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 AALA202607108855Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: LEFT-HAND FORWARD PASSENGER DOOR EMERGENCY CYLINDER/ACCUMULATOR REQUIRES SERVICING. MAINTENANCE CHARGED LEFT-HAND FORWARD PASSENGER DOOR EMERGENCY CYLINDER/ACCUMULATOR TOCORRECT PRESSURE IAW AMM 52-10-00.Jul 7, 2026 · N649AW · Airbus A320232 · Passenger/Crew DoorsSDR YENA2026070900528Unknown · odorFLT # 367, HPN-PBI. STRONG DIRTY SOCK SMALL WHILE DESCENDING THROUGH 13000 FT; COMPLIED WITH INFO NOTICE 2017-TT015 STEPS 1 & 2 IDENT ODOR TYPE 10 MISC. INSPECT A/C & APU. CLEANED APU COMPARTMENT OF RESUDUAL OIL, NO ACTIVE LEAKS FROM APU OR DRAINS.PERFORMED DEJul 7, 2026 · N709JB · Airbus A320232 · Air Distribution SystemSDR AALA202607096674Wire Harness · no testAIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT AT SEAT ROW 4ABC IS INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT ASSEMBLY (AALA202607091732) AND HARNESS (AALA202607096674) PER CMM 25-40-07.Jul 7, 2026 · N649AW · Airbus A320232 · Light System WiringSDR AALA202607091732Light · no testAIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT AT SEAT ROW 4ABC IS INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT ASSEMBLY (AALA202607091732) AND HARNESS (AALA202607096674) PER CMM 25-40-07.Jul 7, 2026 · N649AW · Airbus A320232 · Emergency LightingSDR AALA202607093410Uplock · fault messageAIRCRAFT WAS GROUNDED: THE AIRCRAFT RETURNED TO CLT DUE TO THE FLIGHT CREW REPORTING THAT AFTER GEAR RETRACTION LANDING GEAR DOORS NOT CLOSED. THE AIRCRAFT LANDED SAFELY AT CLT AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE REPLACED THE RIGHT-HAND MAIJul 6, 2026 · N649AW · Airbus A320232 · Landing Gear Position and WarningSDR AALA202607099499Battery · no testAIRCRAFT WAS NOT GROUNDED: ONE OF THE AFT GALLEY FLASHLIGHTS WAS NOT SECURED INTO THE MOUNT AND WILL NOT TURN ON. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY.Jul 6, 2026 · N663AW · Airbus A320232 · Emergency EquipmentSDR CALA2026070917625Unknown · odorFA SMELLED BURNED TOAST ODOR IN AFT GALLEY. INSPECTED AFT GALLEY AND CABIN FOR FUMES AND SIGNS OF SMOKE IAW AMM 05-51-10. NO SIGNS OF ODOR. RAN THE APU AND PACKS AND COULD NOT REPLICATE ODOR. INSPECTED THE 2001VU PANEL REF AMM 24-92-00. NO DAMAGE OR ODOR FOUJul 6, 2026 · N432UA · Airbus A320232 · Air Distribution SystemSDR YENA2026070700516Unknown · odorFLT # 1468, PBI-HPN. LEVEL 2 FUME EVENT. STRONG PERSISTENT MAGIC MARKER SMELL DESCENDING THROUGH12,000; CLOUDS AND PRECIPITATION IN THE AREA. SMELLED BY BOTH PILOTS, BUT NO F/A. SUSPECT PACK 1. SHUT OFF PACK 1 AND CLOSED X BLEED. SMELL GOT WEAKER AFTER SEVERALJul 6, 2026 · N623JB · Airbus A320232 · Air Distribution SystemSDR YENA2026070900558Skin · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND (BY ROTOTEST INSPECTION) IN OPEN FASTENER HOLE LOCATED ON FRAME 35 (FUSELAGE SIDE SHELL) AFT POSITION BELOW STRG 30 R H SIDE, CRACK DIRECTION: 07 OCLOCK, D1-D2= 0.165 INCH APPROX, AD RELAT ED TASK CARD NO. A320-Jul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026070900557Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND (BY ROTOTEST INSPECTION) IN OPEN FASTENER HOLE LOCATED ON FRAME 35 COUPLING AREA