Airbus A320-232

Service difficulty reports · 32,652

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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 aircraft_model_key = 'A320232'
  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 AALA202512157902Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: WHILE ACCOMPLISHING MOD OF THE RUDDER HINGE LINE PER EO 5520Y001 , SEVERAL END FITTING ATTACHMENT HOLES ON THE BR3 HINGE ARM WERE FOUND WITH HOLE DAMAGE. (REPLACEMENT HINGE ARM REQUIRED BY EA 344724). MAINTENANCE ACCOMPLISHED FINAJul 24, 2025 · N665AW · Airbus A320232 · Rudder StructureSDR AALA202512153926Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: WHILE ACCOMPLISHING MOD OF THE RUDDER HINGE LINE PER EO 5520Y001 , SEVERAL END FITTING ATTACHMENT HOLES ON THE BR3 HINGE ARM WERE FOUND WITH HOLE DAMAGE. (REPLACEMENT HINGE END FITTING REQUIRED BY EA 344724). MAINTENANCE ACCOMPLISJul 24, 2025 · N665AW · Airbus A320232 · Rudder StructureSDR CALA2025072806937Unknown · odorSTRANGE ODOR ON PLANE WHEN ON PC AIR AT GATE.OR APU AIR. BURNING CHEMICAL SMELL. CABIN ODOR REPORTING SHEET NOT FILLED OUT. RAN APU AND BOTH PACKS WITH NO ODOR. PERFORMED TSM TASK 05-50-00-810-831-A. NO SMELL OF OIL, HYDRAULIC FLUID, DE-ICING FLUID, ELECTRICALJul 24, 2025 · N452UA · Airbus A320232 · Air Distribution SystemSDR CALA2025072506906Power Supply · inoperativeEPSU UNIT EMER L FAULT UPDATDED LOG WITH SDR REPORTING DUE TO BEING EMERGENCY LIGHTS SYSTEM REF GMM 04-20-16. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT AND BATTERY IAW AMM 33-51-38. OPS CHECK GOOD NO DEFECTS NOTED. NO FAULTS.Jul 24, 2025 · N439UA · Airbus A320232 · Emergency LightingSDR GTIA2025072439013Hinge Fitting · corrodedCORROSION WAS FOUND ON INNER BORE HINGE FITTING N1 AT RH ELEVATOR RAF-01 3550343-01 GENERATED-REPAIRED BORES AND INSTALLED BUSHINGS (2EA) ON HINGE FITTING #1 RH ELEVATOR P/N: D5528000200300, S/N: IC8098, I.A.W A320 SRM 55-26-41-300-004. THIS REPAIR MUST BE INSJul 23, 2025 · N624NK · Airbus A320232 · Elevator StructureSDR GTIA2025072439012Hinge Fitting · corrodedCORROSION WAS FOUND ON INNER BORE HINGE FITTING N4 AT RH ELEVATOR RAF-01 3550343-02 GENERATED-REPAIRED AND INSTALLED BUSHINGS (2EA) ON HINGE FITTING #4 AT RH ELEVATOR P/N: D5528000200300, S/N: IC8098 I.A.W A320 SRM 55-26-41-300-005. THIS REPAIR IS CATEGORY B. Jul 23, 2025 · Airbus A320232 · Elevator StructureSDR GTIA2025072439011Hinge Fitting · corrodedCORROSION WAS FOUND ON INNER BORE HINGE FITTING N6 AT RH ELEVATOR RAF-01 3550342-02 GENERATED-REPAIRED BORES AND INSTALLED BUSHINGS (2EA) ON HINGE FITTING #6 RH ELEVATOR P/N: D5528000200300, S/N: IC8098 I.A.W A320 SRM 55-26-41-300-006. THIS REPAIR IS CATEGORY