# Service difficulty reports: N663AW A list on [N663AW](https://openairdocs.org/aircraft/N663AW.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 6 · 253 reports - [SDR AALA202607202765](https://openairdocs.org/sdr/AALA202607202765.md): Flashlight · no test · Jul 16, 2026 · N663AW · Airbus A320232 · Emergency Equipment > AIRCRAFT WAS NOT GROUNDED: AFT GALLEY FLASHLIGHT INOPERATIVE AND RED INDICATOR NOT FLASHING. MAINTENANCE REPLACED THE FLASHLIGHT PER AMM 25-63-00. - [SDR AALA202607207587](https://openairdocs.org/sdr/AALA202607207587.md): Light · misinstalled · Jul 16, 2026 · N663AW · Airbus A320232 · Emergency Lighting > AIRCRAFT 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. - [SDR AALA202607099499](https://openairdocs.org/sdr/AALA202607099499.md): Battery · no test · Jul 6, 2026 · N663AW · Airbus A320232 · Emergency Equipment > AIRCRAFT 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. - [SDR AALA202607080494](https://openairdocs.org/sdr/AALA202607080494.md): Bottle · low pressure · Jul 4, 2026 · N663AW · Airbus A320232 · Passenger/Crew Doors > AIRCRAFT WAS NOT GROUNDED: L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER JOB CARD 26L80052001. - [SDR AALA202511070484](https://openairdocs.org/sdr/AALA202511070484.md): Slide Raft · cut · Nov 6, 2025 · N663AW · Airbus A320232 · Escape Slide > AIRCRAFT 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 - [SDR AALA202510240190](https://openairdocs.org/sdr/AALA202510240190.md): Plate · cracked · Oct 21, 2025 · N663AW · Airbus A320232 · Fuselage Main, Attach Fittings > AIRCRAFT 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 SRM - [SDR AALA202510171734](https://openairdocs.org/sdr/AALA202510171734.md): Bearing · excess play · Oct 14, 2025 · N663AW · Airbus A320232 · Elevator Structure > AIRCRAFT 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. - [SDR AALA202509296900](https://openairdocs.org/sdr/AALA202509296900.md): Hinge Fitting · excess play · Sep 28, 2025 · N663AW · Airbus A320232 · Fuselage, Door Hinge > EXCESSIVE 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. - [SDR AALA202509262401](https://openairdocs.org/sdr/AALA202509262401.md): Attach Fitting · corroded · Sep 22, 2025 · N663AW · Airbus A320232 · Nacelle/Pylon, Attach Fittings > AIRCRAFT 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. - [SDR AALA202510302962](https://openairdocs.org/sdr/AALA202510302962.md): Hinge Fitting · cracked · Sep 17, 2025 · N663AW · Airbus A320232 · Landing Gear Doors > AIRCRAFT 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. - [SDR AALA202511183478](https://openairdocs.org/sdr/AALA202511183478.md): Fitting · damaged · Sep 13, 2025 · N663AW · Airbus A320232 · Fuselage Miscellaneous Structure > AIRCRAFT 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 LOW - [SDR AALA202510246518](https://openairdocs.org/sdr/AALA202510246518.md): Plate · cracked · Sep 12, 2025 · N663AW · Airbus A320232 · Fuselage Miscellaneous Structure > AIRCRAFT 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 - [SDR AALA202511186370](https://openairdocs.org/sdr/AALA202511186370.md): Hinge Fitting · cracked · Sep 10, 2025 · N663AW · Airbus A320232 · Tire > AIRCRAFT 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. - [SDR AALA202510282854](https://openairdocs.org/sdr/AALA202510282854.md): Keelbeam · cracked · Sep 10, 2025 · N663AW · Airbus A320232 · Fuselage Main, Keel > AIRCRAFT 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, - [SDR AALA202510301205](https://openairdocs.org/sdr/AALA202510301205.md): Fitting · corroded · Sep 8, 2025 · N663AW · Airbus A320232 · Nacelle/Pylon, Main Frame > AIRCRAFT 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. - [SDR AALA202510144984](https://openairdocs.org/sdr/AALA202510144984.md): Shackle · corroded · Sep 8, 2025 · N663AW · Airbus A320232 · Nacelle/Pylon, Attach Fittings > AIRCRAFT 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. - [SDR AALA202510068077](https://openairdocs.org/sdr/AALA202510068077.md): Spigot · corroded · Sep 8, 2025 · N663AW · Airbus A320232 · Nacelle/Pylon, Main Frame > AIRCRAFT 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. - [SDR AALA202509268562](https://openairdocs.org/sdr/AALA202509268562.md): Bolt · corroded · Sep 8, 2025 · N663AW · Airbus A320232 · Nacelle/Pylon, Main Frame > AIRCRAFT 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. - [SDR AALA202510230580](https://openairdocs.org/sdr/AALA202510230580.md): Seat Track · corroded · Sep 7, 2025 · N663AW · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings > AIRCRAFT 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 - [SDR AALA202510155351](https://openairdocs.org/sdr/AALA202510155351.md): Shackle · corroded · Sep 7, 2025 · N663AW · Airbus A320232 · Nacelle/Pylon, Attach Fittings > AIRCRAFT 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. - [SDR AALA202510147260](https://openairdocs.org/sdr/AALA202510147260.md): Shackle · corroded · Sep 7, 2025 · N663AW · Airbus A320232 · Nacelle/Pylon, Attach Fittings > AIRCRAFT 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. - [SDR AALA202510149455](https://openairdocs.org/sdr/AALA202510149455.md): Shackle · corroded · Sep 7, 2025 · N663AW · Airbus A320232 · Nacelle/Pylon, Attach Fittings > AIRCRAFT 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. - [SDR AALA202510311622](https://openairdocs.org/sdr/AALA202510311622.md): Floorbeam · cracked · Sep 5, 2025 · N663AW · Airbus A320232 · Fuselage Main, Floor Beam > AIRCRAFT 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 367962 - [SDR AALA202510319224](https://openairdocs.org/sdr/AALA202510319224.md): Floorbeam · cracked · Sep 5, 2025 · N663AW · Airbus A320232 · Fuselage Main, Floor Beam > AIRCRAFT 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 367962 - [SDR AALA202510311486](https://openairdocs.org/sdr/AALA202510311486.md): Floorbeam · cracked · Sep 5, 2025 · N663AW · Airbus A320232 · Fuselage Main, Floor Beam > AIRCRAFT 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 367962 - [SDR AALA202510239031](https://openairdocs.org/sdr/AALA202510239031.md): Stringer Splice · damaged · Sep 5, 2025 · N663AW · Airbus A320232 · Fuselage Main, Longeron/Stringer > AIRCRAFT 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, IA - [SDR AALA202510236165](https://openairdocs.org/sdr/AALA202510236165.md): Stringer Splice · damaged · Sep 5, 2025 · N663AW · Airbus A320232 · Fuselage Main, Longeron/Stringer > AIRCRAFT 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 51-72 - [SDR AALA202510233940](https://openairdocs.org/sdr/AALA202510233940.md): Stringer Splice · elongated · Sep 5, 2025 · N663AW · Airbus A320232 · Fuselage Main, Longeron/Stringer > AIRCRAFT 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 A3 - [SDR AALA202510235799](https://openairdocs.org/sdr/AALA202510235799.md): Floor Support · corroded · Sep 5, 2025 · N663AW · Airbus A320232 · Fuselage Miscellaneous Structure > AIRCRAFT 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- - [SDR AALA202510239373](https://openairdocs.org/sdr/AALA202510239373.md): Seat Track · corroded · Sep 5, 2025 · N663AW · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings > AIRCRAFT 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 AREA - [SDR AALA202510238657](https://openairdocs.org/sdr/AALA202510238657.md): Shear Plate · cracked · Sep 5, 2025 · N663AW · Airbus A320232 · Fuselage Miscellaneous Structure > AIRCRAFT 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. - [SDR AALA202510148261](https://openairdocs.org/sdr/AALA202510148261.md): Fitting · corroded · Sep 5, 2025 · N663AW · Airbus A320232 · Fuselage Main, Structure > AIRCRAFT 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 51 - [SDR AALA202510088256](https://openairdocs.org/sdr/AALA202510088256.md): Dummy Rail · corroded · Sep 5, 2025 · N663AW · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR DUMMY RAIL AT FR 16 AT +Y503.2. REPLACED DUMMY RAIL PER SRM 51-72-11. - [SDR AALA202510087062](https://openairdocs.org/sdr/AALA202510087062.md): Shear Plate · cracked · Sep 5, 2025 · N663AW · Airbus A320232 