Service difficulty reports

1,770,704 reports of malfunctions and defects, newest first. Air carriers must report; 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'
  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 DALA2026092105247Skin · corrodedON MG FOUND CORROSION AROUND LAV EXHAUST VENT. TRANSFERRED TO NRF 1 IAW TOPP 50-30-05. 278320. SUMMARY: CORROSION REMOVED, DAMAGE CONTAINED, AND REPAIR INSTALLED IAW ER /A 636893-14, REV ORIGINAL. RII'S COMPLIED WITH. (LP: 9490440, AIRCRAFT WAS GROUNDED)Sep 18, 2026 · N344NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2026092105244Unknown · odorVERY STRONG PAINT/CHEMICAL ODOR IN FLIGHT DECK. INITIALLY AFTER APU BLEED ON. SHORTLY AFTER SMELL WAS ALSO NOTICEABLE IN AFT GALLEY. SCENT REMAINED UNTIL BLEED SELECTED OFF. SMOKE AND FUMES REPORT SENT TO MCC. ACCOMPLISHED W/C 0550-2002 EVENT CONSIDERED TYPE Sep 18, 2026 · N344NB · Airbus A319114 · Air Distribution SystemSDR DALA2026092105243Engine · power lossRTO - RIGHT ENG DID NOT SPOOL UP AS FAST AS THE LEFT ENGINE. NR 1 ENG REACHED 80% N1 WHILE END #2 WAS MUCH SLOWER. PERFORMED TSM 71-00-00-810-807-A, ENG SLOW TO ACCEL; PERFORMED A319 AMM 73-21-60-740-028-A, CORRECT FAULTS OF ENG SCHED MAINT RPTS; NO FAULTS RESep 18, 2026 · N336NB · Airbus A319114 · Engine (Turbine/Turboprop)SDR DALA2026091805234Support Fitting · corrodedLEFT MLG FWD TRUNNION SUPPORT FITTING LOWER O/B ATTACH POINT SHOWS SIGNS OF WEAR/CORROSION. C/W ER/A NO 636972-14 (1818779)(AIRCRAFT GROUNDED)Sep 18, 2026 · N592NW · Boeing 757351 · Wing, Landing Gear Attach FittingsSDR DALA2026091805233Support Fitting · corrodedLEFT MLG FWD TRUNNION SUPPORT FITTING LOWER INBD ATTACH POINT SHOWS SIGNS OF WEAR/CORROSION. C/W FINAL ER/A NO 636972-14 (1818773)(AIRCRAFT GROUNDED)Sep 18, 2026 · N592NW · Boeing 757351 · Wing, Landing Gear Attach FittingsSDR DALA2026091805232Support Fitting · corrodedRIGHT MLG FWD TRUNNION SUPPORT FITTING LOWER O/B ATTACH POINT SHOWS SIGNS OF WEAR/CORROSION. C/W ERA 636944-14 (1818772)(AIRCRAFT GROUNDED)Sep 18, 2026 · N592NW · Boeing 757351 · Wing, Landing Gear Attach FittingsSDR DALA2026091805231Support Fitting · corrodedRT MLG FWD TRUNNION SUPPORT FITTING LOWER I/B ATTACH POINT SHOWS SIGNS OF WEAR/CORROSION. CORRECTIVE ACTION: C/W ERA 621582-14 (1818770)(AIRCRAFT GROUNDED)Sep 18, 2026 · N592NW · Boeing 757351 · Wing, Landing Gear Attach FittingsSDR DALA2026091805230Floor Support · corrodedCORROSION ON FLOOR STGRS LBL 2.9 AND RBL 2.9 STA 1510 AT AFT CARGO COMP. REPAIRED PER SRM 53-00-53 (1818942)(AIRCRAFT GROUNDED)Sep 18, 2026 · N595NW · Boeing 757351 · Fuselage Miscellaneous StructureSDR DALA2026091905238Sign · missingDURING SVC CK FOUND OVERHEAD PASS EXIT SIGN LIGHT ASSY OVER WING MISSING. REPLACED INSTALLED OVERHEAD PASS SIGN LIGHT ASSY PER B737 AMM 33-51-01. OPS CK NORMAL. (LP 8898142 - AIRCRAFT WAS GROUNDED)Sep 18, 2026 · N851DN · Boeing 737932ER · Emergency LightingSDR DALA2026091905236Wire · chafedPROX EMERGENCY LIGHTS ROWS 19 TO 21 INOP ALSO L1070 EXIT LOC SIGN INOPERATIVE. WHILE INSPECTING WIRING BETWEEN D16378 AND SEAT ROW 19 FOUND 2 CHAFING WIRES. RE-TERMINATED THE 2 WIRES ALSO REPLACED THE M1695 FUSES, OPS CHK GOOD ALL DONE PER B737 AMM 33-51 ANDSep 18, 2026 · N846DN · Boeing 737932ER · Light System WiringSDR DALA2026091905235Seal · leakingAIRCRAFT 5043, DURING DESCENT AT 19,000 FT. FA'S REPORTED MUSTY ODOR ORIGINATING AT THE AFT GALLEY AND BEING AS STRONG UP TO ROW 30. THE SMELL LESSENED BUT CONTINUED TO THE FORWARD GALLEY. NO SMELL WAS DETECTED ON THE FLIGHT DECK. SMELL LESSENED SLIGHTLY AT LOSep 18, 2026 · N543DE · Airbus A321271NX · Turbine Engine Oil SystemSDR 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 AALA202609185949Ground Wire · brokenAIRCRAFT WAS GROUNDED: WHILE CHECKING EMERGENCY LIGHTING FOR PERIODIC SERVICE CHECK FOUND SEATS 14 AND 15 SEAT MOUNT LIGHT INOPERATIVE - MAINTENANCE FOUND A BROKEN GROUND AT PLUG LOCATION 7260VC5-A AND REPAIRED PER ESPM 20-56-21. LIGHT OPS CHECK GOOD. OK FOR SSep 18, 2026 · N191UW · Airbus A321211 · Light System Wiring