Jul 23, 2025 · N624NK · Airbus A320232 · Elevator StructureSDR GTIA2025072439010Hinge Fitting · corrodedCORROSION WAS FOUND ON INNER BORE HINGE FITTING N1 AT LH ELEVATOR RAF-01 3550342-01 GENERATED-REPAIRED BOTH BORES AND REPLACED BUSHING (2EA) ON HINGE FITTING #1 LH ELEVATOR IAW SRM 55-26-41-300-004 P/N: D5528000200200 S/N: 1C814 THIS REPAIR MUST BE INSPECTED TJul 23, 2025 · N624NK · Airbus A320232 · Elevator StructureSDR GTIA2025072439009Hinge Fitting · corrodedCORROSION WAS FOUND ON INNER BORE HINGE FITTING N4 AT LH ELEVATOR RAF-01 3550341-02 GENERATED-REPAIRED BOTH BORES AND REPLACED BUSHING (2EA) ON HINGE FITTING #4 LH ELEVATOR P/N: D5528000200200 S/N: 1C8114 IAW SRM 55-26-41-300-005, THIS REPAIR IS CATEGORY B. THJul 23, 2025 · N624NK · Airbus A320232 · Elevator StructureSDR GTIA2025072439008Hinge Fitting · corrodedCORROSION WAS FOUND ON INNER BORE HINGE FITTING N6 AT LH ELEVATOR RAF-01 3550341-01 GENERATED-REPAIRED BOTH BORES AND REPLACED BUSHING (2EA) ON HINGE FITTING#6 LH ELEVATOR P/N: D5528000200200 S/N: 1C8114 IAW SRM 55-26-41-300-006, THIS REPAIR IS CATEGORY B MUSTJul 23, 2025 · N624NK · Airbus A320232 · Elevator StructureSDR CALA2025072406868Skin · damagedBREAKAWAY ON PUSHBACK TUG DRIVER MENTIONED SCRAPE ON PAINT. RE-EVALUATED SCRAPE FOUND AS FOLLOWS, SCRAPE MEASURES 17.5 INCH L BY 3 INCH W, TOTAL AREA, DEPTH OF SCRAPE IN TO METAL IS .040 DEEP. APPROX 4 INCHES OUT BOARD FROM FORWARD NLG DOOR. SCRAPE HAS A DENJul 23, 2025 · N487UA · Airbus A320232 · Landing Gear DoorsSDR CALA2025072506922Computer · faultedALL CAPTS AIR DATA AND ANTI ICE PROBES FAILED ON DEPARTURE PILOTS REP MULTI ANTI-ICE CAPT PROBE MSGS ON ECAM. SW'ED AIR DATA SW TO POS 3. MSGS STOPPED. FOUND "NO PHC 1 DATA" FAIL MSG ON PFR. SEE PHOTO. R&R PHC 1. INSTALL TEST GOOD. REF AMM 30-31-34-400-002-A &Jul 22, 2025 · N439UA · Airbus A320232 · Pitot/Static Anti-Ice SystemSDR GTIA2025072439006Oil System · leakingDIRTY SOCK SMELL ON DESCENT AND WITH APU RUNING. CONTINUOUS AND DISCOMFORTABLE, DIRTY SOCK / MUSTY DRY SMELL. APPARENT CABIN SOURCE: CABIN AIR SUPPLY VENTS. FLIGHT DECK. NO VISIBLE SMOKE/HAZE. NO MEDICAL ATTENTION REQUIRED.-REF. TSM 05-50-00-810-831-A PERFORMEJul 22, 2025 · N617NK · Airbus A320232 · APU Oil SystemSDR YENA2025072300751Uplock · failedFLT#488, MCO-ORH. (AIRCRAFT DIVERSION TO BOS) "ON GA AFTER PREVIOUS MDG NOSE LG WOULD NOT RETRACT. RECYCLED GEAR PER EICAM + GEAR RETRACTED; PER TSM 32-31-00 REMOVED AND REPLACED NLG UPLOCK ASSY IAW AMM 32-31-21. OPERATIONAL CHECK AND LEAK CHECK REQUIRED.)Jul 22, 2025 · N505JB · Airbus A320232 · Landing Gear Retraction/Extension SystemSDR 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 GTIA2025072139001Epsu · inoperativeSERVICE CHECK: EPSU (10WL) FWD L FAILED ON SYSTEM TEST -R&R EPSU ( 10WL) & ALL CHECKS GOOD IAW AMM 33-51-38Jul 20, 2025 · N630NK · Airbus A320232 · Emergency LightingSDR AALA202507216697Sign · inoperativeAIRCRAFT WAS GROUNDED: AFT L2 EMERGENCY EXIT LIGHT INOP EVEN AFTER EPSU BATTERY CHANGE REFERENCE MIC 1367669. MAINTENANCE REPLACED 52WL EMERGENCY EXIT SIGN REF AMM 33-51-16.Jul 20, 2025 · N663AW · Airbus A320232 · Emergency LightingSDR AALA202507214031Sign · inoperativeAIRCRAFT WAS GROUNDED: AFT L2 EMERGENCY EXIT LIGHT INOP EVEN AFTER EPSU BATTERY CHANGE REFERENCE MIC 1367669. MAINTENANCE REPLACED 45WL EMERGENCY EXIT SIGN REF AMM 33-51-16.Jul 20, 2025 · N663AW · Airbus A320232 · Emergency LightingSDR YENA2025072300749Unknown · odorFLT#1454, SJU-FLL. "FA'S REPORT ELECTRICAL ODOR DURING LANDING AFTER ARRIVING AT THE GATE (FWD GALLEY); INSPECTED L & R AVIONICS COMPT, INSPECTED FLT DECK CB'S, GALLEYS' CB'S, COFFEEMAKERS, WITH NO ODOR PRESENT. ACCOMPLISHED TSM 24-00-00-810-823-1 WITH NO 30 DJul 19, 2025 · N638JB · Airbus A320232 · Air Distribution SystemSDR 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 AALA202507211563Bottle · low pressureAIRCRAFT WAS GROUNDED: LH FWD PASSENGER DOOR ACCUMULATOR AT 0 PSI. MAINTENANCE CHARGED LH FWD PASSENGER DOOR DAMPER IAW AMM 52-10-00.Jul 19, 2025 · N663AW · Airbus A320232 · Passenger/Crew DoorsSDR AALA202507212190Power Supply · inoperativeAIRCRAFT WAS GROUNDED: DURING PS CHECK FOUND 12 EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED EPSU BATTERY FOR 11WL IAW AMM 33-51-38.Jul 19, 2025 · N663AW · Airbus A320232 · Emergency LightingSDR GTIA2025072138996Unknown · odorFA C ON DECENT TO CHS SMELT A BURNING SMELL ON LANDING. FLYING TO BWI ON LANDING AND TAXI SMELT A BURNING CHEMICAL SMELL AGAIN THAT LASTED 10 MIN. -FOLLOWED TSM 05-50-00-810-831-A INSPECTED APU AND BOTH ENG OIL LEVEL. OIL LEVEL GOOD. INSPECTED APU INLET. NO COJul 18, 2025 · N607NK · Airbus A320232 · Air Distribution SystemSDR CALA2025072106798Probe · faultedREJECTD T/O 50-60 KIAS DUE TO SPLIT POWER SETTING W/ NO ECAM ITEM UPDATED WITH CURRENT P2T2 SENSOR. ENG #2 REPLACED AT ENG #2 , P2T2 SENSOR PER AMM 73-22-11/401 CONFIG 13 . ALL TEST OK.Jul 18, 2025 · N484UA · Airbus A320232 · Fuel Control/Reciprocating EnginesSDR CALA2025072106784Wire · pulledSEAT 30C EMERGENCY LIGHTING INOP - WIRE PULLED FROM PLUG REMOVED OLD PIN AND STRIPPED WIRE RE-CRIMPED NEW SOCKET ON TO WIRE AND INSTALLED IN CONNECTOR AT SEAT 30C REF AWM 33-51-08 PAGE 52A. INSTALLED LIGHT AT SEAT 30C REF TASK 33-51-19-400-002-A OPS CHECK GOODJul 18, 2025 · N427UA · Airbus A320232 · Light System WiringSDR CALA2025072106783Elec Connector · not seatedEMERGENCY EXIT LIGHT IN ROW 