055. () PERFORMED HFEC SURFACE INSPECTION ON DOOR WITH SERIAL NO VH4011 BY EMP#V936054 AT BFM AEROSPACE MOBILE NR#0020651. IAW NTM 51-10-08. CRACK INDICATIONS NOTED AROUND FASTENERS REJan 27, 2022 · N475UA · Airbus A320232 · Emergency ExitsSDR CALA2022012600249Frame · cracked(AD2020-18-06) DURING ROTO INSPECTION OF THE FRAME FOOT AT FR43 RH SIDE. CRACK INDICATION WAS NOTED AT FASTENER HOLE. REPAIR NEF ORE NEXT FLIGHT. () REPAIRED RH FR43 RH IAW UAL EA 5330-06692 OPT 1 & R DWG R5337023 3. ACCOMPLISHED BY EMP#V935774 AT BFM ST AEROSJan 26, 2022 · N475UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2022012600240Frame · crackedA3NB-53-3-6132 RH FWD EMERGENCY EXIT DOOR LH I/B BEAM FRAM CRACK ED DOT 42-054 () RH FWD EMERGENCY EXIT DOOR LH I/B REMOVED ANGLE CRACKED IAW SRM 51-42-11/001 AND INSTALLED NEW ANGLE IAW SRM 51-42-11/001 PN#D52 237902620451 BATCH#0003892709 PAINTED AS NEED IAWJan 26, 2022 · N475UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2022012000198Gusset · damaged(A3NB-53-4-0033) DURING ROTO INSPECTION OF RH FR66 STGR12 GUSSET PLATE. REJECTABLE DAMAGE WAS NOTED IN BOTTOM HOLE DUE TO MECHAN ICAL DAMAGE IN ALL LAYERS WITH OVER 75% SH. CIRCLED IN RED.() DURING ROTO INSPECTION OF RH FR66 STGR 12 GUSET PLATE REJECTABLE MOBIJan 20, 2022 · N475UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2022012000196Gusset · damaged(A3NB-53-4-0033) DURING ROTO INSPECTION OF GUSSET PLATE RH FR68 STGR14 REJECTABLE DAMGE NOTED IN LWR TWO HOLES & STGR16 UPER AND LAST TWO LWR HOLES DUE TO MECHANICAL DAMAGE IN ALL LAYERS WITH OVER 75% SH. CIRCLED IN. DURING ROTO INSPECTION OF GUSSET PLAE RH FRJan 20, 2022 · N475UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2022011800182Shear Tie · corroded(A3NB-5321-1-2706) 2EA SHEAR TIES/CLEATS FR30 STR40R-42R ARE COR RODED (REPLACE SHEAR TIES/CLEATS) REMOVED AND REPLACED (2EA) SHEAR TIES ON FR30 STGR 40R TO 42R IA W A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V928493 AT BFM ST AEROS PACE MOBILE NR#0020647Jan 18, 2022 · N475UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2022011800178Shear Tie · corroded(A3NB-5321-1-2706) 2EA SHEAR TIES/CLEATS FR33 STR40R-42R ARE COR RODED (REPLACE SHEARTIES/CLEATS.) REMOVED AND REPLACED (2E) SHEARTIES ON FR33 STGR 40R TO 42R IAW A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V928493 AT BFM ST AEROSPA CE MOBILE. NR#0020645Jan 18, 2022 · N475UA · Airbus A320232 · Aerodynamic FairingsSDR CALA2022011800177Shear Tie · corroded(A3NB-5321-1-2706) 2EA SHEAR TIES/CLEATS FR31 STR 40R-42R ARE CO RRODED (REPLACE SHEAR TIES/CLEATS.) REMOVED AND REPLACED (2EA) SHEAR TIES ON FR 31 STRG 40R TO 42R I AW A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V928493 AT BFM ST AERO SPACE MOBILE. NR#0020646Jan 18, 2022 · N475UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2022011400149Shear Tie · corroded(A3NB-05-3-6013) FWD CARGO COMPT: FR33 BETWEEN STR42 LH AND STR4 2 RH HAS CORROSION EVIDENCE. DOT 61-081. REMOVED SHEAR TIE FR33 BETWEEN STR43CL AND REPLACED BY SHEAR TIE 3. FABRICATED ON VTMAE TRAVELER#T21/1592356, INSTALLED NEW SHEAR TI E P/N UAD532303992000Jan 13, 2022 · N475UA · Airbus A320232 · DoorsSDR CALA2022011400146Seat Track · corroded(A3NB-53-3-6038) FLOOR MAIN CABIN SEAT TRACK OUTBOARD RH BETWEEN FR 19 AND FR 20 HAS CORROSION. DOT 61-071 () EVALUATED SEAT TRACK Y-1292 OUTBOARD RH BETWEEN FR19 AND FR20 WI 936040 AT BFM ST AEROSPACE MOBILE. NR#0020359. TH CORROSION ON HARD POINT AREA AND WJan 13, 2022 · N475UA · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2022011000094Frame · corroded(SUPPORT TASK) AFT CABIN SUPPORT FRAME BETWEEN FR69-FR70 STGR23R IS CORRODED. () REMOVED AFT CABIN SUPPORT IAW SRM 51-42-11 LOCATED AND DRILLED N EW PART IAW SRM 51-44-11 INSTALLED NEW PART IAW SRM 51-42-11 RES TORED SURFACE PROTECTION IAW SRM 51-23-11. ACCOMPJan 9, 2022 · N475UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2022011000093Beam · corrodedA3NB-53-3-6279 AFT GALLEY FLOOR SUPPORT BEAM Y765 AT FR70 HAVE C ORROSION DOT 42-019 EVALUATED AFT GALLEY FLOOR SUPPORT BEAM Y765 AT FR70 WITH CORROS ION OUT OF LIMITS DIM L=1.782, W=1.516, REMAIN THICKNESS 0.3, RE MOVED AND REPLACED FOR NEW BEAM IAW SRM 51-42Jan 9, 2022 · N475UA · Airbus A320232 · Nacelle/Pylon StructureSDR CALA2018122002622Skin · contaminatedLH UPPER SURFACE, FOUND FLUID ENTRAPMENT AT 22 INCHES FROM I/B E DGE AND 5.5 INCHES FROM TRAILING EDGE. DEFECT IS 5"X3.5" IN SIZE PER HAECO LCQ NR 9292260 GENERATED BY V916887 A3NB-55-4-6016 UPON EVAL OF LH ELEVATOR UPPER SURFACE 22 IN FROM I/B 5.5 IN FROM T/EDec 20, 2018 · N475UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2018122002621Skin · contaminatedLH UPPER SURFACE, FOUND FLUID ENTRAPMENT AT 19.75 INCHES FROM I/ B EDGE AND 3.5 INCHES FROM TRAILING EDGE. DEFECT IS 2"X1.5" IN S IZE AD RELATED TASK 2017-22-03 PER HAECO LCQ NR 9292258 GENERATE D BY V916887 UPON EVAL OF LEFT ELEVATOR UPPER SURFACE 19.75 IN FRDec 20, 2018 · N475UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2018122002620Skin · contaminatedLH UPPER SURFACE, FOUND FLUID ENTRAPMENT AT 18.5 INCHES FROM I/B EDGE AND 6.25 INCHES FROM TRAILING EDGE. DEFECT IS 4.75"X4" IN SIZE AD RELATED TASK 2017-22-03 PER HAECO LCQ NR 9292259 GENERAT ED BY V916887 A3NB-55-4-6016 UPON EVALUATION OF LEFT ELEVATOR UPPERDec 20, 2018 · N475UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2017080802570Battery · failedEMER EXIT BATTERY AT LT OVERWING EXIT FAILED CAPACITY CHECK. REPLACED BATTERY REF AMM 33-51-38 OPS CHECKED OK.Aug 8, 2017 · N475UA · Airbus A320232 · Emergency LightingSDR CALA2016120901064Battery Pack · faultedEPSU UNIT EMEREMERGENCY LIGHT FAULT ON PTP. REPLACED EMERGENCY LIGHT BATTERY AT 21D. OPS CHECKED NORMAL.Dec 