Airbus A320-232

Service difficulty reports · 32,648

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 AALA202604283330Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23 R BTW FR69 AND FR70 AFT GALLEY AREA. MEASURE OF CRACK ON SHEAR PLATE IS L= 1.826 INCH.Feb 8, 2026 · N653AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA202603098225Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM +Y1292 AT LEVEL FR66 AT AFT GALLEY AREA. MEASURES L = 2.732 IN, W = 1.17 IN, D = 0.0210 IN. MAINTENANCE REPLACED FLOOR BEAM +Y1292 LOC. BTW FR64 AND FR66 AT AFT GALLEY AREA IAW A320 SRM 51-42-11-801 AND DWG D5Feb 8, 2026 · N653AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA202603038853Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM -Y765 BTW FR64 AND FR66 AT AFT GALLEY AREA. (MEASURES L: 1.250 IN, W: 1.026 IN D: 0.029 IN). MAINTENANCE REPLACED FLOOR BEAM -Y765 BTW FR64 AND FR66 AT AFT GALLEY AREA. IAW A320 SFeb 8, 2026 · N653AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA202603039183Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM Y765 BTW FR64 AND FR66 AT AFT GALLEY AREA. (MEASURES L: 1.250 IN, W: 1.026 IN D: 0.029 IN). MAINTENANCE REPLACED FLOOR BEAM Y765 BETWEEN FR64 THRU FR66 AT AFT GALLEY AREA. IAW A320 SRM 51-42-11-801, DWG D53142Feb 8, 2026 · N653AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA202602253028Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #4 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.Feb 8, 2026 · N653AW · Airbus A320232 · Elevator StructureSDR AALA202602259815Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #3 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.Feb 8, 2026 · N653AW · Airbus A320232 · Elevator StructureSDR AALA202602255822Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #6 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.Feb 8, 2026 · N653AW · Airbus A320232 · Elevator StructureSDR AALA202602188026Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON HINGE ARM END FITTING N1 ON RH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING #1 ON RH ELEVATOR IAW AMM55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Feb 8, 2026 · N653AW · Airbus A320232 · Elevator StructureSDR AALA202602187296Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: REPLACE HINGE ARM END FITTING N5 ON RH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING #5 ON RH ELEVATOR IAW AMM55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Feb 8, 2026 · N653AW · Airbus A320232 · Elevator StructureSDR AALA202602181427Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: REPLACE HINGE ARM END FITTING N2 ON RH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING #2 ON RH ELEVATOR IAW AMM55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Feb 8, 2026 · N653AW · Airbus A320232 · Elevator StructureSDR YENA2026021100194Skin · dentedDURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN LOCATED FR5 TO FR6 AND 14 INCHES BELOW LH SIDE STRI NGER AT LOWER FUSELAGE; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00006) REF AE WO # 2025-414/1 NR # 2025-717347 EVALUATED DENT EXTERNAL SKIN LOCATED FR5 TO FR6 AND 1Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026021100193Skin · dentedDURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN LOCATED FR30 TO FR31 BTW STR39L TO STR40L AT LOWER FUSELAGE; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00007) REF AE WO # 2025-414/1 NR # 2025-717348 EVALUATED DENT EXTERNAL SKIN LOCATED FR30 TO FR31 BTW STR39L TO STR4Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026021100192Skin · dentedDURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN LOCATED FR70 TO FR71 BTW STR31R TO STR32R AT LOWER FUSELAGE; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00008) REF AE WO # 2025-414/1 NR # 2025-717299 PERFORMED DETAIL VISUAL INSPECTION ON AREA AND NOT FOUND DENT ONLY Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026021100191Skin · dentedDURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN DOOR 812 AT LOWER FUSELAGE; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00009) REF AEROMAN WO # 2025=414/1 NR # 2025-717302 EVALUATED DENT ON EXTERNAL SKIN DOOR 812 AT LOWER FUSELAGE AND FOUND WITHIN LIMITS I.A.W A320 SRFeb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026021100190Skin · bulgedDURING HEAVY MAINTENANCE: BULGE EXTERNAL SKIN LOCATED FR24 TO FR25 BTW STR19L TO STR20L ON UPPER FUSELAGE; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00010) REF AEROMAN WO # 2025-414/1 NR # 2025-717282 EVALUATED BULGE EXTERNAL SKIN LOCATED FR24 TO FR25 BTW STR19LFeb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026021100189Skin · dentedDURING HEAVY MAINTENANCE: DENT SKIN LOCATED LOWER AREA DOOR R2 AT LOWER FUSELAGE; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00011) REF AEROMAN WO # 2025-414/1 NR# 2025-717349 EVALUATED DENTS LOCATED LOWER SKIN AREA DOOR R2 AT LOWER FUSELAGE AND FOUND WITHIN LIMITFeb 8, 2026 · N613JB · Airbus A320232 · Service DoorsSDR YENA2026021100188Frame · crackedDURING HEAVY MAINTENANCE: CRACK NDICATION FOUND ON FRAME 16 RH SIDE IN UPPER DOUBLE JOGGLE AREA AT OPEN FASTENER HOLE 8, CRACK DIRECTION AT 3 OCLOCK LOOKING INBOARD, D=0.120INCH, CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00; (RESOLVED ON W/O:Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026021100187Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16 RH SIDE IN UPPER DOUBLE JOGGLE AREA AT OPEN FASTENER HOLE A, CRACK DIRECTION AT 3 OCLOCK LOOKING INBOARD, D=0.110 INCH, CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00; (RESOLVED ON W/Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026021100186Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 20 RH SIDE IN UPPER DOUBLE JOGGLE AREA AT OPEN FASTENER HOLE 6, CRACK DIRECTION AT 11 O CLOCK LOOKING INBOARD, D=0.125 INCH, CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00; (RESOLVED ON Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026021100185Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 LH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 6 OCLOCK, CRACK DEPTH IS 0.105 INCH, AT AFT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1425349 TASKCARD: NR-00038Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026021100184Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 5 POSITION, CRACK DIRECTION IS 7 OCLOCK, CRACK DEPTH IS 0.090 INCH, AT AFT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1425349 TASKCARD: NR-00039Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026021100183Skin · deformedDURING HEAVY MAINTENANCE: DEFORMATION LOC. FR70 TO FR76 BTW STR31R TO 31L JACKING POINT AREA REAR FUSELAGE; REF AEROMAN N/R 2025-717439, PERFORMED PERMANENT REPAIR LOC. FR70 TO FR76 BTW STR31R TO 31L JACKING POINT AREA REAR FUSELAGE, THIS REPAIR IS CATEGORY A,Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026021100182Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE UPPER INBO ARD AT DOOR STOP FITTING 3 POSITION, CRACK DIRECTIONS ARE 1 AND 6 OCLOCK, CRACK DEPTH IS 0.095 INCH, AT AFT GALLEY AREA (2 EA); (RESOLVED ON W/O: 1425349 TASKCARD: Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026021100181Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE UPPER INBO ARD AT DOOR STOP FITTING 3 POSITION, CRACK DIRECTIONS ARE 1 AND 6 OCLOCK, CRACK DEPTH IS 0.095 INCH, AREA 2 FOR PURPOSE OF TRACKING; (RESOLVED ON W/O: 1425349 TASKCFeb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026021100180Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE UPPER INBO ARD AT DOOR STOP FITTING 3 POSITION, CRACK DIRECTIONS ARE 1 AND 6 OCLOCK, CRACK DEPTH IS 0.095 INCH, AREA 3 FOR PURPOSE OF TRACKING; (RESOLVED ON W/O: 1425349 TASKCFeb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026021100179Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE AT AFT WEB FACE AND STGR 8 HORIZONTAL FLANGE RADIUS, CRACK LENGTH IS 0.095 