N480UA

Service difficulty reports · 116

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 = 'N480UA' 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 CALA2026100920256Battery Pack · no testRAN EMERGENCY LIGHT BATTERY TEST. EPSU LOCATED IN FWD LT. REPLACED EPSU BATTERY IAW AMM 33-51-38-400-002-A.Oct 7, 2026 · N480UA · Airbus A320232 · Emergency LightingSDR CALA2026041315321Fuel Cap · missingFUEL CAP MISSING , PDA 2 REQUIRED IAW GMM 02-30-95Apr 13, 2026 · N480UA · Airbus A320232 · Fuel StorageSDR CALA2026030214209Light · detachedRIGHT RETRACTABLE LANDING, LIGHT HANGING OUT OF RETAINER. LANDING LIGHT RETAINER MISSING . LANDING LIGHT ASSEMBLY ORDERED TO USE THE RETAINER THAT WAS MISSING. 31-3341-9-9001,Feb 26, 2026 · N480UA · Airbus A320232 · Exterior LightingSDR CALA2025111711281Frame · crackedRIGHT FRM 16 DOUBLE JOGGLE HOLE 6 HAS A CRACK INDICATION IN FRAME LAYER, 2 OCLOCK POSITION VIEWED FROM OUTSIDE, 100% SH. ACCOMPLISHED IMPROVED INTERIM REPAIR AT FR16 DBL JOGGLE HOLE 6 IAW ECRA 5311-02923 REV A PART 1.A.1.Oct 27, 2025 · N480UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2025102310433Doubler · crackedNR 1 PYLON UPPER FWD SPAR DOUBLER CRACKED AT LT SKIN. REPAIRED THE NR 1 PYLON UPPER FWD SPAR DOUBLER LT SKIN IAW SRM 54 -52-12-300-024.Oct 20, 2025 · N480UA · Airbus A320232 · Nacelle/Pylon, Main FrameSDR CALA2025101410075Spar · crackedNO.2 PYLON UPPER FWD SPAR DOUBLER HAS CRACKED AT R/H SKIN. GENER ATED BY V919150 ON HAECO LCQ NR 9298226/40226. ESFR INFORMATION UPDATE REPAIR AREA ON #2 PYLON UPPER FWD SPAR DOUBLER AT RT SKIN IAW A3 20 SRM 54-52-12-300-036. ACMP BY V901914Oct 13, 2025 · N480UA · Airbus A320232 · Nacelle/Pylon, Frame/Spar/RibSDR CALA2025081107537Light · no testDURING FUNCTION TEST, RECEIVED ERROR MSG "EPSU INT LOAD EMER L" ATA 33-51-38 C/W TEST OF THE EMERGENCY LIGHTS REF AMM: 33-51-00-710-096-A. TEST OK AND NO OTHER FAULTS NOTED AT THIS TIME.Aug 9, 2025 · N480UA · Airbus A320232 · Emergency LightingSDR CALA2025080707407Slide · not reportedR1 ESCAPE SLIDE ASSEMBLY REPLACED REF AMM 25-62-44. REPLACED R1 ESCAPE SLIDE ASSEMBLY REF AMM 25-62-44. ACP RII INSP REF GMM 09-25-05.Aug 4, 2025 · N480UA · Airbus A320232 · Escape SlideSDR CALA2025072406883Engine · malfunctionedAT TO POWER SET ENG 1 DO UNT ONLY WENT TO 1.2EPR PULLED LEFT. ENG2 EPR NORM AT 1.46. PREFORMED FAULT ISOLATION REF FIM TASK 75-24-00-810-802B TO STEP 3.B.1 AND FOUND FAULT CODE HCCWAF. ACCOMPLISHED TEST NR 11 : HIGH POWER ASSURANCE TEST REF AMM TASK 71-00-00Jul 21, 2025 · N480UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR CALA2025072206843Actuator · faultedAT 60 KTS ENG 2 COMP VANE ECAM ON TO PULLED PFR. SEE PHOTO. INSTALLED RIG PIN INTO FRONT OF BEARING HOUSING CRANK UP TO SUB TASK D (3). WORK ACCOMPLISHED ON LOG 5549419, REMOVED ACC ACTUATOR REF MM 75-24-52-000-010-A PARTS USED: 00-0594-3-2278,QTY :1 31-7520-9Jul 19, 2025 · N480UA · Airbus A320232 · Compressor Bleed ValveSDR CALA2025060305227Pump · unsecureHYD B SYS LO PR IN FLIGH T TURNED BLUE PUMP OFF FOUND EVIDENCE OF HYD LEAK IN LEFT WHEEL WELL AREA