IAE V2500-A1

Service difficulty reports · 306

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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 engine_model_key = 'V2500A1'
  ORDER BY difficulty_date DESC"

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SDR AWXA200400946Shear Plate · corrodedDURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT AFT SHEAR PLATE BETWEEN FR 69 AND FR 70, STR 24 RT. MAINTENANCE REMOVED CORRODED RT AFT SHEAR PLATE FROM FR 69 TO FR 70, STR 24 RT; FABRICATED A NEW REPLACEMENT SHEAR PLATE, AND IAug 15, 2004 · N631AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200400949Floor Panel · delaminatedDURING C-04 CHECK FOUND THE FLOOR PANEL 262 EF DELAMINATED, FR 66 - FR 68, Y765 R/H - Y1292 RT. MAINTENANCE REMOVED DELAMINATED FLOOR PANEL 262 EF; FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW DWG 10D53670053 AND A320 SRM 53-02-00, FIG. 209.Aug 15, 2004 · N631AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200400957Seat Track · corrodedDURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON SEAT RAIL BEAM AT Y1292 RT, BETWEEN FR 64 AND FR 66. MAINTENANCE REMOVED CORRODED SEAT RAIL BEAM FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.Aug 15, 2004 · N631AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200400971Beam · corrodedDURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y512 LT AT FR 66. MAINTENANCE REMOVED CORRODED BEAM Y512 LT AT FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 8.Aug 15, 2004 · N631AW · Airbus A320231 · Fuselage Main, StructureSDR AWXA200400994Floor Panel · delaminatedDURING C-04 CHECK FOUND AFT CARGO COMPARTMENT FLOOR PANEL 151 PF DELAMINATED ON AFT SIDE. MAINTENANCE REMOVED DELAMINATED AFT CARGO COMPARTMENT FLOOR PANEL 151 PF FROM FR 58 TO FR 59; FABRICATED A NEW REPLACEMENT FLOOR IAW A320 SRM 53-02-00, FIG. 209, PG. 233-Aug 15, 2004 · N631AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200400997Web · crackedDURING C-04 CHECK A 1.5 INCH CRACK WAS FOUND IN LT AFT OB TRAY (WEB) BETWEEN FR 68 AND FR 69, OB OF BEAM Y1292 LT. MAINTENANCE REMOVED CRACKED LT AFT OB TRAY FROM FR 68 TO FR 69, Y1732 LT TO Y1792 LT; FABRICATED A NEW REPLACEMENT TRAY; INSTALLED REPAIR PART Aug 15, 2004 · N631AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200400998Shear Plate · corrodedDURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON LT AFT SHEAR PLATE BETWEEN FR 69 AND FR 70, AT STR 24 LT. MAINTENANCE REMOVED CORRODED LT AFT SHEAR PLATE FROM FR 69 TO FR 70, AT STR 24 LT; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW Aug 15, 2004 · N631AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200401001Web · crackedDURING C-04 CHECK A 1.5 INCH CRACK WAS FOUND IN RT AFT OB TRAY (WEB) BETWEEN FR 68 AND FR 69, OB OF BEAM Y1292 RT. MAINTENANCE REMOVED CRACKED RT AFT OB TRAY FROM FR 68 TO FR 69, Y1292 RT; FABRICATED A NEW REPLACEMENT TRAY; INSTALLED REPAIR PART IAW A320 SRAug 15, 2004 · N631AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200400947Dummy Rail · corrodedDURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON DUMMY RAIL Y503 LT BETWEEN FR 14 AND FR 16. MAINTENANCE REMOVED CORRODED DUMMY RAIL Y503 LT FROM FR 14 TO FR 16; FABRICATED A NEW REPLACEMENT RAIL, AND INSTALLED REPAIR PART IAW A320 SRM 51-72-11.Aug 14, 2004 · N631AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200400950Floor Panel · delaminatedDURING