Airbus A320-232

Service difficulty reports · 32,648

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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 AALA202604284966Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND LOCATED ON UPPER TENSION BOLT, WINDSHIELD CENTER POST LH SIDE. CRACK DIRECTION: 1 OCLOCK (VIEW ON LH SIDE), CRACK LEN GHT= 0.200 INCH APPROX, AD-2020-17-03. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR INSFeb 5, 2026 · N653AW · Airbus A320232 · Fuselage Main, StructureSDR CALA2026020913632Hinge Fitting · gougedNR 2 ENG OTBD FAN COWL NR 3 HINGE HAS GOUGE FWD SIDE OF FITTING FROM CONTACT WITH ANTI ICE DUCT V-BAND CLAMP IAW AAR LCQ NR 9294106/3 8106. REMOVED GOUGES ON NR 2 ENG OTBD FAN COWL NR 3 HINGE FITTING FWD SIDE IAW SRM 54-02-00 REPAIR 012 TO A SMOOTH CONTOUR FIFeb 5, 2026 · N497UA · Airbus A320232 · Nacelle/Pylon, Main FrameSDR YENA2026020600151Unknown · odorFLT 1676, KIN- FLL, CREW REPORTS ODOR SIMILAR TO DIRTY SOCKS IN CABIN NEAR ROW 5 APU RUNNING WITH BLEED ON.; COMPLIED WITH INFO NOTICE 2017-T015, STEP Q ISOLATED FAULT TO TYPE 10. RAN A/C PACKS NO ODOR PRESENT PER TSM 05-50-00-810-085B AND TSM 05-50-00-810-0Feb 5, 2026 · N652JB · Airbus A320232 · Air Distribution SystemSDR YENA2026020400150Unknown · odorFLT 1141 BDL-PBI, NR 4 F/A REPORTED ODOR FINAL APPROACH PILOT DID NOT EXPERIENCE ANY ODOR. ACCOMPLISHED INFO NOTICE 2017-T015M. VERIFIED ODOR NOT TO BE PRESENT AND NO HISTORY OF ODOR EVENTS. DETURMINED TO BE MISCELLANEOUS TYPE 10 PER TABLE 2.NO CORRECTIVE AFeb 5, 2026 · N665JB · Airbus A320232 · Air Distribution SystemSDR GTIA2026020539271Flashlight · faultedFWD GALLEY LH FLASHLIGHT BLINKING RED. R & R FLASHLIGHT IN FWD GALLEY LT SIDE IAW DRAWING #A320-EMER EQUIP.Feb 5, 2026 · N635NK · Airbus A320232 · Emergency EquipmentSDR CALA2026022013949Skin · dentedEXTERIOR FUSELAGE SKIN DENTED BETWEEN FR 27-28, S37-38L. EVALUATED DENT AT FR 27-28, S37L-38L IAW SRM 53-21-11-283 -020, FIG 2, SHEET 1 & 2. DENT IS TYPE 1 AS D/A IS LESS THAN 0.1 00IN. PERFORMED DVI WITH NO CRACKS OR DISCREPANCIES IAW NTM 51-9 0-00-007-A. Feb 3, 2026 · N497UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2026020913630Actuator · vibrationUNKOWN VIBRATION FELT ON SHORT FINAL STARTED FLAPS 3 MORE AT FLA PS FULL REF MT 53-005 AND TSM TASK 05-50-00-810-801-A TO IDENTIFYING VIBRATION VIBRATION REPORT REF DOCUMENTS ATTACHED FOR DECISION TABLE. TSM 05-50-00/201 CONFIG 00 RE-EVALUATED VIBRATION FORM GFeb 3, 2026 · N489UA · Airbus A320232 · Trailing Edge Flap ActuatorSDR YENA2026020400147Unknown · odorFLT 1233, MCO-SJU. DURING FLIGHT IDLE DESCENT FROM CRUISE ALTITUDE. DIRTY SOX ODOR AFTER 7-8 MINS INTO DESCENT IN FLT DECK & AFT CABIN. ODOR DISSIPATED AFTER ENGINES POWERED UP & DID NOT RETURN.; COMPLIED WITH INFO NOTICE 2017-T015 STEPS 1 AND 2 IDENTIFY ODFeb 3, 2026 · N595JB · Airbus A320232 · Air Distribution SystemSDR GTIA2026020539269Skin