N663AW

Service difficulty reports · 253

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N663AW' AND registry_match = 'registration'
  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 AALA202607202765Flashlight · no testAIRCRAFT WAS NOT GROUNDED: AFT GALLEY FLASHLIGHT INOPERATIVE AND RED INDICATOR NOT FLASHING. MAINTENANCE REPLACED THE FLASHLIGHT PER AMM 25-63-00.Jul 16, 2026 · N663AW · Airbus A320232 · Emergency EquipmentSDR AALA202607207587Light · misinstalledAIRCRAFT WAS GROUNDED: EXIT SIGN OVER 1L IS INOPERATIVE. MAINTENANCE FOUND CONNECTIONS FOR LIGHTS 41WL AND 21WL SWAPPED AND MAINTENANCE SWAPPED TO RIGHT LOCATION IAW ASM 33-51.Jul 16, 2026 · N663AW · Airbus A320232 · Emergency LightingSDR 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 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 AALA202511070484Slide Raft · cutAIRCRAFT IN BASE MAINTENANCE: DURING PRE-INSTALLATION INSPECTION OF THE SLIDE AT DOOR 841 WASFOUND CUT LOCKWIRE OF THE COVER RELEASE CABLE RETAINING BALLS OF SAID SLIDE. MAONTENANCE REPLACED SLIDE P/N OFF:D31516-717 S/N OFF: M14288 AND P/N ON: D31516-717 S/N Nov 6, 2025 · N663AW · Airbus A320232 · Escape SlideSDR AALA202510240190Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK ON CONNECTING FITTING ON MLG AREA LH SIDE L=0.163 INCH. MAINTENANCE ACCOMPLISHED PERMANET REPAIR INSTRUCTION (REPLACED CONNECTING PLATE) LOC BTW FR42 TO FR43 AT LEVEL OF WEB W10 AT MLG AREA ON LH SIDE IAW EA 368107, A320 SRMOct 21, 2025 · N663AW · Airbus A320232 · Fuselage Main, Attach FittingsSDR AALA202510171734Bearing · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 5 ELEVATOR ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 5 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM-55-16-42-400-001-A.Oct 14, 2025 · N663AW · Airbus A320232 · Elevator StructureSDR AALA202509296900Hinge Fitting · excess playEXCESSIVE PLAY FWD BEARING MAIN DOOR ON LH MAIN LANDING GEAR. MAINTENANCE REPLACED HINGE FITTING ASSY OF RH MLG DOOR IAW AIRBUS CMM 52-81-18, A319 SRM 51-44-11-801, A319 SRM 51-21-11-801 PMS 01-05-26 AND NTM 51-90-00.Sep 28, 2025 · N663AW · Airbus A320232 · Fuselage, Door HingeSDR AALA202509262401Attach Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT ATTACH FITTING AFT POSITION ON LT PYLON MEASURE CORROSION ARE L=0.73 INCH W=0.41 INCH D=0.011 INCH. MAINTENANCE REPLACED AFT ATTACH FITTING AFT POSITION ON LH PYLON.Sep 22, 2025 · N663AW · Airbus A320232 · Nacelle/Pylon, Attach FittingsSDR AALA202510302962Hinge Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON RIGHT MAIN LANDING GEAR DOOR, KEEL BEAM UPPER HINGE ACTUATOR FITTING AT FR 42, S38R. REPLACED FITTING PER EA 369024.Sep 17, 2025 · N663AW · Airbus A320232 · Landing Gear DoorsSDR AALA202511183478Fitting · damagedAIRCRAFT IN BASE MAINTENANCE: ELONGATE HOLE ON SPLICE FITTING L/H LOCATED ON CENTER WINDSHIE LD FRAME POS LOWER ATTACHMENT AREA, MEASURES OF DAMAGE ARE L=0.335IN,W=0.215IN. MAINTENANCE REPLACED SPLICE FITTING L/H LOCATED ON CENTER WINDSHIELD FRAME POST ON LOWSep 13, 2025 · N663AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA202510246518Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK ON CONNECTING FITTING ON MLG AREA RH SIDE L=0.152 INCH. MAINTENNCE ACCOMPLISHED PERMANET REPAIR INSTRUCTION (REPLACED CONNECTING PLATE) LOC BTW FR42 TO FR43 AT LEVEL OF WEB W10 AT MLG AREA ON RH SIDE IAW EA 368105, A320 SRM Sep 12, 2025 · N663AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA202511186370Hinge Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON DOOR MLG KEEL BEAM HINGE FITTING RH SIDE AFT LUG, WEB LOWER RADIUS. CRACK LENGTH IS 0.150 INCH APPROX, AT MAIN WHEEL WELL.Sep 10, 2025 · N663AW · Airbus A320232 · TireSDR AALA202510282854Keelbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON DOOR MLG KEEL BEAM HINGE FITTING LH SIDE FWD LUG, WEB LOWER RADIUS. CRACK LENGTH IS 0.130 IN, AT MAIN WHEEL WELL. ACCOMPLISHED PERMANENT REPAIR INSTRUCTION (REPLACED DOOR HINGE FITTING) LOC. BTW FR42 AND FR43,Sep 10, 2025 · N663AW · Airbus A320232 · Fuselage Main, KeelSDR AALA202510301205Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 6. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-002.Sep 8, 2025 · N663AW · Airbus A320232 · Nacelle/Pylon, Main FrameSDR AALA202510144984Shackle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT ATTACH FITTING (SHACKLES) FWD POSITION ON LH PYLON. MEASURES ARE L=0.520 INCH, W=0.37 INCH AND D=0.012 INCH. MAINTENANCE REPLACED SHACKLE ATTACH FITTING ASSY IAW JC D5463008400000.Sep 8, 2025 · N663AW · Airbus A320232 · Nacelle/Pylon, Attach FittingsSDR AALA202510068077Spigot · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON MEASURES ARE L:13.380 INCH, W: 1.328 INCH, D= 0.005INCH. MAINTENANCE REPLACED SPIGOT FITTING RECEPTACLE LOC. ON RH PYLON IAW A320 SRM 54-51-12-300-002.Sep 8, 2025 · N663AW · Airbus A320232 · Nacelle/Pylon, Main FrameSDR AALA202509268562Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE, CORROSION ON UPPER BOLT AT AFT ATTACH FITTING ON LT PYLON L=0.017 INCH, W=0.033, INCH AND D=0.011 INCH. MAINTENANCE REPLACED BOLT.Sep 8, 2025 · N663AW · Airbus A320232 · Nacelle/Pylon, Main FrameSDR AALA202510230580Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM -Y765 BTW FR 64 TO FR 66 AT AFT GALLEY AREA CORROSION ARE: L:0.378 IN. W=0.500 IN. D=0.019. MAINTENANCE REPLACED FLOOR BEAM -Y765 BTW FR 64 TO FR 66 AT AFT GALLEY AREA I.A.W A320 SRM 51-42-11-801 AND DWG Sep 7, 2025 · N663AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AALA202510155351Shackle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SHACKLES AFT ON RH PYLON. MEASURE CORROSION ARE L=0.020 INCH W=0.020 INCH D=0.001 INCH. MAINTENANCE REPLACED SHACKLE FITTING ASSY IAW JC 26C42554028.Sep 7, 2025 · N663AW · Airbus A320232 · Nacelle/Pylon, Attach FittingsSDR AALA202510147260Shackle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SHACKLES AFT ON RH PYLON MEASURE CORROSION ARE L=0.020 INCH W=0.025 INCH D=0.001. MAINTENANCE REPLACED SHACKLES FITTING ASSY WITH IDENTIACAL PART IAW JOB CARD 26C42554028.Sep 7, 2025 · N663AW · Airbus A320232 · Nacelle/Pylon, Attach FittingsSDR AALA202510149455Shackle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SHACKLES FWD INB SIDE ON RH PYLON (CPCP 545116-01) MEASURE CORROSION ARE L=0.024 INCH W=0.020 INCH D=0.001 INCH. MAINTENANCE REPLACED SHACKLE FITTING ASSY WITH IDENTICAL PART.Sep 7, 2025 · N663AW · Airbus A320232 · Nacelle/Pylon, Attach FittingsSDR AALA202510311622Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FLOOR BEAM COMMON TO VERTICAL STRINGER 2L AT FR 36, AND Y765, CENTER WING BOX FRONT SPAR, FORWARD CARGO COMPARTMENT. REPAIRED FLOOR BEAM PER EA 367962Sep 5, 2025 · N663AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA202510319224Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FLOOR BEAM COMMON TO VERTICAL STRINGER 3L AT FR 36, AND Y254, CENTER WING BOX FRONT SPAR, FORWARD CARGO COMPARTMENT. REPAIRED FLOOR BEAM PER EA 367962Sep 5, 2025 · N663AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA202510311486Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FLOOR BEAM COMMON TO VERTICAL STRINGER 4R AT FR 36, AND -Y254, CENTER FORWARD CARGO COMPARTMENT. REPAIRED FLOOR BEAM PER EA 367962Sep 5, 2025 · N663AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA202510239031Stringer Splice · damagedAIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLE ON LOWER SPLICE OUTBOARD SIDE ON LOWER SILL LOC. STR23R AT LEVEL FR66 AFT GALLEY AREA. MEASURE IS 0.043 IN. MAINTENANCE REPLACED LOWER SPLICE OUTBOARD SIDE ON LOWER SILL LOC. STR23R AT LEVEL FR66 AFT GALLEY AREA, IASep 5, 2025 · N663AW · Airbus A320232 · Fuselage Main, Longeron/StringerSDR AALA202510236165Stringer Splice · damagedAIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLE ON UPPER SPLICE INBOARD SIDE ON LOWER SILL LOC. STR23R AT LEVEL FR66 AFT GALLEY AREA. MEASURE IS 0.049 IN. MAINTENANCE REPLACED UPPER SPLICE INBOARD SIDE LOC. STR23R AT LEVEL FR66 AFT GALLEY AREA, IAW A320 SRM 51-72Sep 5, 2025 · N663AW · Airbus A320232 · Fuselage Main, Longeron/StringerSDR AALA202510233940Stringer Splice · elongatedAIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLE ON UPPER SPLICE OUTBOARD SIDE ON LOWER SILL LOC. STR23R AT LEVEL FR66 AFT GALLEY AREA. MEASURE IS 0.05 IN. MAINTENANCE REPLACED UPPER SPLICE OUTBOARD SIDE LOWER SILL LOC. STR23R AT LEVEL FR66 AFT GALLEY AREA, IAW A3Sep 5, 2025 · N663AW · Airbus A320232 · Fuselage Main, Longeron/StringerSDR AALA202510235799Floor Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION LOWER SILL STR 23R AT LEVEL FR68 AFT GALLEY AREA (CPCP 534195-1).CORROSION MEASURE L=3.870 IN, W=2.035 IN, D=0.030 IN. MAINTENANCE REPLACED LOWER SILL LOC. STR23R AT LEVEL FR68 AFT GALLEY AREA IAW A320 SRM 51-72-11-911-Sep 5, 2025 · N663AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA202510239373Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SEAT TRACK -Y1162.5 AT LEVEL FR 68 AFT GALLEY AREA (CPCPC 5341 95-01) MEASURES OF CORROSION ARE L: 0.898 INCH, W: 0.540 INCH, D: 0.034 INCH. MAINTENANCE REPLACED SEAT TRACK -Y1162.5 AT LEVEL FR68 TO FR69 AFT GALLEY AREASep 5, 2025 · N663AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AALA202510238657Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23 L BTW FR 69 AND FR 70 AT AFT GALLEY AREA. L= 0.780 INCHES. MAINTENANCE REPLACED SHEAR PLATE STR 23L BTW FR69 AND FR70 AT AFT GALLEY AREA IAW A32O SRM 51-42-11-801, SRM 51-72-11-911-001 AND DWG D58474180.Sep 5, 2025 · N663AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA202510148261Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION CENTER FITTING STR 23L BTW FR66 AND FR68 AFT GALLEY AREA. MEASURES OF CORROSION: L= 5.279 IN W=1.586IN D= 0.080 IN. MAINTENANCE REPLACED CENTER FITTING LOCATED STR 23L BTW FR 66 AND FR 68 AFT GALLEY AREA IAW A320 SRM 51Sep 5, 2025 · N663AW · Airbus A320232 · Fuselage Main, StructureSDR AALA202510088256Dummy Rail · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR DUMMY RAIL AT FR 16 AT +Y503.2. REPLACED DUMMY RAIL PER SRM 51-72-11.Sep 5, 2025 · N663AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AALA202510087062Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PER RM 51-72-11.Sep 5, 2025 · N663AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA202511192809Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE (AFT-LOWER POSITION) LOCATED O N FR35 AT LEVEL OF STR30 RH SIDE, LOWER FUSELAGE. CRACK DEPTH = 0.108 INCHES APPROX, CRACK POSITION: 25 AND 8 OCLOCK LOOKING FROM OUTSIDE. MAINTENANCE ACCOMSep 4, 2025 · N663AW · Airbus A320232 · Fuselage Main, Plate/SkinSDR AALA202511188310Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE (AFT-LOWER POSITION) LOCATED ON FR35 AT LEVEL OF STR30 LH SIDE, LOWER FUSELAGE. CRACK DEPTH = 0.100 INCHES APPROX, CRACK POSITION: 11 OCLOCK LOOKING FROM OUTSIDE. MAINTENANCE PERFORMED TIMESep 4, 2025 · N663AW · Airbus A320232 · Fuselage Main, FrameSDR AALA202510280456Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION STRINGER 43L BTW FR 56 AND FR 57 IN AFT CARGO COMPARTMENT MEASURE OF CORROSION AREA L= 8.191 IN, W= 0.848 IN, D= 0.003 IN. MAINTENANCE PERFORMED PERMANENT REPAIR (SPLICE REPAIR) ON STRINGER 43L BTW FR55 TO FR58 IN AFT CSep 4, 2025 · N663AW · Airbus A320232 · Fuselage Main, Longeron/StringerSDR AALA202511104654Beam · crackedAIRCRAFT IN BASE MAINTENANCE: SEGMENT BEAM MUST BE REPLACED BY EO 5210Y228-001. MAINTENANCE ACCOMPLISHED MODIFY OVERWING EMERGENCY EXIT DOOR 844 ON RH SIDE OF PASSENGER CABIN IN ACCORDANCE WITH MANUAL TALLY 110, EO 5210Y228-001.Sep 1, 2025 · N663AW · Airbus A320232 · Emergency ExitsSDR AALA202511106975Beam · crackedAIRCRAFT IN BASE MAINTENANCE: SEGMENT BEAM MUST BE REPLACED BY EO 5210Y228-001. MAINTENANCE ACCOMPLISHED MODIFY OVERWING EMERGENCY EXIT DOOR 844 ON RH SIDE OF PASSENGER CABIN IN ACCORDANCE WITH MANUAL TALLY 110, EO 5210Y228-001.Sep 1, 2025 · N663AW · Airbus A320232 · Emergency ExitsSDR AALA202511107941Beam · damagedAIRCRAFT IN BASE MAINTENANCE: SEGMENT MUST BE REPLACED BY EO 5210Y228-001. MAINTENANCE ACCOMPLISHED MODIFY OVERWING EMERGENCY EXIT DOOR 833 ON LH SIDE OF PASSENGER CABIN IN ACCORDANCE WITH MANUAL TALLY 109, EO 