Airbus A320-231

Service difficulty reports · 3,758

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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 = 'A320231'
  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 AWXA200300909Power Supply · dischargedLAS - EEL - FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHT WAS NOT ILLUMINATED AT CENTER AISLE OVERWING EXITS. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD.Aug 11, 2003 · N631AW · Airbus A320231 · Emergency LightingSDR AWXA200300893Battery · dischargedPHX - EEL - EMERGENCY FLASHLIGHT AT AFT NR 3 FLIGHT ATTENDANT STATION IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY AT THE AFT NR 3 FLIGHT ATTENDANT STATION, OPERATIONAL CHECK WAS GOOD.Aug 7, 2003 · N620AW · Airbus A320231 · Emergency EquipmentSDR AWXA200300883Battery · dischargedLAX - EEL - SEVERAL EMERGENCY LIGHTS ARE INOPERATIVE AT MID CABIN. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT MID CABIN EMERGENCY POWER SUPPLY UNIT, OPERATIONAL CHECK WAS GOOD.Aug 6, 2003 · N626AW · Airbus A320231 · Emergency LightingSDR CA030805006Control Unit · failed(CAN) ON APPROACH, AC APPROACH STATUS REVERTED TO CAT III SINGLE WITH WHEEL PAGE SHOWING AMBER STEERING. N/W STEERING SWITCH CYCLED OFF THEN ON WITH INDICATIONS RETURNING TO NORMAL AND CAT III DUAL. UPON LANDING, IDLE REVERSE WAS SELECTED(NOISE ABATEMENT) BUTAug 3, 2003 · Airbus A320231 · Steering UnitSDR AWXA200300866Pump · defectiveON TAKEOFF, RECEIVED ECAM WARNING FOR NR 1 ENG COMPRESSOR VANE FAULT ALONG WITH N1/N2 OVERSPEED, REJECTED TAKEOFF AT 60 KTS, RETURNED TO BLOCK. MX R & R NR 1 ENG VSV ACTUATOR, FAULT STILL PRESENT DURING ENG RUN. R & R NR 1 ENG FUEL METERING UNIT. REPLACED LOJul 29, 2003 · N634AW · Airbus A320231 · Engine Fuel PumpSDR AWXA200300857Cable · brokenDURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 22 LT WAS FOUND INOPERATIVE. RELAMP, NO HELP. MAINTENANCE REPAIRED A BROKEN WIRE AT SIDE WALL DISCONNECT FOR SEAT ROW 22 LT EMERGENCY ESCAPE PATH LIGHT, OPERATIONAL CHECK WAS GOOD.Jul 28, 2003 · N626AW · Airbus A320231 · Light System WiringSDR AWXA200300840Odor · detectedAFTER TAKEOFF FROM LAS EN ROUTE FOR PDX NOTICED AIRCRAFT VIBRATION, CLIMBING THROUGH FL 180 NR 2 ENGINE VIBRATION AT 2.2, VIBRATION BECAME STRONGER AND AFT CABIN FLIGHT ATTENDANT REPORTED A BURNING ODOR COMING FROM AFT GALLEY AREA. ODOR BECAME STRONGER AS FLIJul 24, 2003 · N631AW · Airbus A320231 · Air Distribution SystemSDR AWXA200300867Fairing · crackedMCN - MINOR REPAIR - DURING C-01 CHECK A 8.5 INCH CRACK WAS FOUND AT THE AFT END OF THE NR 1 PYLON INBOARD UPPER FAIRING WELDED ASSEMBLY, NAC STA 5369-6077, BETWEEN RIBS 7 & 8. MAINTENANCE REMOVED AND REPLACED WELDED ASSEMBLY INBOARD SIDE OF NR 1 PYLON IAW AMMJul 23, 2003 · N644AW · Airbus A320231 · Nacelle/Pylon, Plate/SkinSDR AWXA200300878Battery · dischargedMCN - EMERGENCY EQUIPMENT - DURING C-01 CHECK ALL 4 EMERGENCY FLASHLIGHTS UNDER FLIGHT ATTENDANTS SEATS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED ALL 4 EMERGENCY FLASHLIGHT BATTERY PACKS, OPERATIONAL CHECKS WERE GOOD.Jul 22, 2003 · N644AW · Airbus A320231 · Emergency EquipmentSDR AWXA200300805Eec · failedDURING TAKEOFF AT PHX EN ROUTE FOR DEN THE CREW PUSHED POWER UP FOR TAKEOFF AND THE NR 2 ENGINE DID NOT RESPOND, POWER REMAINED AT IDLE, REJECTED TAKEOFF. FLIGHT CREW NOTED THAT THE NR 1 ENGINE