C-04 CHECK FOUND GALLEY FLOOR PANEL 261 DF DELAMINATED, FR 66 - FR 68, Y765 L/H - Y765 RT. MAINTENANCE REMOVED DELAMINATED FLOOR PANEL 261 DF; FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW DWG 10D53670048 AND A320 SRM 53-02-00, FIG. 209.Aug 14, 2004 · N631AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200400969Seat Track · corrodedDURING C-04 CHECK CORROSION WAS FOUND IN NUMEROUS AREAS OF RT OB SEAT TRACK Y1292, BETWEEN FR 41 AND FR 47. MAINTENANCE REMOVED CORRODED RT OB SEAT TRACK Y1292, FROM FR 41 TO FR 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAWAug 14, 2004 · N631AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200400978Seat Track · corrodedDURING C-04 CHECK, CORROSION WAS FOUND IN NUMEROUS PLACES ON LT IB SEAT TRACK BS 16408 TO BS 17255, FR 37 TO FR 39. MAINTENANCE REMOVED CORRODED SEAT TRACK Y765 LT FROM FR 37 TO FR 39; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SAug 14, 2004 · N631AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200400999Seat Track · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK Y1292 LT BETWEEN FR 16 AND FR 20. MAINTENANCE REMOVED CORRODED SEAT TRACK Y1292 LT FROM FR 12 TO FR 20; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.Aug 14, 2004 · N631AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200401000Seat Track · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON SEAT TRACK Y1292 LT BETWEEN FR 18 AND FR 20. MAINTENANCE REMOVED CORRODED SEAT TRACK Y1292 LT FROM FR 18 TO FR 20; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 53-11-15, FIG. 203, PG. 209Aug 14, 2004 · N631AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200400948Skin · delaminatedDURING C-04 CHECK FOUND THE LT SIDE OF RUDDER DELAMINATED 16 INCHES FROM TOP, RUDDER STA 569 LT. MAINTENANCE CUTOUT DAMAGED AREA ON LT SIDE OF RUDDER 16 INCHES FROM TOP; PERFORMED BOND REPAIR IAW A320 SRM 55-41-00, FIG. 218, PG. 327-328.Aug 13, 2004 · N631AW · Airbus A320231 · Rudder, Plate/SkinSDR AWXA200400995Floor Panel · delaminatedDURING C-04 CHECK FOUND AFT CARGO COMPARTMENT FLOOR PANEL 152 EF DELAMINATED IN THREE AREAS. MAINTENANCE REMOVED DELAMINATED AFT CARGO COMPARTMENT FLOOR PANEL 152 EF FROM FR 49 TO FR 53; FABRICATED A NEW REPLACEMENT FLOOR IAW A320 SRM 53-02-00, FIG. 209, PG. 2Aug 13, 2004 · N631AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200400996Floor Panel · delaminatedDURING C-04 CHECK FOUND AFT CARGO COMPARTMENT FLOOR PANEL 152 MF DELAMINATED ON AFT SIDE. MAINTENANCE REMOVED DELAMINATED AFT CARGO COMPARTMENT FLOOR PANEL 152 MF FROM FR 56 TO FR 58; FABRICATED A NEW REPLACEMENT FLOOR IAW A320 SRM 53-02-00, FIG. 209, PG. 233-Aug 13, 2004 · N631AW · Airbus A320231 · Fuselage Floor PanelSDR AWXA200400952Proximity Switch · brokenDURING C-04 CHECK THE L-2 DOOR WARNING LIGHT DID NOT ILLUMINATE WHEN DOOR WAS ARMED AND HANDLE WAS RAISED. MAINTENANCE REMOVED AND REPLACED EMERGENCY DOOR HANDLE SHAFT PROXIMITY SWITCH IAW A320 AMM SUBTASK 52-71-11-020-051, OPERATIONAL CHECK WAS GOOD.Aug 11, 2004 · N631AW · Airbus A320231 · Door Warning SystemSDR AWXA200400945Doubler · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FUSELAGE SKIN AT PORTABLE WATER SERVICING CUTOUT FR 65 TO FR 66, STR 37 LT TO STR 41 LT. MAINTENANCE REMOVED CORRODED REINFORCEMENT DOUBLER; FABRICATED A NEW REPLACEMENT REINFORCEMENT DOUBLER; INSTALLED REPAAug 6, 2004 · N622AW · Airbus A320231 · Fuselage Main, Plate/SkinSDR AWXA200400908Sill · corrodedDURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON R-2 DOOR SILL AT UPPER IB END BETWEEN FR 66 AND FR 68. MAINTENANCE CUTOUT DAMAGED AREAS OF R-2 DOOR SILL AT UPPER IB END, BOTH AT FR 68; FABRICATED A REPAIR DOUBLER AND 2 EACH FILLERS; INSTALLED REPAIR PAAug 5, 2004 · N622AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200400914Dummy Rail · corrodedMAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL Y1203 RT AFT OF FR 15. MAINTENANCE REMOVED CORRODED DUMMY RAIL Y1203 RT AFT OF FR 15; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.Aug 5, 2004 · N622AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200400915Beam · corrodedMAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON LONGITUDINAL BEAM ASSEMBLY Y460 RT AFT OF FR 66. MAINTENANCE REMOVED CORRODED LONGITUDINAL BEAM ASSEMBLY Y460 RT AFT OF FR 66; FABRICATED A NEW REPLACEMENT BEAM ASSEMBLY; INSTALLED REPAIR PARTAug 5, 2004 · N622AW · Airbus A320231 · Fuselage Main, StructureSDR AWXA200400925Floorbeam · corrodedDURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y1292 LT BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED CORRODED BEAM Y1292 LT FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.Aug 5, 2004 · N622AW · Airbus A320231 · Fuselage Main, Floor BeamSDR AWXA200400851Relay · faultyABORTED TAKEOFF AT BEGINNING OF TAKEOFF ENROUTE FOR LAS WHILE MOVING THRUST LEVERS FORWARD RECEIVED ECAM MESSAGE (HYDRAULIC YELLOW SYSTEM LOW PRESSURE; BRAKE ACCUMULATOR PRESSURE MONITOR), REJECTED TAKEOFF AT 50 KTS. MAINTENANCE PREFORMED GROUND SCAN AUTOMATICAug 4, 2004 · N672AW · Airbus A320232 · Hydraulic Accumulator, AuxiliarySDR AWXA200400843Adiru · faultyAIR TURN BACK, ON CLIMB OUT, EN ROUTE FOR YYZ AT APPROXIMATELY 4000 FT THE FO`S PRIMARY FLIGHT DISPLAY (PFD) SPEED TAPE INDICATED OVER SPEED. REDUCED SPEED TO 235 KTS AND WARNING EXTINGUISHED, AUTOPILOT DISCONNECTED, CAPTAINS PFD WAS NORMAL, TURNED BACK AND LAAug 2, 2004 · N801AW · Airbus A319132 · Inertial Guidance SystemSDR AWXA200400840Pitot Head · obstructedON 2ND ATTEMPT OF TAKEOFF EN ROUTE, CAPTS AIRSPEED IND SLOW TO INCREASE & 35 TO 40 KTS BELOW FO`S IND, REJECTED AT 80 KTS. MX R & R NR 1 ADIRU IAW T/C & NR 1 ADM, OPS CHK GOOD. AGAIN REJECTED T/O FOR CAPTS AIRSPEED IND 35 TO 40 KTS BELOW FO`S IND. MX R & R CAJul 30, 2004 · N620AW · Airbus A320231 · Airspeed/Mach IndicatorSDR YENA200441Odor · detectedPASSENGER OBSERVED BURNING RUBBER SMELL IN ROW 19 LT SIDE. ODOR WENT AWAY AFTER FEW MINUTES.COMPLIED WITH INFO NOTICE 2004-T023TR. NO ABNORMALITIES NOTED, COULD NOT CONFIRM THE BURNING SMELL. OK FOR SERVICE.Jul 23, 2004 · N568JB · Airbus A320232 · Air Distribution SystemSDR AWXA200400801Floorbeam · corrodedDURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y254 RT BETWEEN FR 19 AND FR 20. MAINTENANCE CUTOUT DAMAGE ON BEAM Y254 RT FROM FR 19 TO FR 20; FABRICATED FILLERS AND REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A319 SRM 53-00-14, FIG. 204.Jul 14, 2004 · N807AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200400806Beam · corrodedMAJOR REPAIR - DURING B-04 CHECK GALVANIC CORROSION WAS FOUND IN LAVATORY MOUNT HOLE ON BEAM Y765 LT, FORWARD OF FR 66. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y765 LT FROM FR 64 TO FR 66; FABRICATED NEW REPLACEMENT SECTION OF BEAM, INSTALLED REPAIR PARTJul 14, 2004 · N807AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200400807Floorbeam · corrodedMAJOR REPAIR - DURING B-04 CHECK GALVANIC CORROSION WAS FOUND IN NUT PLATE HOLE ON FLOORBEAM Y1292 LT, FORWARD OF FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 68 TO FR 69; FABRICATED NEW REPLACEMENT SECTION OF BEAM, INSTALLED REPAIR PARJul 14, 2004 · N807AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200400808Floorbeam · corrodedMAJOR REPAIR - DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM Y1292 LT, BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 66 TO FR 68; FABRICATED NEW REPLACEMENT SECTION OF BEAM, INSTALLED REPAIR PART IAW A319Jul 14, 2004 · N807AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200400810Shear Plate · corrodedDURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON LT AFT SHEAR PLATE Y1292 RT BETWEEN FR 69 AND FR70. MAINTENANCE REMOVED CORRODED SECTION OF LT AFT SHEAR PLATE FROM FR 69 TO FR 70; FABRICATED NEW REPLACEMENT SECTION OF SHEAR PLATE, INSTALLED REPAIR PART IAW AJul 14, 2004 · N807AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200400826Seat Track · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON LT IB SEAT TRACK AT Y765, FR 47. MAINTENANCE REMOVED CORRODED LT IB SEAT TRACK AT Y765, FROM FR 41 TO FR 47; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 13, 14Jul 11, 2004 · N654AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200400769Shear Plate · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON RT AFT SHEAR PLATE AT AFT END OF BEAM Y1292, BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED CORRODED RT AFT SHEAR PLATE AT AFT END OF BEAM Y1292, FROM FR 69 TO FR 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE;Jul 10, 2004 · N806AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200400770Seat Track · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK BEAM Y765, AT FR 16. MAINTENANCE CUTOUT DAMAGE ON SEAT TRACK BEAM Y765, AT FR 16; FABRICATED A NEW REPLACEMENT SECTION OF BEAM AND 4 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A319 SRM 53-11-1Jul 10, 2004 · N806AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200400771Seat Track · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK BEAM Y765, AT FR 66. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM Y765 FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW SRM 51-72-11, PG. 1-2Jul 10, 2004 · N806AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200400773Floorbeam · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT BETWEEN FR 67 AND FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 67 TO FR 68. FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW SRM 51-72-11, PG. 1-Jul 10, 2004 · N806AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200400774Splice Plate · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER IB SPLICE PLATE (COUPLING) BEAM Y1292 LT AT FR 68. MAINTENANCE REMOVED CORRODED UPPER IB SPLICE PLATE ON BEAM Y1292 LT AT FR 68. FABRICATED A NEW REPLACEMENT SPLICE PLATE; INSTALLED REPAIR PART IAW SJul 10, 2004 · N806AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200400827Skin · delaminatedDURING B-04 CHECK AN AREA OF DELAMINATION WAS FOUND 3 INCHES FROM TOP OF RUDDER ON LT SIDE PANEL. MAINTENANCE CUTOUT DELAMINATED PLIES ON LT UPPER RUDDER AT FIN STA. 569; FABRICATED, AND BONDED CORE AND REPAIR PLIES TO RUDDER IAW A320 SRM 