N653AW

Service difficulty reports · 293

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 = 'N653AW' 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 AALA202608265779Wire · disconnectedAIRCRAFT IN BASE MAINTENANCE: R1 DOOR LOWER EMERGENCY ESCAPE LIGHT IS INOP. FOUND WIRE FOR CONNECTOR TO R1 DOOR LOWER EMERGENCY ESCAPE LIGHT BROKEN AND OTHER CONNECTOR NOT CONNECTED. MAINTENANCE SPLICED BOTH WIRES PER ESPM 20-53-29, ESPM 20-53-21 AND AWM 33-51Aug 22, 2026 · N653AW · Airbus A320232 · Light System WiringSDR AALA202605150598Battery · dischargedAIRCRAFT WAS NOT GROUNDED: EMERGENCY FLASHLIGHT AT AFT FA JUMPSEAT INOPERATIVE. MAINTENANCE REPLACED BATTERY IN EMERGENCY FLASHLIGHT AT AFT F/A SEAT AMM 25-65-00.May 13, 2026 · N653AW · Airbus A320232 · Emergency LightingSDR AALA202604280098Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON LATERAL WINDOW FRAME UPPER JUNCTION FASTENER HOLE, CRACK DIRECTION: 5 OCLOCK (VIEW AFT LOOKING FWD) . D1-D2= 0.212 INCH; AD 2020-19-03 (L= 0.212 IN). MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR ON RH LAApr 19, 2026 · N653AW · Airbus A320232 · Fuselage Main, StructureSDR AALA202604249791Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: WINDSHIELD FRAMING CENTER POST LH HALF FOUND CRACKED IN AREA A. MAINTENANCE REPLACE CONTINUITY FITTING RH SIDE IAW EA 372184.Apr 17, 2026 · N653AW · Airbus A320232 · Fuselage Main, StructureSDR AALA202604281730Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: REPLACE CONTINUITY FITTING LH SIDE IAW EA 372184. MAINTENANCE REPLACED CONTINUITY FITTING LOCATED Y0 AND FR2 LH SIDE BY EA 372184.Feb 13, 2026 · N653AW · Airbus A320232 · Fuselage Main, StructureSDR AALA202604249438Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: MAINTENANCE: WINDSHIELD FRAMING CENTER POST FITTING LOWER FITTING FOUND CRACKED AT Y0 AND FR2. MAINTENANCE REPLACE LOWER FITTING YO AND FR2 IAW EA 372184.Feb 13, 2026 · N653AW · Airbus A320232 · Fuselage Main, StructureSDR AALA202604241668Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON HORIZONTAL FLOOR BEAM RADIUS BACKSIDE OF THE SPAR VERTICAL STRINGER N2 FR 36. CRACK L= 0.530 INCH. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR INSTRUCTIONS ON FLOOR BEAM Y765 VERTICAL STRINGER #2 AT FR 36 Feb 10, 2026 · N653AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA202604226871Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON HORIZONTAL FLOORBEAM RADIUS BACKSIDE OF THE SPAR VERTICAL STRINGER N3 FR 36. CRACK L= 0.550 INCH. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR INSTRUCTIONS ON FLOORBEAM Y254 VERTICAL STRINGER #3 AT FR 36 IAWFeb 10, 2026 · N653AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA202604225191Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON HORIZONTAL FLOORBEAM RADIUS BACKSIDE OF THE SPAR VERTICAL STRINGER N5 FR 36. CRACK L= 0.875 INCH. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR INSTRUCTIONS ON FLOORBEAM -Y765 VERTICAL STRINGER #5 AT FR 36 IFeb 10, 2026 · N653AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA202604220542Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON HORIZONTAL FLOORBEAM RADIUS BACKSIDE OF THE SPAR VERTICAL STRINGER N4 FR 36. CRACK L= 0.610 INCH. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR INSTRUCTIONS ON FLOORBEAM -Y254 VERTICAL STRINGER #4 AT FR 36 IAFeb 10, 2026 · N653AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA202604282565Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN WEB AFT FACE RADIUS WITH STGR 8 HORIZONTAL FLANGE, AT AFT GALL EY AREA CRACK LENGTH IS 0.430 INCH. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR INSTRUCTIONS ON FR68 BTW STR7 AND STR9 RH SIDFeb 9, 2026 · N653AW · Airbus A320232 · Fuselage Main, FrameSDR AALA202602184795Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: REPLACE HINGE ARM END FITTING ELEVATOR N4 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING ELEVATOR #4 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Feb 9, 2026 · N653AW · Airbus A320232 · Elevator StructureSDR AALA202602189094Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: REPLACE HINGE ARM END FITTING ELEVATOR N3 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING ELEVATOR #3 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Feb 9, 2026 · N653AW · Airbus A320232 · Elevator StructureSDR AALA202602188638Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: REPLACE HINGE ARM END FITTING ELEVATOR N2 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING ELEVATOR #2 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Feb 