INCH, AT AFT GALLEY AREA ( 1 EA); (RESOLVED ON W/O: 1425349 TASKCARD: NR-00045) REF AE WO # 2025-414/1 NR # 2025-717399 PEFeb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026021100178Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE AT AFT WEB FACE AND STGR 8 HORIZONTAL FLANGE RADIUS, CRACK LENGTH IS 0.095 INCH, TRANSVERSAL FLANGE ARE A FOR PURPOSE OF TRACKING; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00046) REF AE WO # 2025-414Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026021100177Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTIONS ARE 12 AND 6 OCLOCK, CRACK DEPTH IS 0.115 INCH, AT AFT GALLEY AREA (2 EA); REF AEROMAN N/R 2025-717397, ACCOMPFeb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026021100176Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK FOUND ON UPPER RADIUS OF WINDSHIELD CENTER POST LOWER ATTACHMENT AREA RH SIDE. CRACK L= 0.109 INCH. CRACK DIRECTION 11 O CLOCK; REF AEROMAN N/R 2025-717306, ACCOMPLISHED THE PERMANENT REPAIR OF THE CRACKS ON THE WINDSHIELD FRAMIFeb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026021100175Window Frame · crackedDURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE TRAILING EDGE LOWER AREA OF SKINAT LEVEL RIB 15 ON RH WING; REF AE WO # 2025-414/1 NR # 2025-716959 ACCOMPLISHED PERMANENT REPAIR ON RH WING/TOP SKIN PANEL 2 / TEOH LWR SURFACE / RIB 15 I.A.W EA 57-0135-25(COVEFeb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026021100174Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE TRAILING EDGE LOWER AREA OF SKINAT LEVEL RIB 15 ON RH WING; REF AE WO # 2025-414/1 NR # 2025-716959 ACCOMPLISHED PERMANENT REPAIR ON RH WING/TOP SKIN PANEL 2 / TEOH LWR SURFACE / RIB 15 I.A.W EA 57-0135-25(COVEFeb 8, 2026 · N613JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026021100173Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE AT LEVEL RIB 8 TO RIB 9 TRAILING EDGE ON RH WNG; REF AEROMAN WO 2025-414/1 NR # 2025-716950 ACCOMPLISHED REPAIR OF CORROSION DAMAGE AT RH WING/TOP SKIN PANEL 2 / TEOH LWR SURFACE / RIB7-RIB9 I.A.W EA 57-0135-2Feb 8, 2026 · N613JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026021100172Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE UPPER SKIN LOWER AREA BTW RIB8 TO RIB 9 ON RH WING; REF AEROMAN WO # 2025-414/1 NR # 2025-717170 PERFORMED PERMANENT REPAIR ON TRAILING EDGE UPPER SKIN LOWER AREA ON RIB 8 RH WING IAW EA # 57-0135-25 (COVER ANDFeb 8, 2026 · N613JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026021100171Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TE UPPER SKIN LOWER AREA SURFACE AT LEVEL RIB 7 ON RT WING; REF AEROMAN WO #2025-414/1 NR # 2025-717174, PERFORMED PERMANENT REPAIR ON TE UPPER SKIN LOWER AREA SURFACE AT LEVEL RIB 7 ON RT WING IAW EA 57-0135 -25 (COVER PARTFeb 8, 2026 · N613JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026021100170Door Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE/ REAR FUSELAGE/ FR68 RH DOOR STOP FITTING #1/ CRACK/ PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-0101-25 (COVER, PART 1+2) /2/ AIRBUS DOSSIER 81714674 /3/ AIRBUS RDAF 81714674/003/2025#A /4/ A320 SRM 53-41-12-300-011. DESFeb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026021100169Skin · corrodedDURING HEAVY MAINTENANCE: RT WING TOP SKIN PANEL CORRODED /1/ - AIRBUS DOSSIER 81709907 /2/ - AIRBUS RDAF REF. & ISSUE.: 81709907/003/2025 ISSUE A /3/ - AIRBUS RI R572-44701 ISSUE B /4/ - AIRBUS RI R572-58616 ISSUE N /5/ - AIRBUS RI R572-58926 ISSUE E /6/ - AFeb 8, 2026 · N613JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026021100168Window Frame · crackedDURING HEAVY MAINTENANCE, WINDSHIELD FRAME CENTER POST, LOWER NODE AREA CRACKED. REFERENCE: EA 53-0097-25, SB A320-53-1331, RDAF 81709993/003/2025 A, MESSAGE 81709993/010, REPAIR INSTRUCTION R53113430, ISSUE G, REPAIR INSTRUCTION R53112919 ISSUE K, REPFeb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, StructureSDR