55-41-00, FIG. 217.Jul 10, 2004 · N654AW · Airbus A320232 · Rudder, Plate/SkinSDR AWXA200400764Adiru · failedAIR TURN BACK, ON CLIMB OUT, EN ROUTE, RECEIVED ADR NR 1 FAULT MESSAGE, SWITCHED TO ADR NR 3 AND LOST NAV DISPLAY AND PRIMARY FLIGHT DISPLAY INTERNAL REF INFO, TURNED BACK FOR REPAIR. MAINTENANCE REMOVED AND REPLACED NR 1 AIR DATA INERTIAL REFERENCE UNIT (ADIRJul 10, 2004 · N819AW · Airbus A319132 · Inertial Guidance SystemSDR AWXA200400756Proximity Sensor · defectiveLANDING GEAR, ON FINAL APPROACH, ENROUTE, AT APPROXIMATELY 170 KTS WITH LANDING GEAR HANDLE PLACED IN DOWN POSITION GEAR DOORS APPEARED TO COME OPEN BUT LANDING GEAR DID NOT EXTEND, RECYCLED LANDING GEAR UP THEN DOWN IAW ECAM INSTRUCTIONS AND GEAR CAME DOWN ANJul 8, 2004 · N802AW · Airbus A319132 · Landing Gear Position and WarningSDR AWXA200400744Floor Panel · delaminatedDURING B-04 CHECK FOUND FLOOR PANEL 262BG MISSING AN INSERT WITH DELAMINATION TO BOTTOM OF LAMINATE. MAINTENANCE REPLACED INSERT AND PERFORMED BOND REPAIR TO BOTTOM LAMINATE OF FLOOR PANEL 262BG IAW SRM 53-02-00, FIG. 201.Jun 28, 2004 · N805AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200400732Floorbeam · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 AT FR 68. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 AT FR 68 IAW SRM 51-42-11 FIG. 2, 3, AND 18.Jun 27, 2004 · N805AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200400733Floorbeam · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 AT FR 66. MAINTENANCE REMOVED AND REPLACED BEAM Y765 AT FR 66 IAW A319 SRM 51-72-11 PG. 1 AND 2.Jun 27, 2004 · N805AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200400734Floorbeam · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 FROM FR 67 TO FR 68. MAINTENANCE REMOVED AND REPLACED BEAM Y765 FROM FR 67 TO FR 68 IAW SRM 51-42-11 FIG. 9-12, AND 18.Jun 27, 2004 · N805AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200400742Floorbeam · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT AFT OF FR 66. MAINTENANCE REMOVED BEAM Y1292 RT FROM FR 64 TO FR 66+5 INCH; FABRICATED A NEW REPLACEMENT BEAM; DRILLED SPLICE COUPLING TO FORWARD END OF NEW BEAM; INSTALLED NEW BEAM NR COUPLINGJun 27, 2004 · N805AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200400743Floorbeam · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT AFT OF FR 66 TO FORWARD SIDE OF FR 68. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 LT FROM FR 66 TO FR 68 IAW A319 SRM 51-42-11, FIG. 2, 3, & 18.Jun 27, 2004 · N805AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200400728Floorbeam · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 AT FR 68. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 AT FR 68 IAW A319 SRM 51-42-11 FIGURES 2-18.Jun 26, 2004 · N805AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200400729Floorbeam · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1732 AT FR 66. MAINTENANCE REPAIRED BEAM Y1732 DOOR SILL AT FR 66 IAW A319 SRM 53-41-14 FIG. 201.Jun 26, 2004 · N805AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200400730Floorbeam · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 (2 PLACES) AT FR 64 AND FR 65. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 FROM FR 64 TO FR 65 IAW A319 SRM 51-42-11 FIG. 2, 3, 8, 18.Jun 26, 2004 · N805AW · Airbus A319132 · Fuselage Main, Floor Beam
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