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 AWXA200600476Seat Track · wornMCN - DURING C06 CHECK DISCOVERED RT OUTBOARD SEAT TRACK WORN BEYOND LIMITS AT FS 41-10. MAINTENANCE REMOVED AND INSTALLED REPLACEMENT SEAT TRACK ON THE RT OUTBOARD SIDE AT FR 41-10 IAW AIRBUS 320 SRM 51-72-11.Feb 26, 2006 · N632AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600388Power Supply · malfunctionedDURING DESCENT RECEIVED BRAKE ANTI-SKID NWS FAULT. TRIED TO CYCLE ANTI-SKID & NW STEERING SWITCH WITH NO HELP. DECLARED EMERGENCY LANDING. ON GROUND, CYCLED CIRCUIT BREAKERS. RECEIVED STEERING BACK. MX REPLACED BSCU, NO HELP. BSCU CHANNEL 1 DEFERRED. ORIFeb 26, 2006 · N625AW · Airbus A320231 · Brake Anti-Skid SectionSDR AWXA200600473Wire · brokenMCN - EEL - DURING C06 CHECK DISCOVERED AFT GALLEY EMERGENCY EXIT LIGHT HAD BROKEN WIRES. MAINTENANCE REPAIRED THE AFT GALLEY EMERGENCY EXIT LIGHT WIRES IAW AIRBUS ESPM 20-43-11. OPERATIONAL CHECKS WERE GOOD IAW AMERICA WEST AIRLINES TASK CARD F1C33301.Feb 25, 2006 · N632AW · Airbus A320231 · Light System WiringSDR AWXA200600474Slide · malfunctionedMCN - EES - DURING C06 CHECK MAINTENANCE WAS UNABLE TO INSTALL THE L2 ESCAPE SLIDE INFLATION BOTTLE LOCK PIN. MAINTENANCE REMOVED AND REPLACED THE L2 ESCAPE SLIDE, OPS CHECKS GOOD IAW AMERICA WEST AIRLINES TASK CARD R1C25304. THIS REPORT WAS GENERATED IN ERROFeb 22, 2006 · N632AW · Airbus A320231 · Escape SlideSDR AWXA200600360Floor Panel · crackedSAL - DURING C5 CHECK DISCOVERED CRACK ON LOWER CORNER FLOOR STRUCTURE OF CUT OUT AT FS 28 ON FORWARD CARGO COMPARTMENT. MAINTENANCE REMOVED AND REPLACED THE LOWER CORNER FLOOR STRUCTURE AT FR 28 IAW AIRBUS 320 SRM 51-72-11.Feb 22, 2006 · N629AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200600346Windshield · crackedREPORTED AT FL350, RT WINDSHIELD CRACKED & HEARD ARCING IN WINDSHIELD. RETURNED & LANDED WITHOUT FURTHER EVENT. MX R & R RT WINDOW IAW AIRBUS 320 MM 56-11-11 AND REPLACED RT WINDOW HEAT CONTROLLER IAW AIRBUS 320 MM 30-42-30. OPS & LEAK CHECKS GOOD. ROOT CAUFeb 20, 2006 · N637AW · Airbus A320231 · Flight Compartment WindowsSDR AWXA200600356Outflow Valve · malfunctionedDURING TAKEOFF ROLL RECEIVED AVIONICS SKIN AIR VALVE FAULT & AN ECAM MESSAGE STATING NOT TO CLIMB ABOVE 10,000 FT. RETURNED & LANDED WITHOUT EVENT. MX R & R SKIN AIR OUTLET VALVE, 22HQ, IAW MM . OPS CHK GOOD. TEARDOWN CONFIRMS FAULT. ON ENTRY TEST, VALVEFeb 19, 2006 · N628AW · Airbus A320231 · Pressure Regulator/Outflow ValveSDR AWXA200600363Stiffener · crackedMCN - DURING C4 CHECK DISCOVERED LEFT A/C BAY FRAME 39 INBOARD VERTICAL STIFFENER CRACKED 1.3" IN LENGTH. MAINTENANCE REMOVED AND INSTALLED NEW STIFFENER AT FRAME 39 AND STR 35L IAW AIRBUS A320 SRM51-42-11 PGS 22 AND 23 AND SRM 51-72-11 PGS 1 AND 2.Feb 18, 2006 · N636AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200600396Floor Panel · corrodedSAL - DURING C5 