Airbus A320-232

Service difficulty reports · 32,646

Newest first. General aviation reporting is voluntary.

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 YENA2026091800855Floorbeam · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON THE HORIZONTAL FLOOR BEAM RADIUS BACKSIDE OF THE FRONT SPAR VERTICAL STRINGER Ñ2 FRAME 36. CRACK L= 0.315 INCH.; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00031 ) REF AEROMAN WO# 2026-279/1 NR# 2026-348509 ACCOMSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026091800854Floorbeam · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON THE HORIZONTAL FLOOR BEAM RADIUS BACKSIDE OF THE FRONT SPAR VERTICAL STRINGER Ñ3 FRAME 36. CRACK L= 0.375 INCH.; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00032 ) REF AEROMAN WO# 2026-279/1 NR# 2026-348510 ACCOMSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026091800853Floorbeam · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON THE HORIZONTAL FLOORBEAM RADIUS BACKSIDE OF THE FRONT SPAR VERTICAL STRINGER Ñ4 FRAME 36. CRACK L= 0.640 INCH.; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00033 ) REF AEROMAN WO# 2026-279/1 NR# 2026-348511 ACCOMPSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026091800852Floorbeam · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON THE HORIZONTAL FLOOR BEAM RADIUS BACKSIDE OF THE FRONT SPAR VERTICAL STRINGER Ñ5 FRAME 36. CRACK L= 0.435 INCH; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00034 ) REF AEROMAN WO# 2026-279/1 NR# 2026 348512 ACCOMPSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026091800851Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 35 BULK HEAD RH SIDE AT LEVEL OF STGR 30 AT OPEN FASTENER HOLE LOWER OUTBOARD COMMON TO MILLED COUPLING, CRACKED DIRECTION IS 9OCLOCK, CRACK DEPTH IS 0.120 INCH APPROX., IN FWD CARGO COMPARTMENT (1EA); (RESOSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800850Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 35 BULK HEAD LH SIDE AT LEVEL OF STGR 30 AT OPEN FASTENER HOLE LOWER OUTBOARD COMMON TO MILLED COUPLING, CRACK DIRECTION ARE 4 AND 9OCLOCK, CRACKDEPTH IS 0.120 INCHAPOROX., IN FWD CARGO COMPARTMENT (2EA); (RESep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800849Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 35 RH SIDE AT LEVEL OF STGR 30 AT OPEN FASTENER HOLE LOWER AFT COMMON TO SKIN,CRACK DIRECTIONS ARE 2 AND 6 OCLOCK, CRACK DEPTH IS 0.110 INCH APPROX, IN FWD CARGO COMPARTMENT (2EA); (RESOLVED ON W/O: 1435456 TSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800848Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 35 LH SIDE AT LEVEL OF STGR 30 AT OPEN FASTENER HOLE LOWER AFT COMMON TO SKIN,CRACK DIRECTIONS ARE 11 AND 6 OCLOCK, CRACK DEPTH IS 0.110 INCH APPROX, IN FWD CARGO COMPARTMENT (2EA); (RESOLVED ON W/O: 1435456Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800847Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE 2 INCH O/B FROM -Y1292 APPROX.,CRACK DIRECTION IS 12 OCLO CK, CRACK DEPTH IS 0.085 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA ); (RESOLVED ON W/O: 14Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800846Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE 3 INCH O/B FROM -Y1292 APPROX.,CRACK DIRECTION IS 6 OCLOC K, CRACK DEPTH IS 0.085 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA); (RESOLVED ON W/O: 1435Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800845Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FASTENER HOLE 5 INCH O/B FROM -Y1292 APPROX.,CRACK DIRECTION IS 12 OCLO CK, CRACK DEPTH IS 0.085 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA ); (RESOLVED ON W/O: 143Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800844Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 20, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.085 I NCH APPROX., IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00058 ) ACCOMSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800843Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 19, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.081 I NCH APPROX., IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00059 ) ACCOMPSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800842Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 14, CRACK DIRECTION IS 6 OCLOCK, CRACK DEPTH IS 0.094 IN CH APPROX., IN FWD CARGO COMPARTMENT ALL WORK ACCOMPLISHED ON AEROMAN WO 2026 279/1 NR2026-3Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800841Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 22, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.085 I NCH APPROX., IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00061 ) ACCOMPSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800840Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 23, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.079 I NCH APPROX., IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00062 ) ACCOMPSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800839Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 24, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.082 I NCH APPROX., IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00063 ) ACCOMPSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800838Pressure Deck · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 27, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.095 I NCH APPROX., IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00064 ) ACCOMPSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800837Pressure Deck · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 26, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.085 I NCH APPROX., IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00065 ) ACCOMPSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800836Pressure Deck · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE 7 INCH O/B FROM -Y1292 APPROX.,CRACK DIRECTION IS 12 OCLO CK, CRACK DEPTH IS 0.085 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA ); (RESOLVED ON W/O: 14Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800835Pressure Deck · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 LH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE 5 INCH O/B FROM Y1292 APPROX., CRACK DIRECTIONS ARE 6 AND 12 OCLOCK, CRACK DEPTH IS 0.080 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA); (RESOLVED ON WSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800834Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 LH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE 6 INCH O/B FROM Y1292 APPROX.,CRACK DIRECTION IS 6 OCLOCK , CRACK DEPTH IS 0.085 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA);(RESOLVED ON W/O: 143545Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800833Pressure Deck · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 LH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE 4 INCH O/B FROM Y1292 APPROX., CRACK DIRECTION IS 12 OCLOC K, CRACK DEPTH IS 0.085 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA); (RESOLVED ON W/O: 143Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800832Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 16, CRACK DIRECTION IS 12 OCLOCK , CRACK DEPTH IS 0.080 INCH APPROX., IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00070 ) ACCOMPSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800831Pressure Deck · corrodedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 LH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE 2 INCH O/B FROM Y1292 APPROX., CRACK DIRECTION ARE 6 AND 1 2 OCLOCK, CRACK DEPTH IS 0.085 INCH APPROX., IN FWD CARGO COMPARTMENT (2 EA); (RESOLVED ON WSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800830Pressure Deck · corrodedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 LH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE 3 INCH O/B FROM Y1292 APPROX.,CRACK