9, 2016 · N475UA · Airbus A320232 · Emergency LightingSDR CALA2016120901063Battery Pack · faultedEPSU BATTERY FWD LIGHT FAULT ON PTP. REPLACED THE EMERGENCY LIGHT BATTERY . OPS CHECKED NORMAL.Dec 9, 2016 · N475UA · Airbus A320232 · Emergency LightingSDR CALA2015051593781Slat · dentedRIGHT WING NR 1 SLAT HAS A DENT APPROX 3" WIDE X 2" TALL, CHORD WISE X .025" DEPTH. DENT IS APPROX 25" IN FROM OTBD SIDE OF SLAT. REMOVED EXISTING REPAIR, CUT OUT DAMAGE & INSTALLED REPAIR PARTS IAW SRM 57-54-00 REPAIR 5G.May 14, 2015 · N475UA · Airbus A320232 · Leading Edge DevicesSDR CALA2013123194061Inlet Bullet · damagedNR 2 ENG RUBBER SPINNER CAP MISSING. R & R INLET CONE ON NR 2 ENG.Dec 30, 2013 · N475UA · Airbus A320232 · Turbine Engine Air Inlet SectionSDR CALA2013120593492Valve · faultyAFTER LANDING ON TAXI, PARKING BRAKE WOULD NOT RELEASE. TRIPLE INDICATOR SHOWING 3000 PSI LT & RT REGARDLESS OF PARKING BRAKE SWITCH POSITION. REPLACED PARKING BRAKE VLV IAW AMM, OPERATION & LEAK CHECKED GOOD.Dec 4, 2013 · N475UA · Airbus A320232 · Landing Gear Brake SystemSDR CALA2013112093126Handset · defectiveAFT CABIN HANDSET INOPERATIVE. CAN TRANSMIT, BUT NOT RECEIVE. TROUBLE SHOT & FOUND AFT ATTENDANTS HANDSET BAD, MFG ST3100-23-10, PCN 582-0042, PARTS 582-0042 & ST3100-23-10U3 HANDSET.Nov 20, 2013 · N475UA · Airbus A320232 · Interphone/Passenger Announcement (PA) SystemSDR CALA2013112193156Amu · faultyTHE FWD & AFT FLIGHT ATTENDANT INTERPHONE HAS HIGH STATIC & WHEN THE FWD FLIGHT ATTENDANT TRIES TO TRANSMIT THE TRANSMISSION SHORTS TO THE PA SYSTEM. SWAPPING HANDSETS BETWEEN THE FWD & AFT CABIN, NO HELP. RESETTING THE AMU IS NO HELP. REPLACED AMU, BOTH HANov 19, 2013 · N475UA · Airbus A320232 · Interphone/Passenger Announcement (PA) SystemSDR CALA2013100791761Stringer · corrodedCORROSION FOUND ON STRINGER 42L BETWEEN FRAMES 63-64 IN AFT CARGO. R & R STRINGER IAW SRM 51-42-11.Oct 4, 2013 · N475UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2013092391325Skin · corrodedLT WING TANK PLATE LANDING AT 540PB HAS CORROSION IN FASTENER HOLE THAT IS OUT OF LIMITS. REAMED, BUSHED & INSTALLED BRIDGE PLATE IAW SRM 57-21-11 FIG 202.Sep 22, 2013 · N475UA · Airbus A320232 · Wing, Plate/SkinSDR CALA2013092391324Skin · dentedNR 2 ENG INLET COWL UPPER INBD LIP EXTERIOR SKIN HAS DENT 2 O'CLOCK. MEASURE DENT NR 2 ENG INLET COWL UPPER LIP AT 2 O'CLOCK WITH DEPTH GAGE TLC 2815 .023" & 8.0" TO NEAREST RIVET SRM 54-10-00 FIG 101 DENT REQ INSP 6000FH, 4500 FC, R 20 MONTHS SRM 54-10-00 FISep 20, 2013 · N475UA · Airbus A320232 · Nacelle/Pylon, Plate/SkinSDR CALA2013092091320Sill · corrodedR2 DOOR SILL CORRODED AT FR68. REPLACED R2 DOOR SILL IAW SRM 51-42-11.Sep 20, 2013 · N475UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2013092091319Sill · corrodedL2 DOOR SILL HAS CORROSION AT FR 68-69. INSTALLED REPAIR ANGLE IAW SRM 53-41-14 