N651AW

Service difficulty reports · 344

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 = 'N651AW' 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 USAA920080573Floorbeam · corrodedSAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3043 /FR 64 - BS 3158 /FR 66, -Y1292. REPLACED CABIN FLOORBEAM, BS 3043 /FR 64 - BS 3158 /FR 66, -Y1292 IAW A320 SRM 51-72-11.Feb 24, 2008 · N651AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA920080572Dummy Rail · corrodedSAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN DUMMY RAIL, BS 3043 /FR 64, +Y765. REPLACED CABIN DUMMY RAIL, BS 3043 /FR 64, +Y765 IAW A320 SRM 51-72-11.Feb 24, 2008 · N651AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA920080571Seat Track · corrodedSAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN SEAT TRACK BS 1590 /FR 36 - BS 1810 /FR 36, -Y1292. REPLACED CABIN SEAT TRACK BS 1590 /FR 36 - BS 1810 /FR 36, -Y1292 IAW A320 SRM 51-72-11.Feb 23, 2008 · N651AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200700933Generator · failedCREW REPORTED THE BLUE HYDRAULIC SYSTEM FAILED DURING CLIMB-OUT OF PHX. THE CREW DECLARED AN EMERGENCY AND RETURNED TO PHX. THE LANDING WAS UNEVENTFUL. MX REPLACED THE CONSTANT SPEED MOTOR/GENERATOR (8XE) IAW AMM 24-24-51-400-001. OPERATIONAL CHECK WAS GOOD.Jul 28, 2007 · N651AW · Airbus A320232 · Hydraulic Indicating SystemSDR AWXA200601840Hinge Fitting · wornRETURN TO SERVICE FLIGHT - CLIMBING C320 KTS, 26,000 FT LIGHT TO MODERATE AIRFRAME VIBRATIONS EXPERIENCED IN THE YAW AXIS, RUDDER INPUTS STOPPED VIBRATION. SLOWING BELOW 300KTS STOPPED VIBRATION. PERFORMED ADJUSTMENT THE ELEVATOR RT AND LT AND OPERATIONAL TOct 27, 2006 · N651AW · Airbus A320232 · Rudder StructureSDR AWXA200601829Feeder Cable · damagedSAL - EEL - BC-6 CHECK - MAIN CABIN NR 1 LEFT PARTITION EMERGENCY LIGHT CABLE ASSEMBLY DAMAGED. REPLACED MAIN CABIN NR 1 LEFT PARTITION EMERGENCY LIGHT CABLE ASSEMBLY IAW A320 AMM 33-51-00.Oct 23, 2006 · N651AW · Airbus A320232 · Light System WiringSDR AWXA200601795Bridge · corrodedSAL - MAJOR REPAIR - CORROSION ON BULK CARGO COMPARTMENT DOOR CUT OUT LOWER SILL (BRIDGE ASSY) EXTERNAL SURFACE, FS 62, -Y640. REPAIRED BULK CARGO COMPARTMENT DOOR CUT OUT LOWER SILL (BRIDGE ASSY) EXTERNAL SURFACE, FS 62 - FS 63, -Y640 IAW A320 SRM 53-41-49, Oct 21, 2006 · N651AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200601770Sill · corrodedSAL - MAJOR REPAIR - CORROSION ON L2 DOOR CUT OUT LOWER SILL BEAM, FS 67+19", +Y1292. REPAIRED L2 DOOR CUT OUT LOWER SILL BEAM, FS 67+19", +Y1292 IAW A320 SRM 53-41-14 FIG. 210, PRINCIPLE 5, 51-21-11 AND 51-42-11.Oct 18, 2006 · N651AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200601769Sill · corrodedSAL - MAJOR REPAIR - CORROSION ON R2 DOOR CUT OUT LOWER SILL BEAM, FS 68, - Y1305. REPAIRED R2 DOOR CUT OUT LOWER SILL BEAM, FS 68, - Y1305 IAW A320 SRM 53-41-14 FIG 201 PRINCIPLE 5, 51-21-11, AND 51-42-11.Oct 18, 2006 · N651AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200601776Seat Track · corrodedSAL - MAJOR REPAIR - BC-6 CHECK, CORROSION ON MAIN CABIN SEAT TRACK, FS 41 - FS 47, +Y1292. REPLACED MAIN CABIN SEAT TRACK, FS 41 - FS 47, +Y1292 IAW A320 SRM 51-72-11.Oct 17, 2006 · N651AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200601775Seat Track · corrodedSAL - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK, FS 41 - FS 47, -Y1292. REPLACED MAIN CABIN SEAT TRACK, FS 41 - FS 47, -Y1292 IAW A320 SRM 51-72-11.Oct 17, 2006 · N651AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200601774Seat Track · corrodedSAL - MAJOR REPAIR - BC-6 - CORROSION ON MAIN CABIN SEAT TRACK, FS 36 - FS 41, +Y1292. REPLACED MAIN CABIN SEAT TRACK, FS 36 - FS 41, +Y1292 IAW A320 SRM 51-72-11.Oct 17, 2006 · N651AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200601772Floorbeam · corrodedSAL - MAJOR REPAIR - CORROSION ON MAIN CABIN RAIL SEAT BEAM, FS 66 + 3", -Y1292. REPLACED MAIN CABIN RAIL SEAT BEAM, FS 66 + 3", -Y1292 IAW A320 SRM 51-72-11.Oct 16, 2006 · N651AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200601771Floorbeam · corrodedSAL - MAJOR REPAIR - CORROSION ON MAIN CABIN LONGITUDINAL FLOORBEAM, FS 66 + 13", -Y1292. REPLACED MAIN CABIN LONGITUDINAL FLOORBEAM, FS 66 + 13", -Y1292 IAW A320 SRM 51-72-11.Oct 16, 2006 · N651AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200601768Floorbeam · corrodedSAL - FOUND CORROSION ON MAIN CABIN LONGITUDINAL BEAM, FS 66 + 13", +Y1292. REPAIRED MAIN CABIN LONGITUDINAL BEAM, FS 66 + 13", +Y1292 IAW A320 SRM 51-72-11 AND A320 SRM 51-42-11.Oct 16, 2006 · N651AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200600042Cover · missingBOS - VIBRATION - CREW REPORTED THAT THE RT EMERGENCY EXIT WINDOWS PRODUCING LOUD SQUEAL AND FLOOR VIBRATION. MAINTENANCE INSPECTION DOORS AND FOUND NO DEFECTS. FOUND MISSING HOIST POINT COVER ON THE FWD DOOR. APPLIED SPED TAPE AND PLACED ON OIL. ON 09JAN0Dec 30, 2005 · N651AW · Airbus A320232 · Emergency ExitsSDR AWXA200501391Flashlight · inoperativePHX - EEL - ON GROUND CREW REPORTED AFT EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT.Nov 14, 2005 · N651AW · Airbus A320232 · Emergency EquipmentSDR AWXA200501286Oven · odorCREW REPORTED FORWARD OVENS EMIT NOXIOUS FUMES WHEN USED. MAINTENANCE REMOVED AND REPLACED FORWARD GALLEY NR 1 OVEN. OPERATIONAL CHECKS GOOD. VENDOR TEAR DOWN REPORT CONFIRMS REASON FOR REMOVAL. UNIT WAS RECEIVED WITH TEMPERATURES OUT OF RANGE. TEMPERATUROct 27, 2005 · N651AW · Airbus A320232 · Buffet/GalleysSDR AWXA200500898Light · inoperativePHX - EEL - DURING PHASE 4 CHECK, OPERATIONAL TEST OF EMERGENCY LIGHTS FAILED EXTERNAL LOAD FAULTING FORWARD LEFT. MAINTENANCE REMOVED AND REPLACED THE L1 DOOR ESCAPE SLIDE IAW AMERICA WEST TASK CARD R1C25305. VENDOR TEAR DOWN REPORT SHOWS SLIDE PASSING ALL Jul 30, 2005 · N651AW · Airbus A320232 · Emergency LightingSDR AWXA200500746Bleed Air Sys · malfunctionedAIR TURN BACK. DURING CLIMB RECEIVED ECAM MESSAGE FOR ENG BLEED 1 FAULT FOLLOWED BY PACK FAULT THEN NR 2 ENG BLEED FAULT FOLLOWED BY PACK FAULT. RETURNED WITHOUT FURTHER INCIDENT. MX REMOVED AND REPLACED NR 1 AND NR 2 BMC. REMOVED AND REPLACED NR 1 ENGINE Jun 23, 2005 · N651AW · Airbus A320232 · Engine Bleed Air SystemSDR AWXA200500472Outflow Valve · malfunctionedIAH - AIR TURN BACK - FLT 0103 - ON DEPARTURE OUT OF IAH EN ROUTE FOR LAS RECEIVED UPPER ECAM MESSAGE FOR AVIONICS VENT FAULT, EXTRACT VALVE INDICATED FULL OPEN NOT ALLOWING AIRCRAFT TO PRESSURIZE, TURNED BACK TO IAH AND LANDED WITHOUT FURTHER EVENT. MAINTENAApr 19, 2005 · N651AW · Airbus A320232 · Pressure Regulator/Outflow ValveSDR AWXA200500376Air Data Module · malfunctionedON TAKEOFF ROLL AT FLL EN ROUTE FOR LAS NOTICED AIR SPEED DIFFERENCE OF 20 KTS, CAPTAINS AIRSPEED 60 KTS, FIRST OFFICERS 40 KTS, REJECTED TAKEOFF AT 60 KTS AND RETURNED TO GATE. AIRCRAFT WAS MAINTENACE FERRIED TO PHX WHERE MAINTENANCE PERFORMED AN INTERFACE TMar 25, 2005 · N651AW · Airbus A320232 · Air Data ComputerSDR AWXA200401234Epsu · faultyDURING 8-DAY