N457UA

Service difficulty reports · 138

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 = 'N457UA' 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 CALA2026021213722Elec Connector · disconnectedL2 DOOR EMERGENCY LIGHT DID NOT TEST, FOUND CONNECTOR 7245VC DISCONNECTED ENTIRELY IAW AIPC 24-92-04-46M, ITEMS 10, AND 20, AWM 33-51-03 PAGE 8, AND ESPM 20-44-29-01. RECONNECTED & OPS CHECKED PERFORMED IAW AMM 31-51-00-710-007-A. OPS CHKD NORMAL.Feb 11, 2026 · N457UA · Airbus A320232 · Light System WiringSDR CALA2026012613283Slide · expiredSCHEDULED REMOVAL. REMOVED AND REPLACED DOOR SLIDE ASSY IAW AMM 25-62-44.Jan 26, 2026 · N457UA · Airbus A320232 · Escape SlideSDR CALA2026021813895Warning Light · false activationAFTER TOUCHDOWN, MASTER CAUTION LIGHTS ILLUMINATED WITH NO CHIME OR ECAM DISPLAYED. ACCOMPLISHED AN OPS TEST OF MASTER CAUTION, WARNING LIGHT IAW AMM 31-50-00-710-011-A. NO FAULTS NOTED.Jan 18, 2026 · N457UA · Airbus A320232 · Central WarningSDR CALA2025091508876Power Supply · no testEPSU UNIT RT MESSAGE AFTER EMERGENCY LIGHTS TEST NEEDS REPLACED. R & R RT ESPU. REF: AMM TASK 33-51-38-000-002-A & TASK 33-51-38-400-002-A. OP CHECK TEST OKAY, IAW AMM TASK 33-51-00-710-001-A.Sep 13, 2025 · N457UA · Airbus A320232 · Emergency LightingSDR CALA2025091108756None · noneRIGHT OVERWING SLIDE INFLATION BOTTLE PINNED FOM, REMOVED PIN, REACTIVATED RH BOTTLE REF AMM 25-62-00-081-001-A. VERIFIED REMOVAL OF THE PIN FROM THE R/H OFF WING SLIDE BOTTLE IN REF TO AMM 25-62-00-061-001-A.Sep 8, 2025 · N457UA · Airbus A320232 · Standard Practices/StructuresSDR CALA2025091008714Sensor · out of alignmentDOOR R FWD EMER EXIT ECAM. DOOR IND OPEN. PRESS NORMAL PERFORMED RENDER SAFE FOR RT FWD OVERWING EXIT HATCH. SLIDE INDICATION OF HATCH IS DEFECTIVE ON LOWER ECAM, HATCH IS IN THE ARM MODE, EMERGENCY EXIT INDICATION IS DEFECTIVE ON LOWER ECAM DU, HATCH IS COSep 8, 2025 · N457UA · Airbus A320232 · Door Warning SystemSDR CALA2025040303469Target · out of adjustDOOR L FWD EMER EXIT ECAM IN FLT DURING DESC ENT. FOUND FLAP COVER TARGET ON L FWD EMERGENCY EXIT DOOR OUT OF RANGE, ADJUSTED TARGET ON FLAP COVER REF AMM 52-71-13-400-001-A. ECAM MESSAGE NO LONGER PRESENT AND SYSTEM OPERATES NORMALLY REF TSM 52-21-00-810-80Mar 30, 2025 · N457UA · Airbus A320232 · Accessory CompartmentSDR CALA2025030302563Engine · stalledDUE TO EVIDENCE OF ENG #2 STALL, REQUIRED BORESCOPE OF HPC STAGES 3, 4, 5, 6, AND 7 REF TSM 71-00-00-810-809-A STEP 4. D. (2) (A) REMOVED ACCESS PORTS A, B, C AND D FOR BORESCOPE OF HPC REMOVED ENGINE CRANK PAD ACCOMPLISHED BOROSCOPE INSPECTION OF HPC COMPRESSMar 2, 2025 · N457UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR CALA2025021702339Fmc · faultedFMGC 1 FAIL REPORTED BY CREW, RESET UNSUCCESSFUL CFDS ATA 22-83-34 FMGC1 SOURCE EFCS 1 PHASE 5 , SEE TSM 22-83-00-810-859-A, 3 HITS LAST 10 LEGS LOCKED UNLOCKED FOR CORRECTIVE ACTION FOLLOWED TSM 22-83-00-810-859-A, REMOVED AND REPLACED TERMINAL BLOCKS 1831VT4Feb 17, 2025 · N457UA · Airbus A320232 · Flight Management Computing Hardware SystemSDR CALA2024121601536Girt Bar · lack of lubeDOOR 2R SLIDE DISARMED SHORTLY AFTER AIRBORNE INDICATED