Panel · cracked"CRACK INDICATION ON FRAME 16 LH SIDE OPEN FASTENER HOLE H2 IN CROSSBEA M SPLICING AREA. CRACK DIRECTION 12 OCLOCK CRACK L=0.187"" D=0.097"" RAF-01 6011272-01 CREATED. -INSTALLED NEW HARDWARE ON HOLE H2 LOC ON FRAME 16 LH SIDE OPEN FASTENER HOLE H2 IN CROSSBEFeb 2, 2026 · N606NK · Airbus A320232 · Fuselage Main, Plate/SkinSDR GTIA2026020539268Skin Panel · corrodedCORROSION CHANNEL RUDDER LOWER AREA ON VERTICAL STABILIZER RAF-01 6011262-02 GENERATED.-PERFORMED PERMANENT REPAIR ON CHANNEL RUDDER LOWER AREA ON VERTICAL STABILIZER I.A.W. A320 SRM 55-41-19-300-011-C1 THIS REPAIR IS CATEGORY A I.A.W. A320 SRN 51-11-14Feb 2, 2026 · N606NK · Airbus A320232 · Vertical Stabilizer, Plate/SkinSDR GTIA2026020539267Skin Panel · damaged"DOUBLER REPAIR EXTERNAL SKIN LOC .BTW FR.31TO FR.33 AND STRG 41R TO STRG 43R ON LOWER FUSELAGE L=0.897"" W=.665"". RAF-01 6011274-02 CREATED. -EVALUATED EXISTING REWORK P1,P2,P3 AND FOUND WITHIN LIMITS IAW A320 SRM 51-21-11-283-018 AND PERFORMED PERMANENT REPFeb 2, 2026 · N606NK · Airbus A320232 · Fuselage Main, Plate/SkinSDR GTIA2026020539266Skin · corrodedCORROSION LOWER SURFACE OF TOP SKIN OVERHANG LOC.BTW RIB7 AND RIB9 ON LH WING RAF-01 6011259-02 GENERATED -PERFORMED PERMANENT REPAIR ON TRAILING EDGE OVERHANG AT LEVEL OF RIB 7 LOC LH WING I.A.W. EA #57-0004-26. THIS REPAIR IS CATEGORY B POST REPAIR INSPECTIOFeb 2, 2026 · N606NK · Airbus A320232 · Wing, Plate/SkinSDR CALA2026020513595Wire · brokenSEAT 36CBA EMERGENCY EXIT LIGHT INOP WIRE IS BROKEN FROM SEAT HARNESS CONNECTOR REQUESTING MEL 3350C FOR SEAT 36CBA EMERGENCY EXIT SEAT LIGHT WIRES HAVE BEEN SECURED OKAY TO DEFER EMERGENCY ESCAPE PATH LIGHT PER MEL 3350C CORRECTION SEAT 36CBA FLOOR PROXIMITY Feb 2, 2026 · N464UA · Airbus A320232 · Light System WiringSDR CALA2026020513591Potable Water · leakingALL FWD DRAIN HOLES ON BOTTOM OF ACFT DRAINING WATER. WATER LINE IS INSTALLED & LEAK CHECKED. DRAIN VALVE INSTALLATION STILL NEEDS TO BE COMPLETED FROM STEP 4 A12. COMPLETED STEPS UP TO D. (1) ON DRAIN VALVE INSTALLATION IAW AMM 38-14-45-400-001-A. GALLEY LEFeb 2, 2026 · N4901U · Airbus A320232 · Potable Water SystemSDR YENA2026020400146Unknown · odorFLT 1229, EWR-CUN. DURING ENG RUN WITH NR 1 ENG AND NR 2 PACK. INFLIGHT IMMEDIATELY NOTICED SIGNIFICANT FUMES ODOR IN VICINITY OF ROW 22. INBOUND CREW HAD 2 FUME INCIDENTS ON INBOUND FLIGHT TO CUN. CREATING NEED FOR ENG RUN PRIOR TO BOARDING. ACCOMPFeb 2, 2026 · N703JB · Airbus A320232 · Air Distribution SystemSDR YENA2026020400142Panel · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND AT KEEL BEAM BOTTOM PANEL FASTENER HOLES 5, CRACK DEPTH 0.105 INCHES FWD DIRECTION; REF AEROMAN NR 2025-682674 WO 2025 413/1 ACCOMPLISHED REPAIR OF CRACK DAMAGE ON HOLE #5 ON THE CENTER FUSELAGE KEEL BEAM BOTTOMFeb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, KeelSDR YENA2026020400141Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CENTER