CHECK DISCOVERED CORROSION ON FLOOR PANEL 131HF IN CARGO COMPARTMENT. MAINTENANCE FOUND THE CORROSION OUT OF LIMITS FOR REPAIR IAW AIRBUS 320 SRM 53-02-00. MAINTENANCE FABRICATED REPLACEMENT PANEL IAW IRM 9701 REV. F PAR. 9 FIG. 4. INSTALLEDFeb 16, 2006 · N629AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200600300Battery · malfunctionedPHX - EEL - DURING OVERNIGHT MAINTENANCE THE EMERGENCY LIGHT SYSTEM TEST "OK" LIGHT WOULD NOT ILLUMINATE AND RECEIVED MESSAGES "COMM EMER R" AND "BATTERY EMER R". MAINTENANCE REMOVED AND REPLACED THE RT OVERWING EMERGENCY POWER SUPPLY BATTERY. OPERATIONAL CHFeb 15, 2006 · N644AW · Airbus A320231 · Emergency LightingSDR AWXA200600298Seat Track · corrodedSAL - DURING C5 CHECK DISCOVERED CORROSION ON THE LT INBOARD SEAT TRACK BETWEEN FS 41 AND FS 47 IN 3 PLACES. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK FROM FS 41 TO FS 47 AND Y765 IAW AIRBUS 320 SRM 51-72-11.Feb 14, 2006 · N629AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600258Warning Light · illuminatedPHX - ABORTED TAKEOFF - FLT 0828 - CREW REPORTED THAT DURING TAKEOFF RECEIVED "RETARD" COMMAND. CREW ABORTED AT 80 KNOTS AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT IAW THE AIRBUS 320 TSM 31-53-00-810-956. NO FAULTS NOTED. GRFeb 13, 2006 · N626AW · Airbus A320231 · Central WarningSDR AWXA200600257Power Supply · inoperativePHX - EEL - DURING OVERNIGHT MAINTENANCE, CIDS FAULTED THE AFT CABIN EMERGENCY LIGHTS. MAINTENANCE REMOVED AND REPLACED THE AFT CABIN POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD.Feb 13, 2006 · N637AW · Airbus A320231 · Emergency LightingSDR AWXA200600395Guide · crackedSAL - DURING C5 CHECK DISCOVERED 4 PLATES CRACKED LOCATED, ONE EACH, AT THE FORWARD AND AFT EMERGENCY EXIT HATCH ON THE RIGHT AND LEFT EMERGENCY EXIT DOORS. MAINTENANCE REMOVED THE CRACKED GUIDE PLATES, ONE AT EACH DOOR, AND INSTALLED NEW REPLACMENT GUIDE PLAFeb 10, 2006 · N629AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200600364Attach Angle · crackedMCN - DURING C4 CHECK DISCOVERED LEFT A/C BAY FRAME 39 STR 35L INSIDE AND OUTSIDE ATTACH ANGLE ON WEB CRACK 2.6" IN LENGTH. REMOVED AND INSTALLED NEW ATTACH ANGLES IN LT A/C BAY FS 39 STR35L IAW AIRBUS A320 SRM 51-72-11 PG 2 AND AIRBUS A320 SRM 51-42-11 PGS 2Feb 8, 2006 · N636AW · Airbus A320231 · Fuselage Main, Attach FittingsSDR AWXA200600362Shear Plate · crackedMCN - DURING C4 CHECK DISCOVERED LEFT AIR CONDITIONING SHEAR PLATE CRACKED, 1.1 INCHES IN LENGTH, AT FS 39 AND STR 35L. MAINTENANCE STOP DRILLED CRACK IN SHEAR PLATE ON WEB AT LT AC BAY FR39 IAW AIRBUS 320 SRM 53-35-11 FIG 222. FABRICATED REPAIR DOUBLER IAW Feb 8, 2006 · N636AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200600335Sill · corrodedMCN - DURING C4 CHECK DISCOVERED LEVEL 2 CORROSION ON THE BULK CARGO DOOR SILL, FORWARD END, UPPER SCREW HOLE AT FS 60 AND STR 38R. