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 AWXA200300627Profile · corrodedMCN - MINOR REPAIR - DURING C-03 CHECK CORROSION WAS FOUND ON PROFILE AT STR 38 RT, JUST FORWARD OF FRAME 48. MAINTENANCE REMOVED DAMAGED PROFILE AT STR 38 RT, JUST FORWARD OF FRAME 48; FABRICATED A NEW REPLACEMENT PROFILE; INSTALLED REPAIR PART IAW A320 SRM May 21, 2003 · N631AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300598Terminal · brokenDURING C-01 CHECK THE EMERGENCY EXIT LIGHT BETWEEN THE L/H OVER-WING HATCHES WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED A BROKEN EMERGENCY EXIT LIGHT TERMINAL LUG BETWEEN L/H OVER-WING EXITS IAW A320 ESPM 20-48-14, PG. 1-3, OPERATIONAL CHECK WAS GOMay 21, 2003 · N646AW · Airbus A320231 · Light System WiringSDR AWXA200300574Cylinder · leakingDURING 4-DAY CHECK THE R-1 DOOR ASSIST BOTTLE PRESSURE WAS FOUND AT 500 PSI. MAINTENANCE REPLACED O-RING SEALS ON R-1 DOOR DAMPER CYLINDER ASSEMBLY; OPERATIONAL CHECK WAS GOOD.May 21, 2003 · N632AW · Airbus A320231 · Passenger/Crew DoorsSDR AWXA200300573Oxygen Mask · leakingFLIGHT CREW REPORTED THE FIRST OFFICERS OXYGEN MASK IS LEAKING. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS OXYGEN MASK IAW T/C R1B35301, OPERATIONAL CHECK WAS GOOD. VENDOR LEAK TEST OF OXYGEN MASK S/N 23208 FOUND NO LEAKS, REASON FOR REMOVAL WAS NOT May 21, 2003 · N632AW · Airbus A320231 · Crew Oxygen SystemSDR AWXA200300601Floor Panel · delaminatedDURING C-01 CHECK CENTER WING FLOOR PANEL 241EF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGED FLOOR PANEL 241EF; FABRICATED A NEW REPLACEMENT PANEL PER DWG 10D536-70057; INSTALLED REPAIR PART IAW AWA T/C R1C25306.May 19, 2003 · N646AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200300600Floor Panel · delaminatedMCN - MAJOR REPAIR - DURING C-01 CHECK CABIN FLOOR PANEL 241FF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGED FLOOR PANEL 241FF; FABRICATED A NEW REPLACEMENT PANEL PER DWG 10D536-70057; INSTALLED REPAIR PART IAW AWA T/C R1C25306.May 19, 2003 · N646AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200300599Floor Panel · delaminatedMCN - MAJOR REPAIR - DURING C-01 CHECK CENTER WING FLOOR PANEL 242FF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGED FLOOR PANEL 242FF; FABRICATED A NEW REPLACEMENT PANEL PER DWG 10D536-70055; INSTALLED REPAIR PART IAW AWA T/C R1C25306.May 19, 2003 · N646AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200300571Floor Panel · delaminatedMCN - MAJOR REPAIR - DURING C-01 CHECK CABIN FLOOR PANEL 242GF WAS FOUND DELAMINATED. MAINTENANCE REMOVED CABIN FLOOR PANEL 242GF; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG D536-70055; INSTALLED NEW PANEL IAW AWA T/C R1C25306, AND A320 SRM 53-02-00, PGMay 19, 2003 · N646AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200300640Floor Panel · delaminatedMCN - MAJOR REPAIR - DURING C-03 CHECK PASSENGER CABIN FLOOR PANEL 251LF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGED FLOOR PANEL 251LF; FABRICATED A NEW REPLACEMENT PANEL PER DWG 10D53670022; INSTALLED REPAIR PART IAW T/C R1C25306 AND SRM 53-02-00 PG 2May 18, 2003 · N631AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200300639Floor Panel · delaminatedMCN - MAJOR REPAIR - DURING C-03 CHECK PASSENGER CABIN FLOOR PANEL 251RF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGED FLOOR PANEL 251RF; FABRICATED