N650AW

Service difficulty reports · 367

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 = 'N650AW' 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 USAA920081053Support · corrodedSAL - MAJOR REPAIR - C7 CHECK - CORROSION ON SUPPORT FRAME, BS 3310 / FR 69 - BS 3366 / FR 70, -Y1732. REPLACED SUPPORT FRAME, BS 3310 / FR 69 - BS 3366 / FR 70, -Y1732 IAW A320 SRM 51-72-11.May 6, 2008 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA920081052Floor Support · corrodedSAL - MAJOR REPAIR - C4 CHECK - CORROSION ON CABIN BEAM, BS 3043 / FR 64 - BS 3158 / FR 66, -Y1292. REPLACED CABIN BEAM, BS 3043 / FR 64 - BS 3158 / FR 66, -Y1292 IAW A320 SRM 51-72-11.May 6, 2008 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA920081051Floor Support · corrodedSAL - MAJOR REPAIR - C4 CHECK - CORROSION ON CABIN BEAM, BS 3101 / FR 65, -Y460. REPLACED CABIN BEAM, BS 3043 / FR 64 - BS 3207 / FR 67, -Y460 IAW A320 SRM 51-72-11.May 6, 2008 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA920081050Floorbeam · corrodedSAL - MAJOR REPAIR - C4 CHECK - CORROSION ON CABIN FLOORBEAM BS 3158 / FR 65, +Y920. REPLACED CABIN BEAM, BS 3101 / FR 65 - BS 3207 / FR 67, +Y920 IAW A320 SRM 51-72-11.May 6, 2008 · N650AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA920081049Shear Web · corrodedSAL - MAJOR REPAIR - C7 CHECK - CORROSION ON LEFT SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / FR 70, +Y1732. REPLACED LEFT SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / FR 70, +Y1732 IAW A320 SRM 51-72-11.May 3, 2008 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA920081048Shear Web · corrodedSAL - MAJOR REPAIR - C7 CHECK - CORROSION ON RIGHT SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / FR 70, -Y1732. REPLACED RIGHT SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / FR 70, -Y1732 IAW SRM 51-72-11.May 3, 2008 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA920081098Structure · crackedSAL - MAJOR REPAIR - C7 CHECK - CRACKED COVER SHEET, BS 2884 / FR 68 - BS 2936 / FR 69, +Y1732. REPLACED COVER SHEET, BS 2884 / FR 68 - BS 2936 / FR 69, +Y1732 IAW A320 SRM 51-72-11.Apr 30, 2008 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA920081097Sill · corrodedSAL - MAJOR REPAIR - C7 CHECK - CORROSION ON L2 DOOR CUTOUT LOWER SILL, BS 2786 / FR 66 - BS 2884 / FR 68, +Y1430. REPAIRED L2 DOOR CUTOUT LOWER SILL, BS 2786 / FR 66 - BS 2884 / FR 68, +Y1430 IAW A320 SRM 53-41-14.Apr 30, 2008 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA920081096Floorbeam · corrodedSAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN BEAM, BS 2786 / FR 66, +Y510. REPAIRED CABIN BEAM, BS 2786 / FR 66, +Y510 IAW A320 SRM 51-72-11.Apr 30, 2008 · N650AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA920081095Sill · corrodedSAL - MAJOR REPAIR - C7 CHECK - CORROSION ON R2 DOOR CUTOUT LOWER SILL, BS 2786 / FR 66, -Y1430. REPAIRED THE R2 DOOR CUT OUT LOWER SILL, BS 2786 / FR 66, -Y1430 IAW USAIRWAYS EA 120744.Apr 30, 2008 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200700045Skin · delaminatedPHX - LEFT WING OUTBOARD FLAP LOWER SURFACE DELAMINATED, WS 8268 - WS 9235. REPAIRED LEFT WING OUTBOARD