AALA202604289710Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 833 ON LOAD TRANSMITTING PROFIL R/H SIDE IN PASSENGER CABIN. LENGTH OF CRACK IS= 0.562 INCH. MAINTENANCE REPLACED LOAD TRANSMITTING PROFILE R/H SIDE (SEGMENT FWD) AND BEAM 1 AND ACCOMPLISHED MODIFY ON EMFeb 7, 2026 · N653AW · Airbus A320232 · Fuselage Main, StructureSDR AALA202604288846Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 844 ON VERTICAL FRAME INTERNAL AREA IN PASENGER CABIN. MAINTENANCE REPLACED LOAD TRANSMITTING (FWD AND AFT SEGMENT) AND UPPER BEAM 1, AND ACCOMPLISHED MODIFY OVERWING EMERGENCY EXIT DOOR 844, IAW EO# 5210Feb 7, 2026 · N653AW · Airbus A320232 · Fuselage Main, StructureSDR AALA202604285695Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 844 ON VERTICAL FRAME INTERNAL AREA IN PASENGER CABIN. MAINTENANCE REPLACED LOAD TRANSMITTING (FWD AND AFT SEGMENT) AND UPPER BEAM 1, AND ACCOMPLISHED MODIFY OVERWING EMERGENCY EXIT DOOR 844, IAW EO# 5210Feb 7, 2026 · N653AW · Airbus A320232 · Emergency ExitsSDR AALA202604286828Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 844 ON VERTICAL FRAME INTERNAL AREA IN PASENGER CABIN. CRACK L: 0.465 INCH.Feb 7, 2026 · N653AW · Airbus A320232 · Emergency ExitsSDR AALA202604240577Profile · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 833 ON LOAD TRANSMITTING PROFIL R/H SIDE I N PASSENGER CABIN. MAINTENACE REPLACED LOAD TRANSMITTING PROFILE R/H SIDE, BEAM 1 AND ACCOMPLISHED MODIFY ON EMERGENCY EXIT DOOR 833 IAW EO 5210Y228-001 AND MANFeb 7, 2026 · N653AW · Airbus A320232 · Emergency ExitsSDR AALA202604242373Profile · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 833 ON LOAD TRANSMITTING PROFIL L/H SIDE IN PASSENGER CABIN. LENGHT OF CRACK = 0.500 INCH. REPLACED LOAD TRANSMITTING PROFILE L/H SIDE AND ACCOMPLISHED MODIFY OVERWING EMERGENCY EXIT 833, IAW EO# 5210Y228Feb 7, 2026 · N653AW · Airbus A320232 · Emergency ExitsSDR AALA202604207450Profile · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 843 ON LOAD TRANSMITTING PROFILE L/H SIDE IN PASSENGER CABIN, CRACK LENGTH 0.520 INCH. MAINTENANCE REPLACED LOAD TRANSMITTING PROFILE L/H SIDE (FWD SEGMENT) BTW BEAM 1 AND BEAM 3; ACCOMPLISHED MODIFICATIOFeb 7, 2026 · N653AW · Airbus A320232 · Emergency ExitsSDR AALA202604205818Profile · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 843 ON LOAD TRANSMITTING PROFIL R/H SIDE IN PASSENGER CABIN, CRACK LENGTH 0.580 INCH. MAINTENANCE REPLACED LOAD TRANSMITTING PROFILE R/H SIDE (AFT SEGMENT) BTW BEAM 1 AND BEAM 3; ACCOMPLISHED MODIFICATIFeb 7, 2026 · N653AW · Airbus A320232 · Emergency ExitsSDR CALA2026021013656Channel · corrodedRT WING, AILERON UPPER SURFACE T/E CORRODED APROX 30 INCHES OTBD OF INNER EDGE. REMOVED AND REPLACED THE RT WING AILERON T/E CHANNEL IAW SRM 51-42-11, & DWG 576-40033, REV R.Feb 7, 2026 · N447UA · Airbus A320232 · AileronsSDR GTIA2026020939272Flex Line · rupturedHYD G RSVR LOW LVL, G ENG 1 PUMP LO PR, G SYS LO PR. -REF TSM 29-11-00-810-803-A CONFIRMED G HYD RSVR LESS THAN 3.5L. (COMPLETELY DEPLETED). PERFORMED INSP OF EXTERNAL LEAKS OF THE HYD COMPONENTS IAW AMM 29-00-00. FOUND THE LT MLG DOOR SWIVEL JOINT ASSY FLEX LFeb 7, 2026 · N613NK · Airbus A320232 · Hydraulic System, MainSDR YENA2026020900159Fcu · leakingFLT 471, LGA-FLL, F4 REPORTED ODOR EVENT BELOW 10000 FT DECENDING INTO FLL DESCRIBED AS METALLIC CHEMICAL ODOR AND FEELING LIGHT HEADED AND HAVING A HEADACHE.; COMPLIED WITH INFO-NOTICE 2017-T015 M . IDENTIFIED SOURCE OF ODOR TO APU FCU FUEL DRIP FROM DRAIN Feb 7, 2026 · N625JB · Airbus A320232 · APU Engine Fuel and ControlSDR AALA202602091145Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: L1 DOOR DAMPER REQ SERVICE. MAINTENANCE SERVICED L1 DOOR DAMPER IAW AMM 52-10-00.Feb 6, 2026 · N651AW · Airbus A320232 · Emergency ExitsSDR AALA202604287088Window 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 INSTFeb 5, 2026 · N653AW · Airbus A320232 · Fuselage Main, Structure
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