9, 2026 · N653AW · Airbus A320232 · Elevator StructureSDR AALA202602188350Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: REPLACE HINGE ARM END FITTING ELEVATOR N5 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING ELEVATOR #5 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Feb 9, 2026 · N653AW · Airbus A320232 · Elevator StructureSDR AALA202602184281Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM END FITTING ELEVATOR N6 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING ELEVATOR #6 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Feb 9, 2026 · N653AW · Airbus A320232 · Emergency LightingSDR AALA202602189099Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM END FITTING ELEVATOR N1 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING ELEVATOR #1 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Feb 9, 2026 · N653AW · Airbus A320232 · Elevator StructureSDR 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 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 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, StructureSDR AALA202604284966Window 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 INSFeb 5, 2026 · N653AW · Airbus A320232 · Fuselage Main, StructureSDR AALA202510033494Sign · inoperativeAIRCRAFT WAS NOT GROUNDED: R2 DOOR EXIT SIGN HAS BULBS INOP. MAINTENANCE REPLACED LIGHT ASSEMBLY IAW AMM 33-51-16.Oct 1, 2025 · N653AW · Airbus A320232 · Emergency LightingSDR AALA202510034506Sign · inoperativeAIRCRAFT WAS NOT GROUNDED: L2 DOOR EXIT SIGN HAS BULBS INOP. MAINTENANCE REPLACED LIGHT ASSEMBLY IAW AMM 33-51-16.Oct 1, 2025 · N653AW · Airbus A320232 · Emergency LightingSDR AALA202510039345Sign · inoperativeAIRCRAFT WAS NOT GROUNDED: FWD GALLEY CENTER EXIT SIGN HAS LIGHT BULBS INOP. MAINTENANCE REPLACED LIGHT ASSEMBLY IAW AMM 33-51-16.Oct 1, 2025 · N653AW · Airbus A320232 · Emergency LightingSDR AALA202510031169Sign · inoperativeAIRCRAFT WAS NOT GROUNDED, R1 DOOR EXIT SIGN HAS LIGHT BULBS INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY IAW AMM 33-51-16.Oct 1, 2025 · N653AW · Airbus A320232 · Emergency LightingSDR AALA202510037170Sign · inoperativeAIRCRAFT WAS GROUNDED: L1 DOOR EXIT SIGN HAS LIGHT BULBS INOP. MAINTENANCE REPLACED LIGHT ASSEMBLY IAW AMM 33-51-16.Oct 1, 2025 · N653AW · Airbus A320232 · Emergency LightingSDR AALA202509031926Power Supply · no testAIRCRAFT WAS NOT GROUNDED: WHILE PERFORMING OPERATIONAL TEST OF EMERGENCY LIGHTING SYSTEM DURING SLIDE CHANGE FOUND RIGHT EPSU FAULT. MAINTENANCE REPLACED RIGHT CENTER EPSU IAW AMM 33-51-38.Sep 2, 2025 · N653AW · Airbus A320232 · Emergency LightingSDR AALA202505293230Bulb · inoperativeAIRCRAFT IN BASE MAINTENANCE: EXIT LIGHT AT ROW 10 FWD SIDE HAS MULTIPLE LIGHTS OUT. MAINTENANCE RELAMPED EXIT SIGN AT ROW 10.May 29, 2025 · N653AW · Airbus A320232 · Emergency LightingSDR AALA202505203025Light · no testAIRCRAFT WAS NOT GROUNDED: FOUND R/H EMERGENCY EXIT MARKER LIGHT INOP AT EMERGENCY EXIT HATCHES. MAINTENANCE REPLACED EMERGENCY EXIT MARKER LIGHT REF AMM 33-51-16.May 17, 2025 · N653AW · Airbus A320232 · Emergency LightingSDR AALA202505202051Light · no testAIRCRAFT WAS NOT GROUNDED: FOUND L/H EMERGENCY EXIT MARKER LIGHT INOP AT EMERGENCY EXIT HATCHES. MAONTENANCE REPLACED EMERGENCY EXIT MARKER LIGHT REF AMM 33-51-16 OPS CHECK GOOD.May 17, 2025 · N653AW · Airbus A320232 · Emergency LightingSDR AALA202505156479Bracket · inoperativeAIRCRAFT WAS NOT GROUNDED: WHILE PERFORMING J/C 26L00005005 FOUND SEAT 11DEF CABIN EMERGENCY LIGHT INOP. MAINTENANCE REPLACED SEAT 11DEF CABIN EMERGENCY LIGHT OUTER BRACKET IAW CMM 25-40-07 AND REINSTALLED EMERGENCY LIGHT IAW AMM 33-51-18,May 13, 2025 · N653AW · Airbus A320232 · Emergency LightingSDR AALA202505158884Light · no testAIRCRAFT WAS GROUNDED: SEAT 19ABC CABIN EMERGENCY LIGHT INOP. MAINTENANCE REPLACED SEAT 19ABC EMERGENCY LIGHT ASSY IAW AMM 33-51-18.May 12, 2025 · N653AW · Airbus A320232 · Emergency LightingSDR AALA202505138884Light · no testAIRCRAFT WAS GROUNDED: SEAT 19ABC CABIN EMERGENCY LIGHT INOP. MAINTENANCE REPLACED SEAT 19ABC EMERGENCY LIGHT ASSY IAW AMM 33-51-18.May 12, 2025 · N653AW · Airbus A320232 · Emergency LightingSDR AALA202503242062Handle · brokenAIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS LAVATORY E DOOR HANDLE HAS BROKEN OFF, AND ARE UNABLE TO OPEN THE DOOR AFTER GETTING IT CLOSED. MAINTENANCE RESECURED AND TIGHTENED LAVATORY DOOR LATCH SCREWS AS REQUIRED..Mar 23, 2025 · N653AW · Airbus A320232 · Fixed Inner Doors
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