FLAP LOWER SURFACE, WS 8268 - WS 9235 IAW A320 SRM 57-30-00.Jan 7, 2007 · N650AW · Airbus A320232 · Trailing Edge FlapsSDR AWXA200601880Sill · corrodedSAL - MAJOR REPAIR - BC-6 CHECK - CORROSION ON L2 DOOR CUT OUT LOWER SILL, FS 67 + 16.5", +Y1732. REPAIRED L2 DOOR CUT OUT LOWER SILL, FS 67 + 16.5", +Y1732 IAW A320 SRM 53-41-14 FIGURE 201.Nov 6, 2006 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200601867Sill · corrodedSAL - MAJOR REPAIR - BC-6 CHECK - CORROSION ON R2 DOOR CUT OUT LOWER SILL, FR 67+19", -Y1732. REPAIRED R2 DOOR CUT OUT LOWER SILL, FS 67+19", -Y1732 IAW A320 SRM 53-41-14, FIGURE 201.Nov 6, 2006 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200601895Fitting · corrodedSAL - MAJOR REPAIR - BC-6 CHECK - CORROSION ON L2 DOOR CUT OUT LOWER SILL CENTER FITTING, FS 66 + 4.5" TO FS 67+17". REPLACED L2 DOOR CUT OUT LOWER SILL CENTER FITTING, FS 66 + 4.5" TO FS 67+17" IAW A320 SRM 51-72-11.Nov 4, 2006 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200601879Dummy Rail · corrodedSAL - MAJOR REPAIR - BC-6 CHECK - CORROSION ON MAIN CABIN DUMMY RAIL, FS 68, -Y1162. REPLACED MAIN CABIN DUMMY RAIL, FS 68, -Y1162 IAW A320 SRM 51-72-11 AND 51-21-11.Nov 4, 2006 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200601866Seat Track · corrodedSAL - MAJOR REPAIR - BC-6 CHECK - CORROSION ON MAIN CABIN DUMMY RAIL, FS 66 + 5"- FS 67+15", - Y1292. REPLACED MAIN CABIN DUMMY RAIL, FS 66 + 5"- FS 67+15", - Y1292 IAW A320 SRM 51-72-11.Nov 4, 2006 · N650AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200601865Sill · corrodedSAL - MAJOR REPAIR - BC-6 CHECK, CORROSION ON BULK CARGO DOOR CUTOUT LOWER SILL, FS 61+19", -Y640. REPAIRED BULK CARGO DOOR CUTOUT LOWER SILL, FS 61+19", -Y640, IAW A320 SRM 53-41-49 FIG 203.Nov 4, 2006 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200600696Wire · brokenPHX - EEL - LOG 7329815 - MAINTENANCE REPORTED THAT DURING AN FAA RAMP CHECK FOUND THE EMERGENCY LIGHT ON ROW 7 INOPERATIVE. MAINTENANCE REPAIRED WIRING AT ROW 7ABC EMERGENCY LIGHT ASSEMBLY IAW 20-48-14. OPERATIONAL CHECKS WERE GOOD.Apr 20, 2006 · N650AW · Airbus A320232 · Light System WiringSDR AWXA200600533Actuator · malfunctionedAFTER TAKEOFF CREW REPORTED THAT THE NOSE GEAR WOULD NOT RETRACT. CREW RETURNED TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE CONFIRMED THAT NLG DOOR ACTUATOR WAS BAD FROM STOCK. REMOVED AND REPLACED THE NOSE GEAR DOOR ACTUATOR IAW AIRBUS 320 SRM 32-Mar 23, 2006 · N650AW · Airbus A320232 · Landing Gear Door ActuatorSDR AWXA200600357Oxygen Mask · failedMCI - FLT 15 - DURING FLIGHT, EN ROUTE TO PHX FROM JFK, CREW REPORTED THAT THE CAPTAINS OXYGEN MASK INFLATE TUBE BROKE. CREW DIVERTED TO MCI AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE SWAPPED CAPTAINS O2 MASK WITH SECOND OBSERVERS MASK AND MEL'D THE SECONFeb 18, 2006 · N650AW · Airbus A320232 · Crew Oxygen SystemSDR AWXA200600341Acm · unknownDURING FLIGHT, EN ROUTE TO YVR FROM PHX, THE CREW REPORTED THE NR 1 PACK OVERHEATED IN FLIGHT, WITH THE NR 2 PACK ALREADY BEING ON MEL. CREW DIVERTED TO LAS AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NR 1 ACM SEIZED. REMOVED AND REPLACED THEFeb 16, 2006 · N650AW · Airbus A320232 · Cabin Cooling SystemSDR AWXA200500774Slide · defectiveCAPTAIN OPENED THE L1 DOOR WITH THE DOOR ARMED. SLIDE DID NOT DEPLOY. MAINTENANCE REMOVED AND REPLACED THE L1 DOOR SLIDE IAW AMERICA WEST AIRLINES IAW R1C25305. VENDOR OVERHAULED SLIDE IAW CMM 25-60-56.Jul 3, 2005 · N650AW · Airbus A320232 · Escape SlideSDR AWXA200500772Fmu · failedDURING TAKE OFF AFTER APPLYING POWER, RECEIVED MULTIPLE WARNINGS ALONG WITH NR 1 ENGINE OVERSPEED. ACFT ABORTED TAKEOFF AT APPROX 80 KNOTS. TAXIED BACK TO GATE WITHOUT FURTHER INCIDENT. MX TROUBLESHOT IAW MFG MANUAL. R & R NR 1 FMU IAW TASK CARD R5M73308. Jul 3, 2005 · N650AW · Airbus A320232 · Fuel Controlling SystemSDR AWXA200500093Epsu · faultyLAS - EEL - DURING 8-DAY CHECK FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM, RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL) FAULTED. MAINTENANCE REMOVED AND REPLACED RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD.Jan 29, 2005 · N650AW · Airbus A320232 · Emergency LightingSDR AWXA200401226Fuel Control · failedDURING TAXI, FLAMES REPORTED AT APU BY ANOTHER ACRFT, FIRE CHIEF CONFIRMED SMALL FLAME IN TAILPIPE, DISCHARGED APU FIRE BOTTLE PER FIRE CHIEFS RECOMMENDATION. NO INDICATIONS NOTED IN COCKPIT, APU HAD BEEN SHUTDOWN LESS THAN TWO MINUTES FOLLOWING NR 2 ENG STARTNov 2, 2004 · N650AW · Airbus A320232 · APU Engine Fuel and ControlSDR AWXA200400942Wire · brokenDURING P-05 CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 7 LT INOPERATIVE. MAINTENANCE FOUND A GROUND WIRE AT LIGHT ASSEMBLY CONNECTOR SEAT ROW 7 LT BROKEN, RE-TERMINATED GROUND WIRE, EMERGENCY LIGHT OPERATIONAL CHECK WAS GOOD.Aug 16, 2004 · N650AW · Airbus A320232 · Light System WiringSDR AWXA200400653Wire · brokenPHX - EEL - DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE FOR THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT, OPERATIONAL CHECK WAS GOOD.Jun 15, 2004 · N650AW · Airbus A320232 · Light System WiringSDR AWXA200400020Stowage Box · stickingMCI - DIVERSION - FLT 0688 - EN ROUTE, 2 HOURS AND 20 MINUTES INTO FLIGHT, CREW OXYGEN PRESSURE INDICATED 20 PSI, DIVERTED. MAINTENANCE FOUND FIRST OFFICERS MASK TEST BUTTON STUCK KEEPING VALVE PARTIALLY OPEN, AFTER TAPPING ON BUTTON THE VALVE RESET, OPERATIOJan 6, 2004 · N650AW · Airbus A320232 · Crew Oxygen SystemSDR AWXA200301533Power Supply · faultyLT OVERWING EMERGENCY POWER SUPPLY UNIT INDICATES INTERNAL FAULT. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL) IAW AMM 33-51-38-401, OPERATIONAL CHECK WAS GOOD.Dec 12, 2003 · N650AW · Airbus A320232 · Emergency LightingSDR AWXA200301174Floor Panel · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOOR PANEL 151LF. MAINTENANCE REMOVED DAMAGED FLOOR PANEL; FABRICATED A NEW REPLACEMENT PANEL IAW A320 SRM 53-02-00 PG 231-234.Oct 6, 2003 · N650AW · Airbus A320232 · Fuselage Floor PanelSDR AWXA200301171Floor Panel · corrodedMCN - MINOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOOR PANEL 151AF. MAINTENANCE REMOVED DAMAGED FLOOR PANEL; FABRICATED A NEW REPLACEMENT PANEL IAW A320 SRM 53-02-00, PG 231-234.Oct 6, 2003 · N650AW · Airbus A320232 · Fuselage Floor PanelSDR AWXA200301172Skin