CHECK, OPERATIONAL TEST OF THE EMERGENCY LIGHT SYSTEM FOUND THE RT OVERWING EMERGENCY POWER SUPPLY UNIT FAULTED. MAINTENANCE REMOVED AND REPLACED THE RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD.Nov 6, 2004 · N651AW · Airbus A320232 · Emergency LightingSDR AWXA200401040Wire · backed outDURING 4-DAY CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 15 LT INOPERATIVE. MAINTENANCE FOUND A WIRE PULLED FROM CONNECTOR 7260VC), RE-PINNED WIRE, OPERATIONAL CHECK GOOD.Sep 19, 2004 · N651AW · Airbus A320232 · Light System WiringSDR AWXA200401012Engine · failedON TAKEOFF AT ORD EN ROUTE FOR PHX, WHEN FLEX THRUST APPLIED HEARD A LOUD BANG WITH MOMENTARY STALL INDICATED ON ECAM, REJECTED TAKEOFF AND UPON CLEARING RUNWAY NOTICED NR 1 ENGINE N2 VIB AT 7.4, SHUTDOWN ENGINE AND RETURNED TO GATE. MAINTENANCE PERFORMED A VSep 10, 2004 · N651AW · Airbus A320232 · Engine (Turbine/Turboprop)SDR AWXA200400860Wire · brokenPHX - EEL - DURING 4-DAY CHECK FOUND THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 RT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT CABLE HARNESS UNDER SEAT ROW 11 RT, OPERATIONAL CHECK OF LIGHT WAS GOOD.Aug 9, 2004 · N651AW · Airbus A320232 · Light System WiringSDR AWXA200400062Battery · dischargedLAS - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT BATTERY PACK, OPERATIONAL CHECK WAS GOOD.Jan 22, 2004 · N651AW · Airbus A320232 · Emergency EquipmentSDR AWXA200301083Skin · erodedDURING C-04 CHECK THE NR 2 ENGINE PYLON AFT FAIRING INBOARD SKIN WAS FOUND ERODED AT THE LOWER SECTION. MAINTENANCE REMOVED ERODED INBOARD SKIN ON THE NR 2 ENGINE PYLON; FABRICATED A NEW SECTION OF REPLACEMENT SKIN; INSTALLED REPAIR PART IAW A320 SRM 51-42-11,Sep 14, 2003 · N651AW · Airbus A320232 · Nacelle/Pylon, Plate/SkinSDR AWXA200301075Skin · erodedDURING C-04 CHECK THE LOWER SECTION OF THE NR 2 PYLON AFT FAIRING OUTBOARD SKIN WAS FOUND ERODED. MAINTENANCE REMOVED ERODED AFT FAIRING SKIN; FABRICATED NEW REPLACEMENT SKIN; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 8-13, & A24-A25 FIG 2-4, & 61.Sep 14, 2003 · N651AW · Airbus A320232 · Nacelle/Pylon, Plate/SkinSDR AWXA200301072Floorbeam · corrodedDURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON UPPER SURFACE OF Y1292 FLOORBEAM 3 INCHES FORWARD OF FR 68. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED CORRODED Y1292 FLOORBEAM FR 68; FABRICATED A NEW REPLACEMENTSep 9, 2003 · N651AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200301071Floor Support · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON Y254 FLOOR SUPPORT AT FR 20. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. CUT OUT CORRODED AREA OF FLANGE ON Y254 FLOOR SUPPORT AT FR 20; FABRICATED A FILLER AND 2 EACH REPAIRSep 9, 2003 · N651AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200301065Fitting · damagedDURING C-04 CHECK FOUND UPPER OUTBOARD MOUNTING HOLE ELONGATED FROM WEAR ON STRUT ATTACH FITTING AT UPPER AFT CORNER OF NOSE WHEEL WELL AT FR 20, Z120. MAINTENANCE REMOVED DAMAGED STRUT ATTACH FITTING AT UPPER AFT CORNER OF NOSE WHEEL WELL AT FR 20, Z120; FABSep 9, 2003 · N651AW · Airbus A320232 · Nose/Tail Landing Gear Attach SectionSDR AWXA200301064Web · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER AND LOWER SURFACE OF RT AFT WEB (SHEAR PLATE), FORWARD SIDE OF FR 70, JUST BELOW CABIN FLOOR PANEL. MAINTENANCE REMOVED CORRODED SHEAR PLATE BETWEEN FR 69 AND FR 70; FABRICATED A NEW REPLACEMENT SSep 9, 2003 · N651AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200301074Skin · corrodedDURING C-04 CHECK THE NR 1 PYLON AFT FIXED FAIRING SKIN WAS FOUND PITTED. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED CORRODED AFT FIXED FAIRING SKIN; FABRICATED NEW REPLACEMENT SKIN; INSTALLED REPAIR PART IAW A320 Sep 8, 2003 · N651AW · Airbus A320232 · Nacelle/Pylon, Plate/SkinSDR AWXA200301070Seat Track · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF Y1292 SEAT TRACK AT FR 66. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED CORRODED Y1292 SEAT TRACK FR 64-66; FABRICATED A NEW REPLACEMENT SEAT TRACK; ISep 8, 2003 · N651AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200301069Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF Y1292 FLOORBEAM BETWEEN FR 65-66. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS. REMOVED CORRODED Y1292 FLOORBEAM BETWEEN FR 65-66; FABRICATED A NEW REPLACSep 8, 2003 · N651AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200301068Floorbeam · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF Y924 FLOORBEAM AT FR 66. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED CORRODED Y924 DUMMY RAIL AT FR 66; INSTALLED NEW REPLACEMENT RAIL IAW A320 SRM 5Sep 8, 2003 · N651AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200301084Seat Track · corrodedDURING C-04 CORROSION WAS FOUND ON THE FORWARD OUTBOARD END OF THE RT OUTBOARD SEAT TRACK AT FR 20. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SEAT TRACK FROM FS 6053 TO FS 9766, Y1292; FABRICATED A NEW REPLACESep 7, 2003 · N651AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200301073Floor Panel · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF R-1 DOOR SILL FLOOR PANEL (222FF), AT INBOARD AFT CORNER FR 20. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL ASSEMBLY IAW T/C C1D25306.Sep 7, 2003 · N651AW · Airbus A320232 · Fuselage Floor PanelSDR AWXA200301032Plate · crackedDURING C-04 CHECK A .5 INCH CRACK WAS FOUND ON RT FUSELAGE UNDER BELLY BODY FAIRING CLOSING PLATE AT FR 34. MAINTENANCE REMOVED CRACKED CLOSING PLATE AT FR 34; FABRICATED A NEW REPLACEMENT CLOSING PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 8-9, FISep 6, 2003 · N651AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200300336Wire · brokenPHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT WAS INOPERATIVE. MAINTENANCE REPAIRED BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE UNDER SEAT 9 LT, OPERATIONAL CHECK WAS GOOD.Apr 5, 2003 · N651AW · Airbus A320232 · Light System WiringSDR AWXA200200879Display · shortedFLL - BURNING SMELL - FLT 0888 - EN ROUTE FROM LAS TO FLL THE NR 1 MULTI PURPOSE CONTROL DISPLAY UNIT (MCDU) WENT BLANK, AT THE SAME TIME NOTICED AN ELECTRICAL BURNING SMELL THAT LASTED APPROXIMATELY TWO MINUTES. CONTRACT MAINTENANCE AT FLL INSPECTED THE NR 1Sep 11, 2002 · N651AW · Airbus A320232 · Central DisplaySDR AWXA200200579Power Supply · dischargedDURING INSPECTION THE FORWARD SECTION EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT ABOVE (10WL) OVER THE L1 DOOR, OPERATIONAL CHECK WAS GOOD.Jul 3, 2002 · N651AW · Airbus A320232 · Emergency LightingSDR AWXA200100606Bracket · looseDURING PHASE 5 INSPECTION FOUND L/E PANEL 521EB LT DISCOLORED. INVESTIGATION REVEALED DAMAGE TO 2 FIRE LOOPS, 6 GENERATOR FEEDER WIRES, A WIRE HARNESS BRACKET, AND THE FORWARD WING SPAR INSIDE L/E FLAP BAY. DAMAGE OCCURRED WHEN HARDWARE THAT SECURED LANDING Nov 21, 2001 · N651AW · Airbus A320232 · Main Landing Gear
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