N802AW

Service difficulty reports · 325

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
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 n_number = 'N802AW' AND registry_match = 'registration'
  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 USAA920080769Shear Plate · corrodedSAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / 70, +Y1732. REPLACED CABIN SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / 70, +Y1732 IAW A319 SRM 51-72-11.Mar 24, 2008 · N802AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA920080768Shear Plate · corrodedSAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / 70, -Y1732. REPLACED CABIN SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / 70, -Y1732 IAW A319 SRM 51-72-11.Mar 24, 2008 · N802AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA920080767Floorbeam · corrodedSAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3043 / FR 64 - BS 3101 / 65, -Y1292. REPLACED CABIN FLOORBEAM, BS 3043 / FR 64 - BS 3101 / 65, -Y1292 IAW A319 SRM 51-72-11.Mar 24, 2008 · N802AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA920080766Floorbeam · corrodedSAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3043 / FR. 64 - BS 3101 / 65, -Y765. REPLACED CABIN FLOORBEAM, BS 3043 / FR 64 - BS 3101 / 65, -Y765 IAW A319 SRM 51-72-11.Mar 24, 2008 · N802AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA920080765Floorbeam · corrodedSAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3158 / FR 66 - BS 3257 / 68, +Y1292. REPLACED CABIN SHEAR PLATE, BS 3158 / FR 66 - BS 3257 / 68, +Y1292 IAW A319 SRM 51-72-11. Mar 24, 2008 · N802AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA920080764Floorbeam · corrodedSAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3257 / FR 68 - BS 3310 / 69, +Y1292. REPLACED CABIN SHEAR PLATE, BS 3257 / FR 68 - BS 3310 / 69, +Y1292 IAW A319 SRM 51-72-11.Mar 24, 2008 · N802AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA920080763Shear Plate · crackedSAL - MAJOR REPAIR - C7 CHECK - CRACK ON CABIN SHEAR PLATE, BS 3257 / FR 68 - BS 3310 / 69, +Y1732. REPLACED CABIN SHEAR PLATE, BS 3257 / FR 68 - BS 3310 / 69, +Y1732 IAW A319 SRM 51-72-11.Mar 24, 2008 · N802AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA920080723Hinge Fitting · wornSAL - MAJOR REPAIR - C7 CHECK - RUDDER HINGE FITTING NR 2 HAS PLAY, VERTICAL STABILIZER STATION 1926 / RIB 4. REPLACED RUDDER HINGE FITTING NR 2, VERTICAL STABILIZER STATION 1926 / RIB 4 IAW A319 AMM 55-36-00.Mar 23, 2008 · N802AW · Airbus A319132 · Rudder StructureSDR SA07079Battery · failedPHX - DURING THE EMERGENCY LIGHTS TEST, THE FORWARD LEFT EMERGENCY LIGHT BATTERY FAILED. MAINTENANCE REPLACED THE FORWARD LEFT EMERGENCY LIGHT BATTERY. OPERATIONALLY TEST OK.Dec 5, 2007 · N802AW · Airbus A319132 · Emergency LightingSDR SA07077Battery Pack · dischargedATL - THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE IN THE FORWARD CABIN. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY LIGHTS. OPERATIONALLY CHECKS OK.Nov 20, 2007 · N802AW · Airbus A319132 · Emergency LightingSDR SA07075Battery Pack · dischargedMAINTENANCE FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK.Nov 20, 2007 · N802AW · Airbus A319132 · Emergency LightingSDR AWXA200700580Wire · brokenPHX - EEL - EMERGENCY ESCAPE PATH AISLE LIGHT AT SEAT ROW 12 HAS A BROKEN WIRE. REPAIRED AND OPERATIONAL CHECKED EMERGENCY ESCAPE PATH AISLE LIGHT AT SEAT ROW 12 IAW AIRBUS ESPM 20-48-14 AND A319 AMM 33-50-00.May 9, 2007 · N802AW · Airbus A319132 · Light System WiringSDR AWXA200700353Transducer · failedLAS - DIVR - DURING APPROACH, THE CREW DISCOVERED THE RIGHT BRAKE PRESSURE INDICATED 500 PSI - 3000 PSI. THE CREW DIVERTED TO LAX, DECLARED AN EMERGENCY. THE PAX DID NOT BRACE. THE LANDING WAS UNEVENTFUL. MX REPLACED 62GG ALTERNATE BRAKE TRANSDUCER IAW AMMMar 11, 2007 · N802AW · Airbus A319132 · Landing Gear Brake SystemSDR AWXA200700117Power Supply · failedLAX - EEL - EMERG EXIT LIGHTING REMAINS ON WITH SWITCH IN ARMED POSITION. MX REMOVED AND REPLACED AFT CABIN POWER SUPPLY PER AMM 33-51-38PB401, OPS CHECK WAS OK.Jan 23, 2007 · N802AW · Airbus A319132 · Emergency LightingSDR AWXA200700096Battery Pack · failedPHX - EEL - AFT EMERGENCY LIGHTS FAIL TEST. REMOVED AND REPLACED BATTERY FOR EMERGENCY LIGHT POWER SUPPLY 13WL. OPS CHECK GOOD IAW AMM 33-51-38.Jan 13, 2007 · N802AW · Airbus A319132 · Emergency LightingSDR AWXA200601758Sill · corrodedCORROSION ON R2 DOOR CUT OUT LOWER SILL, FS 68 -2.5 INCHES, -Y1732. REPAIRED DOOR CUT OUT LOWER SILL, FS 68 - 2.5 INCHES - FS 68 - 5 INCHES, -Y1732 IAW A319 SRM 53-41-14 FIG 201 SHEET 3.Oct 16, 2006 · N802AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601757Sill · corrodedCORROSION ON L2 DOOR CUT OUT LOWER SILL, FS 68-5 INCHES, +Y1732. REPAIRED L2 DOOR CUT OUT LOWER SILL, FS 68-5 INCHES, +Y1732 BETWEEN FS 68-7 INCHES TO FS 68-1 INCH IAW A319 SRM 53-41-14 FIG 201.Oct 16, 2006 · N802AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601756Fitting · corrodedSAL - MAJOR REPAIR - CORROSION ON L2 DOOR CUT OUT LOWER SILL CENTER FITTING, FS 67+11", S23L. REPLACED L2 DOOR CUT OUT LOWER SILL CENTER FITTING, BETWEEN FS 66+4" TO FS 68-5", S23L IAW A319 SRM 51-72-11.Oct 7, 2006 · N802AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601755Floorbeam · corrodedSAL - MAJOR REPAIR - CORROSION ON MAIN CABIN FLOORBEAM, FR20, -Y765. REPAIRED MAIN CABIN FLOORBEAM, FS 18+ 6" TO FS 19 - 5", -Y765 IAW A319 SRM 53-11-15, FIG 202.Oct 4, 2006 · N802AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200601754Floorbeam · corrodedSAL - MAJOR REPAIR - CORROSION ON MAIN CABIN FLOORBEAM, FS 20, -Y1292. REPAIRED MAIN CABIN FLOORBEAM, FS 18+10" TO FS 24, -Y1292 IAW A319 SRM 53-11-15, FIG 202.Oct 3, 2006 · N802AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200601753Sill · corrodedSAL - MAJOR REPAIR - CORROSION ON AFT CARGO COMPARTMENT DOOR CUTOUT SILL PLATE, FS 58, -Y645. REPLACED AFT CARGO COMPARTMENT DOOR CUTOUT SILL PLATE, FS 58, -Y645 IAW A319 SRM 51-72-11 AND 51-42-11, FIG 5.Oct 3, 2006 · N802AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601752Sill · corrodedSAL - MAJOR REPAIR - CORROSION ON AFT CARGO COMPARTMENT DOOR CUTOUT SILL PLATE, FS 56+19.5", -Y665. REPLACED AFT CARGO COMPARTMENT DOOR CUTOUT SILL PLATE, FS 56+19.5", -Y665 IAW A319 SRM 51-72-11 AND 51-42-11, FIG 5.Oct 3, 2006 · N802AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601751Sill · corrodedSAL - MAJOR REPAIR - CORROSION ON AFT CARGO COMPARTMENT DOOR CUTOUT SILL PLATE, FS 56+9.5", -Y665. REPLACED AFT CARGO COMPARTMENT DOOR CUTOUT SILL PLATE, FS 56+9.5", -Y665 IAW A319 SRM 51-72-11 AND 51-42-11, FIG 5.Oct 3, 2006 · N802AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601750Sill · corrodedSAL - MAJOR REEPAIR - CORROSION ON AFT CARGO COMPARTMENT DOOR CUT OUT SILL PLATE, FS 56, -Y665. REPLACED AFT CARGO COMPARTMENT DOOR CUT OUT SILL PLATE, FS 56, -Y665 IAW A319 51-72-11 PAGE 1 AND 2 AND SRM A319 51-42-11 PAGE 24 TO 48.Oct 3, 2006 · N802AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601749Threshold · corrodedSAL - MAJOR REPAIR - CORROSION ON AFT CARGO COMPARTMENT DOOR CUTOUT THRESHOLD SHEET, FS 55A TO FS 59, -Y565 TO -Y685. REPLACED AFT CARGO COMPARTMENT DOOR CUTOUT THRESHOLD SHEET, FS 55A TO FS 59, -Y565 TO -Y 685 IAW A319 SRM 51-72-11.Oct 3, 2006 · N802AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601675Battery Pack · no testLAX - EEL - DURING ROUTINE MAINTENANCE, THE LEFT FWD EPSU BATTERY FAILED BITE. MAINTENANCE REPLACED THE BATTERY IAW AMM 33-51-38-000. OP CHECKS WERE GOOD.Sep 28, 2006 · N802AW · Airbus A319132 · Emergency LightingSDR AWXA200601540Flap · delaminatedPHX - LEFT WING O/B T/E FLAP DELAMINATED 6 IN AREA LOCATED JUST O/B OF R/B NR 5 OF FLAP. REPAIRED LEFT WING O/B T/E FLAP 6 IN AREA LOCATED JUST O/B OF R/B NR 5 OF FLAP IAW ER NR 25-5753-06150-RA1308A.May 31, 2006 · N802AW · Airbus A319132 · Trailing Edge FlapsSDR AWXA200600354None · noneLAS - FLIGHT CONTROL - CREW REPORTED THE SLATS OVERSPEED ON DEPARTURE, APPROXIMATELY 5 KTS FOR 5 SECS WITH SLATS IN MOTION FROM 1 TO ZERO POSITION. MAINTENANCE INSPECTED THE SLATS IAW AIRBUS 319 MM 05-51-13. NO DEFECTS WERE NOTED AND NO FURTHER ACTION WAS REFeb 20, 2006 · N802AW · Airbus A319132 · Standard Practices/StructuresSDR AWXA200600231Terminal · inoperativePHX - EEL - DURING INSPECTION DISCOVERED EMERGENCY LIGHT INOPERATIVE AT SEAT 12ABC. MAINTENANCE REPLACED BOTH TERMINALS AT SEAT 12ABC LIGHT. OPERATIONAL CHECKS WERE GOOD.Feb 7, 2006 · N802AW · Airbus A319132 · Light System WiringSDR AWXA200500836Eec · malfunctionedNR 1 ENG STALLED. CREW RETURNED TO LAS WITHOUT INCIDENT. ENG BORESCOPED & FERRIED BACK TO PHX. MX R & R NR 1 ENG 7TH STAGE BLEED VALVE, 7A & 7C BLEED VALVE, & 7C BLEED VALVE SOLENOID. LUBED VSV ON NR 1 ENG & R & R NR 1 EEC. PERFORMED POWER RUNS IAW TASK CJul 19, 2005 · N802AW · Airbus A319132 · Engine (Turbine/Turboprop)SDR AWXA200500540Battery Pack · dischargedJFK - EEL - DURING 8-DAY CHECK THE LT OVERWING EMERGENCY LIGHT POWER SUPPLY BATTERY FAILED DURING EMERGENCY LIGHT TEST. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOODMay 9, 2005 · N802AW · Airbus A319132 · Emergency LightingSDR AWXA200500245Epsu · inoperativeLAS - EEL - DURING 4-DAY CHECK FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM, THE FORWARD LT EMERGENCY POWER SUPPLY UNIT HAD AN INTERNAL FAULT. MAINTENANCE REMOVED AND REPLACED LT EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD.Feb 22, 2005 · N802AW · Airbus A319132 · Emergency LightingSDR AWXA200401081Epsu · failedDURING 4-DAY CHECK RT OVER WING EMERGENCY POWER SUPPLY UNIT (EPSU) AND AFT ESPU FAILED EMERGENCY TEST. MAINTENANCE REMOVED AND REPLACED RT OVER WING EPSU (12WL) AND AFT EPSU (13WL) AND BATTERY PACKS; OPERATIONAL CHECK WAS GOOD. PART NAME; EPSU, MFG; DIEHL GSep 30, 2004 · N802AW · Airbus A319132 · Emergency LightingSDR 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 AWXA200400583Proximity Sensor · faultyEMERGENCY LANDING - FLT 0280 - ON APPROACH, EN ROUTE WITH LANDING GEAR SELECTED DOWN GEAR DID NOT EXTEND, MANUALLY SELECTED GEAR DOWN AND DECLARED EMERGENCY. MAINTENANCE PERFORMED WIRING CHECK AND FOUND RESISTANCE ON LT MAIN LANDING GEAR (MLG) DOOR OPEN PROXIMay 28, 2004 · N802AW · Airbus A319132 · Landing Gear Position and WarningSDR AWXA200400503Epsu · dischargedPHX - EEL - DURING OPERATIONAL TEST OF EMERGENCY LIGHTS RECEIVED FAILURE INDICATION, EPSU INT LOAD FWD L. MAINTENANCE REMOVED AND REPLACED LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD.May 11, 2004 · N802AW · Airbus A319132 · Emergency LightingSDR AWXA200400436Power Supply · faultyPHX - EEL - DURING 8-DAY CHECK WHILE PERFORMING PUSH BUTTON TEST OF EMERGENCY LIGHT SYSTEM RECEIVED MESSAGE "EPSU UNIT FWD L". MAINTENANCE REMOVED AND REPLACED L/H FORWARD EMERGENCY POWER SUPPLY UNIT 10WL, OPERATIONAL CHECK WAS GOOD.Apr 27, 2004 · N802AW · Airbus A319132 · Emergency LightingSDR AWXA200400035Wire · arcedON CLIMBOUT, ECAM INDICATED RT WINDOW HEAT ACCOMPANIED BY ARCING COMING FROM THE FIRST OFFICERS RT SLIDING WINDOW AREA, TURNED BACK TO RDU AND LANDED WITHOUT FURTHER INCIDENT. MAINT FOUND RT SLIDING WINDOW ELECTRICAL CORD SHORTED TO GROUND WHERE CORD COMES OUJan 11, 2004 · N802AW · Airbus A319132 · Ice/Rain Protection System WiringSDR AWXA200301588Slide · misalignedWHILE CATERING WAS OPENING THE L-2 DOOR THE EMERGENCY ESCAPE SLIDE UNRAVELED ON GALLEY FLOOR AND CATERING TRUCK RAMP, DOOR WAS NOT OPENED ALL THE WAY AND SLIDE NEVER DEPLOYED. MAINTENANCE WAS CALLED OUT AND FOUND THE GIRT BAR NEVER DETACHED FROM THE AIRCRAFT EDec 22, 2003 · N802AW · Airbus A319132 · Escape SlideSDR AWXA200301321Battery · dischargedFLIGHT CREW REPORTED 2 EACH AFT EMERGENCY FLASHLIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERIES IN 2 EACH AFT FLASHLIGHTS, OPERATIONAL CHECK WAS GOOD.Oct 26, 2003 · N802AW · Airbus A319132 · Emergency EquipmentSDR AWXA200300938Attach Angle · crackedDURING C-04 CHECK A 1 INCH CRACK WAS FOUND ON ATTACH ANGLE UNDER PANEL 191 AT AT BS 1483. MAINTENANCE REMOVED CRACKED ATTACH ANGLE UNDER PANEL 191AT AT BS 1483; FABRICATED A NEW REPLACEMENT ATTACH ANGLE; INSTALLED REPAIR PART IAW A319 SRM 51-24-00, PG. 3, FIG.Aug 8, 2003 · N802AW · Airbus A319132 · Fuselage Main, Attach FittingsSDR AWXA200300960Floor Panel · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON AFT SIDE OF AFT CABIN FLOOR PANEL 262FF. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED AND REPLACED AFT CABIN FLOOR PANEL 262FF IAW A319 SRM 53-02-00, PG. 108, FIG. 104.Aug 7, 2003 · N802AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200300942Floor Panel · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON AFT SIDE OF AFT CABIN FLOOR PANEL 261FF. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED AND REPLACED FLOOR PANEL 261FF IAW A319 SRM 53-02-00, PG. 108, FIG. 104.Aug 7, 2003 · N802AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200300957Angle · crackedDURING C-04 CHECK A 1/4 INCH CRACK WAS FOUND ON RT PYLON PANEL ATTACH ANGLE AT RIB 08, OUTBOARD SIDE. MAINTENANCE CUTOUT DAMAGED AREA OF ATTACH ANGLE AT RIB 08; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW A319 SRM 51-42-11, PG. 6 & 7.Aug 6, 2003 · N802AW · Airbus A319132 · Nacelle/Pylon Miscellaneous StructureSDR AWXA200300966Floorbeam · corrodedDURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF Y1162 FLOORBEAM FORWARD OF FR 68. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS, REMOVED CORRODED Y1162 FLOORBEAM FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT FAug 5, 2003 · N802AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200300962Sill · corrodedDURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF LOWER R-2 DOORWAY SHAPE SILL BS 2280, STR 23 RT. MAINTENANCE REMOVED CORRODED SHAPE SILL AT BS 2280, STR 23 RT; FABRICATED A REPLACEMENT SHAPE SILL; INSTALLED REPAIR PART IAW A319 SRM 51-42-11,Aug 5, 2003 · N802AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200300961Floorbeam · corrodedDURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON PANEL MOUNTING HOLE OF FLOORBEAM Y1792, AFT OF FR 66, INBOARD OF L-2 DOOR FORWARD GIRT BAR MOUNTING BLOCK. MAINTENANCE ENLARGED MOUNTING HOLE TO MAXIMUM ALLOWABLE DIAMETER, CORROSION STILL PRESENT; CUTOUT DAMAGAug 5, 2003 · N802AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200300959Floorbeam · corrodedDURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF Y1162 FLOORBEAM AT FR 68. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF Y1162 FLOORBEAM FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENTAug 5, 2003 · N802AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200300956Cargo Track · corrodedDURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF Y503 DUMMY RAIL BETWEEN FR 14 AND FR 16. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED Y503 DUMMY RAIL BETWEEN FR 14 AND FR 16; FABRICATED A NEW REPLACEMENTAug 5, 2003 · N802AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200300952Floorbeam · corrodedDURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y765 AT FR 16. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF FLOORBEAM Y765 AT FR 16; FABRICATED A NEW SECTION OF BEAM AND Aug 5, 2003 · N802AW · Airbus A319132 · Fuselage Main, Floor Beam
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