AND AFT BELLY - FOUND BLUE PUMP 2074GJ PRESSURE SWITCH EXTREMLY LOOSE AND NOT SAFETY WIRED. SECURED SWITCH REF AMM 29-12-17/401. NO LEAKS NOTEDJun 1, 2025 · N480UA · Airbus A320232 · Hydraulic Pump (Electric/Engine), MainSDR CALA2025041603902Life Vest · unsecure1L JUMPSEAT LIFEVEST INBRD AND OUTBRD NEED SECURING RE-SECURED 1L JUMPSEAT I/B & O/B LIFEVESTS AS REQUIRED REF. AMM 25-66-00.Apr 15, 2025 · N480UA · Airbus A320232 · Life JacketSDR CALA2025040403544Warning Message · false activationHYD Y ENG 2 PUMP LO PR ECAM. SERVICED YELLOW HYDRAULIC SYSTEM. RAN YELLOW AND BLUE AND GREEN SYSTEMS WITH APU BOOSTED. CHECKED FOR LEAKS NO LEAK FOUND. RAN THE ENGINE, OPERATED FLIGHT CONTROLS PUSHED BRAKES PADDLES, RECHECKED FOR LEAKS, NO LEAK FOUND AS PER TApr 2, 2025 · N480UA · Airbus A320232 · Central WarningSDR CALA2025021302312Fan · failedBLOWER FAULT WITH POPPED BLOWER CB. FOUND AVIOUCS VENT BLOWER CB AD10 POPPED AND WOULD NOT RESET . POST FLIGHT REPORT SHOWED BLOWER FAN 20 HQ FAULT . FAN HAD BURNT ELECTRONICS SMELL.REPLACED BLOWER FAN 20HQ. OPS AND LEAK CHECK GOOD. PARTS USED: 31-2126-9-90Feb 11, 2025 · N480UA · Airbus A320232 · Air Distribution FanSDR CALA2025012201970Battery · no testCABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK - EPSU BAT CAP AFT L FAILED TEST. NEED BATTERY REPLACEMENT. REMOVED AND REPLACED AFT EPSU BATTERY, BITE CHECK PASSED. REF AMM 33-51-38-400-002-A PARTS USED: 18-3351-3-0001,QTY :1Jan 21, 2025 · N480UA · Airbus A320232 · Emergency LightingSDR CALA2024121601522Light · malfunctionedEMERGENCY CABIN LIGHTS AND EMERGENCY EXIT LIGHTS ARE COMING ON A ND OFF INTERMITTENTLY PERFORMED TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00-710-001-A. NO FAULTS FOUND LIGHTS FUNCTION NORMAL.Dec 12, 2024 · N480UA · Airbus A320232 · Emergency LightingSDR CALA2024110502799Skin · damagedL/H ELEVATOR HAS LIQUID INGRESS DAMAGE 105 INCHES FROM I/B EDGE 5 1/2 INCHES FROM TRAILING EDGE 5 INCHES IN DIAMETER PER HAECO LCQ N/R 9298194/22194 GEN BY V061632 REPAIRED L/H ELEVATOR 105 IN FROM I/B 5.5 IN FROM T/E 5 IN DIA ZONE C IAW A320 SRM 55-21-11-300-Nov 4, 2024 · N480UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2024110502796Skin · contaminatedL/H ELEVATOR HAS LIQUID INGRESS 176IN FROM INBOARD EDGE 5IN FROM TRAILING EDGE 4IN IN DIAMETER PER HAECO LCQ N/R 9298195/22195 GEN BY V061632 DRILLED WITNESS ON L/H ELEVATOR 176 IN FROM I/B 5 IN FROM T/E 1.5 IN DIA ZONE C IAW A320 AMM 55-20-00-200-006-A01 PARANov 4, 2024 · N480UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2023061401859Unknown · unknownWHEEL N/W STRG FAULT APPEARED AFTER EXTENDINGGEAR. LOCKED BY TOMC, MUST HAVE POSITIVE FIX PER TOMC SR MGR DUE CREW DECLARING EMERGENCY CREW REPORTED STEERING AVAILABLE UPON LANDING,RESET NOSE WHEEL STEERING/ANTI SKID SWITCH. PERFORMED GROUND TEST ON BSCU 1&2,Jun 12, 2023 · N480UA · Airbus A320232 · Landing Gear SystemSDR CALA2022120703315None · nonePLANNING TO CONTACT ENGINEEERING AFTER 02APR23, BUT BEFORE 02MAY23 FOR EC/RA 5341-01359 PART 2 STEP 2 INSPECTION REQUIREMENTS. ITEM PLACED ON DIP OK TO CARRY PER ECRA 5341-01359, PLANNING TO CONTACT ENGINEERING TOMC-APPROVAL FROM SC1ELBYC COMMENT AFTER 02-APRIDec 6, 2022 · N480UA · Airbus A320232 · Standard Practices/StructuresSDR CALA2022120703314None · noneFR66 AND FR68 DOOR STOPS RH EXISTING UNDOCUMENTED REPAIRS. REPAIR IS EXPECTED TO BE A PERMANENT SOLUTION WITH INSPECTION OF THE LATEST REVISION OF EC/RA 5341-01359 ON OR BEFORE THE REQUIRED. ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2, STEP 1 AIRCRAFT REACHDec 6, 2022 · N480UA · Airbus A320232 · Standard Practices/StructuresSDR CALA2022120703313None · nonePLANNING TO CONTACT ENGINEEERING AFTER 25635 TOTAL FLIGHT CYCLES, BUT BEFORE 25685 TOTAL FLIGHT CYCLES FOR EC/RA 5341-01359 PART 2 STEP 1 INSPECTION REQUIREMENTS. ITEM PLACED ON DIP OK TO CARRY PER ECRA 5341-01359, PLANNING TO CONTACT ENGINEERING TOMC-APPROVALDec 6, 2022 · N480UA · Airbus A320232 · Standard Practices/StructuresSDR CALA2022120703312None · noneFR66 AND FR68 DOOR STOPS LH EXISTING UNDOCUMENTED REPAIRS. REPAIR IS EXPECTED TO BE A PERMANENT SOLUTION WITH INSPECTION OF THE LATEST REVISION OF EC/RA 5341-01359 ON OR BEFORE 02JUN23. REQUIRED. ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2, STEP 2 LH FR66 &Dec 6, 2022 · N480UA · Airbus A320232 · Standard Practices/StructuresSDR CALA2022120203262Door Frame · damagedDURING ROTO PROBE INSPECTION OF RHS FR16 #7 DOOR STOP, HOLE#1 AND #3 FOUND WITH REJECTABLE INDICATIONS FRAME AND INTERCOSTAL LAYERS. REPAIR BEFORE NEXT FLIGHT. AND #3 AND ASSOCIATED HOLES #2 AND #4 AT FR16 RHS DOOR STOP 5311-02919. THERE AFTER REPEAT INSPECTIONov 30, 2022 · N480UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2022113003244Stop Fitting · crackedDURING ROTO INSP PF LH FR16 DOOR STOP #7 CRACK INDICATIONS WERE NOTED ON I/B UPPER AND LOWER HOLES, FRAME AND INTERCOSTAL LAYERS . REPAIR BEFORE NEXT FLIGHT.Nov 28, 2022 · N480UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2022112503218Stringer · corrodedA3NB-53-4-6179 BULK CARGO BET FR63-64 STRINGER 42L IS CORRODEDNov 23, 2022 · N480UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2022111103106Doubler · corrodedBULK CARGO BETWEEN FRS 63-64, STRG 40L-43L EXISTING DOUBLER HAS CORROSION OR RE-INSPECTION PER SRI. SRI REQUIREMENTS AS FOLLOWS: FIRST INS ER OCCURS 1ST, SUBSEQUENT INSPECTIONS AT INTERVALS OF 2,000FC/4, OR CONCERNING NTM CHAPTERS IAW SRI 53-00-11-205-017, REFNov 9, 2022 · N480UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2022111103109Floor Support · corrodedCABIN FLOOR SUPPORT FR16 BETWEEN Y254 AND Y765 CORRODED. REMOVED CORROSION IAW SRM 51-42-11 AND FOUND WITHIN ALLOWA BLE LIMITS A-320 SRM 53-11-14-283-007.Nov 9, 2022 · N480UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2022110403034Floorbeam · corrodedCABIN FLOOR SUPPORT FR16 BETWEEN Y254 AND Y765 CORRODED. REMOVED CORROSION IAW A-320 SRM 51-42-11 AND FOUND WITHIN ALLOWA BLE LIMITS UAW A-320 SRM 53-11-14-283-007 L=1.900" W=1.350" D=.0 40" T93987,T93998 EMP#: V936039 WORK ACCOMPLISHED AT ST ENGINEER ING OF MNov 4, 2022 · N480UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2022102402915None · crackedDURING ROTO INSP OF LH FRAME FOOT AT FR43 CRACK INDICATION WAS NOTED ON FASTER HOLE. REAPIR BEFORE NEXT FLIGHTOct 22, 2022 · N480UA · Airbus A300* · Fuselage Main, Plate/SkinSDR CALA2022102402913None · corrodedBULK CARGO BET FR57 -5 STRINGER 37R IS CORRODEDOct 22, 2022 · N480UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2022102402914None · crackedDURING ROTO INSP OF RH FRAME FOOT AT FR43 CRACK INDICATION WAS NOTED OF FASTENER HOLE. REPAIR BEFORE NEXT FLIGHTOct 22, 2022 · N480UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2022101802826Stringer · corrodedBULK CARGO STRINGER 41L BET FR63-64 IS CORRODED. REMOVED AND REPLACED STRG 41L IAW A320 SRM 51-42-11/001, RECEIVE D NEW STRG 41L P/N=D5347041821600 B/N:0003899727. EMP# V936039 W ORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOBILE AT BFM ON NR# 38657.Oct 14, 2022 · N480UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2022101802825Stringer · corrodedBULK CARGO BET FR63-64 STRINGER 43L IS CORRODED REMOVED AND REPLACED STRG 43L IAW A320 SRM 51-42-11/001, RECEIVE D NEW STRG 43L P/N:D5347041822000, B/N=0003900958. EMP# V936039 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOBILE AT BFM O N NR# 38665.Oct 14, 2022 · N480UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2022101802822Seat Track · corroded(A3NB-53-3-6038) CABIN SEAT TRACK -Y1292 FR20 CORRODED. DOT NO.1 7-23() SEAT TRACK -Y1292 BETWEEN FR1224 REPLACED IAW A320 SRM 51-42-11. EMP# V934585 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF M OBILE AT BFM ON NR# 38978.Oct 14, 2022 · N480UA · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2022101802821Floor Support · corroded(A3NB-53-3-6038) CABIN FLOOR SUPPORT FR21 Y254 TOP SURFACE CORRO DED. DOT NO.17-19() REMOVED AND REPLACED FLOOR SUPPORT Y254 IAW A320 SRM 51-42-11/00 1. RECEIVED NEW FLOOR SUPPORT P/N=D5311281820401 B/N=0003925620 EMP# V936039 WORK ACCOMPLISHED AT ST ENGINEERIOct 14, 2022 · N480UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2022101202771Seat Track · corroded(A3NB-53-3-6038) CABIN SEAT TRACK -Y1292 FR20 CORRODED. DOT NO.1 7-23() SEAT TRACK -Y1292 BETWEEN FR1224 REPLACED IAW A320 SRM 51-42-11. EMP# V934585 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF M OBILE AT BFM ON NR# 38978.Oct 12, 2022 · N480UA · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2022101202770Floor Support · corroded(A3NB-53-3-6038) CABIN FLOOR SUPPORT FR21 Y254 TOP SURFACE CORRO DED. DOT NO.17-19() REMOVED AND REPLACED FLOOR SUPPORT Y254 IAW A320 SRM 51-42-11/00 1. RECEIVED NEW FLOOR SUPPORT P/N=D5311281820401 B/N=0003925620 EMP# V936039 WORK ACCOMPLISHED AT ST ENGINEERIOct 12, 2022 · N480UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2022101002753Seat Track · corrodedCABIN SEAT TRACK -Y765 FR20 CORRODED.Oct 8, 2022 · N480UA · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2022100702733Stringer · corrodedA3NB-53-4-6179 BULK CARGOSTRINGER 43L BET FR64-65 IS CORRODED() REPAIRED STRINGER 43L BETWEEN FR64 TO FR65 IAW A320 SRM 53-41-13 -300-004. EMP#V934585 