DID RESPOND NORMALLY. APPROXIMATELY 5 MINUTES LATER; RECEIVED ECJul 16, 2003 · N645AW · Airbus A320231 · Fuel Controlling SystemSDR AWXA200300775Servo Valve · faultyON TAKEOFF PILOT REPORTED A NOSE WHEEL STEERING FAULT. AIRCRAFT PROCEEDED AFTER WHICH AN UNEVENTFUL LANDING OCCURED. AIRCRAFT TAXIED TO GATE UNDER ITS OWN POWER. MECHANIC PERFORMED BSCU BITE CHECKS THAT IDENTIFIED FAULT CODE 4E. REMOVED AND REPLACED THE NOSEJul 4, 2003 · N622AW · Airbus A320231 · Steering UnitSDR AWXA200300806Profile · crackedDURING C-03 CHECK A .5 INCH CRACK WAS FOUND ON INBOARD UPPER ANGLE (PROFILE) AT ATTACH SCREW HOLE JUST AFT OF RIB 7 ON THE NR 2 PYLON. MAINTENANCE CUT OUT CRACKED AREA OF ANGLE JUST AFT OF RIB 7 ON THE NR 2 PYLON; FABRICATED A REPAIR SPLICE AND FILLER; INSTALJun 28, 2003 · N624AW · Airbus A320231 · Nacelle/Pylon, Frame/Spar/RibSDR AWXA200300800Attach Angle · crackedMCN - MAJOR REPAIR - DURING C-03 CHECK A .5 INCH CRACK WAS FOUND ON RT PYLON UPPER ATTACH ANGLE AT SCREW HOLE FORWARD OF RIB 8. MAINTENANCE CUT OUT DAMAGE ON RT PYLON ATTACH ANGLE FORWARD OF RIB 8; FABRICATED A FILLER AND SPLICE; INSTALLED REPAIR PARTS IAW A3Jun 28, 2003 · N624AW · Airbus A320231 · Nacelle/Pylon, Attach FittingsSDR AWXA200300799Attach Angle · crackedDURING C-03 CHECK A .5 INCH CRACK WAS FOUND ON LT PYLON PANEL ATTACH ANGLE AT INBOARD SIDE, AFT OF RIB 7. MAINTENANCE CUT OUT DAMAGE ON LT PYLON PANEL ATTACH ANGLE AT INBOARD SIDE, AFT OF RIB 7; FABRICATED A FILLER AND SPLICE; INSTALLED REPAIR PARTS IAW A320 Jun 28, 2003 · N624AW · Airbus A320231 · Nacelle/Pylon, Attach FittingsSDR AWXA200300790Rib · crackedDURING C-03 CHECK A .125 INCH CRACK WAS FOUND ON NR 1 PYLON RIB, 4TH LOWER RIB FROM UPPER DRAIN LINE CLEARANCE HOLE, OUTBOARD EDGE IN AFT FIXED FAIRING. MAINTENANCE REMOVED CRACKED RIB; FABRICATED A NEW REPLACEMENT RIB; INSTALLED REPAIR PART IAW A320 SRM 51-4Jun 28, 2003 · N624AW · Airbus A320231 · Nacelle/Pylon, Frame/Spar/RibSDR AWXA200300807Panel · delaminatedDURING C-03 CHECK THE LOWER CENTER BELLY FAIRING (191BB) WAS FOUND DELAMINATED ALONG THE FORWARD LOWER EDGE AT THE RT AFT OUTBOARD CORNER, FR 34. MAINTENANCE REMOVED AND REPLACED THE LOWER CENTER BELLY FAIRING (191BB) IAW A320 AMM SUBTASK 53-35-13-020-052-AO Jun 27, 2003 · N624AW · Airbus A320231 · Aerodynamic FairingsSDR AWXA200300736Actuator · faultyAT CRUISE FL 360, NR 2 ENG COMPRESSOR VANE ECAM MSG, AT FL 290 NR 2 ENG STALLED. SHUTDOWN ENG, EMERGENCY EQUIP TO STANDBY. LANDED, TAXIED TO GATE. REPORT INDICATED NR 2 ENG OVERTEMP 663'C APPX 7 SEC. MX INSPECTED INTERMEDIATE PRESSURE CHECK VALVE, FAULT ISJun 25, 2003 · N645AW · Airbus A320231 · Compressor Bleed ControlSDR AWXA200300733Line · chafedON DECENT, EN ROUTE RECEIVED ECAM MESSAGE GREEN HYDRAULIC SYSTEM LOW QUANTITY; DECLARED EMERGENCY, NO NOSE WHEEL STEERING, AIRCRAFT TOWED OFF RUNWAY. MAINTENANCE FOUND GREEN SYSTEM HYDRAULIC PRESSURE LINE CHAFED AND LEAKING IN LT WHEEL WELL ON AFT SPAR BETWEENJun 23, 2003 · N625AW · Airbus A320231 · Hydraulic System, MainSDR AWXA200300727Ballast · faultyFLIGHT ATTENDANT REPORTED A BURNING RUBBER ODOR ABOVE SEAT ROW 20. MAINTENANCE REMOVED AND REPLACED THE LIGHT BALLAST UNIT ABOVE SEAT ROW 21 RT IAW AMM 33-21-11; OPERATIONAL CHECK WAS GOOD, NO ODOR NOTED.Jun 23, 2003 · N626AW · Airbus A320231 · Passenger Compartment LightingSDR AWXA200300717Bottle · dischargedIND - DIVERSION - FLT 0687 - EN ROUTE FROM PHX TO EWR CREW OXYGEN INDICATED ZERO PSI. ONE-HOUR PRIOR OXYGEN INDICATED 1300 PSI, PRIOR TO DEPARTING PHX CREW OXYGEN WAS AT 1425 PSI. MASKS WERE NOT USED, DIVERTED TO IND. MAINTENANCE REMOVED AND REPLACED THE CRJun 19, 2003 · N633AW · Airbus A320231 · Crew Oxygen SystemSDR AWXA200300788Floorbeam · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM AT FR 66, Y1292. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED FLOORBEAM; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PARJun 17, 2003 · N620AW · Airbus A320231 · Fuselage Main, Floor BeamSDR AWXA200300762Stiffener · crackedDURING C-04 CHECK A .5 INCH CRACK WAS FOUND ON LT OUTBOARD FLOOR SUPPORT SIDE RAIL STIFFENER (PROFILE) FR 37, Y-1732. MAINTENANCE REMOVED DAMAGED PROFILE FR 37, Y-1732; FABRICATED A NEW REPLACEMENT PROFILE PER DWG D53370039; INSTALLED REPAIR PART IAW A320 SRMJun 16, 2003 · N620AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300698Actuator · looseTEARDOWN REPORT OF ENG IDENTIFIED HIGH INTERNAL LEAKAGE AT VSV ACT ALONG WITH SLOW PISTON VELOCITY. TEARDOWN REVEALED THAT CONTROL SERVO VALVE & SEAL WERE WORN BEYOND LIMITS & CAUSED INTERNAL LEAKAGE AT VSV ACT. FAILURE MODE & EFFECTS ANALYSIS CONSIDER THIS A Jun 14, 2003 · N624AW · Airbus A320231 · Compressor Bleed ControlSDR AWXA200300697Slide · tornDURING C-04 CHECK FOUND THE R-2 DOOR SLIDE LACING TORN. MAINTENANCE REMOVED AND REPLACED THE R-2 DOOR SLIDE IAW T/C R1C25304MT-82.Jun 14, 2003 · N625AW · Airbus A320231 · Escape SlideSDR AWXA200300787Floor Support · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF AFT CARGO COMPARTMENT FLOOR SUPPORT (PROFILE) AT FR 56, Y10. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED PROFILE AT FR 56, Y10; FABRICATED A NEW REPLACEMEJun 12, 2003 · N620AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300763Profile · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON RT PROFILE IN AFT CARGO COMPARTMENT AT FR 51+17, STR 37 RT. MAINTENANCE CUT OUT DAMAGED SECTION OF PROFILE AT FR 51+17, STR 37 RT; FABRICATED A NEW REPLACEMENT SECTION OF PROFILE, A DOUBLER, AND SPJun 12, 2003 · N620AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300746Floor Support · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF AFT CARGO COMPARTMENT FLOOR SUPPORT (SEALING PROFILE) AT FR 58, Y-25. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS, REMOVED CORRODED FLOOR SUPPORT AT FR 58, Y-25; FABRICATEDJun 12, 2003 · N620AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300695Splice · brokenMCN - EEL - DURING C-04 CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 RT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED SPLICES ON WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 9 RT, OPERATIONAL CHECK WAS GOOD.Jun 12, 2003 · N625AW · Airbus A320231 · Light System WiringSDR AWXA200300786Seat Track · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF SEAT TRACK EXTRUSION AT FR 67, Y1321. MAINTENANCE REMOVED DAMAGED SEAT TRACK EXTRUSION BETWEEN AT FR 67, Y1321; FABRICATED A NEW REPLACEMENT SEAT TRACK EXTRUSION; INSTAJun 11, 2003 · N620AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200300785Web · crackedDURING C-04 CHECK A 4.75 INCH CRACK WAS FOUND ON FLOOR WEB BETWEEN FR 68-69, Y1270. MAINTENANCE REMOVED DAMAGED FLOOR WEB BETWEEN FR 68-69, Y1270; FABRICATED A NEW