BULKHEAD ABOVE STR 30RH, CRACK DIREC TION: 07 OCLOCK, D1-D2= 0.073 INCH APPROX AD RELATED TASK CARD NO. A32 0-53-1372-01. ACCOMPLJul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026070900556Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 6, OPEN FASTENER H OLE ON ZONE 1, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.110 INCH , IN FWD CARGO COMPARTMENT (1 EA)(-Y1292); ACCOMPLISHED REPAIR OF CRACK DAMAGES ON THE CENTEJul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026070900555Floorbeam · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 HORIZONTAL FLOOR BEAM VERTICAL RADIUS OF THE BACK SIDE OF THE SPAR VERTICAL STRINGER 2 ZONE 2 CRACK LENGTH IS 0 .650 INCH APPROX, IN FWD CARGO COMPARTMENT (1 EA); REF AEROMAN NR 2026-299175 WO 2026 196/1 Jul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026070900553Floorbeam · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 HORIZONTAL FLOORBEAM VERTICAL RADIUS OF THE BACK SIDE OF THE SPAR VERTICAL STRINGER 3 ZONE 2 CRACK LENGTH IS 0 .380 INCH APPROX, IN FWD CARGO COMPARTMENT (1 EA); ACCOMPLISHED PERMANENT REPAIR OF CRACK DAMJul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026070900552Floorbeam · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 HORIZONTAL FLOORBEAM VERTICAL RADIUS OF THE BACK SIDE OF THE SPAR VERTICAL STRINGER 3 ZONE 1 CRACK LENGTH IS 0 .850 INCH APPROX, IN FWD CARGO COMPARTMENT. ACCOMPLISHED PERMANENT REPAIR OF CRACK DAMAGES ONJul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026070900551Floorbeam · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 HORIZONTAL FLOORBEAM VERTICAL RADIUS OF THE BACK SIDE OF THE SPAR VERTICAL STRINGER 4 ZONE 2 CRACK LENGTH IS 0 .510 INCH APPROX, IN FWD CARGO COMPARTMENT (1 EA)(-Y254); ACCOMPLISHED PERMANENT REPAIR OF CJul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026070900550Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 4,OPEN FASTENER HOLE ON ZONE1, CRACK DIRECTION IS 1 OCLOCK, CRACK DEPTH IS 0.095 INCH,IN FWD CARGO COMPARTMENT (1EA)(-Y254); REF AEROMAN WO 2026-196/1 NR 299010 ACCOMPLISHED PERMANENTJul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026070900549Beam · crackedDURING HEAVY MAINTENANCE, ACCOMPLISHED PERMANENT REPAIR OF CRACK DAMAGES ON THE CENTER WING BOX FRONT SPAR HORIZONTAL BEAMS AT LEVEL FR36 (Y-254)(RADIUS ON ZONE 1) IAW AEROMAN EA 57-0036-26, REV. 0 (COVER PLUS PARTS 1 AND 2); AIRBUS RDAF 81801723/003/2026, Jul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026070900548Floorbeam · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 HORIZONTAL FLOOR BEAM VERTICAL RADIUS OF THE BACK SIDE OF THE SPAR VERTICAL STRINGER 5 ZONE 2 CRACK LENGTH IS 0 .520 INCH APPROX, IN FWD CARGO COMPARTMENT (1 EA); REF AEROMAN NR 2026 299168 WO 2026 196/1Jul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026070900547Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 HORIZONTAL FLOOR BEAM VERTICAL RADIUS OF THE BACK SIDE OF THE SPAR VERTICAL STRINGER 5 ZONE 1 CRACK LENGTH IS 0.480 INCH APPROX, IN FWD CARGO COMPARTMENT (1 EA), REF AEROMAN NR 2026 299167 WO 2026 196/1 Jul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026070900546Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 