WORK ACCOMPLISHED AT ST ENGINEERING AEROSP ACE OF MOBILE AT BFM ON NR# 38656.Oct 6, 2022 · N480UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2022100602723Stringer · corrodedA3NB-53-4-6179 BULK CARGOSTRINGER 43L BET FR64-65 IS CORRODED() REPAIRED STRINGER 43L BETWEEN FR64 TO FR65 IAW A320 SRM 53-41-13 -300-004. EMP#V934585 WORK ACCOMPLISHED AT ST ENGINEERING AEROSP ACE OF MOBILE AT BFM ON NR# 38656.Oct 5, 2022 · N480UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2019080501313Stringer · corrodedAFT CARGO PIT STRINGER 43 LEFT BETWEEN FRAME 56-58 HAS CORROSION. FOUND STRINGER OUT OF LIMITS PER SRM 53-00-13-300-002. PERFORMED STRINGER REPAIR IAW SRM 53-00-13-300-001, SHT. 02, COUPLING TYP E 1.Aug 4, 2019 · N480UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2019080501312Stringer · corrodedFWD CARGO COMPT FR 31-33 STRINGER 43R HAS CORROSION. FOUND STRINGER TO BE OUT OF LIMITS PER SRM 53-21-13-283-001. PER FORMED STRINGER REPAIR IAW SRM 53-00-13-300-001 SHEET 01, COUPLI NG TYPE 1.Aug 4, 2019 · N480UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2019080501311Stringer · corrodedAFT CARGO PIT STR 42RT BETWEEN FR62-64 HAS CORROSION . FOUND STRINGER TO BE OUT OF LIMITS PER SRM 53-00-13-300-002. PER FORMED STRINGER REPAIR PER SRM 53-00-13-300-001 SHEET 02, COUPLI NG TYPE 1.Aug 4, 2019 · N480UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2019080501310Stringer · corrodedAFT CARGO PIT STRINGER 42 LEFT BETWEEN FRAMES 54-56 HAS CORROSIO N PER HAECO LCQ NR LP 9294479 GENERATED BY V052030 UPON FURTHER EVAL STRG 42L BETWEEN FR 54-56 FOUND TO BE OUT OF L IMTS WITH ESS THAN .031IN REMAINING MATERIAL REMOVED AND REPALCE D STR 42L FR 5Aug 4, 2019 · N480UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2019080501309Threshold · corrodedFWD CARGO THRESHOLD SPLICE PLATE HAS CORROSION. REMOVED AND REPLACED DISCREPANT FWD CARGO THRESHOLD PLATE IAW SRM 51-42-11-001 AND 51-72-11.Aug 4, 2019 · N480UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2019080101285Cleat · corrodedFWD CARGO FR 31-32 STGR 40R-41R CLEAT HAS CORROSION. REMOVED AND REPLACED CLEAT FR 31-32 STR 40R-41R IAW SRM 51- 72-11.Aug 1, 2019 · N480UA · Airbus A320232 · Fuselage Main, Attach FittingsSDR CALA2019072901266Web · crackedAFT CABIN LT FLOOR WEB IS CRACKED AT FR68-69 JUST AFT OF L2 DOOR SILL ON REF 9294422 SPEC A3NB-53-3-6222. REMOVED, FABRICATED & INSTALLED NEW FLOOR WEB AT FRAME 68-69 JUS T AFT OF L2 DOOR SILL IAW SRM 51-42-11-001 PARA E, H, F & SRM 51-31-00-801, SRM 51-23-11-Jul 26, 2019 · N480UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2017072802386Lamp · inoperativeRIGHT FWD OVERWING EXIT LIGHT FWD LAMP INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-51-15. OPS CHECKED GOOD.Jul 26, 2017 · N480UA · Airbus A320232 · Emergency LightingSDR CALA2016121900001Battery · faultedCIDS REPORTED LEFT AND RIGHT BATT PACK FAULTS. REMOVED AND REPLACED LEFT AND RIGHT EMERGENCY LIGHT BATTERY PACKS. OPS CHECK GOOD.Dec 19, 2016 · N480UA · Airbus A320232 · Emergency Lighting
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