24 SEAT C NOT ILLUMINATING CHECKED CONNECTION, CONNECTION SECURE. RELAMPED EMERGENCY LIGHT IN ROW 24 SEAT C PER AMM TASK 33-51-19-000-002-A. NO HELP. RESEATED CONNECTOR OPS CHECKED GOOD.Jul 18, 2025 · N445UA · Airbus A320232 · Light System WiringSDR CALA2025072106780Light · broken29C EMERGENCY EXIT LIGHT BROKEN PLACED ON MEL OK TO MEL COMPLIED WITH MEL REMOVED AND REPLACED 29C EMERGENCY EXIT LIGHT REF AMM 33-51-18. OPS CHECK GOOD AT THIS TIME.Jul 18, 2025 · N481UA · Airbus A320232 · Emergency LightingSDR CALA2025072106779Power Supply · no testOPERATIONAL CHECK OF THE EMERGENCY POWER SUPPLY UNITS BY BITE-CHECK EMERGENCY LIGHTS FAIL TEST AT CIDS PANEL. FAULT EPSU INT LOAD FWD L ATA 33-51-38. CYCLED BREAKERS NO HELP. REMOVED CEILING PANEL AT DOOR 1 LEFT. DID TEST OF LIGHTING BOX FAULTING INTERIOR LIGJul 18, 2025 · N466UA · Airbus A320232 · Emergency LightingSDR CALA2025072106777Elec Connector · damagedEMERGENCY EXIT LIGHT OVERHEAD IN ROW 27 SEAT C NOT ILLUMINATING CHECKED CONNECTION, CONNECTION SECURE. NEEDS MORE TROUBLESHOOTING RELAMPED LIGHT BULBS FOR OVERHEAD EMERGENCY LIGHT IN ROW 27 SEAT C REF IPC 33-51-11-01. NO HELP. REINSTALLED 2 EACH PINS IN THE CJul 18, 2025 · N445UA · Airbus A320232 · Light System WiringSDR YENA2025072200745Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON LOWER INB FASTENER HOLE DOOR STOP FITTING #1 FR 68 LH. CRACK DIRECTION 12 OCLOCK. CRACK D= 0.160 INCH; (RESOLVED ON W/O: 1396415 TASKCARD: NR-00049) REF AEROMAN WO 2025 187/1 NR 2025-367243 PERFORMED PERMANENJul 17, 2025 · N537JT · Airbus A320232 · Fuselage Main, StructureSDR YENA2025072200743Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE 3 (LOWER/INBOARD POSITION) LOCATED AT FR16 LH, DOOR STOP FITTING 1. AT PASSENGER CABIN. CRACK DEPTH = 0.080 INCHES, CRACK DIRECTION: 7 OCLOCK; (RESOLVED ON W/O: 1396415 TASKCARD: NR-00032) REF AJul 17, 2025 · N537JT · Airbus A320232 · Fuselage Main, StructureSDR CALA2025071806709Seal · brokenFOUND ENGINE NR 1 FWD PYLON TO NACELLE PROFILES PANEL BROKEN. INSTALLED E#1 FWD PYLON TO NACELLE PROFILES PANEL REFERENCE AMM TASK 54-57-22-400-003-A.Jul 17, 2025 · N430UA · Airbus A320232 · Nacelle/Pylon, Main FrameSDR AALA202507185241Wire Harness · damagedAIRCRAFT WAS GROUNDED: 22C WHITE SEAT MOUNTED EMERGENCY AISLE LIGHT INOP. MAINTENANCE REPLACED HARNESS 5409VB AT SEAT 22C IAW AWM 33-51-08.Jul 16, 2025 · N655AW · Airbus A320232 · Light System WiringSDR CALA2025072206836Frame · crackedLH FR 35 AT STR 30 FRAME FWD FACE HAS CRACK JUST BELOW FASTENER ADJACENT HOLE 2 IN OUTER FLANGE CRACK EXTENDS FROM FASTENER APPROX .200 IN RADIUS PER HAECO LCQ N/R 9298611/28611 GEN BY V892444 ACCOMPLISHED INTERIM REPAIR AT LH FR35 STGR30L HOLE NO. 