DIRECTION IS 12 OCLOC K, CRACK DEPTH IS 0.085 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA); (RESOLVED ON W/O: 1435Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800829Pressure Deck · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 LH SIDE IN PRESSURE DECK MEMBRANE OPEN F ASTENER HOLE 9 INCH O/B FROM Y1292 APPROX.,CRACK DIRECTION IS 12 OCLO CK, CRACK DEPTH IS 0.105 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA ); (RESOLVED ON W/O: 143Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800828Pressure Deck · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 28, CRACK DIRECTION IS 6 OCLOCK, CRACK DEPTH IS 0.084 IN CH APPROX., IN FWD CARGO COMPARTMENT ; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00074 ) ACCOMPSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800827Pressure Panel · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON FRAME 36 LH SIDE IN PRESSURE DECK MEMBRANE A REA IN OPEN FASTENER HOLE Ñ 13 CRACK DIRECTION: 05 OCLOCK , CRACK DEPT H=0.113 INCH; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00075 ) ACCOMPLISH MAJOR REPAIR ON THE Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800826Pressure Deck · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE 6 INCH O/B FROM -Y1292 APPROX.,CRACK DIRECTION IS 6 OCLOC K, CRACK DEPTH IS 0.085 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA); (RESOLVED ON W/O: 1435Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800825Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION ON BOTTOM SKIN PANEL ON INBOARD SIDE FLAP TRACK CENTERLINE LH WING BTW RIB 5 THRU RIB 6; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00077 ) ACCOMPLISHED MEJOR REPAIR OF CORROSION AFFECTING LA WING BOTTOM SKIN PANEL 3, UPPER SURFSep 18, 2026 · N523JB · Airbus A320232 · Trailing Edge FlapsSDR YENA2026091800824Fire Bottle · dischargedDURING HEAVY MAINTENANCE, AEROMAN DISCHARGED FIRE EXTINGUISHER BOTTLE APU; REF: ARM W/O 2026-279/1 N/R 2026-348729 R&R DISHARGED FIR BOTTLE IAW AMM 26-22-41-000-001-A AND 26-22-42-400-001-A TEST OK IAW 26-13-00-710-001-ASep 18, 2026 · N523JB · Airbus A320232 · Extinguishing SystemSDR YENA2026091800823Pressure Panel · crackedDURING HEAVY MAINTENANCE, EA A26-699-01, CENTER FUSELAGE, FR36 LH PRESSURE PANEL ATTACHMENT HOLES CRACKED. TIME LIMITED REPAIR (CONSIDERED AS A MAJOR REPAIR)Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800822Floorbeam · crackedDURING HEAVY MAINTENANCE, EA A26-595-01, CENTER BOX / FRONT SPAR VERTICAL STRINGERS & HORIZONTAL FLOORBEAMS, AT LEVEL OF FR36. CRACKS – PERMANENT REPAIR (CONSIDERED AS A MAJOR REPAIR)Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026091800821Pressure Blkhd · crackedDURING HEAVY MAINTENANCE, EA A26-716-01, FR35 FWD FACE TO PRESSURE BULKHEAD ATTACHMENT @ LEVEL OF STGR 30RH, FASTENER HOLES W1 & H2, CRACK DAMAGE – TIME LIMITED REPAIR (CONSIDERED A MAJOR REPAIR)Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, BulkheadSDR YENA2026091800820Pressure Panel · damagedDURING HEAVY MAINTENANCE, EA A26-700-01, FR36 RH PRESSURE PANEL ATTACHMENT HOLES CRACKED - TIME LIMITED REPAIR (CONSIDERED A MAJOR REPAIR)Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800819Skin · corrodedDURING HEAVY MAINTENANCE, EA A26-815-01. LH WING BOTTOM SKIN PANEL 3 UPPER SURFACE RIBS 6A BTWN FALSE SPAR TO REAR SPAR CORRODED. TIME LIMITED REPAIRSep 18, 2026 · N523JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026091800818Pressure Blkhd · crackedDURING HEAVY MAINTENANCE, EA A26-710-01, FR35 PRESSURE BULKHEAD CRACKED - TIME-LIMITED REPAIR (CONSIDERED A MAJOR REPAIR)Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, BulkheadSDR 2026F00212Cone · wrong partMLG WHEEL ASSY P/N C20195162 S/N 42248 WAS RECEIVED FROM CUSTOMER AIR SERBIA AS FAIL-ON-FIT. DURING THE SHOP INSPECTION IT WAS FOUND THAT INAPPROPRIATE BEARING CONE P/N NP542842-20629 WAS INSTALLED INSTEAD OF P/N 48290-20629 (REF. CMM 32-47-46 R15). WHEEL WASep 18, 2026 · Airbus