ON COCKP IT DOORS PAGE. CREW STATED THEY LOST WHITE SLIDE INDICATION FOR DOOR ARMED AT DR-2R ON ECAM DOOR/OXY PAGE AS SOON AS THEY TOOK OFF. AFTER TAKEOFF DOOR ARMED HANDLE HAD MOVE SLIGHTLY OUT AND FA CDec 13, 2024 · N457UA · Airbus A320232 · Emergency EquipmentSDR CALA2024121301508Proximity Sensor · faultedDOOR 2R INDICATING DISARMED AT CRUISE ALT PREV WRITE UP EARLIER TODAY. DEFERRED DOOR 2R SLIDE INDICATION REF MEL 2560T INOP PLACARD INSTALLED VERIFIED DOOR 2R IS CLOSED AND SECURED. DEFERRED DOOR 2R SLIDE INDICATION REF MEL 2560T INOP PLACARD INSTALLED VERIFDec 11, 2024 · N457UA · Airbus A320232 · Door Warning SystemSDR CALA2024111202836Stringer · corrodedMAIN CABIN BELOW FLOOR AT FRAME 65 RT STRINGER 25RT HAS EXFOLIAT ED CORROSION. REMOVED AND REPLACED STRINGER 25RT FR 65-66 IAW A320 SRM 51-72-1 1.Nov 6, 2024 · N457UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2024111102813Fitting · crackedCRACK INDICATION AROUND FASTENER AS MARKED AT 2 O''CLOCK POSITION BTW FR 40 AND 41 LH SIDE KEEL BEAM SIDE PANEL BEHIND THE VAPOR SEAL. GENERATED BY V947494 ON HAECO LCQ NR 9290461/36461 REMOVED + REPLACED CRACKED KEEL BEAM FITTING AT L/H FR40-41 IAW A320 SRM 5Nov 6, 2024 · N457UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2024110602804Door Frame · crackedRT AFT EMERGENCY EXIT DOOR CRACKED. REMOVED & REPLACED FR SEGMENT @ R/H AFT EMERGENCY HATCH IAW A320 SRM 51-72-11-911-001.Oct 31, 2024 · N457UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2024110402791Seat Track · corrodedR/H CABIN FLOOR BEAM -Y1292 HAS CORROSION BETWEEN FR.24-36.Oct 29, 2024 · N457UA · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2024110402792Stringer · corrodedAFT CARGO PIT FRAME 58-59 RT STRINGER 41 HAS CORROSION ON VERTIC AL FLANGE AND HORZ. FLANGE. GENERATED BY V052030 ON HAECO LCQ NR 9290433 / 36433Oct 28, 2024 · N457UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2024102802745Reinforcement · corrodedUNDER AFT CABIN FLOOR CORROSION AROUND WASTE WATER DRAIN MAST HARDWARE AND SKIN REINFORCEMENT PLATE. REMOVED & REPLACED REINFORCEMENT PLATE AT WASTE WATER DRAIN MAST IAW SRM 51-72-11.Oct 24, 2024 · N457UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2024102202702Web · crackedFLIGHT DECK FLOOR STRUCTURE WEB CRACKED FR 8-11 LBL20. FLIGHT DECK FLOOR STRUCTURE WEB REMOVED AND REPLACED PER A320 SR M 51-72-11-911-002.Oct 17, 2024 · N457UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2024102102694Skin · contaminatedR/H ELEVATOR HAS LIQUID INGRESS AT TOP SIDE 20 1/2 INCHES FROM I /B END, 7 INCHES FROM TRAILING EDGE, 1 INCHE DIAMETER, "REPAIR P RIOR TO NEXT FLIGHT" PER HAECO LCQ NR 9290689/36689 REPAIRED R/H ELEVATOR,TOP SIDE, 20.5" FROM I/B END, 7" FROM TRAI LING EDGE IAWOct 15, 2024 · N457UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2024102102693Skin · contaminatedR/H ELEVATOR HAS LIQUID INGRESS AT TOP SIDE 103 1/2 INCHES FROM I/B END, 21 INCHES FROM TRAILING EDGE, INCHES DIAMETER, "REPAIR PRIOR TO NEXT FLIGHT" PER HAECO LCQ NR 9290690/36690 REPAIRED R/H ELEVATOR, TOP SIDE, 103.5 INCHES FROM I/B END, 21 I NCHES FROM TRAOct 15, 2024 · N457UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2024101602665Floorbeam · corrodedMAIN CABIN AFT WET AREA FLOORBEAM -Y1292 IAW A320 SRM 51-42-11.Oct 14, 2024 · N457UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2024101402636Floor Support · corrodedCABIN R2 DOOR SILL AT FRAME 65 HAS CORROSION AROUND NUT PLATE HO LE. REMOVED AND REPLACED R2 DOOR SILL FR65-68 IAW A320 SRM 51-72-11.Oct 10, 2024 · N457UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2024101402633Angle · crackedLH INTERNAL FUSELAGE FRAME 68 FLANGE IS CRACKED @ DOORSILL ATTACH. REMOVED AND REPLACED 1EA FLANGE AT FRM68 IAW A320 SRM 51-42-11/0 01 AND 51-72-11-911-001.Oct 10, 2024 · N457UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2024101102626Angle · corrodedL-2 DOOR SILL REPAIR ANGLE CORRODED AT FR68 GENERATED BY V061642 ON HAECO LCQ NR 9290605/36605 PERFORM REPAIR ON L-2 DOOR SILL IAW A320 SRM 53-41-14-300-001.Oct 8, 2024 · N457UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2024100802607Shear Web · corrodedCABIN FLOOR STRUCTURE FWD OF FR70 LH SHEAR WEB AFT HOLE HAS CORR ISION REMOVED CORRODED SHEAR WEB AT L/H CABIN FWD OF FR70 AND REPLACED IAW A320 SRM 51-42-11/001 AS DIRECTED BY EA 5346-01001 REV.L OP 003.Oct 6, 2024 · N457UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2024100702597Seat Track · corrodedCABIN SEAT TRACK Y-765 FR 24-35 CORRODED OUT OF LIMITS. REMOVED SEAT TRACK OUT OF LIMITS IAW A320 SRM 51-42-11/001 REV 1 50, REPLACED SEAT TRACK Y-765 FR 24-35 IAW A320 SRM 51-42-11/001 REV 150.Oct 5, 2024 · N457UA · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2024100702598Seat Track · corrodedCABIN SEAT TRACK Y-1292 FR 36-42 CORRODED OUT OF LIMITS.Oct 4, 2024 · N457UA · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2024032000800Indication Sys · false indicationGREEN HYD RESEVOIR SEEMS TO BE LOSING FLUID LOCKED ALL HYD SYSTEM WAS AT NORMAL ON GROUND WITH NO INDICATION OF TOMC RECOMMENDS ENGINE RUN TO CK EDP AND LEAKS DUE TO HYD SEE AMM TASK 29-11-00-710-001-A OPERATIONAL TEST OF THE GREEN LEAKS. POWERED ALL 3 SYSTEMSMar 18, 2024 · N457UA · Airbus A320232 · Hydraulic Indicating SystemSDR CALA2024021200383Fuel Cap · missingPDA 2 FUEL CAP NOT INSTALLED ON AIRCRAFT. NO LEAKS NOTED AT COUPLING. INOP STICKER APPLIED BY CREW. OK TO DEFER PER CDL 28A. INSTALLED NEW FUEL CAP.Feb 9, 2024 · N457UA · Airbus A320232 · Fuel StorageSDR CALA2023050301344Fuel Cap · missingPDA 2 FOUND FUEL CAP MISSING ON ARRIVAL TO DCA FROM ORD SUSPECT FUEL CAP DEPARTED AIRCRAFT DURING FLIGHT. INSPECTED AIRCRAFT FOR DAMAGE REF GMM-02-30-95. NO DAMAGE FOUND. REPLACED MISSING FUEL CAP AS REQ.May 3, 2023 · N457UA · Airbus A320232 · Fuel StorageSDR CALA2022111703161Pipe · leakingECAM CAUTION MESSAGE - Y RSVR LO LVL MESSAGE INOP - HYD HYD YELLOW SYSTEM LO MASSIVE LEAK SOMEHERE ON TOP OF THE #2 ENG UNDERNEATH THE PYLON. FOUND HYD PIPE CUT AND LEAKING HYD FLUID AT DOWNSTREAM OF T/R CHECK OF THE YELLOW HYD SYSTEM PER AMM 29-13-00-710-002-Nov 17, 2022 · N457UA · Airbus A320232 · Hydraulic Pump (Electric/Engine), MainSDR CALA2022110703051Web · crackedFR 68 STR22R INNER CAP AND WEB FLANGE HAS A 1.068 IN CRACK. ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF LATEST REVISION OF ECRA 5341-01351 ON OR BEFORE APPROVED DIP TO ACCOMPLISH A PERMANENT REPAIR AT THE RH FR 68, STR 22RNov 4, 2022 · N457UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2022082402162Spring · missingPDA 3 NOSE GEAR BYPASS LEVER ONE SPRING CLIP MISSING OUT OF TWO...SEE PHOTO PHOTO ADDED INSTALLED NEW SPRING CLIP AT NLG BYPASS LEVER...REF IPC 32-51-12-01E.Aug 24, 2022 · N457UA · Airbus A320232 · Steering UnitSDR CALA2022072701885Radar · inoperativeWEATHER RADAR SYSTEM INOP - NAV RED WR ANT DISPLAYED AND ECAM PRED WS INOP UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V933475 PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. RESET THE MAC RELATED WORK ORDER 0000000Jul 27, 2022 · N457UA · Airbus A320232 · Doppler SystemSDR CALA2022051301226None · noneHYD G RSVR LO LVL ECAM DISPLAYED. CREW CONFIRMS FOLLOWED QRH 130.19 AND TURNED OFF GREEN ENG 1 PUMP AS SOON AS ECAM MSG DISPLAYED. TOMC MX CNTL HILL. SVC GREEN HYD TO FULL PERFORMED LEAK CHECK AFTER LEAK CORRECTED.May 13, 2022 · N457UA · Airbus A320232 · Hydraulic Power Accumulator, MainSDR CALA2022021600406Reservoir · low*EMERGENCY* Y RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN. - HYD ECAM HYD Y RSVR LO LVL CREW REPORTS NO ALTERNATE EXTEND REPLACED YELLOW SYSTEM LOW LEVEL SWITCH PER AMM 29-13-41. ECAM MESSAGE CLEARED NO FURTHER ISSUES ADD EMP:U377618 ROTABLE PARTS CHANGE WAS INFeb 16, 2022 · N457UA · Airbus A320232 · Hydraulic Pressure IndicatorSDR CALA2021111502103Landing Gear · faultyL/G DOORS NOT CLOSEDECAM NLG DOORS BYPASS IS IN THE OPEN POSITION. PHOTO IS FROM PILOTS PHONE. REMOVED AND REPLACED NLG DOOR ACTUATOR WITH NEW SERVICEABLE ONE, REF AMM 32-31-16-400-001-A, OPS CHECK GOOD. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1936428 SN OFNov 14, 2021 · N457UA · Airbus A320232 · Nose/Tail Landing Gear Strut/AxleSDR CALA2020111101259Pressure Panel · crackedCRACK INDICATION FOUND AT OUTBOARD FASTENER HOLE OUTSIDE OF REPAIR AREA FR 35 LT PRESSURE PANEL, REF EA-5330-05216 REV "B", REF AAR N/R: 9469368 GENERATED BY: V903469. ACCOMPLISHED INTERIM REPAIR PART 1, AS PER ECRA 5330-06774 AND EA 5330-05216 REV B ON OR BENov 11, 2020 · N457UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2020110401241Pressure Blkhd · crackedCRACK FOUND AT RT SIDE FASTENER HOLE ''B'' ON THE PRESSURE PANEL BETWEEN FR 35 & FR 36, REF EA 5330-05216 REV. "B". CRACK LOCATION 6 O'CLOCK, REF AAR N/R: 9469143 GENERATED BY: V909151. INSTALLED REPAIR AT RT SIDE PRESSURE PANEL BETWEEN FR 35-FR 36, AS PER UNov 3, 2020 · N457UA · Airbus A320232 · Fuselage Main, BulkheadSDR CALA2018111602389Actuator · leakingREMOVE AND REPLACE L1 PAX DOOR POST ACTUATOR DUE TO LEAKAGE. SN OFF 1934 IPC REFERENCE ACTUATOR, PAX DOOR OFF 31-5210-9-9001 1934 ON 31-5210-9-9001 0031.Nov 16, 2018 · N457UA · Airbus A320232 · Passenger/Crew DoorsSDR CALA2018111202351Bulkhead · crackedREF TO AAR NON ROUTINE-9813264, CRACK IN VERTICAL WEB R/H SIDE BELOW F/O SLIDING WINDOW RAIL. REPAIRED VERTICAL WEB R/H SIDE BELOW F/O SLIDING WINDOW AT FR4 IAW ECRA 5311-02040, ACCOMPLISH THE INITIAL INSPECTION REQUIRMEN TS PER PART 2 OF ECRA 5311-02040 AT