Airbus A320-232

Service difficulty reports · 32,646

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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 YENA2026092500905Check Valve · failedFLT 1077, MCO-PUJ, RETURN TO FIELD. Y HYD RSVR OVHT. ECAM AFTER T/O. Y HYD ENG2 PUMP LOW PRESSURE, FOLLOWING QRH / ECAM BELOW 10,000 OVHT CLEARED. T/S IAW TSM 29-13-00-810-802-A. FOUND UNUSUAL NOISE WHEN E-PUMP OPERATED. REMOVED CHK VALVE 3083GM, FOUND CHK Sep 24, 2026 · N657JB · Airbus A320232 · Hydraulic System, MainSDR CALA2026092819844Oxygen Mask · no discrepancyAFT SAFETY DEMO KIT NEED TO BE REPLACED FA REPORT IT HAS A FOUL ODOR. DEMO KIT DEFERRED UNDER NEF 2522JH WITH LOCAL FBO. NO FOUL ODOR NOTED AT THIS TIME. NO BAG SENT. O2 MASK SMELLS FINE ALSO.Sep 23, 2026 · N475UA · Airbus A320232 · Passenger Compartment EquipmentSDR YENA2026092500904Unknown · odorFLT 1938, SDQ-SJU. NR 4 IFC SMELLED STRONG CHLORINE LIKE ODOR ON TAKEOFF, FOR 3-5 MINUTES. DISSIPATED ON ITS OWN.; COMPLIED WITH INFORMATION NOTICE 2017–T015 STEP 1 ISOLATED FAULT TO TYPE 10, CHLORINE ODOR, TO TSM 05–50–00–810–085–B/TSM 05–50–00–810–085–D.Sep 23, 2026 · N640JB · Airbus A320232 · Air Distribution SystemSDR CALA2026092419794Light · inoperativeEMERGENCY LIGHT ON SEAT 7C INOP. REMOVED AND INSTALLED NEW LIGHT ASSY REF AMM 33-51-11/401 CONFIG 00. OPS CHECK GOOD AT THIS TIME.Sep 23, 2026 · N472UA · Airbus A320232 · Emergency LightingSDR CALA2026092419781Light · inoperativeEMERGENCY LIGHT AT SEAT 38ABC INOPERATIVE. R & R AISLE SEAT MOUNTED EMERGENCY LIGHT. OPS CHKD OK.Sep 23, 2026 · N464UA · Airbus A320232 · Emergency LightingSDR AALA202610053912Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT MAIN LANDING GEAR DOOR FORWARD HINGE FITTING ON THE KEEL BEAM SIDE WORN ON THE LUG INNER FACE BETWEEN FR 42 AND FR 43 AT S42R - REPLACED HINGE FITTING PER EA 379411Sep 22, 2026 · N655AW · Airbus A320232 · Fuselage, Door HingeSDR AALA202609308134Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: LEFT MAIN LANDING GEAR DOOR FORWARD HINGE FITTING WORN ALLOWING THE BEARING TO MIGRATE - REPLACED THE HINGE FITTING PER CMM 52-81-18Sep 21, 2026 · N655AW · Airbus A320232 · Fuselage, Door HingeSDR YENA2026092300899Pylon · no discrepancyDURING HEAVY MAINTENANCE, ELONGATED CENTER HOLE ENTRANCE AFT POSITION PYRAMID MATING FACE FWD MOUNT ON RH PYLON; (RESOLVED ON W/O: 1477496 TASKCARD: NR-00012 ) FUR-A320-54-03371, REF AEROMAN N/R 2026-432556, PERFORMED DETAIL VISUAL INSPECTION ON CENTER HOLE ENSep 21, 2026 · N588JB · Airbus A320232 · Standard Practices/StructuresSDR YENA202609230089Pylon · no discrepancyDURING HEAVY MAINTENANCE, ELONGATED CENTER HOLE ON FWD MOUNT OF RT PYLON. PERFORMED DETAIL VISUAL INSPECTION ON CENTER HOLE ENTRANCE AFT POSITION PYRAMID MATING FACE FWD MOUNT ON RT PYLON IAW NTM 51-90-00 AND FOUND NO ELONGATED HOLE ONLY FOUND EXISTING REWORKSep 21, 2026 · N588JB · Airbus A320232 · Standard Practices/StructuresSDR YENA2026092300898Floor Support · corrodedDURING HEAVY MAINTENANCE, CORRODED FLOOR SUPPORT +Y1292, BTWN FR 12 - 24. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, SRM 51-72-11-911-001, DWG D53112813, & DWG D53110876.Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2026092300897Floor Support · corrodedDURING HEAVY MAINTENANCE, CORRODED FLOOR SUPPORT, BTWN FR 12 - 24. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, SRM 51-72-11-911-001, DWG D53112813, AND DWG D53110876.Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2026092300896Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION FLOOR SUPPORT +Y765. REMOVED AND REPLACED THE FLOOR SUPPORT BTWN FR 66 - 70 IAW SRM 51-72-11, SRM 51-42-11, DWG D53472794, DWG D53472777, AND DWG 53472809804.Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2026092300895Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND IN HOLE C LOCATED AT DOUBLE JOGGLE AREA, FR16 RT SIDE. CRACK DIRECTION IS 9 OCLOCK VIEW FROM OUTSIDE. CRACK DEPTH IS 0.165 INCH APPROX. CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00. PERFORMED Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026092300894Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND IN HOLE 7 LOCATED AT DOUBLE JOGGLE AREA, FR 20 R H SIDE. CRACK DIRECTION IS 3 OCLOCK VIEW FROM OUTSIDE. CRACK DEPTH IS 0.165 INCH APPROX. CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00. PERMANESep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026092300893Frame · crackedDURING HEAVY MAINTENANCE, A CRACK INDICATION WAS FOUND IN HOLE B IN DOUBLE JOGGLE AREA, FR 16. CRACK DIRECTION IS 3 OCLOCK VIEWED FROM OUTSIDE. CONFIRMED CRACK INDICATION USING BOROSCOPE IAW NTM 51-90-00. PERFORMED A PERMANENT REPAIR OF FRAME 16 IAW SRM 53Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026092300892Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION FLOOR SUPPORT -Y464.8 IN AFT GALLEY. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, & SRM 51-42-11.Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2026092300891Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION ON FLOORBEAM -Y765 IN THE AFT GALLEY AREA. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11, SRM 51- 42-11, DWG D53472809, DWG D53472777, & DWG D53472195.Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026092300890Fitting · corrodedDURING HEAVY MAINTENANCE, CORRODED CENTER FITTING, BTWN FR 66 - 68, STR 23R. REMOVED AND REPLACED THE FITTING IAW SRM 51-42-11, SRM 51-72-11, AND DWG D53480505.Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Attach FittingsSDR YENA2026092300889Shear Plate · corrodedDURING HEAVY MAINTENANCE, CORROSION SHEAR PLATE BTWN FRAMES 69 TO 70, STR 23R. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-72-11, SRM 51-42-11, & DWG D53474180.Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2026092300888Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION ON EXTERNAL SKIN UPPER SURFACE BTWN RIBS 2 & 3, STR 11 RT WING. TOOK MEASURES OF CORROSION L= 1.023 IN, W= 0.826 IN, MEASURES AFTER REWORK ARE L= 2.780 IN, W= 2.418 IN. EVALUATED REWORK ON SKIN & FOUND WITHIN LIMITS IAW SSep 21, 2026 · N588JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026092300887Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION UPPER SKIN, BTWN RIBS 8 & 9, LT WING