A NEW REPLACEMENT PANEL PER DWG 10D53670022; INSTALLED REPAIR PART IAW T/C R1C25306 AND SRM 53-02-00 PG 2May 18, 2003 · N631AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200300595Structure · crackedDURING C-03 CHECK A 1/2 INCH CRACK WAS FOUND ON RT PYLON ATTACH ANGLE (EXTRUSION PROFILE) AT THE INBOARD FORWARD CORNER OF PANEL 4230 LT. MAINTENANCE CUTOUT DAMAGED SECTION OF ATTACH ANGLE; FABRICATED A FILLER AND REPAIR SPLICE; INSTALLED REPAIR PARTS IAW A320May 18, 2003 · N631AW · Airbus A320231 · Nacelle/Pylon, Frame/Spar/RibSDR AWXA200300597Terminal · brokenDURING C-01 CHECK THE L-1 DOOR CLASS DIVIDER EMERGENCY EXIT LIGHT CONNECTOR WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR CLASS DIVIDER EMERGENCY EXIT LIGHT CONNECTOR IAW A320 ESPM 20-48-24, PG. 18, OPERATIONAL CHECK WAS GOOD IAW AMM SUBTASKMay 15, 2003 · N646AW · Airbus A320231 · Light System WiringSDR AWXA200300570Fitting · brokenMCN - EES - DURING C-01 CHECK THE LT OVERWING HATCH SLIDE BOTTLE CABLE FITTING WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING HATCH SLIDE BOTTLE IAW AMM SUBTASK 25-62-46-020-050-A, AND 25-62-46-420-050-A, OPERATIONAL CHECK WAS GOOD IAW AMMMay 15, 2003 · N646AW · Airbus A320231 · Escape SlideSDR AWXA200300544Damper · shearedMCN - EES - DURING C-04 CHECK THE R-1 DOOR DAMPER CYLINDER KNURLED KNOB WAS FOUND SHEARED. MAINTENANCE REMOVED AND REPLACED THE R-1 DOOR DAMPER CYLINDER IAW AMM TASK 52-11-14-000-001, 52-11-14-400-001, AND 52-11-14-04 FIG 401 & 402, SHT 1.May 8, 2003 · N625AW · Airbus A320231 · Passenger/Crew DoorsSDR AWXA200300504Wire · brokenDURING C-03 CHECK THE LT EMERGENCY ESCAPE SLIDE ARMED LIGHT WOULD NOT COME ON WITH THE FORWARD OR AFT OVER WING EXIT DOOR HANDLES OPEN AND BOTH EXITS ARMED. MAINTENANCE TROUBLESHOT SYSTEM USING A320 ASM 52-73-00 AND FOUND A WIRE BROKEN AT TERMINAL A OF LT EMERMay 7, 2003 · N622AW · Airbus A320231 · Equipment/Furnishings WiringSDR AWXA200300705Floorbeam · corrodedDURING C-04 EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y1292 RT, FORWARD FO FR 67. MAINTENANCE REMOVED FLOORBEAM BETWEEN FR 66 AND FR 68, FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 6 AND 7.May 6, 2003 · N625AW · Airbus A320231 · Fuselage Main, Floor BeamSDR AWXA200300694Profile · crackedDURING C-04 CHECK A .25 INCH CRACK WAS FOUND ON FORWARD CARGO COMPARTMENT FLOOR SUPPORT SPLICE AT FR 31, RBL 28. MAINTENANCE REMOVED DAMAGED SECTION OF PROFILE AT FR 31, RBL 28; FABRICATED A NEW REPLACEMENT SECTION OF PROFILE, AND SPLICE REPAIR DOUBLERS; INSTMay 5, 2003 · N625AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300529Wire · brokenMCN - EEL - DURING C-03 CHECK THE EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 7 LT READS OPEN. MAINTENANCE SPLICED BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 7 LT IAW ESPM 20-43-11 PG 9, OPERATIONAL CHECK WAS GOOD.May 4, 2003 · N622AW · Airbus A320231 · Light System WiringSDR AWXA200300528Wire Harness · shortedMCN - EEL - DURING C-03 CHECK THE EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 13 LT READS OPEN. MAINTENANCE REPAIRED EMERGENCY ESCAPE PATH LIGHT WIRING AT SEAT ROW 13 LT IAW ESPM 20-48-14, PG 12-13, OPERATIONAL CHECK WAS GOOD.May 4, 2003 · N622AW · Airbus A320231 · Light System WiringSDR AWXA200300625Profile · corrodedMCN - MINOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT CENTER FLOOR PROFILE