2 WITH NO DJul 15, 2025 · N465UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2025072206835Plate · damagedR/W FUEL PANEL LANDING AT 640KB HAS HOLES OUT OF ROUND PER HAECO LCQ N/R 9298704/28704 GEN BY N078348ESFR COMPLETED AFTER EVALUATION, PERFORMED REPAIR ON ONE OUT OF ROUND HOLE AT RIGHT WING FUEL PANEL 640KB BETWEEN RIBS 15-16 IAW SRM 57-21-11-300-002. REAMED HJul 15, 2025 · N465UA · Airbus A320232 · Wing, Plate/SkinSDR CALA2025072206834Skin · damagedR/W FUEL PANEL LANDING AT 640LB HAS HOLES OUT OF ROUND PER HAECO LCQ N/R 9298705/28705 GEN BY N078348ESFR COMPLETED AFTER EVALUATION, PERFORMED REPAIR ON ONE OUT OF ROUND HOLE AT RIGHT WING FUEL PANEL 640LB BETWEEN RIBS 16-17 IAW SRM 57-21-11-300-002. REAMED HJul 15, 2025 · N465UA · Airbus A320232 · Wing, Plate/SkinSDR CALA2025071806735Fuel Cap · missingFUEL CAP MISSING ON ARRIVAL. ACFT DOES NOT HAVE A FUEL CAP. NO DAMAGE AROUND COUPLING NOTED AT THIS TIME. INSTALLED UNDERWING FUEL CAP AS REQUIRED IAW AMM 28-25-41.Jul 15, 2025 · N444UA · Airbus A320232 · Fuel StorageSDR CALA2025071606620Floor Support · corrodedAFT CARGO COMPARTMENT, BETWEEN FRS 48-52A STRINGER 38R, FLOOR SUPPORT PROFILE HAS CORROSION AND ELONGATED FASTENER HOLES. REMOVED FLOOR SUPPORT PROFILE IAW SRM 51-44-11/001 REPLACED FLOOR PANEL IAW SRM 51-42-11/001.Jul 15, 2025 · N461UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2025072206833None · noneCOMPLY WITH CFR 121.1109" EX ISTING REPAIR FOUND WITH NO RECORDS AT L/H FR 66-67 STR 24L-26L ACCOMPLISHED INTERIM REPAIR AT LH FR66-67 STGR 24L - 28L WITH NO DEVIATION IAW ECRA 5341-01507. ACCOMPLISH INITIAL INSPECTION OF LH FR 66-67 STGR 24LH ? 28LH REPAIR Jul 14, 2025 · N465UA · Airbus A320232 · Standard Practices/StructuresSDR YENA2025071600729Engine · failedFLT#2922, NAS-JFK. (AIRCRAFT PERFORMED AIR TURNBACK TO NAS) "ENGINE #2 BANG AND SEIZE. INSPECTED ENGINE #2 IAW AMM 05-51-26 FOUND NO AIRFRAME DEFECTS ENGINE #2 METAL, DEBRIS FOUND IN EXHAUST REMOVED AND REPLACED #2 ENGINE IAW AMM 71-00-20-400-040. REFERENCE Jul 13, 2025 · N793JB · Airbus A320232 · Engine (Turbine/Turboprop)SDR CALA2025071506596None · no discrepancyOIL DRIPPING FROM NR 2 ENG DRAIN MAST INSPECTED ENGINE 2 DRAIN MAST, FOUND DRIPS FROM ACOC. OPENED ENGINE FAN COWLINGS, FOUND NO EVIDENCE OF LEAK AT ACOC, ALL SURFACES UNDER COWLING DRY, AIRCRAFT OK FOR SERVICE AT THIS TIME REF TSM 05-50-00-810-822-AJul 13, 2025 · N464UA · Airbus A320232 · Standard Practices/StructuresSDR GTIA2025071438990Door · leakingEME EXIT ROW 134A,B,C IS MAKING LOUD NOISE-SWAPPED EMERGENCY DOOR LH SIDE WITH RH SIDE FWD AND AFT PER AMM 52-21-11, PERFOMED PRESSURIZATION PER AMM 05-28-30. LH SIDE NO LEAKING, RH SIDE AFT LEAKING. THE HATCH