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-41-49 FIG 101. MAINTENANCE REMOVED DAMAGED AREA ON SILL BEAM IAWFeb 7, 2006 · N636AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200600240Epsu · inoperativeREPORTED ACFT LEFT OVERWING EXIT LIGHT, CENTER AISLE & ROW 3 FLOOR LIGHTING INTERMITTENT. MX R & R BATTERY PACK & EMERGENCY POWER SUPPLY IAW AIRBUS MM 33-51-30. OP CHECKS GOOD. CONFIRMED FAILURE. VENDOR REPLACED 28 VOLT FUSE AND FS 101. REPAIRED AND TESTEFeb 7, 2006 · N631AW · Airbus A320231 · Emergency LightingSDR AWXA200600397Seat Track · corrodedSAL - DURING C5 CHECK DISCOVERED CORROSION THE RT OUTBOARD SEAT TRACK AT FR 39+2 AND Y-1292. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIGURE 101, PAGE 102. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK FROM FS 36 TO FS 41 AND Y-Feb 6, 2006 · N629AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600418Floor Panel · delaminatedMCN - DURING C4 CHECK DISCOVERED THE AFT RT FLOOR PANEL DELAMINATED FROM FR 64 TO FR 66 AT WL Z-240 AND FROM BL Y-765 TO BL Y-1292. MAINTENANCE REMOVED DAMAGED AREA AND BONDED REPAIR PATCH W/FILLER TO THE AFT RT FLOOR PANEL FROM FR 64 TO FR 66 AT WL Z-240 ANDFeb 5, 2006 · N636AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200600469Frame · corrodedSAL - DURING C4 CHECK DISCOVERED CORROSION ON AFT SIDE OF FR 16 AT THE L1 ENTRY WAY. ORIGINAL DISCREPANCY WAS REPORTED ON SDR AWXA200400680. MAINTENANCE CLOSED OUT THE OPEN MONITOR FOR PREVIOUS TEMP REPAIR IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 26-5Feb 4, 2006 · N629AW · Airbus A320231 · Fuselage Main, StructureSDR AWXA200600367Intercostal · corrodedMCN - DURING C4 CHECK DISCOVERED LEVEL 2 CORROSION ON INTERCOSTAL (BRIDGE ASSY) AT FS 59 ABOVE STR 38R AFT CARGO COMPARTMENT. REMOVED AND INSTALLED NEW INTERCOSTAL (BRIDGE ASSY) AT FS 59 ABOVE STR 38R AFT CARGO COMPARTMENT IAW AIRBUS A320 SRM 51-72-11 AND 51Feb 4, 2006 · N636AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200600245Seat Track · corrodedMCN - DURING C5 CHECK DISCOVERED LEVEL 2 CORROSION LOCATED ON THE RT INBOARD SEAT TRACK BETWEEN FS 41 AND FS 47 IN TWO AREAS. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 103. REMOVED AND INSTALLED NEW SEAT TRACK FROM FS 41Feb 2, 2006 · N633AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600230Power Supply · inoperativeSAL - EEL - DURING C4 CHECK DISCOVERED EMERGENCY LIGHTS AT EMERGENCY DOORS ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BOTH POWER SUPPLIES AT THE RT AND LT OVERWING EXITS. OPERATIONAL CHECKS WERE GOOD IAW AIRBUS 320 AMM 33-51-38. UNIT, POWER SUPPLY; PFeb 2, 2006 · N637AW · Airbus A320231 · Emergency LightingSDR AWXA200600233Sill · corrodedDURING C4 CHECK DISCOVERED CORROSION AROUND NUT PLATES IN TWO LOCATIONS ON BULK CARGO SILL FROM FS 60+1" TO FS 60+11" AT Y-740. CORROSION WAS REMOVED AND FOUND OUT OF LIMITS IAW AIRBUS 320 SRM 53-41-49. MX