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PER RM 51-72-11. - [SDR AALA202511192809](https://openairdocs.org/sdr/AALA202511192809.md): Skin · cracked · Sep 4, 2025 · N663AW · Airbus A320232 · Fuselage Main, Plate/Skin > AIRCRAFT 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 ACCOM - [SDR AALA202511188310](https://openairdocs.org/sdr/AALA202511188310.md): Frame · cracked · Sep 4, 2025 · N663AW · Airbus A320232 · Fuselage Main, Frame > AIRCRAFT 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 TIME - [SDR AALA202510280456](https://openairdocs.org/sdr/AALA202510280456.md): Stringer · corroded · Sep 4, 2025 · N663AW · Airbus A320232 · Fuselage Main, Longeron/Stringer > AIRCRAFT 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 C - [SDR AALA202511104654](https://openairdocs.org/sdr/AALA202511104654.md): Beam · cracked · Sep 1, 2025 · N663AW · Airbus A320232 · Emergency Exits > AIRCRAFT 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. - [SDR AALA202511106975](https://openairdocs.org/sdr/AALA202511106975.md): Beam · cracked · Sep 1, 2025 · N663AW · Airbus A320232 · Emergency Exits > AIRCRAFT 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. - [SDR AALA202511107941](https://openairdocs.org/sdr/AALA202511107941.md): Beam · damaged · Sep 1, 2025 · N663AW · Airbus A320232 · Emergency Exits > AIRCRAFT 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. - [SDR AALA202511102080](https://openairdocs.org/sdr/AALA202511102080.md): Beam · cracked · Sep 1, 2025 · N663AW · Airbus A320232 · Emergency Exits > AIRCRAFT 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. - [SDR AALA202511104126](https://openairdocs.org/sdr/AALA202511104126.md): Beam · cracked · Sep 1, 2025 · N663AW · Airbus A320232 · Emergency Exits > AIRCRAFT 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. - [SDR AALA202511108915](https://openairdocs.org/sdr/AALA202511108915.md): Beam · cracked · Sep 1, 2025 · N663AW · Airbus A320232 · Emergency Exits > AIRCRAFT 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. - [SDR AALA202511109520](https://openairdocs.org/sdr/AALA202511109520.md): Beam · cracked · Sep 1, 2025 · N663AW · Airbus A320232 · Emergency Exits > AIRCRAFT 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 - [SDR AALA202511106241](https://openairdocs.org/sdr/AALA202511106241.md): Beam · cracked · Sep 1, 2025 · N663AW · Airbus A320232 · Emergency Exits > AIRCRAFT 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. - [SDR AALA202510309718](https://openairdocs.org/sdr/AALA202510309718.md): Profile · cracked · Sep 1, 2025 · N663AW · Airbus A320232 · Emergency Exits > AIRCRAFT IN BASE MAINTENANCE: CRACK IN EMERGENCY EXIT DOOR 844 RIGHT HAND LOAD TRANSMITTING PROFILE AFT SEGMENT. REPLACED AFT SEGMENT PER EO 5210Y228. - [SDR AALA202510303210](https://openairdocs.org/sdr/AALA202510303210.md): Profile · cracked · Sep 1, 2025 · N663AW · Airbus A320232 · Emergency Exits > AIRCRAFT IN BASE MAINTENANCE: CRACK IN EMERGENCY EXIT DOOR 833 LEFT HAND LOAD TRANSMITTING PROFILE AFT SEGMENT. REPLACED AFT SEGMENT PER EO 5210Y228. - [SDR AALA202510305614](https://openairdocs.org/sdr/AALA202510305614.md): Profile · cracked · Sep 1, 2025 · N663AW · Airbus A320232 · Emergency Exits > AIRCRAFT IN BASE MAINTENANCE: CRACK IN EMERGENCY EXIT DOOR 843 RIGHT HAND LOAD TRANSMITTING PROFILE AFT SEGMENT. REPLACED AFT SEGMENT PER EO 5210Y228. - [SDR AALA202510303819](https://openairdocs.org/sdr/AALA202510303819.md): Profile · cracked · Sep 1, 2025 · N663AW · Airbus A320232 · Emergency Exits > AIRCRAFT IN BASE MAINTENANCE: CRACK IN EMERGENCY EXIT DOOR 834 LEFT HAND LOAD TRANSMITTING PROFILE AFT SEGMENT. REPLACED AFT SEGMENT PER EO 5210Y228. - [SDR AALA202511183580](https://openairdocs.org/sdr/AALA202511183580.md): Fitting · cracked · Aug 30, 2025 · N663AW · Airbus A320232 · Fuselage Main, Structure > AIRCRAFT 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 AR Next page: https://openairdocs.org/aircraft/N663AW/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/aircraft/N663AW/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.