2, OPEN FASTENER HO LE ON ZONE 2, CRACK DIRECTION IS 11 OCLOCK, CRACK DEPTH IS 0.100 INCH, IN FWD CARGO BAY (1 EA)(+Y765). REF AEROMAN NR 2026 299015 WO 2026 196/1 ACCOMPLISHED PERMAJul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026070900530Hinge Arm · damagedDURING HEAVY MAINTENANCE, STABILIZERS, VERTICAL STABILIZER, HINGE ARM BR3 & FORK END FITTING ASSY ELONGATED HOLES. TIME LIMITED REPAIR (CONSIDERED MAJOR REPAIR)Jul 5, 2026 · N806JB · Airbus A320232 · Vertical StabilizerSDR AALA202607095553Proximity Sensor · defectiveAIRCRAFT WAS GROUNDED: LANDING GEAR LEVER REMAINED LOCKED FOR SEVERAL MOMENTS AFTER BEING AIRBORNE BEFORE UNLOCKING AND ALLOWING GEAR TO BE RETRACTED. MAINTENANCE REPLACED MAIN LNDING GEAR PROXIMITY SENSORS 20GA (AALA202607098789) AND 22GA (AALA202607095553) PJul 5, 2026 · N601AW · Airbus A320232 · Landing Gear Position and WarningSDR AALA202607098789Proximity Sensor · defectiveAIRCRAFT WAS GROUNDED: LANDING GEAR LEVER REMAINED LOCKED FOR SEVERAL MOMENTS AFTER BEING AIRBORNE BEFORE UNLOCKING AND ALLOWING GEAR TO BE RETRACTED. MAINTENANCE REPLACED MAIN LNDING GEAR PROXIMITY SENSORS 20GA (AALA202607098789) AND 22GA (AALA202607095553) PJul 5, 2026 · N601AW · Airbus A320232 · Landing Gear Position and WarningSDR YENA2026070900545Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 2, OPEN FASTENER HO LE ON ZONE 1, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.095 INCH, IN FWD CARGO COMPARTMENT (1 EA)(+Y765); (RESOLVED ON W/O: 1457737 TASKCARD: NR-00041 ) REF Jul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026070900544Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 3, OPEN FASTENER HO LE ON ZONE 2, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.110 INCH, IN FWD CARGO COMPARTMENT (1 EA)(+Y254); ACCOMPLISHED PERMANENT REPAIR OF CRACK DAMAGES ON TJul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026070900543Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 3, OPEN FASTENER HO LE ON ZONE 1, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.120 INCH, IN FWD CARGO COMPARTMENT (1 EA)(+Y254); ACCOMPLISHED PERMANENT REPAIR OF CRACK DAMAGES ON TJul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026070900542Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 4, OPEN FASTENER HO LE ON ZONE 2, CRACK DIRECTION IS 11 OCLOCK, CRACK DEPTH IS 0.100 INCH, IN FWD CARGO COMPARTMENT (1 EA)(-Y254); (RESOLVED ON W/O: 1457737 TASKCARD: NR-00044 ) REF Jul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026070900541Skin · damagedDURING HEAVY MAINTENANCE, EVIDENCE OF REWORK LOCATED ON EXTERNAL SKIN IN FROM O FFR28 PLUS1.487 IN AT LEVEL STR32 PLUS 1.795 INCH UNDER,LH LOWER FUSELAGE. ACCOMPLISHED REPAIR ON EXISTING REWORK LOCATED ON FR28 PLUS 1.487 IN AT LEVEL STR32 PLUS 1.795 INCH UJul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026070900540Skin · damagedDURING HEAVY MAINTENANCE, EVIDENCE OF REWORK LOCATED ON EXTERNAL SKIN BTW FR26 PLUS1.681 IN AT LEVEL STR 32 PLUS 2.567 IN UNDER, LT LOWER FUSELAGE. REF AEROMAN WO 2026-196/1NR 299252.ACCOMPLISHED REPAIR ON EXISTING REWORK LOCATED ON EXTERNAL SKIN BTW FR26 PLJul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026070900539Skin · damagedDURING HEAVY