CUTOUT DAMAGED AREA IAW AIRBUS 320 SRM 53-41-49 AND Jan 30, 2006 · N637AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200600381Fitting · corrodedMCN - DURING C4 CHECK IT WAS DISCOVERED THAT THE R1 DOOR AFT GIRT BAR ANGLE FITTING BRACKET WAS CORRODED AT FS 20. CORROSION WAS EVALUATED AT LEVEL 2 AND THE DAMAGE WAS 4.2" IN LENGTH, 0.007" WIDE AND 0.120" DEEP. MAINTENANCE REMOVED THE DAMAGED ANGLE FITTINJan 29, 2006 · N636AW · Airbus A320231 · Escape SlideSDR AWXA200600377Seat Track · corrodedMCN - DURING C4 CHECK LEVEL 2 EXFOLIATION CORROSION WAS FOUND ON RIGHT HAND OUTBOARD SEAT TRACK FROM FS 20 TO FS 24. ORIGINAL DAMAGE WAS OUT OF LIMITS. MAINTENANCE REMOVED THE DAMAGED SEAT TRACK, FABRICATED 4 REPAIR ANGLES. INSTALLED NEW SEAT TRACK EXTRUSIOJan 29, 2006 · N636AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600375Seat Track · corrodedMCN - DURING C4 CHECK IT WAS DISCOVERED THAT THE RIGHT INBOARD SEAT TRACK AT FS 20-24 HAD LEVEL 2 EXFOLIATION CORROSION 19" IN LENGTH, 3" WIDE AND 0.015" DEEP. ORIGINAL DAMAGE WAS OUT OF LIMITS PER A320 SRM 53-00-15 FIG 10. MAINTENANCE FABBED 4 NEW REPAIR ANJan 29, 2006 · N636AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600361Attach Fitting · corrodedMCN - DURING C4 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION LOCATED ON THE R1 LOWER SILL OUTBOARD ATTACH FITTING FROM FS 17 TO FS 19 AND AT STR 23R. NO CORROSION LIMITS AVAILABLE IN THE AIRBUS SRM. MAINTENANCE REMOVED AND INSTALLED NEW FITTING ON THE R1 LOWEJan 29, 2006 · N636AW · Airbus A320231 · Fuselage Main, Attach FittingsSDR AWXA200600295Seat Track · corrodedMCN - DURING C4 CHECK DISCOVERED LEVEL 2 CORROSION ON THE LT OUTBOARD SEAT TRACK BETWEEN FS 46 AND FS 47 AT Y1292. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 103. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK ON THE LT OUTBOARJan 29, 2006 · N636AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600294Seat Track · corrodedMCN - DURING C4 CHECK DISCOVERED LEVEL 2 CORROSION ON THE RT OUTBOARD SEAT TRACK BETWEEN FS 43 AND FS 44 AND AT Y-1292. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 103. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK ON THE RT OUJan 29, 2006 · N636AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600293Seat Track · corrodedMCN - DURING C4 CHECK DISCOVERED LEVEL 2 CORROSION ON THE RT OUTBOARD SEAT TRACK BETWEEN FS 36 AND FS 41 AND AT Y-1292. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 103. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK ON THE RT OUJan 29, 2006 · N636AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600292Seat Track · corrodedMCN - MAJOR REPAIR - DURING C4 CHECK DISCOVERED LEVEL 2 CORROSION ON THE LT INBOARD SEAT TRACK BETWEEN FS 41 AND FS 47 AND AT Y765. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 103. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK Jan 29, 2006 · N636AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600291Seat Track · corrodedMCN - DURING C4 CHECK DISCOVERED LEVEL 2 CORROSION ON THE LT AND RT INBOARD SEAT TRACK AT FS 40 AND FROM Y765 TO Y-765. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK ON THE LT ANJan 29, 2006 · N636AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600282Floorbeam · corrodedMCN - DURING C4 CHECK DISCOVERED CORROSION ON Y254 BEAM, AT FS 16 AND FS 20+4". CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-11-14 FIG 104. MAINTENANCE REMOVED AND INSTALLED NEW FLOORBEAM AT Y254 FROM FS 12 TO FS 24 IAW AIRBUS 320 SRM 51-47-Jan 29, 2006 · N636AW · Airbus A320231 · Fuselage Main, Floor BeamSDR AWXA200600276Floorbeam · corrodedMCN - DURING C4 CHECK DISCOVERED CORROSION ON THE Y-1350 FLOORBEAM PLATE AT FS 16. NO CORROSION REMOVAL LIMITS AVAILABLE IN THE AIRBUS SRM. MAINTENANCE REMOVED AND INSTALLED NEW FLOOR BEAM PLATE AT Y-1350 AND FR16 IAW AIRBUS 320 SRM 51-42-11 FIG 8.Jan 29, 2006 · N636AW · Airbus A320231 · Fuselage Main, Floor BeamSDR AWXA200600368Floor Panel · delaminatedMCN - DURING C4 INSPECTION IT WAS DISCOVERED THAT GALLEY FLOOR PANEL NR 261 WAS DELAMINATED. THE FLOORPANEL NR 261DF WAS REPAIRED IAW AIRBUS A320 SRM 53-12-00 FIG 204.Jan 28, 2006 · N636AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200600274Floor Panel · crackedMCN - DURING C4 CHECK DISCOVERED CABIN FLOOR PANEL, 221DF, CRACKED 6 INCHES. MAINTENANCE REMOVED FLOOR PANEL 221DF, FABRICATED REPLACEMENT PANEL AND INSTALLED IAW AIRBUS DWG D53610334.Jan 28, 2006 · N636AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200600273Floor Panel · delaminatedMCN - DURING C4 CHECK DISCOVERED CABIN FLOOR PANEL, 232DF, DELAMINATED. MAINTENANCE REMOVED FLOOR PANEL 232DF AND FABRICATED REPLACEMENT PANEL AND INSTALLED IAW AIRBUS DWG D53610331.Jan 28, 2006 · N636AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200600369Seal · corrodedDURING C4 CHECK LEVEL 2 GALVANIC CORROSION WAS DISCOVERED ON FWD CARGO BAY DOOR THRESHOLD LOWER STRAP SEAL BUTT AT FS 27 JUST ABOVE NR 5 LATCH ROLLER. CORROSION WAS 4.5" IN LENGTH AND 1" WIDE. MAINTENANCE REMOVED AND INSTALLED NEW STRAP SEAL BUTT AT FS 27 JUJan 27, 2006 · N636AW · Airbus A320231 · Cargo/Baggage DoorsSDR AWXA200600304Beam · corrodedMCN - DURING C4 CHECK DISCOVERED CORROSION ON 2 FASTENER HOLES AT THE FWD END OF THE BULK CARGO DOOR CUTOUT, LOWER SILL BEAM AT FR60+6" AND STR 38R. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-41-49 FIG 203. MAINTENANCE REMOVED DAMAGE FROM Jan 27, 2006 · N636AW · Airbus A320231 · Fuselage Main, StructureSDR AWXA200600151Fuel Control · malfunctionedDURING GROUND HANDLING OPERATIONS, WAS REPORTED THAT THERE WAS AN APU TAIL PIPE FIRE AFTER SHUTDOWN. T-HANDLE WAS PULLED, BOTTLE WAS NOT BLOWN. MAINTENANCE INSPECTED THE APU AND TAILPIPE. REMOVED AND REPLACED THE APU FUEL FLOW DIVIDER