N647AW

Service difficulty reports · 393

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 = 'N647AW' 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 USAA920070969Cover · crackedSAL - MAJOR REPAIR - C-07 CHECK - CRACKED CABIN COVER SHEET, BS 3257 / FR 68 - BS 3310 / FR 69, +Y1732. REPLACED CABIN COVER SHEET, BS 3257 / FR 68 - BS 3310 / FR 69, +Y1732 IAW A320 SRM 51-72-11.Oct 14, 2007 · N647AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA920070967Sill · corrodedSAL - MAJOR REPAIR - C-07 CHECK - CORROSION ON THE R2 DOOR CUTOUT LOWER SILL PREVIOUSLY REPAIRED AREA, BS 3101 / FR 65, -Y1732. REPAIRED THE R2 DOOR CUTOUT LOWER SILL, BS 3101 / FR 65, -Y1732 IAW A320 SRM 53-41-14.Oct 13, 2007 · N647AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200602102Power Supply · failedLAS - EEL - CABIN PASSENGER LEFT EMERGENCY EXIT EPSU INOPERATIVE. MX REMOVED AND REPLACED CABIN PASSENGER AFT EMERGENCY EXIT EPSU PER AMM 33-51-38. OPS CHECK WAS GOOD.Dec 19, 2006 · N647AW · Airbus A320232 · Emergency LightingSDR AWXA200601620Valve · faultyON APPROACH, THE CREW MADE 3 ATTEMPTS TO EXTEND THE GEAR WITH NO SUCCESS. IAW THE QRH, THE CREW PERFORMED A MANUAL GEAR EXTENSION. EXTENSION WAS SUCCESSFUL. AS A PRECAUTIONARY MEASURE, THE CREW PERFORMED A TOWER FLYBY. THE TOWER VERIFIED THAT THE GEAR WAS DOWNSep 13, 2006 · N647AW · Airbus A320232 · Landing Gear Retraction/Extension SystemSDR AWXA200601567Wire · damagedPHX - ATB - FLT 675 - DURING CLIMB, THE CREW RECEIVED A NR 2 ENGINE FIRE WARNING. ENGINE INDICATIONS WERE NORMAL. THE CREW WAS AWARE OF THE HISTORY FOR THIS INDICATION AND DID NOT INITIATE AN IFSD. CREW RETURNED TO PHX. CRITICAL ALERT - 9505723 WAS INITIATAug 27, 2006 · N647AW · Airbus A320232 · Fire Protection System WiringSDR AWXA200601558Fire Detector · intermittentDURING INITIAL CLIMB, THE CREW RECEIVED A NR 2 ENGINE FIRE WARNING. ENGINE INDICATIONS WERE NORMAL. THE CREW INITIATED AN IN-FLIGHT SHUTDOWN OF THE NR 2 ENGINE IAW THE QRH. THE CREW DECLARED AN EMERGENCY AND RETURNED TO LAS. THE PASSENGERS DID NOT BRACE. MAug 27, 2006 · N647AW · Airbus A320232 · Fire DetectionSDR AWXA200600690Fitting · corrodedMCN - DURING C6 CHECK DISCOVERED CORROSION, LEVEL 2 EXFOLIATION, ON FORWARD CARGO COMPARTMENT SILL AFT CORNER FITTING AT FS 28, STR 38R. MAINTENANCE REMOVED CORROSION ON DOOR SILL FITTING AT FR 28, STR 38R IAW AIRBUS 320 SRM 51-74-00. NO ALLOWABLE LIMITS WERApr 13, 2006 · N647AW · Airbus A320232 · Fuselage Main, Attach FittingsSDR AWXA200600691Floor Panel · delaminatedMCN - DURING C6 CHECK DISCOVERED AFT PIT FLOOR PANEL NR 161 AF AFT SIDE DELAMINATED FROM FS 59 TO FS 63. MAINTENANCE REMOVED AND INSTALLED FABRICATED AFT PIT FLOOR PANEL NR 161 AF FROM FS 59 TO FS 63 IAW AIRBUS 320 SRM 53-02-00 PARA G AND MCG IRM 9701 REV F.Apr 12, 2006 · N647AW · Airbus A320232 · Fuselage Floor PanelSDR AWXA200600688Floor Panel · delaminatedMCN - DURING C6 CHECK DISCOVERED FORWARD PIT FLOOR PANEL NR 131 HF AFT SIDE DELAMINATED. MAINTENANCE REMOVED AND INSTALLED FABRICATED REPLACEMENT FORWARD PIT FLOOR PANEL NR 131 HF IAW AIRBUS 320 SRM 53-02-00 FIG 209 AND MCG IRM 9701 REV F.Apr 12, 2006 · N647AW · Airbus A320232 · Fuselage Floor PanelSDR AWXA200501441Connector · unknownATL - EEL - DURING TURN, FOUND EMERGENCY LIGHT INOPERATIVE AT SEAT 15 LEFT. MAINTENANCE FOUND SEAT 15ABC CONNECTOR FROM WALL TO SEAT NOT WORKING PROPERLY. MAINTENANCE REMOVED AND REPLACED CONNECTOR AT ROW 15ABC. OPERATIONAL TESTS WERE GOOD.Nov 25, 2005 · N647AW · Airbus A320232 · Light System WiringSDR AWXA200500379Power Supply · faultyPHX - EEL - DURING P-06 CHECK FOUND THE RIGHT OVERWING EMERGENCY POWER SUPPLY UNIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED RIGHT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD.Mar 31, 2005 · N647AW · Airbus A320232 · Emergency LightingSDR AWXA200500360Cable · brokenLAX - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 21 LT, OPERATIONAL CHECK WAS GOOD.Mar 24, 2005 · N647AW · Airbus A320232 · Light System WiringSDR AWXA200500276Floor Panel · delaminatedMCN - MAJOR REPAIR - DURING 8-DAY CHEC, FOUND AFT GALLEY FLOOR PANEL 261QF DELAMINATED. MAINTENANCE REMOVED DELAMINATED AFT GALLEY FLOOR PANEL 261QF, FABRICATED AND INSTALLED NEW REPLACEMENT FLOOR PANEL IAW DWG D53671754.Feb 17, 2005 · N647AW · Airbus A320232 · Fuselage Floor PanelSDR AWXA200500274Floorbeam · corrodedMCN - MAJOR REPAIR - DURING 8-DAY CHECK, CORROSION WAS FOUND ON FLOORBEAM Y29 AT FS 68. MAINTENANCE REMOVED CORRODED FLOORBEAM Y29 AT FS 68; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11.Feb 17, 2005 · N647AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200500273Plate · corrodedMCN - MAJOR REPAIR - DURING 8-DAY CHECK, CORROSION WAS FOUND ON SHEAR PLATE Y50 BETWEEN FS 69 AND FS 70. MAINTENANCE REMOVED CORRODED SHEAR PLATE Y50 FROM FS 69 TO FS 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE, INSTALLED REPAIR PART IAW A320 SRM 51-42-11.Feb 17, 2005 · N647AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200500272Floorbeam · corrodedMCN - MAJOR REPAIR - DURING 8-DAY CHECK, CORROSION WAS FOUND ON FLOORBEAM -Y29 BETWEEN FS 64 AND FS 66. MAINTENANCE REMOVED CORRODED FLOORBEAM -Y29 FROM FS 64 TO FS 66; FABRICATED A NEW REPLACEMENT FLOOR BEAM, INSTALLED REPAIR PART IAW A320 SRM 51-49-00.Feb 17, 2005 · N647AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200500271Floorbeam · corrodedMCN - MAJOR REPAIR - DURING 8-DAY CHECK, CORROSION WAS FOUND ON FLOORBEAM -Y50 AT FS 66. MAINTENANCE REMOVED CORRODED FLOORBEAM -Y50 AT FS 66; FABRICATED A NEW REPLACEMENT FLOORBEAM, INSTALLED REPAIR PART IAW A320 SRM 51-42-11.Feb 17, 2005 · N647AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200500270Floorbeam · corrodedMCN - MAJOR REPAIR - DURING 8-DAY CHECK, CORROSION WAS FOUND ON FLOORBEAM -Y50 BETWEEN FS 66 AND FS 68. MAINTENANCE REMOVED CORRODED FLOORBEAM -Y50 FROM FS 66 TO FS 68; FABRICATED A NEW REPLACEMENT FLOORBEAM, INSTALLED REPAIR PART IAW A320 SRM 51-72-11.Feb 17, 2005 · N647AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200500266Floorbeam · corrodedMCN - MAJOR REPAIR - DURING 8-DAY CHECK, CORROSION WAS FOUND ON FLOORBEAM -Y50 BETWEEN FS 68 AND FS 69. MAINTENANCE REMOVED CORRODED FLOORBEAM -Y50 FROM FS 68 TO FS 69; FABRICATED A NEW REPLACEMENT FLOORBEAM, INSTALLED REPAIR PART IAW A320 SRM 51-72-11.Feb 17, 2005 · N647AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200500265Plate · corrodedMCN - MAJOR REPAIR - DURING 8-DAY CHECK, CORROSION WAS FOUND ON SHEAR PLATE -Y50 BETWEEN FS 64 AND FS 70. MAINTENANCE REMOVED CORRODED SHEAR PLATE -Y50 FROM FS 64 TO FS 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE, INSTALLED REPAIR PART IAW A320 SRM 51-72-11.Feb 17, 2005 · N647AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200500275Floorbeam · corrodedMCN - MAJOR REPAIR - DURING 8-DAY CHECK, CORROSION WAS FOUND AROUND FASTENER HOLES ON FLOORBEAM Y44 JUST FORWARD OF FS 68. MAINTENANCE REMOVED CORRODED FLOORBEAM Y44 AT FS 68; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11Feb 15, 2005 · N647AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200500268Floorbeam · corrodedMCN - MAJOR REPAIR - DURING 8-DAY CHECK, CORROSION WAS FOUND ON FLOORBEAM Y29 FORWARD OF FR 68. MAINTENANCE REMOVED CORRODED FLOORBEAM Y29 AT FS 68; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-49-00.Feb 15, 2005 · N647AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200500264Floorbeam · corrodedMCN - MAJOR REPAIR - DURING 8-DAY CHECK, CORROSION WAS FOUND ON FLOORBEAM Y19 AT FS 64. MAINTENANCE REMOVED CORRODED FLOORBEAM Y19 AT FS 64; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.Feb 15, 2005 · N647AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200500263Floorbeam · corrodedMCN - MAJOR REPAIR - DURING 8-DAY CHECK, CORROSION WAS FOUND ON FLOORBEAM Y35 AT FS 64. MAINTENANCE REMOVED CORRODED FLOORBEAM Y35 AT FS 64; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-49-00.Feb 15, 2005 · N647AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200500277Floorbeam · corrodedMCN - MAJOR REPAIR - DURING 8-DAY CHECK, CORROSION WAS FOUND AROUND MOUNT HOLE OF FLOORBEAM -Y18 BETWEEN FS 68 AND FS 69. MAINTENANCE REMOVED CORRODED FLOORBEAM -Y18 FROM FS 68 TO FS 69; FABRICATED A NEW REPLACEMENT FLOORBEAM, INSTALLED REPAIR PART IAW A320 SFeb 11, 2005 · N647AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200401135Actuator · faultyORD - ABORTED TAKEOFF - FLT 0738 - ON TAKEOFF AT ORD EN ROUTE FOR LAS, RECEIVED NR 2 ENGINE COMPRESSOR VANE FAULT, REJECTED TAKEOFF AT 65 KTS. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE VARIABLE STATOR VANE (VSV) ACTUATOR IAW T/C R5M75303, ENGINE RUN OPERATIOct 17, 2004 · N647AW · Airbus A320232 · Compressor Bleed ControlSDR AWXA200400295Epsu · defectivePHX - EEL - EMERGENCY LIGHTS NEAR LT OVERWING EMERGENCY EXIT STAY ON AND FAIL TEST AT FORWARD ATTENDANT PANEL. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD.Mar 19, 2004 · N647AW · Airbus A320232 · Emergency LightingSDR AWXA200400026Battery · dischargedPHX - EEL - DURING INSPECTION HAD A BATTERY TEST FAULT AT AFT LT EMERGENCY POWER SUPPLY UNIT (13WL). MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT AFT LT EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL CHECK WAS GOOD.Jan 9, 2004 · N647AW · Airbus A320232 · Emergency LightingSDR AWXA200301645Battery · dischargedATL - EEL - DURING 8-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 13, 17, 22, 26 AND EMERGENCY EXIT SIGNS AT L-2 & R-2 DOORS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK AT LT AFT EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIDec 30, 2003 · N647AW · Airbus A320232 · Emergency LightingSDR AWXA200301066Pressure Switch · failedON CLIMBOUT OF PHX EN ROUTE FOR SNA RECEIVED ECAM GREEN HYDRAULIC PUMP LOW PRESSURE INDICATION, TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED GREEN HYDRAULIC SYSTEM ENGINE PUMP LOW PRESSURE SWITCH IAW AMM 29-11-17-04, ASep 21, 2003 · N647AW · Airbus A320232 · Hydraulic Pressure Regulator, MainSDR AWXA200300098Computer · failedPHX - AIR TURN BACK - FLT 0014 - AFTER TAKEOFF FROM PHX EN ROUTE TO JFK, MAXIMUM OPERATING LIMIT SPEED (VMO/MMO) ALERT WOULD SOUND AND REMAIN ON IN ACCESS OF 240 KNOTS, AND EXTINGUISH AT 230 KNOTS. NR 1 AIR DATA INERTIAL REFERENCE UNIT (ADIRU) DISPLAYED ERRONEJan 31, 2003 · N647AW · Airbus A320232 · Inertial Guidance SystemSDR AWXA200300062Beam · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER SURFACE OF CREASE BEAM AT FORWARD EDGE OF RT AFT SERVICE DOOR ENTRANCE AT RT AFT LAVATORY ATTACH STUD, FR 66, STR 23 RT. MAINTENANCE FOUND CORROSION TO BE BEYOND ALLOWABLE LIMITS WITH 100 PERCENT MJan 8, 2003 · N647AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200300084Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND FLOORBEAM AT FR 16, THIRD BEAM FROM OUTBOARD RT SIDE. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW AJan 7, 2003 · N647AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200300083Plate · crackedDURING C-04 CHECK A 1 INCH CRACK WAS FOUND ON RT WING TO BODY FAIRING SUPPORT STRUCTURE ANGLE CLOSING PLATE FRAME 34. MAINTENANCE REMOVED CRACKED RT WING TO BODY FAIRING SUPPORT STRUCTURE ANGLE CLOSING PLATE AT FR 34; FABRICATED A NEW REPLACEMENT CLOSING PLATEJan 7, 2003 · N647AW · Airbus A320232 · Aerodynamic FairingsSDR AWXA200300082Floorbeam · corrodedDURING C-04 CHECK GALVANIC CORROSION WAS FOUND RT SIDE OUTBOARD TRACK BEAM EXTENSION OF CABIN FLOORBEAM FRAME 16. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS; CUT OUT DAMAGED SECTION OF FLOORBEAM FR 16; FABRICATED A FILLER AND 2 EACH REJan 7, 2003 · N647AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200300059Plate · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON THE LOWER SURFACE OF LT SHEAR PLATE BETWEEN FR 69 AND 70. MAINTENANCE FOUND CORROSION ON LOWER SURFACE OF LT SHEAR PLATE BETWEEN FR 69 AND 70 TO BE BEYOND 50 PERCENT OF MATERIAL LOSS; REMOVED SHEAR PLATE; FAJan 7, 2003 · N647AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200300035Crease Beam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON THE LOWER SURFACE OF RT CREASE BEAM (SHEAR PLATE) FROM BS 69 TO BS 70. MAINTENANCE REMOVED DAMAGED CREASE BEAM; FABRICATED A REPLACEMENT CREASE BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-Jan 7, 2003 · N647AW · Airbus A320232 · Fuselage Main, StructureSDR AWXA200300036Structure · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON AFT CARGO DOOR CUTOUT LOWER SILL JUST FORWARD OF FRAME SUPPORT FITTING NR 7, FR 52A. MAINTENANCE REMOVED DAMAGED SEALING PROFILE AT AFT CARGO DOOR CUTOUT LOWER SILL; FABRICATED A NEW REPLAJan 5, 2003 · N647AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200200672Connector · brokenPHX - EEL - DURING INSPECTION VARIOUS EMERGENCY LIGHTS OUT IN CABIN 4 (EA) SEAT 1 (EA) CEILING WERE FOUND INOPERATIVE. MAINTENANCE REPAIRED A CONNECTOR AT SEAT ROW 22 L/H, OPERATIONAL CHECK OF LIGHTING SYSTEM WAS GOOD.Jul 26, 2002 · N647AW · Airbus A320232 · Emergency LightingSDR AWXA0001137Thermostat · intermittentPHX - AIR TURNBACK - ON CLIMB, NR 1 ENG. BLEED FAULT OCCURED; A RESET WAS PERFORMED PER MAINTENANCE CONTROL AND BLEED WORKED, RETURNED TO NORMAL; A/C RETURNED TO PHX DUE TO POSSIBLE REPEAT AND WEATHER CONDITIONS IN DCA. MAINTENANCE TROUBLESHOT AND REPLACED THEDec 21, 2000 · N647AW · Airbus A320232 · Pneumatic Distribution SystemSDR AWXA0000005Safety Valve · failedAFTER TAKEOFF APPROX 1.5 MINUTES FOLLOWING GEAR RETRACTION, NOSE GEAR DOOR OPENS AND SHUTS. NO ECAM INDICATION OF FAULT. COMPLIED WITH CRITICAL ALERT REF LP 9501148. REMOVED AND REPLACED LANDING GEAR SAFETY VALVE (TT 0046159). REPLACED RELAYS 28GA, 48GA, AJan 11, 2000 · N647AW · Airbus A320232 · Landing Gear Door Retract SectionSDR AWXA9900324Filter · dirtySTRONG ODOR NOTICED ON DESCENT, UNABLE TO ISOLATE WHICH PACK WAS PRODUCING SMELL. ENGINE BLEEDS OK, APU BLEED ON SEEMS TO PRODUCE SMELL. REMOVED AND REPLACED LT AND RT OZONE FILTERS, INSPECTED APU INLET, NO OIL LKS NOTED.Sep 21, 1999 · N647AW · Airbus A320232 · Humidity Control SystemSDR AWXA9800228Valve · malfunctionedLOUD NOISE BANGING TYPE HEARD AND FELT IN COCKPIT TO ROW 4 DURING FLIGHT. UNABLE TO IDENTIFY SOURCE OF NOISE, DIVERTED FLIGHT TO TPA. REMOVED AND REPLACED SAFETY VALVE 49GA PER MM 32-31-17. OPERATIONAL CHECK GOOD PER 32-31-00-710-005.Nov 29, 1998 · N647AW · Airbus A320232 · Landing Gear Door Retract Section
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