THNov 10, 2018 · N457UA · Airbus A320232 · Fuselage Main, BulkheadSDR CALA2018110902340Door Frame · crackedA3NB-05-3-6159 A-34-023 RH AFT EMERGENCY EXIT. RH AFT IB LOWER V ERTICAL FRAME CRACKED. REMOVED AND REPLACED RH AFT EMERGENCY EXIT RH AFT IB LOWER VERTI CAL FRAME IAW A320 SRM 51-42-11, SRM 51-44-11, SRM 51-75-12 ADD EMP:V925284 INSP C/WNov 9, 2018 · N457UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2018110502279Frame · cracked(SUPPORT TASK) (A-38 NO DOT) L/H FWD EMERGENCY EXIT 833 R/H VER TICAL FRAME CRACKED AAR NONROUTINE 9813987 REMOVED AND REPLACED L/H FWD EMERGENCY EXIT 833 R/H VERTICAL FRA ME IAW A320 SRM 51-42-11-001 PARA 2.E. AAR NONROUTINE 9813987 ADD EMP:V919097Nov 2, 2018 · N457UA · Airbus A320232 · Emergency ExitsSDR CALA2018110502278Frame · cracked(SUPPORT TASK) (A-38) NO DOT) R/H FWD EMERGENCY EXIT 843 R/H VER ICAL FRAME CRACKED AAR NONROUTINE 9813988 REMOVED AND REPLACED CRACKED FRAME AT R/H FWD EMERGENCY EXIT, IA W A320 SRM 51-42-11. AAR NONROUTINE 9813988 ADD EMP:V925284Nov 2, 2018 · N457UA · Airbus A320232 · Emergency ExitsSDR CALA2018110502277Frame · crackedA3NB-05-3-6159 A34-26 RH FWD EMERGENCY EXIT 843 LH VERTICAL F RAME CRACKED. AAR NONROUTINE 9813613 REMOVED AND REPLACED CRACKED FRAME AT L/H VERTICAL OF DOOR, R/H FWD EMERGENCY EXIT IAW A320 SRM 51-42-11 AAR NONROUTINE 98136 13 ADD EMP:V925284Nov 2, 2018 · N457UA · Airbus A320232 · Emergency ExitsSDR CALA2018110502276Frame · crackedA3NB-05-3-6159 A34-24 LH AFT EMERGENCY EXIT 834 AFT VERTICAL FRAMES CRACKED 2PL AAR NONROUTINE 9813595 REMOVED AND REPLACED LH AFT EMERGENCY EXIT AFT VERTICAL FRAME IA W A320 SRM 51-42-11, 51-72-11, 51-24-00-001, 51-23-11-001, 51-23 -12-001 AAR NONROUNov 2, 2018 · N457UA · Airbus A320232 · Emergency ExitsSDR CALA2018110502275Frame · cracked(SUPPORT TASK) A-38 NO-DOT) L/H AFT EMERGENCY EXIT 834 FWD VERTI CAL FRAME CRACKED AAR NONROUTINE 9813986 REMOVED AND REPLACED LH AFT EMERGENCY EXIT FWD VERTICAL FRAME IA W A320 SRM 51-42-11, 51-72-11, 51-23-12-001, 51-24-00-001. AAR NONROUTINE 9813986 ADD Nov 2, 2018 · N457UA · Airbus A320232 · Emergency ExitsSDR CALA2018110302268Plate · damagedWHILE PERFORMING REPAIR ON +Y1292 AT FR24 DAMAGE WAS FOUND ON CROSSBEAM AFT VERTICAL FACE AROUND 5 HI LOKS. REMOVED & REPLACED FR24 UPPER FISHPLATE, P/N D5323252020000 AND LOWERFISH PLATE, P/N D5323074920000 IAW SRM 51-42-11-001, AND SRM 51-72-11.Nov 2, 2018 · N457UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018110202232Door Sill · corrodedAFT CARGO PIT DOOR THRESHOLD HAS CORROSION AROUND THE FWD NR 2 TIEDOWN FITTING AND ALONG THE OUTER EDGE FR 53-56. REMOVED AND REPLACED AFT CARGO DOOR SILL IAW SRM 51-42-11-0 01. INSP COMPLIED WITH.Oct 29, 2018 · N457UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018102902227Door Sill · corroded(CUSTOMER REQUEST) AFT CARGO PIT DOOR THRESHOLD HAS CORROSION AROUND THE FWD NR 2 TIEDOWN FITTING AND ALONG THE OUTER EDGE FR 53-56. N/R 9813949. REMOVED AND REPLACED AFT CARGO DOOR SILL IAW SRM 51-42-11-0 01. INSP. COMPLIED WITH.Oct 29, 2018 · N457UA · Airbus A320232 · Fuselage Miscellaneous Structure
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