AND THE APU FUEL CONTRJan 27, 2006 · N628AW · Airbus A320231 · APU Engine Fuel and ControlSDR AWXA200600289Bolt · corrodedMCN - LEVEL 2 CORROSION WAS FOUND ON THE RT WING, SPOILERS 1 THROUGH 5, INNER HINGE PIN BOLTS AT THE THREAD AND HEAD RADIUS. NO CORROSION LIMITS WERE AVAILABLE. ALL SPOILER, INNER HINGE, PIN BOLTS WERE REMOVED AND REPLACED ON SPOILERS 1 THROUGH 5 IAW AIRBUS Jan 26, 2006 · N636AW · Airbus A320231 · SpoilersSDR AWXA200600275Floor Panel · corrodedMCN - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ON THE AFT SIDE OF FLOOR PANEL 262FF. NO CORROSION REMOVAL LIMITS WERE FOUND IN THE AIRBUS SRM. MAINTENANCE REMOVED FLOOR PANEL 262FF AND INSTALLED NEW FLOOR PANEL.Jan 26, 2006 · N636AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200600366Plate · corrodedDURING C4 CHECK LEVEL 2 CORROSION WAS FOUND ON THE R2 FORWARD GIRT FITTING PLATE AT FS 66 TO FS 67. MAINTENANCE REMOVED AND INSTALLED NEW PLATE ON THE R2 FWD GIRT FITTING AT FS 66 TO FS 67 IAW AIRBUS A320 AMM 52-11-31. CORROSION HAS BEEN RE-LEVELED TO A LEVEJan 25, 2006 · N636AW · Airbus A320231 · Escape SlideSDR AWXA200600365Shear Plate · corrodedMCN - DURING C4 CHECK LEVEL 1 CORROSION WAS DISCOVERED ON THE BOTTOM SURFACE OF THE LEFT HAND LATERAL SHEAR PLATE AT Y1295 AND FS 69-70. MAINTENANCE REMOVED AND INSTALLED NEW LATERAL SHEAR PLATE AT Y1295 AND FS 69-70 IAW AIRBUS A320 SRM 51-42-11 PGS 22-23 FIGJan 25, 2006 · N636AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200600303Beam · corrodedMCN - DURING C4 CHECK DISCOVERED CORROSION ON 2 FASTENER HOLES AT THE AFT END OF THE BULK CARGO DOOR CUTOUT, LOWER SILL BEAM AT FS 62 AND STR 38R. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-41-49 FIG 203. MAINTENANCE REMOVED DAMAGE FROM THJan 25, 2006 · N636AW · Airbus A320231 · Fuselage Main, StructureSDR AWXA200600290Bolt · corrodedMCN - LEVEL 2 CORROSION WAS FOUND ON THE LT WING, SPOILERS 3 THROUGH 5, INNER HINGE PIN BOLTS AT THE THREAD AND HEAD RADIUS. NO CORROSION LIMITS WERE AVAILABLE. ALL SPOILER, INNER HINGE, PIN BOLTS WERE REMOVED AND REPLACED ON THE LT WING, SPOILERS 3 THROUGH Jan 25, 2006 · N636AW · Airbus A320231 · SpoilersSDR AWXA200600288Floorbeam · corrodedMCN - DURING C4 CHECK DISCOVERED CORROSION ON Y765 BEAM AND FS 68. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-04 FIG 102. MAINTENANCE REMOVED AND INSTALLED NEW FLOORBEAM AT Y765 AND FS 68 IAW AIRBUS 320 SRM 51-72-11.Jan 25, 2006 · N636AW · Airbus A320231 · Fuselage Main, Floor BeamSDR AWXA200600287Floorbeam · corrodedMCN - DURING C4 CHECK DISCOVERED CORROSION ON Y-765 BEAM, BETWEEN FS 67 AND FS 68. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14 FIG 102. MAINTENANCE REMOVED AND INSTALLED NEW FLOORBEAM AT Y-765 FROM FS 67 TO FS 68 IAW AIRBUS 320 SRM 51Jan 25, 2006 · N636AW · Airbus A320231 · Fuselage Main, Floor Beam
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