WITH SN UH25387 WAS IDENTIFIED AS THE SOURCE OF TJul 13, 2025 · N617NK · Airbus A320232 · Emergency ExitsSDR YENA2025071400727Unknown · odorFLT#887, JFK-SXM. "STRONG ODOR DIRTY SOCK SMELL ON APPROACH AT 7500 FEET; C/W INFO NOTICE 2017-T015 SECTION A, ISOLATED FAULT TO TYPE 10 ODOR ENVIRONMENTAL. NO 30-DAY HISTORY. PERF LEVEL A ECS DECON IAW TSM 05-50-00-810-085-B. A.C OK FOR SVC. MCC LEO NOTIFIED.Jul 11, 2025 · N661JB · Airbus A320232 · Air Distribution SystemSDR AALA202507149840Light · inoperativeAIRCRAFT WAS NOT GROUNDED: OVER WING EMERGENCY EXIT LIGHT (2R) DOES NOT ILLUMINATE. MAINTENANCE REPLACED EMERGENCY "EXIT" LIGHT PLATE IAW AMM 33-51-17.Jul 11, 2025 · N663AW · Airbus A320232 · Emergency LightingSDR CALA2025071406503Wire Splice · damagedPROCEDURE - AFTER DOING CABIN EMERGENCY LIGHTING TEST, FAULT INDICATED EPSU INT LOAD EMER L. EMERGENCY LIGHTS INOP FROM SEAT ROW 26- 28. BITE TEST EMER L PWR SUPPLY, SHOWED SHORT IN LIGHTING SYSTEM. AT ROW 27ABC, FOUND DAMAGED SPLICE AT FLOOR-TO-SEAT CONNECTORJul 11, 2025 · N475UA · Airbus A320232 · Light System WiringSDR YENA2025071400726Unknown · odorFLT#205, EWR-FLL. INFLIGHT REPORTED SLIGHT ODOR OF FUEL DURING TRANSITION FROM CRUISE TO DECENT; COMPLIED WITH INFO NOTICE 2017-T015, SECTION A ISOLATED FUALT TO TYPE 10-SUSPECT CUSTOMER WAS USING VIC'S IN ROW 3-4-PER TSM 05-50-00-810-085-B/TSM 05-50-00-810-08Jul 11, 2025 · N547JB · Airbus A320232 · Air Distribution SystemSDR CALA2025071606634Elec Connector · looseDOOR AFT CARGO ECAM. PLACED AFT CARGO DOOR INDICATION ON MEL. VERIFIED AFT CARGO DOOR IS CLOSED AND LATCHED. OK TO CONTINUE. PLR SHOWS AFT CARGO DR SAFETY MECHANICAL PROXIMITY SENSOR (32WV) TGT POS, POSSIBLE SENSOR 32WV OR DOOR HANDLE LINKAGE MAY NEED ADJUJul 10, 2025 · N435UA · Airbus A320232 · Door System WiringSDR CALA2025071606612Intercostal · corrodedUPON REMOVAL OF PROFILE PANEL AFT CARGO, FRS 58-59 FOUND CORROSION ON UPPER FLANGE. REMOVED AND REPLACED INTERCOSTAL PLATE IN AFT CARGO FR 58-FR59 STR 38R IAW A320 SRM 51-42-11/001 51-44-11/001.Jul 9, 2025 · N461UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2025071100720Sign · detachedFLT#2931, SJU-PUJ. "R1 ABOVE DOOR EMERGENCY EXIT SIGN BROKEN / FELL OFF IN FLIGHT; REMOVED AND REPLACED R1 DOOR EXIT LIGHT LENS ALL NORMAL. REF 33-20-00, MX-4 UPDATED."Jul 9, 2025 · N594JB · Airbus A320232 · Emergency LightingSDR YENA2025071100719Unknown · odorFLT#69, BOS-FLL. "F/A INDICATE MUSTY SMELL FROM ROW 4-13 FAINT SMELL; COMPLIED WITH INFO NOTICE 2017-T015,SECTION B2 IDENTIFIED ODOR TYPE 1 DECON LEVEL 2 IAW AMM TSM 05-50-00-810-831-A"Jul 9, 2025 · N809JB · Airbus A320232 · Air Distribution System
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