REPLACEMENT FLOOR WEB; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG 21-22, FIG 8.Jun 11, 2003 · N620AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300768Plate · corrodedDURING C-04 CHECK TWO AREAS OF EXFOLIATION CORROSION WERE FOUND ON LOWER SURFACE OF FLOOR WEB (SHEAR PLATE) AT FR 70, Y-1193. MAINTENANCE REMOVED CORRODED SHEAR PLATE AT FR 70, Y-1193; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SJun 11, 2003 · N620AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300761Web · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK A 6 INCH CRACK WAS FOUND ON FLOOR WEB BETWEEN FR 68-69, Y-1270. MAINTENANCE REMOVED DAMAGED FLOOR WEB BETWEEN FR 68-69, Y-1270; FABRICATED A NEW REPLACEMENT FLOOR WEB; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 7-12 Jun 11, 2003 · N620AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300748Floorbeam · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND AT TWO PLACES ON UPPER SURFACE OF FLOORBEAM AT FR 66, Y-915. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED FLOORBEAM Y-915, FROM FR 65 TO FR 67; FABRICATED A NEW REJun 11, 2003 · N620AW · Airbus A320231 · Fuselage Main, Floor BeamSDR AWXA200300743Floorbeam · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND IN TWO PLACES ON UPPER SURFACE OF FLOORBEAM BETWEEN FR 67-78, Y-1193. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FLOORBEAM Y-1193 BETWEEN FR 66-68; FABRICATED A NEW REPLJun 11, 2003 · N620AW · Airbus A320231 · Fuselage Main, Floor BeamSDR AWXA200300767Stringer · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 30 RT 3 INCHES AFT OF FR 65 IN A 6 X 3 INCH AREA. MAINTENANCE REMOVED DAMAGED AREA OF STRINGER 30 RT 3 INCHES AFT OF FR 65; FABRICATED A NEW SECTION OF STRINGER PER DWG 18D5348Jun 10, 2003 · N620AW · Airbus A320231 · Fuselage Main, Longeron/StringerSDR AWXA200300722Angle · crackedDURING C-04 CHECK A .2500 INCH CRACK WAS FOUND ON ANGLE AT FR 34, STR 31 LT. MAINTENANCE REMOVED ANGLE AT FR 34, STR 31 LT; PROCURED AND DRILLED NEW ANGLE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 28-30, 39-41, FIG. 12 & 18.Jun 10, 2003 · N620AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300703Angle · crackedDURING C-04 CHECK A 2 INCH CRACK WAS FOUND ON ANGLE AFT R 34, STR 31 RT. MAINTENANCE REMOVED CRACKED ANGLE AT FR 34, STR 31 RT; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW A320 SRM 51-44-11, PG. 11,16, AND 20.Jun 10, 2003 · N620AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300747Attach Fitting · crackedDURING C-04 CHECK A .5000 INCH CRACK WAS FOUND ON LT WING LEADING EDGE ACCESS PANEL ATTACH FITTING, OUTBOARD OF NR 1 PYLON. MAINTENANCE REMOVED CRACKED ATTACH FITTING; FABRICATED A NEW REPLACEMENT ATTACH FITTING; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PGJun 9, 2003 · N620AW · Airbus A320231 · Nacelle/Pylon Miscellaneous StructureSDR AWXA200300679Slide · leakingFLIGHT CREW REPORTED R-2 DOOR SLIDE PRESSURE INDICATOR NOT IN THE GREEN AREA. MAINTENANCE REMOVED AND REPLACED R-2 DOOR SLIDE IAW T/C R1C25304, OPERATIONAL CHECK WAS GOOD.Jun 9, 2003 · N634AW · Airbus A320231 · Escape SlideSDR AWXA200300716Skin · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON SKIN AT AFT LOWER FUSELAGE FR 62 AND FR 63, BETWEEN STR 41 LT AND STR 41 RT, IFPC ANTENNA CUTOUT. MAINTENANCE CLEANED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. CUT