FIG 201 PRINCIPLE 5.Sep 20, 2013 · N475UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2013090290930Strap · defectiveYELLOW & BLACK STRAP AT DOOR 1L WILL NOT STOW. REPLACED SAFETY BARRIER STRAP AT DOOR 1L.Sep 1, 2013 · N475UA · Airbus A320232 · Emergency EquipmentSDR CALA2013072990015Microphone · inoperativeCAPTAIN'S OXYGEN MASK MICROPHONE IS INOPERATIVE. AMU IAW MM 23-51-34 AND CF DS TEST OK AND BOTH MASKS FUNCTION NORMAL.Jul 28, 2013 · N475UA · Airbus A320232 · Interphone/Passenger Announcement (PA) SystemSDR UALA2013071905073Control Box · failedON TAXI ACFT TRACKS LEFT AND REQUIRES 5-8 DEGREES RT NOSE TILLER. BSCU SHOWS FAILED ON PFR. REPLACEED BSCU IAW AMM 32-42-34. R & R BSCU BOX IAW AMM 32-42-34-000-001 A AND 32-42-34-400-001-A. OPS CHECKED NORMAL.Jul 18, 2013 · N475UA · Airbus A320232 · BrakeSDR UALA2013071504931Windshield · failedRIGHT WINDSHIELD ANTI-ICE DISPLAYED ON UPPER ECAM SCREEN. REPLACED WINDSHIELD IAW MM.Jul 13, 2013 · N475UA · Airbus A320232 · Windshield/Door Rain/Ice RemovalSDR UALA2013062504389Unknown · unknownFIRST OFFICER`S SLIDING WINDOW HEAT INOPERATIVE. TEST WINDSHIELD HEAT CONTROLLER, NO PROBLEMS FOUND.Jun 21, 2013 · N475UA · Airbus A320232 · Windshield/Door Rain/Ice RemovalSDR UALA2013052803674Windshield · leakingVERY LOUD WIND NOISE ON RT SIDE AFT WINDOW. EXTERNAL SEAL AFT EDGE COMING OFF. REPLACED NR 3 RT FIXED WINDOW, OP'S TEST ANTI-ICING AND DEFOGGING, TESTED GOOD.May 24, 2013 · N475UA · Airbus A320232 · Flight Compartment WindowsSDR UALA2013051403349Wire · shortedEMERGENCY LIGHTS FAIL TEST. EPSU INT EMERGENCY LIGHT AND EPSU EXT LOAD EMERGENCY LIGHT. REPAIRED WIRE SHORTED TO GROUND AT SEAT ROW 30 IAW SWP CH 20. EMERGENCY LIGHTS TEST SATISFACTORY IAW AMM 33-51-00.May 14, 2013 · N475UA · Airbus A320232 · Light System WiringSDR UALA2013050803224Wire · shortedCAPTAIN'S OXYGEN MASK MICROPHONE IS INOPERATIVE. FOUND MICROPHONE WIRE IS INTERMITTENT IN O2 BOX. WHEN WIGGLED, COMMS IS INTERMITTENT. REPLACED CAPTAIN'S OXYGEN MASK STOWAGE BOX REF AMM35-12-41-00-0-001 A. CHECKS OK REF AMM 35-12-41-710-001A.May 6, 2013 · N475UA · Airbus A320232 · Communications System WiringSDR UALA2013040902361Apu · malfunctionedBCL 1 FAULT, FLT DIVERTED. REPLACED APU.Apr 8, 2013 · N475UA · Airbus A320232 · Airborne Auxiliary Power Unit (APU) SystemSDR UALA2013040402249Indicator · detachedL1 DOOR SLIDE ARM INDICATOR DETACHED. ATTACHED INDICATOR TO DOOR, CHECKED OKAY.Apr 2, 2013 · N475UA · Airbus A320232 · Passenger/Crew DoorsSDR UALA2013040102079Seal · brokenAFT GALLEY WATER EXT HAS BROKEN SEAL. REPLACED SEAL.Mar 30, 2013 · N475UA · Airbus A320232 · Potable Water SystemSDR UALA2013030701354Microphone · inoperativeCAPTAIN'S OXYGEN MASK MICROPHONE IS INOPERATIVE. REPLACED WITH SECOND OBSERVER. OPS CHECKS NORMAL.Mar 6, 2013 · N475UA · Airbus A320232 · Interphone/Passenger Announcement (PA) SystemSDR UALA2013030401297Seal · peelingOUTSIDE WEATHER STRIPPING ON F/O REAR SIDE WINDOW PEELING BACK CAUSING LOUD WIND NOISE RESEALED AFT DAMAGED SECTION WITH SEA3750-21 REF MT 56-001. ALSO REF AMM 56-11-11.Mar 3, 2013 · N475UA · Airbus A320232 · Flight Compartment WindowsSDR UALA2013012300400Unknown · vibrationABNORMAL EXCESSIVE VIBRATION WITH FLAPS FULL SELECTED 140 KTS. LOWERED FLAPS AND SLATS TO PERFORM VISUAL INSP. NO DEFECTS NOTED AND FLAPS AND SLATS SECURE. DID FIND ICE ACCUMULATION AND REQUESTED DE-ICE.Jan 22, 2013 · N475UA · Airbus A320232 · Trailing Edge Flap Control SystemSDR UALA2012121407222Pan · crackedDOOR 2L FWD LAV FLOOR PAN IS CRACKED. INSPECTED AFT FWD LAV FLOOR PAN SENT PHOTOS TO FOR DISPOSITION AND PARTS. APPLIED CLEAR VINYL FLOOR TAPE OVER AFFECTED AREA. VERIFIED PAN IS CRACKED. REMOVED FLOOR FOUND DAMAGED MEMBRANE. REPLACED FLOOR PAN.Dec 12, 2012 · N475UA · Airbus A320232 · Passenger Compartment EquipmentSDR UALA2012121407204Wire · chafedL2 DOOR EMERGENCY LIGHT WIRES CHAFED. FOUND NO BROKEN STRANDS. REPAIRED CHAFED WIRES.Dec 12, 2012 · N475UA · Airbus A320232 · Light System WiringSDR UALA2012091805272Unknown · malfunctionedNOSE WHEEL STEERING PULLING RIGHT AND REQUIRES RUDDER TRIM TO TRACK STRAIGHT. STRAIGHT TRACKING REQUIRED RUDDER TRIM (UNITS LEFT OR RIGHT) TO BE SET AT: CREW COMMENTS: 4.5-ACCOMPLISHED TSM32-51-00- 201 REVIEW OF AMSDIS AND PFR. NO FAULT HISTORY NOTED. ACCOSep 16, 2012 · N475UA · Airbus A320232 · Landing Gear Steering SystemSDR UALA2012091305158Power Supply · failedCABIN EMERGENCY LIGHT TEST FAILS WITH MSG EPSU INTERNAL FAULT LEFT. REPLACED OVERWING POWER SUPPLY AND BATTERY.Sep 13, 2012 · N475UA · Airbus A320232 · Emergency LightingSDR UALA2012080904328Tire · vibrationEXCESSIVE MODERATE VIBRATION FROM THE NOSE GEAR ON TAKEOFF UNTIL GEAR FULLY RETRACTED. REMOVED & REPLACED BOTH NOSE GEAR TIRE ASSEMBLIES.Aug 8, 2012 · N475UA · Airbus A320232 · TireSDR UALA2012071603830Ground Stud · looseRIGHT FWD CABIN DOOR ECAM ILLUMINATED 4 TIMES DURING DESCENT. DOOR OPS NORMAL. FOUND GROUND STUD 2050VN LOOSE CAUSING INTERMITTENT ECAM DOOR WARNING FAULT. SECURED GROUND WIRE, FWD RT DOOR INDICATION CHECKS NORMAL.Jul 14, 2012 · N475UA · Airbus A320232 · Door System WiringSDR UALA2012070503607Oxygen Mask · leakingFIRST OFFICERS OXYGEN HARNESS FAILS TO INFLATE AND IS LEAKING. REPLACED 2ND OBSERVER MASK ASSY.Jul 3, 2012 · N475UA · Airbus A320232 · Crew Oxygen SystemSDR UALA2012062903433Analyzer · defectiveENGINE 1 VIBRATION N1 INDICATION ENGINE 1 INOP ON ENGINE ECAM SYSTEM PAGE - ENGINE. ACCOMPLISHED EG7182, FOUND 121.8 OHMS RESISTANCE BETWEEN PINS 7 AND 8 OF TERMINAL BLOCK 4 000VS, REF TASK77-30-00-810-821-A. SPEED SENSOR IS FAULTING, NEEDS ENG CHANGE.Jun 25, 2012 · N475UA · Airbus A320232 · Engine Vibration Analyzer
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