A320232 · Wheel/Ski/FloatSDR YENA2026092100859Unknown · odorFLT 8348, LAS-JFK. DURING DESENT BOTH PILOTS DETECTED 'MAGIC MARKER' SMELL REPORTED BY PREVIOUS CREW SMELL WAS STRONG ENOUGH THAT BOTH PILOT NEEDED O2 AS A PRECAUSTION AIRCRAFT IS NOT FIT GOR SERVICCE (EVENT LASTED FROM 23000-5000) ; APU WAS REPLACED DUE TO ODSep 17, 2026 · N715JB · Airbus A320232 · Air Distribution SystemSDR CALA2026092119596Transceiver · faultedELECTRICAL BURNING ODOR AFTER LANDINGPICTURE UPDATE. BRIEFED FLIGHT CREW. CREW STATED A BURNING ODOR WAS PRESENT IN FLIGHT DECK, AND WAS NOTIEABLE UPON ENTERING THE COCKPIT. CAPT ALSO REPORTED HEARING A CRACKLING/POPPING NOISE NEAR THE LT INSTRUMENT PANEL. VSep 17, 2026 · N438UA · Airbus A320232 · Weather Radar SystemSDR YENA2026091800817Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE OVER HANGLOC. RIB 8 ON LH WING (CORROSIONFINDING) ONLY FOR TRACKING. ON UPPER SURFACE LOWER SURFACE AT FALSE REAR SPAR AND TEOH BTW RIB WX4010.2-WX4349; REF AEROMAN WO 2026 217/1 NR 41Sep 17, 2026 · N793JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026091800816Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE OVERHANG LOC. RIB 8 ON LH WING (CORROSIONFINDING); REF AEROMAN WO 2026 217/1 ACCOMPLISHED REPAIR OF CORROSION DAMAGE ON THE LH WING TOP SKIN PANEL 2, LOWER SURFACE AT FALSE REAR SPAR ASep 17, 2026 · N793JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026091800815Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE OVERHANG LOC. RIB 7 ON LT WING (CORROSION FINDING); FREF AEROMAN WO 2026 217/1 NR 414483 ACCOMPLISHED REPAIR OF CORROSION DAMAGE ON THE LH WING TOP SKIN PANEL 2, LOWER SURFACE AT FALSE RESep 17, 2026 · N793JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026091800814Dummy Rail · corrodedDURING HEAVY MAINTENANCE, CORROSION FOUND ON RAIL DUMMY Y503.2 LOCATED BETWEEN FR 12 AND FR 16 AT FWD GALLEY AREA; (RESOLVED ON W/O: 1480444 TASKCARD: NR-00014 ) REMOVED AND REPLACED RAIL DUMMY Y503.2 LOCATED BTW FR 12 AND FR 16 AT FWD GALLEY AREA IAW A320 SRSep 17, 2026 · N793JB · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR YENA2026091800813Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION FOUND AT FLOORBEAM Y940 AT FWD GALLEY AREA. (CPCP FINDING ); (RESOLVED ON W/O: 1480444 TASKCARD: NR-00016 ) REF AEROMAN WO# 2026-217/1 N/R# 2026 - 414659; REMOVED AND REPLACED FLOORBEAM Y940 AT FWD GALLEY AREA I.A.W. A320 SRSep 17, 2026 · N793JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026091800811Unknown · odorFLT 066, ABQ-JFK. CABIN ODOR EVENT. THE FLIGHT CREW REPORTED THAT THERE WAS A FOUL ODOR FROM THE ENVIRONMENTAL SYS ON DESCENT INTO JFK WITH IDLE THRUST SELECTED. ODOR ISOLATION PROCEDURE PERFORMED & NR 1 A/C PACK WAS ISOLATED, ODOR DISSIPATED. ODOR CAME BACK Sep 17, 2026 · N636JB · Airbus A320232 · Air Distribution SystemSDR AALA202609180655Oil System · leakingAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND TRHGE AIRCRAFT RETURNED TO PHL DUE TO THE FLIGHT CREW REPORTING THAT AN ODOR WAS PRESENT IN THE AFT CABIN INITIALLY AFTER ENGINE START BUT QUICKLY DISSIPATED HOWEVER AFTER TAKE OFF THE FLIGHT ATTENDANTS REPOSep 17, 2026 · N657AW · Airbus A320232 · APU Oil SystemSDR YENA2026091800810Repair · corrodedDURING HEAVY MAINTENANCE, CORROSION FOUND ON EXISTING REPAIR LOCATED AT LEVEL FR68 STR23 RH AFT GALLEY AREA. (RESOLVED ON W/O: 1480444 TASKCARD: NR-00017 ) REF AEROMAN WO 2026-217/1 NR 2026-414626, REMOVED AND REPLACED EXISTING REPAIR LOCATED AT LEVEL FR68 Sep 17, 2026 · N793JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026091800809Battery Pack · failedDURING HEAVY MAINTENANCE, DURING PERFORM OPERATIONAL OF EPSU BY TEST CHECK IAWAMM33-51-00-710-001 BATTERY12WL FAULT. THE BATTERY MUST BE REPLACED; (RESOLVED ON W/O: 1480444 TASKCARD: NR-00037 ) REFERENCE AEROMAN WO 2026 217/1 NR 414952 REMOVED AND REPLACED BATSep 17, 2026 · N793JB · Airbus A320232 · Emergency Lighting
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