OPOST LOWER ATTACHMENT, VERTICAL FLANGE AREA RH SIDE. CRACK LENGTH 0.196 INCHES APPROX; REF AEROMAN NR 2025-682430 WO 2025 413/1 ERFORMED REPAIR TO CRACKS AFFECTING THE WINDSHIELD FRAME CENTFeb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026020400140Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FR 36 IN FASTENER HOLE LOC Y1292 MORE 2 INCH UPPER SURFACE OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX CRACK AT 12 O'CLOCK CRACK DEPTH 0.157 INCH APPROX IN FWD CARGO COMPARTMENT; PERFORMED REPAIR IAW EC A26-01Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026020400139Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 36 IN OPEN HOLE FASTENER LOC Y1292 MORE 4 INCH UPPER SURFACE OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX CRACK AT 5 O'CLOCK, CRACK DEPTH 0.160 INCH APPROX IN FWD CARGO COMPARTMENT (1 EA); PERFORMED REPAIFeb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026020400138Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 36 IN OPEN HOLE FASTENER LOCATION Y1292 MORE 5 INCH UPPER SURFACE OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX CRACK AT 6 O'CLOCK POSITION, CRACK DEPTH 0.131 INCH APPROX IN FWD CARGO COMPARTMENT (1EA); PEFeb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026020400137Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FR 36 IN OPEN FASTENER LHOLE LOC Y1292 MORE 8 INCH UPPER SURFACE OF THE PRESSURE DECK MEMBRANE TO CNETER WING BOX. CRACK AT 1 O'CLOCK CRACK DEPTH 0,140 INCH APPROX IN FWD CARGO COMPARTMENT (1 EA); REF AEROMAN NR 2Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026020400136Fitting · crackedDURING HEAVY MAINTENANCE: CRACK ON CONTINUITY FITTING LH AT COCKPIT; REF AEROMAN NR 2025-682704 WO 2025 413/1 PERFORMED REPAIR TO CRACKS AFFECTING THE WINDSHIELD FRAME CENTER POST LOWER NODE AREA R/H VERTICAL FLANGE AND CONTINUITY FITTINGS ASPER AEROMAN EA# 53Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026020400135Structure · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE ZONE 1, POSITION 4 OF VERTICAL STRINGER RADIUS IN CENTER FUSELAGE ON FR 36, CRACK DEPTH 0.129 INCH CRACK DIRECTION 3 AND 4 O'CLOCK VIEW LOOKING AFT; REF AEROMAN NR 2025-682309 WO 2025 413/1 PERFORMEFeb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026020400134Stringer · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE ZONE 1 POSITION 6 OF VERTICAL STRINGER REDIUS IN CNETER FUSELAGE ON FRAME 36 CRACK DEPTH O.085 INCH CRACK DIRECTION 6 O'CLOCK VIEW LOOKING AFT; PERFORMED REPAIR IAW EC NO. A25-1157-01 AND EA NO. 57-Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2026020400133Stringer · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE ZONE W1, POSITION 1 OF VERTICAL STRINGER RADIUS IN CENTER FUSELAGE ON FRAME 36 CRACK DEPTH 0.100 INCH CRACK DIRECTION 12 O'CLOCK VIEW LOOKING AFT; PERFORMED REPAIR IAW EC A25-1157-01 AND EA 