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"

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SDR AWXA200300517Skin · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON EXTERNAL SKIN BETWEEN FRAMES 62 AND 63, STR 42-43 LT, UNDER IFPC ANTENNA. MAINTENANCE CUT OUT CORROSION ON EXTERNAL SKIN BETWEEN FRAMES 62 AND 63, STR 42-43 LT, UNDER IFPC ANTENNA; FABRICATED A DOUApr 26, 2003 · N625AW · Airbus A320231 · Fuselage Main, Plate/SkinSDR AWXA200300516Skin · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON EXTERNAL SKIN BETWEEN FRAMES 60 AND 61, AT BL 0, UNDER ANTENNA CUTOUT. MAINTENANCE CUT OUT CORROSION ON EXTERNAL SKIN BETWEEN FRAMES 60 AND 61, AT BL 0; FABRICATED A DOUBLER; INSTALLED REPAIR PART Apr 26, 2003 · N625AW · Airbus A320231 · Fuselage Main, Plate/SkinSDR AWXA200300434Light · looseLAS - EEL - DURING INSPECTION MAINTENANCE DISCOVERED THE L-1 DOOR EMERGENCY EXIT LIGHT FIXTURE LOOSE. REMOVED AND REPLACED L-1 DOOR EMERGENCY EXIT LIGHT, OPERATIONAL CHECK WAS GOOD.Apr 26, 2003 · N636AW · Airbus A320231 · Emergency LightingSDR AWXA200300704Plate · crackedDURING C-04 CHECK 2 EACH .5000 INCH CRACKS WERE FOUND ON AFT CARGO COMPARTMENT FORWARD BULKHEAD, LT UPPER CORNER FRAME PLATE. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED, FABRICATED A REPAIR DOUBLER AND SHIMS; IApr 25, 2003 · N625AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300489Indicator · false indicationMCN - EES - DURING C-03 CHECK THE L-2 DOOR ASSIST CYLINDER GAUGE READ 400 PSI WITH ZERO PRESSURE IN CYLINDER. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR DAMPER EMERGENCY OPERATION CYLINDER IAW AMM TASK 52-13-14-000-001, AND TASK 52-13-14-400-001.Apr 25, 2003 · N622AW · Airbus A320231 · Passenger/Crew DoorsSDR AWXA200300465Rod · out of adjustMCN - EES - DURING C-04 CHECK THE R-1 DOOR PLUNGER TO STRIKE LEVER CLEARANCE WAS FOUND OUT OF LIMITS BETWEEN DIMENSIONS A (J) AND B (J2). MAINTENANCE ADJUSTED THE R-1 DOOR PLUNGER TO STRIKE LEVER CLEARANCE IAW AMM TASK 52-11-14-820-002, SUB TASK 52-11-14-820-0Apr 25, 2003 · N625AW · Airbus A320231 · Passenger/Crew DoorsSDR AWXA200300488Panel · crackedMCN - MAJOR REPAIR - DURING C-03 CHECK A 1.25 INCH CRACK WAS FOUND ON LT PYLON INBOARD SIDE AT FORWARD UPPER CORNER OF PANEL 414CR ATTACH POINT, STA 537. MAINTENANCE CUT OUT DAMAGED SECTION OF EXTRUSION PROFILE AT PYLON STA 537; FABRICATED A FILLER AND REPAIRApr 24, 2003 · N622AW · Airbus A320231 · Nacelle/Pylon, Plate/SkinSDR AWXA200300424Stringer · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON STRINGER 31 RT AT FR 65. MAINTENANCE REMOVED TREATED CORROSION ON STRINGER 31 RT AT FR 65; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW A320 SRM 53-00-13 PG 207-209, & 211-213.Apr 19, 2003 · N632AW · Airbus A320231 · Fuselage Main, Longeron/StringerSDR AWXA200300448Fitting · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK A 1/2 INCH CRACK WAS FOUND ON FITTING AT AFT SIDE OF FORWARD CARGO DOOR FRAME CUTOUT. MAINTENANCE REMOVED DAMAGED FITTING AT AFT SIDE OF FORWARD CARGO DOOR FRAME CUTOUT FR 28, STR 35 R/H; FABRICATED A NEW REPLACEMENT FITTApr 17, 2003 · N632AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300415Fitting · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK A .5 INCH CRACK WAS FOUND FORWARD CARGO FRAME CUTOUT AFT SIDE FITTING, FR 28, STR 35 RT. MAINTENANCE REMOVED DAMAGED FORWARD CARGO FRAME CUTOUT AFT SIDE FITTING, FR 28, STR 