MAINTENANCE, EVIDENCE OF REWORK LOCATED ON EXTERNAL SKIN BTW FR27 TO FR28 AT LEVEL STR32 TO STR33 LH LOWER FUSELAGE;(RESOLVED ON W/O: 1457737 TASKCARD: NR-00047 ) REF AEROMAN WO 2026 196/1 NR 299041.ACCOMPLISHED REPAIR ON EXISTING REWORK ON EXACTJul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026070900538Skin · damagedDURING HEAVY MAINTENANCE, EVIDENCE OF REWORK LOCATED ON EXTERNAL SKIN BTW FR 28 TO FR 29 AT LEVEL STR 32 LH LOWER FUSELAGE; (RESOLVED ON W/O: 1457737 TASKCARD: NR-00048 ) REF AEROMAN WO 2026 196/1 NR 299042 ACCOMPLISHED REPAIR ON EXISTING REWORK LOCATED ON Jul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026070900537Skin · damagedDURING HEAVY MAINTENANCE, EVIDENCE OF REWORK LOCATED ON EXTERNAL SKIN BTW FR26 TO FR 27 AT LEVEL STR 32 TO STR 33 LH LOWER FUSELAGE; (RESOLVED ON W/O: 1457737 TASKCARD: NR-00049 ) REF AEROMAN WO 2026-196/1 NR 299039 ACCOMPLISHED REPAIR ON EXISTING REWORK ONJul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026070900536Skin · damagedDURING HEAVY MAINTENANCE, EVIDENCE OF REWORK LOCATED ON EXTERNAL SKIN FR27 AT LEVEL STR 32 TO STR 33 LH LOWER FUSELAGE IAW AEROMAN WO 2026-196/1 NR 299040 ACCOMPLISHED REPAIR ON EXISTING REWORK LOCATED ON EXTERNAL SKIN FR27 BTW STR 32LH AND STR 33LH IAW EA 53-Jul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026070900535Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FRAME 36 CWB VERTICAL STRINGER 5,OPEN FASTENER HOLE ON ZONE 2,CRACK DIRECTION IS 12 OCLOCK,CRACK DEPTH IS 0.105 INCH ,IN FWD CARGO BAY (1EA)(-Y765) REF AEROMAN WO 2026 196/1 NR 299009 ACCOMPLISHED PERMANENT REPAIR OJul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026070900534Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 5, OPEN FASTENER HOLEON ZONE 2, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.105 INCH, IN FWD CARGO COMPARTMENT (1EA)(-Y765). (RESOLVED ON W/O: 1457737 TASKCARD: NR-00031 ) REF AEJul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026070900533Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER5 ,OPEN FASTENER HOLEON ZONE1, CRACK DIRECTION IS 12OCLOCK, CRACK DEPTH IS 0.080 INCH , INF WD CARGO COMPARTMENT (1EA)(-Y765: (RESOLVED ON W/O: 1457737 TASKCARD: NR-00029 ) ACCOMPLISHJul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026070900532Skin · damagedDURING HEAVY MAINTENANCE, EA A26-514-01. FUSELAGE FWD FUSELAGE EXTERNAL SKIN BTWN FR26-FR29 & STGR 32LH-33LH, EXISTING REWORKS – TIME LIMITED REPAIR(CONSIDERED MAJOR REPAIR)Jul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026070900531Floorbeam · crackedDURING HEAVY MAINTENANCE, CENTER BOX, FRONT SPAR HORIZONTAL FLOORBEAMS, @ LEVEL OF FR36 & Y-765, Y-254, Y+254, Y+765 & Y-1292. CRACKS PERMANENT REPAIR (CONSIDERED MAJOR REPAIR)Jul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA202607080494Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER JOB CARD 26L80052001.Jul 4, 2026 · N663AW · Airbus A320232 · Passenger/Crew DoorsSDR YENA2026070700523Oil System · leakingFLT # 375, PHL-FLL. INFLIGHT NOTICED DIRTY SOCK ODOR IN CABIN AFTER APU BLEED TURNED ON; COMPLIED WITH I/N 2017-T015-M. INDENTIFIED SOURCE OF ODOR TYPE 1 APU OIL SATURATION. PERFORMED LVL A ECS DECON. AIR QUALITY CK GOOD.Jul 3, 2026 · N618JB · Airbus A320232 · APU Oil SystemSDR AALA202607074916Bottle · low pressureAIRCRAFT IN BASE MAINTENANCE: L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. REPLACED DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-14.Jul 3, 2026 · N669AW · Airbus A320232 · Passenger/Crew DoorsSDR YENA2026070700519A/C Pack · contaminatedFLT # 87, FLL-ALB. CABIN ODOR ON DESCENT PASSING THROUGH 11,000 FT ( PACKS ); PERFORMEDLEVEL B DECONTAMINATIO OF PACKS IAW AMM 21-00-00. NO ODOR NOTED AT THIS TIME. MDDR CLRD.MX-4 UPDATED. PLACARD REMVOEDJul 2, 2026 · N558JB · Airbus A320232 · Cabin Cooling SystemSDR YENA2026070700518Unknown · odorFLT # 438, MCO-BDL. ON DESCENT FROM 6,000 FT TO 2500 FT STRONG DIRTY SOCK SMELL IN THE FLIGHT DECK. WE DID DESCENDED THROUGH SOME CLOUDS AND THAT IT WAS VERY HOT IN BDL 98F. FLIGHT ATTENDANTS REPORTED NOT SMELLING IT; C/W INFORMATION NOTICE 2017-T015 STEP 1 Jul 2, 2026 · N644JB · Airbus A320232 · Air Distribution SystemSDR YENA2026070700514Controller · failedFLT# 1009, JFK-SDQ(EMERGENCY DECLARED AIR RETURN).CAB PR SYSTEM 1 FAULT WAS RESET AT GATE BY MX TECH. CAME BACK ON CLIMBOUT; REPLACED CAB PR CONTROLLER SYS 1 (11HL) REF AMM 12-31-34. PERFORMED OPS CHK OF PRESSURE CNTROL AND MONITORING SYS REF AMM 21-31-00. A/CJul 1, 2026 · N661JB · Airbus A320232 · Cabin Pressure ControllerSDR CALA2026070717600Battery Pack · no testCABIN EMERGENCY LIGHTING BATTERY CAPACITY - REPLACED ON A-CHECK. REQUIRES 4 BATTERIES, REMOVED AND REPLACED ALL 4 EPSU BATTERIES 10WL, 11WL, 12WL, 13WL REF AMM 33-51-38-400-001-A OPS CHECKED GOOD, NO FAULTS FOUND AT THIS TIME.Jun 29, 2026 · N459UA · Airbus A320232 · Emergency LightingSDR CALA2026063017479Power Supply · faultedLEFT AFT EPSU IS FAULTING DURING EMERGENCY LIGHT TEST. R & R EPSU BOX PER AMM33-51-38, OPS CHECKED GOOD.Jun 28, 2026 · N467UA · Airbus A320232 · Emergency LightingSDR YENA2026062900502Unknown · odorFLT 462, SJU-BOS. FA'S REPORT THE ODOR OF A SWEET SMOKE IN THE AFT GALLEY DURING DECENT TILL LANDING. LAVS UNOCCUPIED AT THE TIME. ; ACCOMPLISHED INFO NOTICE 2017-T015M. VERIFIED NO ODOR PRESENT & NO RECENT HISTORY. DETERMINED TO BE MISC TYPE 10 TABLE 2 REF TSJun 27, 2026 · N665JB · Airbus A320232 · Air Distribution SystemSDR CALA2026063017485Door Sill · corrodedR-2 DOOR SILL CORRODED AT FR68. REMOVED AND REPLACED R-2 DOOR SILL IAW AMM 52-13-31-000-003-A SR M 53-41-14-283-002 AMM 52-13-31-000-007A SRM 51-72-11-911-001 SR M 53-41-14-22-A SRM 51-23-11/001 SRM 51-42-11/001 AMM 52-13-31-0 00-003-A AND AMM 52-13-00-820-00Jun 26, 2026 · N489UA · Airbus A320232 · Fuselage Main, StructureSDR AALA202606296795Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: AFT LEFT DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER JOB CARD 26L80052001.Jun 26, 2026 · N667AW · Airbus A320232 · Passenger/Crew DoorsSDR YENA2026062900499Unknown · odorFLT 65, JFK-ABQ(DIVERTED TO ICT). PAX AND FA'S REPORTED STRONG ODOR OF GASOLINE IN THE AFT CABINN AND AFT GALLEY AFTER LANDING CUSTOMERS SAID IT WAS MORE OF A ROTTEN EGG ODOR THAN GASOLINE ( PACKS ); PERFORMED LEVEL C DECONTAMINIATION APG 1 IAW AMM 05-50-00-80Jun 25, 2026 · N706JB · Airbus A320232 · Air Distribution System
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