Panel · corrodedDURING C-04 CHECK PITTING CORROSION WAS FOUND ON THE NR 2 PYLON AFT FIXED FAIRING OUTBOARD SKIN. MAINTENANCE REMOVED NR 2 PYLON AFT FIXED FAIRING OUTBOARD SKIN; FABRICATED A NEW REPLACEMENT SKIN; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 7-12, & 21-22, FOct 5, 2003 · N650AW · Airbus A320232 · Nacelle/Pylon, Plate/SkinSDR AWXA200301176Container · faultyDURING C-04 CHECK THE R-2 DOOR EMERGENCY OXYGEN DOOR FAILED TO DEPLOY ON MASK DROP TEST. MAINTENANCE REMOVED AND REPLACED THE R-2 DOOR EMERGENCY OXYGEN CONTAINER IAW AMM 35-21-41-020-051, AND 35-21-41-420-051, OPS CHECKED GOOD IAW AMM 35-23-00-710-050-A.Oct 4, 2003 · N650AW · Airbus A320232 · Crew Oxygen SystemSDR AWXA200301175Skin Panel · corrodedDURING C-04 CHECK PITTING CORROSION WAS FOUND ON THE NR 2 PYLON AFT FIXED FAIRING INBOARD SKIN. MAINTENANCE REMOVED NR 2 PYLON AFT FIXED FAIRING INBOARD SKIN; FABRICATED A NEW REPLACEMENT SKIN; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 7-11, FIG 2, 3.Sep 25, 2003 · N650AW · Airbus A320232 · Nacelle/Pylon, Plate/SkinSDR AWXA200301173Floor Panel · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOOR PANEL 151DF. MAINTENANCE REMOVED DAMAGED FLOOR PANEL; FABRICATED A NEW REPLACEMENT PANEL IAW A320 SRM 53-02-00, PG 231-236, FIG 209.Sep 25, 2003 · N650AW · Airbus A320232 · Fuselage Floor PanelSDR AWXA200301167Angle · crackedDURING C-04 CHECK A .5 INCH CRACK WAS FOUND ON WING TO BODY FAIRING VERTICAL ATTACH ANGLE, AFT OF FR 34 LT, BELOW LOWER FASTENER HOLE. MAINTENANCE REMOVED AND REPLACED VERTICAL ATTACH ANGLE AT FR 34 LT IAW A320 SRM 51-42-11 PG 21-22, FIG 8.Sep 25, 2003 · N650AW · Airbus A320232 · Aerodynamic FairingsSDR AWXA200301216Profile · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT LT PROFILE BETWEEN FR 57 AND FR 58. MAINTENANCE REMOVED DAMAGED LT PROFILE BETWEEN FR 56 AND FR 58; INSTALLED NEW REPLACEMENT PROFILE IAW A320 SRM 51-42-11, PG. 21-22, FIG. 8, PG. 8-10, FIG. 2, ANDSep 24, 2003 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200301215Profile · crackedDURING C-04 CHECK A 1 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT LT PROFILE AT FR 57. MAINTENANCE REMOVED DAMAGED LT PROFILE BETWEEN FR 56 AND FR 57; INSTALLED NEW REPLACEMENT PROFILE IAW A320 SRM 51-42-11, PG. 21-22, FIG. 8, PG. 8-10, FIG. 2, AND PG. 12,Sep 24, 2003 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200301214Profile · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT RT PROFILE BETWEEN FR 51 AND FR 52. MAINTENANCE REMOVED DAMAGED AREA ON RT PROFILE BETWEEN FR 51 AND FR 52; FABRICATED A REPAIR SPLICE AND DOUBLER; INSTALLED REPAIR PARTS IAW AWA E.R. 26-5320-03154Sep 24, 2003 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200301205Profile · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT CENTER PROFILE FR 31, AT FASTENER HOLES. MAINTENANCE REMOVED AND REPLACED CENTER PROFILE AT FR 31 IAW A320 SRM 51-42-11, PG. 21 AND 22, FIG. 8, AND PG. 7-10, AND 12, FIG. 2 & 3.Sep 24, 2003 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200301204Profile · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON FWD CARGO COMPARTMENT RT PROFILE BETWEEN FR 28 AND FR 