35 RT; FABRICATED A NEW REPLACEMENT FITTING; INApr 17, 2003 · N632AW · Airbus A320231 · Fuselage Main, Attach FittingsSDR AWXA200300370Engine · malfunctionedDURING TOGA POWER APPLICATION NR 2 ENGINE SPOOLED UP SLOWER THAN NR 1 ENGINE CAUSING AN ISSUE ON WET RUNWAY, REJECTED TAKEOFF APPROX 15 KTS. INITIAL SPOOL DIFFERENCE WAS ATTRIBUTED TO ENGINES NOT BEING EXACTLY MATCHED AT 1.05 EPR. ON 2ND ATTEMPT ENGINES MATCApr 14, 2003 · N645AW · Airbus A320231 · Engine (Turbine/Turboprop)SDR AWXA200300358Window · failedEN ROUTE FROM PHX TO SNA AT CRUISE THE FIRST OFFICER`S WINDSHIELD INNER PANE SHATTERED SENDING GLASS ALL OVER FLIGHT DECK. EMERGENCY DECLARED, LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICER`S WINDSHIELD ASSEMBLY IAW AMM. ASApr 9, 2003 · N631AW · Airbus A320231 · Flight Compartment WindowsSDR AWXA200300450Floor Support · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK TWO EACH 3/8" CRACKS WERE FOUND AT SCREW HOLES ON FLOOR SUPPORT IN FORWARD CARGO COMPARTMENT FR 28-29, RBL 29. MAINTENANCE CUTOUT DAMAGED SECTION OF FLOOR SUPPORT; FABRICATED A NEW REPLACEMENT SECTION OF FLOOR SUPPORT ANDApr 4, 2003 · N632AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300420Floor Support · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK A .5 INCH CRACK WAS FOUND AT NUT PLATE RIVET HOLE ON AFT CARGO COMPARTMENT FLOOR SUPPORT AT FR 53, LBL 16. MAINTENANCE REMOVED CRACKED FLOOR SUPPORT (PROFILE JOINT) AT FR 53, LBL 16; FABRICATED A NEW REPLACEMENT PROFILE Apr 4, 2003 · N632AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300449Floor Support · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON FITTING FLOOR SUPPORT IN AFT CARGO COMPARTMENT FR 52, RBL 28. MAINTENANCE CUTOUT DAMAGED SECTION OF FLOOR SUPPORT; FABRICATED A NEW REPLACEMENT SECTION OF FLOOR SUPPORT AND SPLICE PLATE; INSTALLED RApr 1, 2003 · N632AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300452Angle · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK A 1/4 INCH CRACK WAS FOUND ON ATTACH ANGLE AT AFT UPPER CORNER OF PANEL 192AB ATTACH POINT FR 34, STR 31 R/H. MAINTENANCE REMOVED DAMAGED ATTACH ANGLE; FABRICATED A NEW REPLACEMENT ANGLE PER DWG C3 D53230256; INSTALLED REMar 31, 2003 · N632AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300451Angle · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK A 5/16 INCH CRACK WAS FOUND ON ATTACH ANGLE AT AFT UPPER CORNER OF PANEL 191AB ATTACH POINT FR 34, STR 31 LT. MAINTENANCE REMOVED DAMAGED ATTACH ANGLE; FABRICATED A NEW REPLACEMENT ANGLE PER DWG C3 D53230256; INSTALLED REMar 31, 2003 · N632AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300409Frame · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK A .125 INCH CRACK WAS FOUND AT THE SIXTH FASTENER HOLE DOWN ON FRAME 39, BETWEEN STR 14-15 LT. MAINTENANCE CUT OUT DAMAGED SECTION OF FRAME 39 BETWEEN STR 14-15 LT; FABRICATED A REPAIR ANGLE AND FILLER; INSTALLED REPAIR Mar 31, 2003 · N632AW · Airbus A320231 · Fuselage Main, FrameSDR AWXA200300408Frame · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK A .1875 INCH CRACK WAS FOUND AT THE FORTH FASTENER HOLE DOWN ON FRAME 41, BETWEEN STR 14-15 LT. MAINTENANCE CUT OUT DAMAGED SECTION OF FRAME 41 BETWEEN STR 14-15 LT; FABRICATED A REPAIR ANGLE AND FILLER; INSTALLED REPAIRMar 31, 2003 · N632AW · Airbus A320231 · Fuselage Main, FrameSDR AWXA200300338Floor Panel · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK A DAMAGED SCREW INSERT, AND 1 1/2 INCH CRACK WERE FOUND ON AFT LAVATORY FLOOR PANEL (261 PF). MAINTENANCE PERFORMED COMPOSITE REPAIR OF CRACK, AND REPLACED DAMAGED SCREW INSERT ON AFT LAVATORY FLOOR PANEL (261 PF) IAW A32Mar 31, 2003 · N632AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200300331Brake · malfunctionedON TAKEOFF ROLL AT PHX EN ROUTE FOR ONT FLIGHT CREW THOUGHT THEY MAY HAVE EXPERIENCED A POSSIBLE BRAKE LOCKUP. AS A PRECAUTION, DECLARED AN EMERGENCY AT ONT.Mar 31, 2003 · N627AW · Airbus A320231 · Master Cylinder/Brake ValveSDR AWXA200300447Skin · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON SKIN AT FR 63 BETWEEN STR 43 AND STR 44 LT. MAINTENANCE CUTOUT DAMAGED SKIN AT FR 63 BETWEEN STR 43 AND STR 44 LT; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW A320 SRM 53-51-11, FIG. 203,Mar 29, 2003 · N632AW · Airbus A320231 · Fuselage Main, Plate/SkinSDR AWXA200300430Floor Support · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR PANEL SUPPORT ANGLE FORWARD OF FR 13, INBOARD AND OUTBOARD OF FLOORBEAM Y-1292. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT ANGLE FR 13, INBOARD AND OUTBOARD OF FLOORBEAM Y-12Mar 29, 2003 · N632AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300423Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y-919 AT FORWARD SIDE OF FR 66. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE WITHIN ALLOWABLE LIMITS PER AWA ER 26-5341-03105-SS1; TREATED, PRIMEDMar 29, 2003 · N632AW · Airbus A320231 · Fuselage Main, Floor BeamSDR AWXA200300421Fitting · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF L-1 DOORWAY LOWER OUTBOARD SILL ATTACH FITTING FR 18, STR 24 LT. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED L-1 Mar 29, 2003 · N632AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300419Seat Track · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF SEAT TRACK Y-1292 AT FR 66. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF BEAM Y-1292 FROM FR 64 TO FR 66; FABRICATMar 29, 2003 · N632AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200300389Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON THE UPPER SURFACE OF FLOORBEAM Y-512 ON FORWARD SIDE OF FR 66 TO FR 66 + 127MM. MAINTENANCE BLENDED OUT CORROSION ON UPPER SURFACE OF FLOORBEAM Y-512, FORWARD SIDE OF FR 66; PERFORMED 10 X Mar 29, 2003 · N632AW · Airbus A320231 · Fuselage Main, Floor BeamSDR AWXA200300385Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF RAIL Y-503, BETWEEN FR 14 AND FR 16. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED CORRODED RAIL Y-503, BETWEEN FR 14 AND FR 16. FABMar 29, 2003 · N632AW · Airbus A320231 · Fuselage Main, Floor BeamSDR AWXA200300384Shear Tie · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK, A 1 INCH CRACK WAS FOUND ON SHEAR WEB AFT SIDE OF FR 68 AND OUTBOARD OF Y-1292 LT. MAINTENANCE REMOVED CRACKED SHEAR WEB AFT SIDE OF FR 68, Y1292 LT; FABRICATED A NEW REPLACEMENT SHEAR WEB. INSTALLED REPAIR PART IAW A3Mar 29, 2003 · N632AW · Airbus A320231 · Fuselage Main, StructureSDR AWXA200300383Shear Tie · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK A CRACK WAS FOUND ON SHEAR WEB AFT SIDE OF FR 68, AND OUTBOARD OF Y-1292 RT. MAINTENANCE REMOVED CRACKED SHEAR WEB AFT SIDE OF FR 68, Y1292 RT. FABRICATED A NEW REPLACEMENT SHEAR WEB. INSTALLED REPAIR PART IAW A320 SRMMar 29, 2003 · N632AW · Airbus A320231 · Fuselage Main, StructureSDR AWXA200300366Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y189, AFT SIDE OF FR 20. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FLOORBEAM TRACK Y189, FR 20; FABRICATED A NEW REPLACEMar 29, 2003 · N632AW · Airbus A320231 · Fuselage Main, Floor BeamSDR AWXA200300412Web · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK 2 AREAS OF CORROSION WERE FOUND ON LOWER SURFACE OF SHEAR WEB FR 69+331MM, FORWARD SIDE OF FR 70, RBL 1275. MAINTENANCE BLENDED OUT CORROSION LOWER SURFACE OF SHEAR WEB FR 69+331MM, FORWARD SIDE OF FR 70, RBL 1275; MATERMar 28, 2003 · N632AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300411Attach Angle · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK A .75 INCH CRACK WAS FOUND ON PARTITION FRAME IN AFT CARGO COMPARTMENT FORWARD BULKHEAD, UPPER RT CORNER. MAINTENANCE PERFORMED HFEC INSPECTION TO DETERMINE WHERE CRACK ENDS; STOP DRILLED CRACK; FABRICATED A REPAIR DOUBLMar 27, 2003 · N632AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300410Attach Angle · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK A .75 INCH CRACK WAS FOUND ON PARTITION FRAME IN AFT CARGO COMPARTMENT FORWARD BULKHEAD, UPPER LT CORNER. MAINTENANCE PERFORMED HFEC INSPECTION TO DETERMINE WHERE CRACK ENDS; STOP DRILLED CRACK; FABRICATED A REPAIR DOUBLMar 27, 2003 · N632AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300318Damper · leakingDURING C-03 CHECK THE L-2 DOOR DAMPER ASSEMBLY WAS FOUND LEAKING. MAINTENANCE REMOVED AND REPLACED THE L-2 DAMPER ASSEMBLY IAW AMM TASK 52-13-14-400-001, OPERATIONAL CHECK WAS GOOD. VENDOR CONFIRMED FAILURE OF DAMPER CYLINDER ASSEMBLY S/N 280 FINDING LEAKAGE TMar 26, 2003 · N633AW · Airbus A320231 · Passenger/Crew DoorsSDR AWXA200300298Selector Valve · leakingEN ROUTE FROM PHX TO PDX APPROXIMATELY 2 HOURS INTO FLIGHT RECEIVED A GREEN HYDRAULIC SYSTEM RESERVOIR LOW LEVEL ECAM MESSAGE, FOLLOWED BY A NR 1 ENGINE GREEN SYSTEM HYDRAULIC PUMP LOW PRESSURE. FOLLOWED ECAM PROCEDURES AND SHUTDOWN THE POWER TRANSFER UNIT ANDMar 23, 2003 · N626AW · Airbus A320231 · Hydraulic System, MainSDR AWXA200300297Battery · dischargedFLIGHT CREW REPORTED THE EMERGENCY FLASHLIGHT AT R-1 DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FLASHLIGHT ASSEMBLY AT THE R-1 DOOR, OPERATIONAL CHECK WAS GOOD.Mar 20, 2003 · N620AW · Airbus A320231 · Emergency EquipmentSDR AWXA200300307Floor Panel · debondedDURING C-03 CHECK THE UPPER SURFACE OF CABIN FLOOR PANEL WAS FOUND DISBONDED FROM BS 3158, FR 66, TO BS 3257, FR 68. MAINTENANCE REMOVED DAMAGED FLOOR PANEL BS 3158, FR 66, TO BS 3257, FR 68; FABRICATED A NEW REPLACEMENT FLOOR PANEL; INSTALLED REPAIR PART IAW Mar 16, 2003 · N633AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200300306Floor Panel · debondedDURING C-03 CHECK THE UPPER SURFACE OF CABIN FLOOR PANEL WAS FOUND DISBONDED FROM BS 2136, FR 47, TO BS 2350, FR 51. MAINTENANCE REMOVED DAMAGED FLOOR PANEL BS 2136, FR 47, TO BS 2350, FR 51; FABRICATED A NEW REPLACEMENT FLOOR PANEL; INSTALLED REPAIR PART IAW Mar 16, 2003 · N633AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200300305Floor Panel · debondedDURING C-03 CHECK THE UPPER SURFACE OF CABIN FLOOR PANEL WAS FOUND DISBONDED FROM BS 950, FR 24, TO BS 1163, FR 28. MAINTENANCE PERFORMED BOND REPAIR ON UPPER SURFACE OF CABIN FLOOR PANEL BS 950, FR 24, TO BS 1163, FR 28 IAW A320 SRM 53-02-00, PG. 203-207, FIGMar 16, 2003 · N633AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200300304Floor Panel · debondedDURING C-03 CHECK THE UPPER SURFACE OF CABIN FLOOR PANEL WAS FOUND DISBONDED FROM BS 3093, FR 64, TO BS 3158, FR 66. MAINTENANCE PERFORMED BOND REPAIR ON UPPER SURFACE OF CABIN FLOOR PANEL BS 3093, FR 64, TO BS 3158, FR 66 IAW A320 SRM 53-02-00, PG. 203-207, FMar 16, 2003 · N633AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200300303Floor Panel · debondedDURING C-03 CHECK THE UPPER SURFACE OF CABIN FLOOR PANEL WAS FOUND DISBONDED FROM BS 3158, FR 66, TO BS 3257, FR 68. MAINTENANCE REMOVED DAMAGED FLOOR PANEL BS 3158, FR 66, TO BS 3257, FR 68; FABRICATED A NEW REPLACEMENT FLOOR PANEL; INSTALLED REPAIR PART IAW Mar 16, 2003 · N633AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200300302Floor Panel · debondedDURING C-03 CHECK THE UPPER SURFACE OF CABIN FLOOR PANEL WAS FOUND DISBONDED FROM BS 2723, FR 58, TO BS 2936, FR 62. MAINTENANCE PERFORMED BOND REPAIR ON UPPER SURFACE OF CABIN FLOOR PANEL BS 2723, FR 58, TO BS 2936, FR 62 IAW A320 SRM 53-02-00, PG. 203-207, FMar 16, 2003 · N633AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200300276Light · missingDURING C-03 THE EMERGENCY ESCAPE PATH LIGHT WAS FOUND MISSING FROM SEAT ROW 19 L/H. MAINTENANCE INSTALLED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT IAW A320 SRM 51-42-11, AND SRM 51-44-11. OPERATIONAL CHECK WAS GOOD IAW T/C F1C33301.Mar 14, 2003 · N629AW · Airbus A320231 · Emergency LightingSDR AWXA200300317Floorbeam · corrodedDURING C-03 CHECK CORROSION WAS FOUND AT 6 EACH NUT PLATES ON LOWER SURFACE OF FLOORBEAM BETWEEN FR 66+10 AND FR 68, LBL 57, Y1732. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED AREA OF FLOORBEAM BETWEEN FR 66+10 ANDMar 13, 2003 · N633AW · Airbus A320231 · Fuselage Main, Floor BeamSDR AWXA200300301Floorbeam · corrodedDURING C-03 CHECK CORROSION WAS FOUND ON THE UPPER SURFACE OF FLOORBEAM WHERE THE LT AFT FLIGHT ATTENDANT SEAT MOUNTS, (OUTBOARD FORWARD MOUNT) FR 66, LBL 35. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OFMar 13, 2003 · N633AW · Airbus A320231 · Fuselage Main, Floor BeamSDR AWXA200300266Cable · brokenLAS - EEL - DURING INSPECTION THE EMERGENCY PATH LIGHT AT SEAT ROW 11 R/H WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT EMERGENCY PATH LIGHT ASSEMBLY SEAT ROW 11 R/H, OPERATIONAL CHECK WAS GOOD.Mar 13, 2003 · N626AW · Airbus A320231 · Emergency LightingSDR AWXA200300265Terminal · brokenFLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT WAS INOPERATIVE. MAINTENANCE REPAIRED WALL PLUG CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT SEAT ROW 26 LT, OPERATIONAL CHECK WAS GOOD.Mar 13, 2003 · N644AW · Airbus A320231 · Light System WiringSDR AWXA200300249Pressure Switch · faultyON CLIMB OUT FROM PHX EN ROUTE FOR BDL THE NR 1 ENGINE DRIVEN (GREEN) HYDRAULIC PUMP FAILED. TURNED BACK TO PHX, TOUCHED DOWN AT 144,000 LBS AT LESS THAN 100 FPM. MAINTENANCE TROUBLESHOT AND FOUND GREEN HYDRAULIC SYSTEM PRESSURE SWITCH (1074GK) DEFECTIVE. REMOMar 11, 2003 · N622AW · Airbus A320231 · Hydraulic Pressure SensorSDR AWXA200300262Connector · brokenMCN - EEL - DURING C-02 CHECK THE EMERGENCY LIGHT SIDEWALL CONNECTOR WAS FOUND BROKEN AT SEAT ROW 10 L/H. MAINTENANCE REPLACED THE EMERGENCY LIGHT SIDEWALL CONNECTOR AT SEAT ROW 10 L/H, OPERATIONAL CHECK WAS GOOD.Mar 5, 2003 · N637AW · Airbus A320231 · Emergency Lighting
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