5210Y228-001.Sep 1, 2025 · N663AW · Airbus A320232 · Emergency ExitsSDR AALA202511102080Beam · crackedAIRCRAFT IN BASE MAINTENANCE: SEGMENT BEAM MUST BE REPLACED BY EO 5210Y228-001. MAINTENANCE ACCOMPLISHED MODIFY OVERWING EMERGENCY EXIT DOOR 833 ON LH SIDE OF PASSENGER CABIN IN ACCORDANCE WITH MANUAL TALLY 109, EO 5210Y228-001.Sep 1, 2025 · N663AW · Airbus A320232 · Emergency ExitsSDR AALA202511104126Beam · crackedAIRCRAFT IN BASE MAINTENANCE: SEGMENT BEAM MUST BE REPLACED BY EO 5210Y228-001. MAINTENANCE ACCOMPLISHED MODIFY OVERWING EMERGENCY EXIT DOOR 834 ON LH SIDE OF PASSENGER CABIN IN ACCORDANCE WITH MANUAL TALLY 107, EO 5210Y228-001.Sep 1, 2025 · N663AW · Airbus A320232 · Emergency ExitsSDR AALA202511108915Beam · crackedAIRCRAFT IN BASE MAINTENANCE: SEGMENT BEAM MUST BE REPLACED BY EO 5210Y228-001. MAINTENANCE ACCOMPLISHED MODIFY OVERWING EMERGENCY EXIT DOOR 834 ON LH SIDE OF PASSENGER CABIN IN ACCORDANCE WITH MANUAL TALLY 107, EO 5210Y228-001.Sep 1, 2025 · N663AW · Airbus A320232 · Emergency ExitsSDR AALA202511109520Beam · crackedAIRCRAFT IN BASE MAINTENANCE: SEGMENT BEAM MUST BE REPLACED BY EO 5210Y228-001. MAINTENANCE ACCOMPLISHED MODIFY OVERWING EMERGENCY EXIT DOOR 843 ON RH SIDE OF PASSENGER CABIN IN ACCORDANCE WITH MANUAL TALLY 108, EO 5210Y228-001Sep 1, 2025 · N663AW · Airbus A320232 · Emergency ExitsSDR AALA202511106241Beam · crackedAIRCRAFT IN BASE MAINTENANCE: SEGMENT BEAM MUST BE REPLACED BY EO 5210Y228-001. MAINTENANCE ACCOMPLISHED MODIFY OVERWING EMERGENCY EXIT DOOR 843 ON RH SIDE OF PASSENGER CABIN IN ACCORDANCE WITH MANUAL TALLY 108, EO 5210Y228-001.Sep 1, 2025 · N663AW · Airbus A320232 · Emergency ExitsSDR AALA202510309718Profile · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN EMERGENCY EXIT DOOR 844 RIGHT HAND LOAD TRANSMITTING PROFILE AFT SEGMENT. REPLACED AFT SEGMENT PER EO 5210Y228.Sep 1, 2025 · N663AW · Airbus A320232 · Emergency ExitsSDR AALA202510303210Profile · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN EMERGENCY EXIT DOOR 833 LEFT HAND LOAD TRANSMITTING PROFILE AFT SEGMENT. REPLACED AFT SEGMENT PER EO 5210Y228.Sep 1, 2025 · N663AW · Airbus A320232 · Emergency ExitsSDR AALA202510305614Profile · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN EMERGENCY EXIT DOOR 843 RIGHT HAND LOAD TRANSMITTING PROFILE AFT SEGMENT. REPLACED AFT SEGMENT PER EO 5210Y228.Sep 1, 2025 · N663AW · Airbus A320232 · Emergency ExitsSDR AALA202510303819Profile · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN EMERGENCY EXIT DOOR 834 LEFT HAND LOAD TRANSMITTING PROFILE AFT SEGMENT. REPLACED AFT SEGMENT PER EO 5210Y228.Sep 1, 2025 · N663AW · Airbus A320232 · Emergency ExitsSDR AALA202511183580Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON LH CONTINUITY FITTING OF THE WINDSHIELD CENTER POST LOWER ATTACHMENT AREA INTERNAL SIDE. CRACK L= 0.200 INCH. MAINTENANCE REPLACED CONTINUITY FITTINGS LH OF THE WINDSHIELD CENTER POST LOWER ATTACHMENT ARAug 30, 2025 · N663AW · Airbus A320232 · Fuselage Main, Structure
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