T/E. MEASURES OF CORROSION ARE L=3.377IN W=1.465IN , REWORKED CORROSION ON LT WING UPPER SKIN IAW SRM 51-74-00 AND MEASURES AFTER REWORK ARE P1 L=4.042IN, W=2.842IN, EVALUATED REWORK &Sep 21, 2026 · N588JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026092300886Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION ON UPPER SKIN, BTWN RIBS 6 - 7, STRINGER 11, LT WING. REWORKED POINTS OF CORROSION (3E/A) IAW SRM 51-74-00, MEASURES OF POINTS OF CORROSION AFTER REWORK ARE P1 L= 1.858 IN, W= 1.232 IN, P2 L= 2.063 IN, W= 1.354, P3 L= 2.1Sep 21, 2026 · N588JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026092300885Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION ON STRINGER 30L, BTWN FR 61 - 62, IN THE AFT CARGO BAY. PERFORMED A REPAIR ON STRINGER 30L IAW SRM 53-00-13-300-001. THIS REPAIR IS CAT B.Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2026092300884Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION ON STRINGER 32L, BTWN FR 57 - 59 IN THE AFT CARGO BAY. PERFORMED A REPAIR ON STRINGER 32L, BTWN FR 57 - 58 IAW SRM 53-00-13-300-001, THIS REPAIR IS CLASSIFIED CATEGORY B.Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2026092300883Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION ON STRINGER 32L, BTWN FR 60 - 61. IN AFT CARGO BAY. PERFORMED A REPAIR ON STRINGER 32L, BTWN FR 60 +14 INCHES, & 2 INCHES AFT FACE OF FR 61 IAW SRM 53-00-13-300-001, THIS REPAIR IS CLASSIFIED CATEGORY B.Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2026092300882Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION ON STRINGER 32L. BTWN FR 60 - 61 IN THE CARGO BAY. PERFORMED A REPAIR ON STRINGER 32L, BTWN FR 60 + 14 INCHES & 2 INCHES AFT FACE FR 61 IAW SRM 53-00-13-300-001, THIS REPAIR IS CLASSIFIED CATEGORY B.Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2026092300881Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION IN STRINGER 33L, FR57 - 58 IN THE AFT CARGO BAY. PERFORMED A REPAIR ON STRINGER 33L BTWN FR 57 - 58 IAW SRM 53-00-13-300-001. THIS REPAIR IS CLASSIFIED CATEGORY B.Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2026092300880Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION STRINGER 33L LOCATED AT FR59 IN AFT CARGO BAY. PERFORMED A REPAIR ON STRINGER 33L, FR 59 IAW SRM 53-00-13-300-001, THIS REPAIR IS CLASSIFIED CATEGORY B,Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2026092300879Stringer · corrodedDURING HEAVY MAINTENANCE, STRINGER 36L CORRODED, BTWN FR 57 - 58. REPAIRED STRINGER 36L AND FR57 PLUS 18 INCHES IAW SRM 53-00-13-300-001, THIS REPAIR IS CLASSIFIED CATEGORY B.Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2026092300878Stringer · corrodedDURING HEAVY MAINTENANCE, CORRODED STRINGER 37L, BTWN FRAMES 56 & 57. REPAIRED THE STRINGER 37L AND 15 INCHES PLUS FR56, IAW SRM 53-00-13-300-001, THIS REPAIR IS CLASSIFIED CATEGORY B.Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2026092300877Stringer · corrodedDURING HEAVY MAINTENANCE, STRINGER 43L CORRODED BTWN FR 56 - 58. REPAIRED STRINGER 37L IAW SRM 53-00-13-300-001, THIS REPAIR IS CLASSIFIED CATEGORY B.Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YEN2026F00005Stringer · corrodedDURING HEAVY MAINTENANCE, STRINGER 43L CORRODED, BTWN FRAMES 56 - 58. REPAIR STRINGER 37L, IAW SRM 53-00-13-300-001, THIS REPAIR IS CLASSIFIED CATEGORY B.Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2026092300876Skin · damagedDURING HEAVY MAINTENANCE, ELONGATED HOLE LOWER SKIN BTWN RIBS 18 - 19, RT WING. PERFORMED A REPAIR TO THE RT WING SKIN. IAW SRM 57-27-11-283-002, AND SRM 57-21-11-300-002.Sep 21, 2026 · N588JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026092300875Fitting · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON CONTINUITY FITTING OF WINDSHIELD, CRACK LENGTH 0.125 INCH APPROX. ACCOMPLISHED A PERMANENT REPAIR IAW EA 53-0079-26 PART 5 ( COVER PLUS PARTS 1-5), RDAF 81851269/004/2026, ISSUE A, & EC A26-782-01.Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026092300874Fitting · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON CONTINUITY FITTING OF WINDSHIELD, CRACK LENGTH 0.125 INCH APPROX. ACCOMPLISHED A PERMANENT REPAIR OF THE CONTINUITY FITTING ON WINDSHIELD IAW EA 53-0079-26, PART 5, RDAF 81851269/004/2026, ISSUE A, & EC A26-Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026092300873Window Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON CENTER POST OF WINDSHIELD UPPER BOLT, CRACK LENGTH 0.062 INCH APPROX. CRACK DIRECTION 1 OCLOCK. ACCOMPLISHED A PERMANENT REPAIR OF THE WINDSHIELD FRAMED CENTER POST IAW EA 53-0079-26, RDAF 81851269/004/2026Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026092300872Window Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON CENTER POST OF WINDSHIELD UPPER BOLT, CRACK LENGTH 0.125 INCH APPROX. CRACK DIRECTION 11 OCLOCK. ACCOMPLISHED A PERMANENT REPAIR OF THE WINDSHIELD FRAME CENTER POST IAW EA 53-0079-26, RDAF 81851269/004/202Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026092300871Window Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON CENTER POST OF WINDSHIELD LOWER CORNER, CRACK LENGTH 0.100 INCH APPROX. ACCOMPLISHED A PERMANENT REPAIR OF THE WINDSHIELD FRAME CENTER POST IAW EA 53-0079-26, RDAF 81851269/004/2026, ISSUE A, & EC A26-782-0Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026092300870Window Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON CENTER POST OF WINDSHIELD LOWER CORNER, CRACK LENGTH 0.200 INCH APPROX. ACCOMPLISHED A PERMANENT REPAIR OF THE WINDSHIELD FRAME CENTER POST LOWER ATTACHMENT AREAS A & C IAW EA 53-0079-26, RDAF 81851269/004Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026092300869Skin · corrodedDURING HEAVY MAINTENANCE, RT WING UPPER SURFACE SKIN CORRODED BTWN RIBS 8 - 9, STR 11. EVALUATED REWORK ON RH WING AND FOUND WITHIN LIMITS IAW SRM 57-21-11-283-014, FIGURES 001 & 002 (SHEET 1) AND FIGURE 6 (SHEET 2); THIS ADL IS CLASSIFIED CATEGORY B.Sep 21, 2026 · N588JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026092300868Spigot · corrodedDURING HEAVY MAINTENANCE, RT PYLOHN RECEPTACLE FITTING AND SPIGOT BALL JOINT CORRODED. REMOVED AND REPLACED RECEPTACLE FITTING (SPIGOT LOWER FITTING) IAW SRM 54-51-12-300-002, STEP 2.A AND PERFORMED VISUAL INSPECTION ON