STR 38 LT TO STR 38 RT, FR-50. MAINTENANCE REMOVED CENTER FLOOR PROFILE FROM STR 38 LT TO STR 38 RT, FR-50; FABRICATED A NEW REPLACEMENT CENTER FLOOR PROFMay 2, 2003 · N625AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300624Profile · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT CORNER PROFILE FR 56-58, LBL 686MM. MAINTENANCE CUT OUT DAMAGED AREA OF AFT CARGO COMPARTMENT CORNER PROFILE FR 56-58, LBL 686MM; FABRICATED A FILLER AND DOUBLER; INSTALMay 2, 2003 · N625AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300619Profile · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT CORNER PROFILE FR 59-60, RBL 686 MM. MAINTENANCE REMOVED DAMAGED AFT CARGO COMPARTMENT CORNER PROFILE FR 59-60, RBL 686MM, FABRICATED A NEW REPLACEMENT PROFILE; INSTALLEMay 2, 2003 · N625AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300618Profile · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT FLOOR PROFILE FR 59, LBL 660 MM TO RBL 660 MM. MAINTENANCE REMOVED AND REPLACED AFT CARGO COMPARTMENT FLOOR PROFILE FR 59, LBL 660MM TO RBL 660MM IAW AWA E.R. 26-5341-031May 2, 2003 · N625AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300617Profile · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT CENTER FLOOR PROFILE FR 53, STR 38 L/H TO STR 38 R/H. MAINTENANCE REMOVED AND REPLACED AFT CARGO COMPARTMENT CENTER FLOOR PROFILE FR 53, STR 38 L/H TO STR 38 R/H IAW A320May 2, 2003 · N625AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300616Profile · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT CENTER FLOOR PROFILE FR 50, STR 38 LT. MAINTENANCE CUTOUT DAMAGED SECTION OF AFT CARGO COMPARTMENT CENTER PROFILE FR 50, STR 38 LT; FABRICATED A NEW REPLACEMENT SECTION OMay 2, 2003 · N625AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300615Profile · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT CORNER PROFILE FR 56-58, RBL 686 MM. MAINTENANCE CUTOUT DAMAGED SECTION OF AFT CARGO COMPARTMENT CORNER PROFILE FR 56-58, RBL 686 MM; FABRICATED 2 EACH FILLERS AND DOUBLEMay 2, 2003 · N625AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300614Profile · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT FLOOR PROFILE FR 58, LBL 660MM TO RBL 660MM. MAINTENANCE REMOVED AND REPLACED AFT CARGO COMPARTMENT FLOOR PROFILE FR 58, LBL 660MM TO RBL 660MM IAW AWA E.R. 26-5341-03142May 2, 2003 · N625AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300613Profile · corrodedMCN - MINOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT CORNER PROFILE FR 59-61, LBL 686MM. MAINTENANCE CUTOUT DAMAGED SECTION OF AFT CARGO COMPARTMENT CORNER PROFILE FR 59-61, LBL 686MM; FABRICATED A NEMay 2, 2003 · N625AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300612Structure · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT CORNER PROFILE FR 58 - 59, LBL 686 MM. MAINTENANCE REMOVED AND REPLACED AFT CARGO COMPARTMENT CORNER PROFILE FR 58-59, LBL 686 MM IAW A320 SRM 53-41-14, FIG. 24, PG. B31-May 2, 2003 · N625AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300611Frame · crackedDURING C-04 CHECK AFTER FIRST OVERSIZE OF FASTENER HOLE COMMON TO SKIN 2 EACH 1/8 INCH CRACKS WERE FOUND ON FRAME 39, THIRD FASTENER HOLE BELOW STR 14 L/H. MAINTENANCE REAMED OUT HOLE TO SECOND OVERSIZE AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXISTMay 2, 2003 · N625AW · Airbus A320231 · Fuselage Main, FrameSDR AWXA200300610Frame · crackedDURING C-04 CHECK AFTER FIRST OVERSIZE OF FASTENER HOLE COMMON TO SKIN A 1/8 INCH CRACK WAS FOUND ON FRAME 41, THIRD FASTENER HOLE BELOW STR 14 LT. MAINTENANCE REAMED OUT HOLE TO SECOND OVERSIZE AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; CUTOUTMay 2, 2003 · N625AW · Airbus A320231 · Fuselage Main, FrameSDR AWXA200300543Floor Support · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK A .5 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT FLOOR PANEL SUPPORT AT FR 63, LBL 406MM. MAINTENANCE REMOVED DAMAGED FLOOR PANEL SUPPORT AT FR 63, LBL 406MM; FABRICATED A NEW REPLACEMENT FLOOR PANEL SUPPORT; INSTALLEDMay 2, 2003 · N625AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300706Fitting · arcedDURING C-04 CHECK A HOLE WAS FOUND BURNT INTO THE INBOARD EDGE OF NR 2 PYLON TO WING ATTACH FITTING, ARCING CAUSED FROM NR 2 IDG FEEDER CABLE. MAINTENANCE REMOVED SPIGOT FITTING AND FORWARD INBOARD PYLON ATTACH FITTING; FABRICATED A NEW REPLACEMENT INBOARD PYMay 1, 2003 · N625AW · Airbus A320231 · Wing, Attach FittingsSDR AWXA200300626Skin · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON CORNER FITTING AT AFT LOWER CORNER OF FORWARD CARGO DOOR CUTOUT. MAINTENANCE REMOVED DAMAGED CORNER FITTING AT AFT LOWER CORNER OF FORWARD CARGO DOOR CUTOUT; FABRICATED A NEW REPLACEMENT FITTING; INSTALLED May 1, 2003 · N625AW · Airbus A320231 · Fuselage Main, Plate/SkinSDR AWXA200300623Angle · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SPLICE ANGLE AT AFT LOWER CORNER OF THE FORWARD CARGO DOOR CUTOUT, FR-28. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SPLICE ANGLE AT AFT May 1, 2003 · N625AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300693Floor Support · crackedMCN - MINOR REPAIR - DURING C-04 CHECK A .4375 INCH CRACK WAS FOUND ON FORWARD CARGO COMPARTMENT FLOOR SUPPORT AT FR 28, LBL 28. MAINTENANCE CUT OUT DAMAGED SECTION OF FLOOR SUPPORT AT FR 28, LBL 28; FABRICATED A NEW REPLACEMENT SECTION OF FLOOR SUPPORT AND SApr 29, 2003 · N625AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300542Floor Support · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK A 1.5 INCH CRACK WAS FOUND ON FORWARD CARGO COMPARTMENT FLOOR SUPPORT AT FR 28, RBL 11. MAINTENANCE REMOVED DAMAGED FLOOR SUPPORT AT FR 28, RBL 11; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; INSTALLED REPAIR PART IAW A3Apr 29, 2003 · N625AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300497Support · crackedDURING C-04 CHECK 4 EACH CRACKS WERE FOUND AT RIVET HOLES ON FORWARD CARGO COMPARTMENT CEILING PANEL SUPPORT, AFT BULKHEAD FR 34, RBL 10 & 28, LBL 10 & 28. MAINTENANCE ROUTED OUT HOLES; FABRICATED ANGLE DOUBLERS AND FILLERS; INSTALLED REPAIR PARTS IAW AWA E.R.Apr 29, 2003 · N625AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300490Floor Panel · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK A 1.5 INCH CRACK WAS FOUND IN CENTER OF FLOOR PANEL 261NF. MAINTENANCE PERFORMED COMPOSITE REPAIR OF CRACK IN CENTER OF FLOOR PANEL 261NF IAW A320 SRM 53-02-00 PG 203-207 FIG 202.Apr 29, 2003 · N625AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200300577Angle · crackedDURING C-04 CHECK A 3 INCH CRACK WAS FOUND ON ATTACH ANGLE AT FR 34 ON SUPPORT STRUCTURE AT AFT UPPER EDGE OF PANEL 191AB. MAINTENANCE REMOVED CRACKED ATTACH ANGLE AT FR 