57-117-Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YEN2026F00001Stringer · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE ZONE 2, POSITION 2 OF VERTICAL STRINGER RADIUS IN CENTER FUSELGAE ON FRAME 36, CRACK DEPTH 0.130 INCH. CRACK DIRECTION 8 O'CLOCK VIEW LOOKING AFT; PERFORMED REPAIR IAW EC A25-1157-01 AND EA 57-0017-Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2026020400131Stringer · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE ZONE 2, POSITION 5 OF VERTICAL STRINGER RADIUS IN CENTER FUSELAGE ON FRAME 36. CRACK DEPTH 0.127 INCH, CRACK DIRECTION 8 AND 9 O'CLOCK VIEW LOOKING AFT; PERFORMED REPAIR IAW EC A25-1157-01 AND EA 5Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2026020400132Stringer · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLDE ZONE 2, POSITION 5 OF VERTICAL STRINGER RADIUS IN CENTER FUSELAGE ON FRAME 36. CRACK DEPTH 0.127 INCH CRACK DIRECTION 8 AND 9 O'CLOCK VIEW LOOKING AFT; PERFORMED REPAIR IAW EC NO. A25-1157-01 AND Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2026020400130Stringer · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE ZONE 2, POSITION 5 OF VERTICAL STRINGER RADIUS IN CNETER FUSELAGE ON FRAME 36. CRACK DEPTH 0.127 INCH, CRACK DIRECTION 8 AND 9 O'CLOCK VIEW LOOKING AFT; PERFORMED REPAIR IAW EC A25-1157-01 AND EA 5Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2026020400129Seat Track · brokenDURING HEAVY MAINTENANCE: BROKEN SEAT TRACK Y1292, -Y765 AND -Y1292 BOLT AT LEVEL FR47 IN PASSENGER CABIN (3EA); REF AEROMAN WO# 2025-413/1 WCC# 2025-682634 FOR WORK PERFORMED; REMOVED AND REPLACED SEAT TRACK BOLTS LOC. Y1292, -Y765 AND -Y1292 AT LEVEL FR47 IFeb 2, 2026 · N587JB · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR YENA2026020400128Stringer · corrodedDURING HEAVY MAINTENANCE: CORROSION STRINGER 43L LOC BTW FR 56 TO FR 57 IN AFT CARGO COMPARTMENT (CPCP FINDING); REF AEROMAN NR 2025-682543 WO 2025 413/1 REMOVED AND REPLACED STRINGER 43LH LOC BTW FR 54 TO FR 60 IN AFT CARGO COMPARTMENT IAW A320 SRM 51-72-11, Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2026020400127Structure · crackedDURING HEAVY MAINTENANCE: CRACK FLOOR STRUCTURE UPPER SECTION CONNECTION LOC FR 66 AT LEVEL STR 23KH AT AFT GALLEY AREA (1EA); REMOVED AND REPLACED FLOOR STRUCTURE UPPER SECTION CONNECTION LOC FR 66 AT LEVEL STR 23LH SIDE AT AFT GALLEY AREA (1EA)IAW A320 SRM 5Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2026020400126Stringer · corrodedDURING HEAVY MAINTENANCE: CORROSION STRINGER 43L LOC BTW FR 57 TO FR 58 IN AFT CARGO COMPARTMENT (CPCP FINDING); REF AEROMAN NR 2025-682544 WO 2025 413/1 REMOVED AND REPLACED STRINGER 43LH LOC BTW FR 54 TO FR 60 IN AFT CARGO COMPARTMENT IAW A320 SRM 51-72-11, Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2026020400125Stringer · corrodedDURING HEAVY MAINTENANCE:CORROSION STRINGER 43L LOC BTW FR 54 TO FR 56 IN AFT CARGO