31, AT FASTENER HOLES. MAINTENANCE CUTOUT CORROSION ON RT PROFILE BETWEEN FR 28 AND FR 31; FABRICATED A PROFILE REPAIR SECTION AND SPLICE DOUBLERS; INSTALLED REPAIR Sep 24, 2003 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200301203Profile · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON FWD CARGO COMPARTMENT RT PROFILE BETWEEN FR 31 & FR 34, AT FASTENER HOLES. MAINTENANCE CUTOUT CORROSION ON RT PROFILE BETWEEN FR 31 AND FR 34; FABRICATED A PROFILE REPAIR SECTION AND SPLICE DOUBLERS; INSTALLED REPAIR PASep 24, 2003 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200301202Profile · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON FWD CARGO COMPARTMENT LT PROFILE BETWEEN FR 31 AND FR 34, AT FASTENER HOLES. MAINTENANCE REMOVED DAMAGED L/H PROFILE BETWEEN FR 31 AND FR 34; FABRICATED A NEW REPLACEMENT PROFILE; INSTALLED REPAIR PART IAW AWA E.R. 26-5Sep 24, 2003 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200301201Profile · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT RT PROFILE AT FR 49. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED SECTION OF RT PROFILE AT FR 49; FABRICATED PROFILE REPAIR SECTION AND REPAIR DOUBLERSSep 24, 2003 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200301200Profile · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT LT PROFILE BETWEEN FR 48 AND FR 49. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED SECTION OF LT PROFILE BETWEEN FR 48 AND FR 49; FABRICATED PROFILE REPSep 24, 2003 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200301170Plate · crackedMCN - MINOR REPAIR - DURING C-04 CHECK A .375 INCH CRACK WAS FOUND ON LT WING TO BODY FAIRING SUPPORT STRUCTURE CLOSING PLATE AT FR 34. MAINTENANCE REMOVED CLOSING PLATE AT FR 34, AND U-CHANNEL ABOVE CLOSING PLATE; FABRICATED A NEW REPLACEMENT CLOSING PLATE ASep 24, 2003 · N650AW · Airbus A320232 · Aerodynamic FairingsSDR AWXA200301169Seat Track · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON PASSENGER SEAT RAIL AT Y765 AT FR 66. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SEAT RAIL Y765 AT FR 66; FABRICATED A NEW REPLACEMENT SEAT RAIL; INSSep 24, 2003 · N650AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200301165Plate · crackedDURING C-04 CHECK A .25 INCH CRACK WAS FOUND ON RT WING TO BODY FAIRING SUPPORT STRUCTURE CLOSING PLATE AT FR 34. MAINTENANCE REMOVED CLOSING PLATE AT FR 34; FABRICATED A NEW REPLACEMENT CLOSING PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 7, SECT 6,Sep 24, 2003 · N650AW · Airbus A320232 · Aerodynamic FairingsSDR AWXA200301163Floorbeam · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON Y1292 FLOORBEAM AT FR 66. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF Y1292 FLOORBEAM FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT FLOORBEAM; ISep 24, 2003 · N650AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200301162Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON Y1292 FLOORBEAM BETWEEN FORWARD SIDE OF FR 67 TO FR 68. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF Y1292 FLOORBEAM FROM FR 67 Sep 24, 2003 · N650AW · Airbus A320232 · Fuselage Main, Floor Beam
Back to N650AW