SPIGOT BALL JOINT, IAW AMM 54-51-41-400Sep 21, 2026 · N588JB · Airbus A320232 · Nacelle/Pylon, Main FrameSDR YENA2026092300867Ball Joint · rustedDURING HEAVY MAINTENANCE, CORROSION RECEPTACLE FITTING AND SPIGOT BALL JOINT LT PYLON. REMOVED AND REPLACED RECEPTACLE FITTING (SPIGOT LOWER FITTING) IAW SRM 54-51-12-300-002, STEP 2.A AND PERFORMED VISUAL INSPECTION ON SPIGOT BALL JOINT IAW AMM 54--51-41-40Sep 21, 2026 · N588JB · Airbus A320232 · Nacelle/Pylon, Main FrameSDR YENA2026092300866Support Fitting · damagedDURING HEAVY MAINTENANCE, EXCESSIVE PLAY SUPPORT FITTING, FR20 IN LATERAL AVIONIC BAY. REMOVED AND REPLACED THE SUPPORT FITTING IAW SRM 51-42-11, SRM 51-72-11-911-001, AND DWG D53113601.Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2026092300865Window Frame · crackedDURING HEAVY MAINTENANCE, EA A26-782-01, WINDSHIELD FRAME, CENTER POST, LOWER NODE AREA CRACKED. PERMANENTLY REPAIRED (CONSIDERED A MAJOR REPAIR).Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, StructureSDR AALA202609238188Pressure Switch · brokenAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INTO MEX DUE TO THE FLIGHT CREW REPORTING GREEN HYDRAULIC SYSTEM ENGINE 1 PUMP LOW PRESSURE ALONG WITH A GREEN HYDRAULIC SYSTEM LOW QUANTITY ECAM WARNINGS - THE FLIGHT CREW ACCOMPLISHED THE ECAM PROCEDURES AND TSep 21, 2026 · N669AW · Airbus A320232 · Hydraulic System, MainSDR CALA2026092219683Actuator · faultedTHE AIRCRAFT CAN BE RELEASED BACK TO SERVICE AFTER EXPERIENCING A DIVERSION OR AIR TURN BACK DUE TO A MECHANICAL REASON, LOCKED BY SYSTEM. PERFORMED TSM TASK 21-61-00-810-802-A AND OPS TEST OF THE PACK TEMP-CONTROL SYSTEM IAW AMM 21-61-00, OPS TEST FAILED. RSep 21, 2026 · N441UA · Airbus A320232 · Cabin Temperature Control SystemSDR AALA202609303067Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT MAIN LANDING GEAR DOOR FORWARD HINGE FITTING HAS EXCESSIVE PLAY UE TO WEAR - REPLACED HINGE FITTING PER CMM 52-81-18Sep 20, 2026 · N655AW · Airbus A320232 · Fuselage, Door HingeSDR AALA202609225934Accelerometer · faultedAIRCRAFT WAS NOT GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO PIT DUE TO THE FLIGHT CREW REPORTING THAT ON DEPARTURE CLIMBING THROUGH APPROX 5000 MSL RECEIVED ENGINE 1 HIGH VIBRATION - THE FLIGHT CREW REPORTED THAT THE VIB VALUES RANGED INTSep 19, 2026 · N654AW · Airbus A320232 · Engine Vibration AnalyzerSDR YENA2026092100860Unknown · odorFLT 2275, PHL-FLL. FA FLIGHT ATTENADNT SMELLED ODOR AFT GALLEY ( APU SYSTEM ), ITEM PACED ON MEL 49-10-01 PLACARD INSTALLED MX-4 UPDATED MCC NOTIFIED MDDR # 630825 PULLED AND COLLARED L41 AND L42 PER MEL 49-10-01. ; C/W APU COMPRESSOR AND COMPARTMENT CLEANING Sep 19, 2026 · N537JT · Airbus A320232 · Air Distribution SystemSDR CALA2026092119564Power Supply · faultedDURING EMERGENCY LIGHT TEST FAIL MESSAGE EPSU INT LOAD EMER RT APPEARED. IAW FIM 33-51-00-810-807-A, REMOVED AND REPLACED EPSU AND BATTERY 12WL IAW AMM 33-51-38-000-001-A. NO FIX. SUGGEST FURTHER TROUBLESHOOTING OF WIRING PER FIM. CONFIRMED ALL EXIT MARKERS Sep 19, 2026 · N487UA · Airbus A320232 · Emergency Lighting
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