COMPARTMEN T (CPCP FINDING); REF AEROMAN NR 2025-682549 WO 2025 413/1 REMOVED AND REPLACED STRINGER 43LH LOC BTW FR 54 TO FR 60 IN AFT CARGO COMPARTMENT IAW A320 SRM 51-72-11, Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2026020400124Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION FALSE SPAR BOX LOWER SKIN UPPER SURFACE AT LEVEL RIB 6A ON RH WING (CPCP FINDING); ACCOMPLISHED REPAIR OF CORROSION DAMAGE ON THE RH WING, BOTTOM SKIN PANEL 3 UPPER SURFACE AT LEVEL RIB 6A, FALSE SPAR BOX AREA I.A.W AEM AE Feb 2, 2026 · N587JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026020400123Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION SKIN PANEL INTERNAL STRUCTURE LOC BTW FR 16 AND 17 LOWER AREA ON LATERAL AVIONIC COMPARTMENT LT SIDE. PERFORMED PERMANENT REPAIR IAW EA# 53-0089-25, EC# A26-029-0. REPAIR IS CAT A AND NO FURTHER INSPECTION IS REQUIRED. WORFeb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026020400122Fitting · corrodedDURING HEAVY MAINTENANCE: CORROSION ON SPIGOT LOWER FITTING ON LH PYLON; (RESOLVED ON W/O: 1420259 TASKCARD: NR-00037) REF AEROMAN NR 2025-682782 WP 2025-413/1. REMOVED AND REPLACED THE SPIGOT LOWER FITTING ON LH PYLON IAW SRM 54-51-283-002, SRM 51-44-11-801, Feb 2, 2026 · N587JB · Airbus A320232 · Nacelle/Pylon, Main FrameSDR YENA2026020400121Fitting · corrodedDURING HEAVY MAINTENANCE: CORROSION IN THE SPIGOT LOWER FITTING ON RH PYLON; (RESOLVED ON W/O: 1420259 TASKCARD: NR-00038) REF AEROMAN NR 2025-682784 WP 2025-413/1. REMOVED AND REPLACED THE SPIGOT LOWER FITTING ON RHPYLON IAW SRM 54-51-283-002, SRM 51-44-11-80Feb 2, 2026 · N587JB · Airbus A320232 · Nacelle/Pylon, Main FrameSDR YENA2026020400120Web · corrodedDURING HEAVY MAINTENANCE: CORROSION FLOOR STRUCTURE WEB LOC. BTW FR69/70 AT LEVEL STR23L AT AFT GALLEY AREA (1 EA) (CPCP FINDING); REF AEROMAN NR 2025-682631 WO 2025 413/1 REMOVED AND REPLACED FLOOR STRUCTURE WEB LOC BTW FR69 TO FR70 AT LEVEL STR23L AFT GALLEYFeb 2, 2026 · N587JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2026020400119Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION SKIN PANEL INTERNAL STRUCTURE LOC BTW FR 16 AND 17 LOWER AREA ON LATERAL AVIONIC COMPARTMENT LH SIDE; PERFORMED PERMANENT REPAIR IAW EA# 53-0089-25, EC# A26-029-0. REPAIR IS CAT A AND NO FURTHER INSPECTION IS REQUIRED. WORKFeb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026020400118Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE BOTTOM SKIN PANEL NO. 3, BTW REAR SPAR AND FA LSE REAR SPAR, AND BTW WX2825 STIFFENER DATUM AND RIB DATUM INBOARD DI AGONAL ON LH WING (CPCP FINDING); REF AEROMAN NR 2025-682418 WO 2025 413/1 CCOMPLISH REPAIR OFeb 2, 2026 · N587JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026020400117Doubler · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / NLG COMPARTMENT REINFORCEMENT DOUBLER AT FR16-17 AND Y+250 / CORROSION - PERMANENT REPAIR; REFERENCES: /1/ AEM EA 53-0089-25 REV 0 (COVER AND PARTS 1 - 5) /2/ AIRBUS RDAF 81702470/003/2025#A /3/ REPAIR IFeb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026020400116Floorbeam · crackedDURING HEAVY MAINTENANCE: WINGS / CENTER WING BOX / FRONT SPAR VERTICAL STRINGERS & HORIZONTAL FLOOR BEAMS / @ LEVEL OF FR36 & Y-1292, Y-765, Y-254, Y+254, Y+765 & Y+1292 / CRACKS - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 57-0117-25 REV. 0 (COVER + PARTS Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026020400115Skin · corrodedDURING HEAVY MAINTENANCE: WINGS / LH WING / BOTTOM SKIN PANEL 3 / RIBS 6A, REAR SPAR-FALSE REAR SPAR / CORROSION - TEMPORARY REPAIR; REFERENCES: /1/ AEROMAN EA 57-0122-25 COVER & PARTS 1-11 /2/ AIRBUS RDAF 81692663/023/2025 ISSUE A /3/ AIRBUS TD/81692663/012/2Feb 2, 2026 · N587JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026020400114Pressure Deck · crackedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / PRESSURE DECK PANEL / FR36 RHS / ATTACHMENT HOLES / CRACKS – TIME LIMITED REPAIR; REFERENCES: /1/ AEROMAN EA 53-0085-25 REV. 0 (COVER + PARTS 1-8) /2/ AIRBUS DOSSIER 81696490 /3/ AIRBUS RDAF 81696490/003/2Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026020400113Window Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / WINDSHIELD FRAME / CTR POST LOWER NODE AREA VERTICAL FLANGE RHS & CONT. FITTING LHS / CRACKS - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-0081-25 (COVER + PARTS 1-5) /2/ AIRBUS DOSSIER 81689336 /3/ Feb 2, 2026 · N587JB · Airbus A320232 · Fuselage Main, StructureSDR GTIA2026020239265Megaphone · inoperativeAFT MEGAPHONE INOPERATIVE. R & R AFT MEGAPHONE IAW EMERGENCY EQUIP DRAWINGS.Feb 2, 2026 · N603NK · Airbus A320232 · Emergency EquipmentSDR CALA2026020313534Potable Water · leakingFOUND AFT GALLEY FLOODED WITH WATER. REMOVED ALL GALLEY CARTS FROM AFT GALLEY & COULD NOT FIND SOURCE OF LEAK. ATTEMPTED TO SERVICE POTABLE WATER, BUT ACFT WOULD NOT RECEIVE & HOLD WATER. WATER SAME OUT OF EVERY DRAIN ORFICE ON BELLEY OF ACFT. OPENED AFT CFeb 1, 2026 · N4901U · Airbus A320232 · Potable Water SystemSDR YENA2026020200111None · noneFLT 2252, SJU - SJU. LEVEL 1 ODOR EVENT, FWD GALLEY & ROWS 1 - 5. COMPLIED WITH INFORMATION NOTICE 2017-T015, STEP 1. ISOLATED FAULT TO TYPE 10, POSIBLE SOURCE PASSENGER OR CREW HYGIENE , WIPE OUT SEATS COVERS FROM ROW 1 TO 5 FOLLOWED TSM 05-50-00-810-085-BFeb 1, 2026 · N603JB · Airbus A320232 · Standard Practices/StructuresSDR YENA2026020200110Apu · contaminatedFLT 813, HPN- PBI. AFTER PARKING AT THE GATE THE F3 ADVISED ME OF A VINEGAR SCENT ON FINAL APPROACH. NO MEDICAL ATTENTION REQUIRED, DEICED IN HPN. ADVISED THE SCENT WAS DIFFERENT, THIS WAS ONLY EXPERIENCED BY F3 & F4. REF INFO NOTICE 2017-T015M, FOUND SOURFeb 1, 2026 · N807JB · Airbus A320232 · Airborne Auxiliary Power Unit (APU) System
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