OUT DAMAGED SKIN; FABRICATED A REPAIR DOJun 8, 2003 · N620AW · Airbus A320231 · Fuselage Main, Plate/SkinSDR AWXA200300729Cylinder Damper · inoperativeDURING C-04 CHECK THE R-2 DOOR DAMPER CYLINDER WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE R-2 DOOR DAMPER CYLINDER IAW AMM SUBTASK 52-13-14-020-050. VENDOR TEARDOWN OF R-2 DOOR DAMPER CYLINDER S/N 215 FOUND UNIT HEAVILY CONTAMINATED DUE TO LEJun 7, 2003 · N620AW · Airbus A320231 · Passenger/Crew DoorsSDR AWXA200300715Cylinder Damper · out of adjustDURING C-04 CHECK THE R-1 DOOR ASSIST MECHANISM WAS FOUND OUT OF ADJUSTMENT. MAINTENANCE ADJUSTED THE R-1 DOOR ASSIST MECHANISM IAW AMM TASK 52-11-14-820-002 AND 52-11-14-501.Jun 7, 2003 · N620AW · Airbus A320231 · Passenger/Crew DoorsSDR AWXA200300680Thermocouple · faultyON TAKEOFF ROLL AT LAS EN ROUTE FOR PDX NR 2 BRAKE TRIGGERED HOT BRAKE ECAM MESSAGE, REJECTED TAKEOFF AT 85 KTS. NR 2 BRAKE INDICATED 580 CELSIUS MAXIMUM TEMPERATURE. MAINTENANCE PLACED SYSTEM ON MEL 32-47-01, COND 1 NR 2 BRAKE TEMP MONITORING UNIT INOP AND Jun 7, 2003 · N626AW · Airbus A320231 · Overheat DetectionSDR AWXA200300769Bulkhead · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK A .1875 INCH CRACK WAS FOUND ON RT BULKHEAD WEB FR 35 AT LOWER MOST OUTBOARD HOLE. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICATED REPAIR DOUBLERS AND A BRACKET ASJun 6, 2003 · N620AW · Airbus A320231 · Fuselage Main, BulkheadSDR AWXA200300669Fire Detector · malfunctionedFALSE FIRE WARNING - NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED AT GATE WITH BOTH ENGINES SHUTDOWN. MAINTENANCE REMOVED AND REPLACED NR 2 FIRE DETECTION UNIT IAW AMM 26-12-34, OPERATIONAL CHECK WAS GOOD.Jun 6, 2003 · N620AW · Airbus A320231 · Fire DetectionSDR AWXA200300670Slide · faultyDOOR EMERGENCY ESCAPE SLIDE ARM LIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE R-1 DOOR EMERGENCY ESCAPE SLIDE IAW T/C R1C25304, OPERATIONAL CHECK WAS GOOD.Jun 6, 2003 · N629AW · Airbus A320231 · Escape SlideSDR AWXA200300652Transmitter · defectiveSTEERING FAILURE - BSCU 1 FAULT ON TAXI AIRCRAFT COULD NOT BE STEERED WITH RUDDER PEDALS OR TILLER. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS N/W/S HAND WHEEL TRANSMITTER UNIT (1GC) IAW AMM 32-51-11-401, OPERATIONAL CHECK WAS GOOD. VENDOR TEARDOWN REPORT Jun 4, 2003 · N622AW · Airbus A320231 · Steering UnitSDR AWXA200300671Power Supply · faultyDURING C-04 CHECK THE LT OVERWING EMERGENCY POWER SUPPLY UNIT INDICATED A FAULT. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL) AND BATTERY PACK IAW AMM TASKS 33-51-38-000-001 AND 33-51-38-400-001, OPERATIONAL CHECK WAS GOOD.Jun 3, 2003 · N625AW · Airbus A320231 · Emergency LightingSDR AWXA200300635Wire · brokenLAS - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT CONNECTOR OF EMERGENCY ESCAPE PATH LIGHT SEAT ROW 16 LT, OPERATIONAL CHECK WAS GOOD.Jun 2, 2003 · N626AW · Airbus A320231 · Light System WiringSDR AWXA200300628Attach Angle · crackedDURING C-03 CHECK A .3125 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT FORWARD BULKHEAD PANEL ATTACH ANGLE AT UPPER LT CORNER. MAINTENANCE REMOVED EXISTING REPAIR DOUBLER; STOP DRILLED CRACK; FABRICATED A NEW REPAIR DOUBLER; INSTALLED REPAIR PART IAW AWA ER May 21, 2003 · N631AW · Airbus A320231 · Fuselage Main, Attach Fittings
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