34; FABRICATED A NEW REPLACEMENT ATTACH ANGLE; INSTALLED REPAIR PART IAW AWA E.R. 26-5323-Apr 28, 2003 · N625AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300546Angle · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK A .5 INCH CRACK WAS FOUND ON ATTACH ANGLE AT FR 34 ON FAIRING SUPPORT STRUCTURE AT AFT UPPER EDGE OF PANEL 192AB. MAINTENANCE REMOVED DAMAGED ATTACH ANGLE AT FR-34; FABRICATED A NEW REPLACEMENT ATTACH ANGLE; INSTALLED REApr 28, 2003 · N625AW · Airbus A320231 · Aerodynamic FairingsSDR AWXA200300551Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER SURFACE OF FLOORBEAM Y179 AT FR 20. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED FLOORBEAM; FABRICATED A NEW REPLACEMENT FLOORBEAApr 27, 2003 · N625AW · Airbus A320231 · Fuselage Main, Floor BeamSDR AWXA200300541Floor Support · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y254, FR-16 -17, RBL 254MM. UPON FURTHER INSPECTION A .625 INCH CRACK WAS FOUND IN SAME LOCATION; MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM Y254, FR-16 -17, RBL 25Apr 27, 2003 · N625AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300531Floor Support · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR SUPPORT Y254, FR 16 TO FR 20. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED FLOOR SUPPORT Y254, FR 16 TO FR 20; FABRICATED 4 EACH REPAApr 27, 2003 · N625AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200300506Frame · crackedMCN - MAJOR REPAIR - DURING C-03 CHECK A .0625 INCH CRACK WAS FOUND AT THE FIFTH FASTENER HOLE DOWN ON FRAME 39, STR 14 LT. MAINTENANCE CUT OUT DAMAGED SECTION OF FRAME 39 AT STR 14 LT; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW AWA EO 5Apr 27, 2003 · N622AW · Airbus A320231 · Fuselage Main, FrameSDR AWXA200300505Fitting · brokenMCN - EES - DURING C-03 CHECK THE R-1 DOOR REDUCER SHAFT MECHANISM RIG PIN FITTING WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE R-1 DOOR REDUCER SHAFT MECHANISM RIG PIN FITTING PER AIRBUS INDUSTRIES CMM 52-11-15, PG. 319, 745, FIG. 308.Apr 27, 2003 · N622AW · Airbus A320231 · Passenger/Crew DoorsSDR AWXA200300495Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y1292, AT AFT SIDE OF FR 66 TO FORWARD SIDE OF FR 68. MAINTENANCE REMOVED DAMAGED FLOORBEAM Y1292, FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT BEAM; INSApr 27, 2003 · N625AW · Airbus A320231 · Fuselage Main, Floor BeamSDR AWXA200300494Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y1292, AT FR 68. MAINTENANCE REMOVED DAMAGED FLOORBEAM Y1292, FROM FR 68 TO FR 70; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42Apr 27, 2003 · N625AW · Airbus A320231 · Fuselage Main, Floor BeamSDR AWXA200300493Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y1292, FORWARD OF FR 66. MAINTENANCE REMOVED DAMAGED FLOORBEAM Y1292, FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SApr 27, 2003 · N625AW · Airbus A320231 · Fuselage Main, Floor BeamSDR AWXA200300491Floor Support · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK A 1 INCH CRACK WAS FOUND AT FASTENER HOLE ON FLOOR SUPPORT Y1292, FR 18. MAINTENANCE CUTOUT DAMAGED AREA ON FLOOR SUPPORT Y1292, AT FR 18; FABRICATED 2 EACH REPAIR ANGLES AND A FILLER; INSTALLED REPAIR PARTS IAW A320 SRMApr 27, 2003 · N625AW · Airbus A320231 · Fuselage Miscellaneous Structure
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