N649AW

Service difficulty reports · 290

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 = 'N649AW' 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 AWXA200601305Seat Track · corrodedFOUND CORROSION ON SEAT TRACK LOC FS 36 TO Y 1292. SEAT TRACK REPLACED FROM FS 36 TO FS 41 IAW SRM 51-72-11. DUE FOUND OUT OF LIMITS.Jul 12, 2006 · N649AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200601303Seat Track · corrodedFOUND CORROSION ON SEAT TRACK LOC FR 38 + 6" - Y 1292 RT PASSENGER CABIN. SEAT TRACK REPLACED FROM FR 36 TO FR 41 - Y 1292 DUE FOUND OUT OF LIMITS. REPLACEMENT IAW SRM 51 - 72 - 11.Jul 12, 2006 · N649AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200601302Seat Track · corrodedFOUND CORROSION ON SEAT TRACK LOC FS 47 + 8" - Y 1292 RT PASSENGER CABIN. SEAT TRACK REPLACED FROM FS 47 TO FS 47 - Y 1292 IAW SRM SL7211 DUE FOUND OUT OF LIMITS.Jul 12, 2006 · N649AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200601291Floor Panel · delaminatedSAL - DELAMINATION WAS FOUND ON FLOOR PANEL 151GF IN AFT CARGO COMPARTMENT AND DOUBLER DAMAGED. THE FLOOR PANEL NR 151GF WAS REPLACED IAW SRM 53-02-00 AND IRM 9701 REV F. PROTECTIVE DOUBLER WAS BONDED IAW ER 5326-01007 AND FABRICATED IAW AWA CARD M2M53305.Jul 12, 2006 · N649AW · Airbus A320232 · Fuselage Floor PanelSDR AWXA200601290Floor Panel · delaminatedSAL - CHECK NR BC-6 NR 5959122, DELAMINATION WAS FOUND ON FLOOR PANEL 131 BF IN FWD CARGO COMPARTMENT. THE FLOOR PANEL 131 BF WAS REPLACED IAW SRM 53 - 02 - 00 PAR 8G, 8H AND SRM 9701 REV F. PROTECTIVE DOUBLER WAS REPLACED IAW ER NR 36 - 5326 - 05209 - RC1C.Jul 12, 2006 · N649AW · Airbus A320232 · Fuselage Floor PanelSDR AWXA200601288Seat Track · corrodedSAL - CHECK NR BC - 6. NR 5910348, CORROSION ON SEAT TRACK LOC FS 46 -Y 765 RT PASSENGER CABIN. SEAT TRACK LOC FS 41 TO FS 47 - Y 765 RT PASSENGER CABIN WAS REPLACED IAW SRM A320 51-72-11 PAGE 1, 2.Jul 12, 2006 · N649AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200601345Floor Panel · delaminatedFOUND DAMAGE FLOOR PANEL NR 231 NF ON PASSENGER CABIN. THE FLOOR PANEL NR 231 NF WAS REPLACED IAW IRM 9701 REV F.Jul 6, 2006 · N649AW · Airbus A320232 · Fuselage Floor PanelSDR AWXA200601289Floor Panel · delaminatedSAL - CHECK NR BC - 6, NR 5958704, DAMAGE FLOOR PANEL 23 ON PASSENGER CABIN. THE FLOOR PANEL 23 WAS REPLACED IAW IRM 9701 REV F.Jul 6, 2006 · N649AW · Airbus A320232 · Fuselage Floor PanelSDR AWXA200600689Bleed Valve · malfunctionedPHX - ENGINE ANOMALY - FLT 0091 - CREW REPORTED THAT THE NR 1 ENGINE STALLED WHEN CREW LEVELED OFF AT 370. ENGINE RECOVERED AND OPERATED NORMALLY THE REMAINDER OF THE FLT. MX PERFORMED BOROSCOPE INSPECTION OF THE HPC STAGES 3 AND 6 IAW AWA TASK CARD I5M72308Apr 16, 2006 · N649AW · Airbus A320232 · Compressor Bleed ValveSDR AWXA200600626Power Supply · inoperativePHX - EEL - NR 3820084 - DURING OVERNIGHT MAINTENANCE DISCOVERED ROW 1 & 6 LEFT AISLE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD PSU, 10WL. OPERATIONAL CHECKS WERE GOOD IAW AIRBUS 320 AMM 33-51-38.Apr 7, 2006 · N649AW · Airbus A320232 · Emergency LightingSDR AWXA200600004Sill · corrodedMCN - MAJOR REPAIR - DURING INSPECTION FOUND SILL CORRODED FROM FS 66 TO FS 68 AND Y-1732. MAINTENANCE REMOVED EXISTING REPAIR FILLER AND TRIMMED OUT ADDITIONAL .040 FROM I-BEAM. FOUND MATERIAL LOSS TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-41-14. FABRICATEJan 2, 2006 · N649AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200600006Floorbeam · corrodedMCN - DURING INSPECTION DISCOVERED CORROSION ON CABIN FLOORBEAM AT FS 68-60 MM AND BL Y-1225. CORROSION ON FLOORBEAM WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14 FIG 102. MAINTENANCE REMOVED AND INSTALLED NEW FLOORBEAM AT FR 68-60 MM AND BL Y-12Dec 17, 2005 · N649AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200600001Floorbeam · corrodedMCN - DURING INSPECTION CORROSION DISCOVERED ON CABIN FLOORBEAM AT FS 68 TO FS 79 AND AT BL Y-1235. MAINTENANCE REMOVED CORROSION AND WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 310 SRM 53-00-14 FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM AT FR 68 TO FR 69 ANDDec 17, 2005 · N649AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200600007Seat Track · corrodedMCN - DURING INSPECTION DISCOVERED SEAT RAIL BEAM CORRODED AT AFT WALL OF LAVE, INBOARD ATTACH POINT, AT FS 65 TO FS 68 AND BL Y-1225. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14 FIG 102. REMOVED AND INSTALLED NEW SEAT TRACK RDec 16, 2005 · N649AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600005Seat Track · corrodedDURING INSPECTION DISCOVERED CORROSION ON SEAT TRACK AT FORWARD WALL OF LAVE E OUTBOARD ATTACH POINT FROM FS 65 TO FS 68 AND BL Y-1292. CORROSION ON SEAT RAIL BEAM WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14 FIG 102. MAINTENANCE REMOVED AND INSDec 16, 2005 · N649AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200501482Servo · failedON CLIMB, FELT VIBE IN RUDDER PEDALS. TURNED A/P OFF, INCREASED PITCH OF AC TO SLOW DOWN TO 270 IAS & FL 330, VIBE STOPPED. INSP AC & ELEV SERVO HINGE BRGS FOR CONDITION IAW MM. AC FERRIED BACK FOR REPAIR. DURING FERRY FLT, REPORTED AC CRABBING 2 DEGREES TODec 4, 2005 · N649AW · Airbus A320232 · Elevator Control SystemSDR AWXA200501227Wire · brokenPHX - EEL - DURING OVERNIGHT INSPECTION DISCOVERED EMERGENCY EXIT LIGHT AT ROW 7 LEFT INOPERATIVE. MAINTENANCE FOUND WIRES BROKEN UNDER ROW 7 LEFT. SPLICED WIRES TOGETHER, OPERATIONAL CHECKS WERE GOOD.Oct 15, 2005 · N649AW · Airbus A320232 · Light System WiringSDR AWXA200500348Wire Harness · brokenPHX - EEL - DURING E-07 CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON EMERGENCY ESCAPE PATH LIGHT HARNESS SEAT ROW 5 LT, OPERATIONAL CHECK WAS GOOD.Mar 19, 2005 · N649AW · Airbus A320232 · Light System WiringSDR AWXA200500129Epsu · dischargedPHX - EEL - DURING E-06 CHECK FUNCTIONAL TEST OF THE EMERGENCY LIGHT SYSTEM FOUND THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 1-5 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL TEST WAS GOOD.Feb 1, 2005 · N649AW · Airbus A320232 · Emergency LightingSDR AWXA200401391Seal · leakingON CLIMBOUT OF PHX EN ROUTE TO DTW THE NR 2 ENGINE OIL QUANTITY INDICATED ZERO, OIL PRESSURE AND OIL TEMERATURE INDICATED NORMAL, TURNED BACK TO PHX FOR REPAIR, SHUTDOWN ENGINE DURING TAXI BACK TO GATE. MAINTENANCE INSPECTED NR 2 ENGINE AND FOUND DE-OILER LEADec 13, 2004 · N649AW · Airbus A320232 · Engine Oil Distribution (Airframe Furnished)SDR AWXA200301648Radar · bird strikeORD - AIR TURNBACK - FLT 0010 - SHORTLY AFTER TAKEOFF AT ORD EN ROUTE FOR PHX A BIRD STRUCK THE AIRCRAFT, LOST WEATHER RADAR AND HAD A LOT OF NOISE COMING FROM AREA. TURNED BACK TO ORD AND LANDED WITHOUT EVENT. MAINTENANCE FOUND DAMAGE TO RADOME AND WEATHER Dec 31, 2003 · N649AW · Airbus A320232 · Weather Radar SystemSDR AWXA200300404Sill · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND AT 3 AREAS ON UPPER SURFACE OF THE AFT BULK CARGO DOOR SILL FROM BS 2829.6 TO 2882.9. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUT OUT DAMAGED AREAS OF AFT BApr 7, 2003 · N649AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200300425Panel · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK A 1 INCH CRACK WAS FOUND ON WING TO BODY FAIRING CLOSING PLATE AT FR 34, LBL 64. MAINTENANCE REMOVED DAMAGED CLOSING PLATE AT FR 34, LBL 64; FABRICATED A NEW REPLACEMENT CLOSING PLATE; INSTALLED REPAIR PART IAW A320 SRM Apr 5, 2003 · N649AW · Airbus A320232 · Aerodynamic FairingsSDR AWXA200300407Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK FILIFORM CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y-1732, FORWARD SIDE OF FR 66. MAINTENANCE REMOVED CORROSION ON UPPER SURFACE OF FLOORBEAM Y-1732, AND DOOR SILL FITTING FORWARD SIDE OF FR 66; MATERIAL LOSS FOUApr 5, 2003 · N649AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200300406Attach Angle · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK A 1 INCH CRACK WAS FOUND ON LT FORWARD BELLY FAIRING VERTICAL ATTACH ANGLE BS 1483.4, 13 INCHES FROM OUTBOARD GROUND AIR CONDITIONING ATTACH POINT. MAINTENANCE REMOVED CRACKED LT FORWARD BELLY FAIRING VERTICAL ATTACH ANGApr 5, 2003 · N649AW · Airbus A320232 · Aerodynamic FairingsSDR AWXA200300402Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK FILIFORM CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y-81 FROM FORWARD SIDE OF FR 18 TO FR 20. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED FLOORBEAM Y-81 FROM FORWARD SIDE OFApr 5, 2003 · N649AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200300401Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK FILIFORM CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y-1292, FORWARD AND AFT SIDE OF FR 67. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED FLOORBEAM Y-1292, FORWARD AND AFT SIDEApr 5, 2003 · N649AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200300400Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK FILIFORM CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y-1292, FORWARD AND AFT SIDE OF FR 68. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED FLOORBEAM Y-1292, FORWARD AND AFT SIDEApr 5, 2003 · N649AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200300399Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y-1292, FORWARD SIDE OF FR 68. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED FLOORBEAM Y-1292, FORWARD SIDE OF FR 68 TO Apr 5, 2003 · N649AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200300398Floor Support · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK FILIFORM CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR SUPPORT BEAM Y-254, AFT OF FR 16. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED FLOOR SUPPORT BEAM Y-254 FROM FR 12 TO FR 21; FApr 5, 2003 · N649AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200300396Plate · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK FILIFORM CORROSION WAS FOUND ON UPPER SURFACE OF WEB BETWEEN FR 69 AND FR 70, AND AFT OF BEAM Y-1292. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED SHEAR PLATE WEB BETWEEN FR 69 AND FApr 5, 2003 · N649AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200300391Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y-1292 FROM AFT SIDE OF FR 66 TO AFT SIDE OF FR 67. MAINTENANCE REMOVED CORROSION ON UPPER SURFACE OF FLOORBEAM Y-1292 AT FR 66 TO FR 67 AND FOUND MATERIAL LOApr 5, 2003 · N649AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200300390Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y-765 AT FR 16. MAINTENANCE REMOVED CORROSION ON UPPER SURFACE OF FLOORBEAM Y-765 AT FR 16 AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. CUT OUT DAMAGED SECTIApr 5, 2003 · N649AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AWXA200300405Seat Track · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK FILIFORM CORROSION WAS FOUND ON UPPER SURFACE OF RT INBOARD CABIN SEAT TRACK AT FORWARD END OF FR 20. MAINTENANCE REMOVED CORRODED RT INBOARD CABIN SEAT TRACK AT FORWARD END OF FR 20; FABRICATED A NEW REPLACEMENT SEAT TRApr 4, 2003 · N649AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200300397Support · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK FILIFORM CORROSION WAS FOUND ON LOWER SURFACE OF SHEAR WEB (SUPPORT) 147MM FORWARD OF FR 70, AND INBOARD OF THE RT OUTBOARD CREASE BEAM ANGLE. MAINTENANCE REMOVED CORRODED SUPPORT FR 70; FABRICATED A NEW REPLACEMENT SUPPApr 4, 2003 · N649AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AWXA200300395Seat Track · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK FILIFORM CORROSION WAS FOUND ON UPPER SURFACE OF RT OUTBOARD CABIN SEAT TRACK FORWARD END AT FR 20. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED RT OUTBOARD CABIN SEAT TRACK FORWARDApr 4, 2003 · N649AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200201016Battery Pack · dischargedDURING INSPECTION EMERGENCY EXIT LIGHTS FAILED OPERATIONAL TEST. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT THE RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL); OPERATIONAL CHECK WAS GOOD IAW AWA T/C 18M05319, STEP 5.Oct 19, 2002 · N649AW · Airbus A320232 · Emergency LightingSDR AWXA200200875Coffeemaker · shortedDURING CLIMBOUT FLIGHT CREW OBSERVED AN ELECTRICAL BURNING SMELL AND SMOKE COMING FROM FORWARD GALLEY, UPON INVESTIGATION THE F/A NOTICED ARCING AT THE NR 1 COFFEEMAKER. THE AIRCRAFT TURNED BACK TO PHX AND THE NR 1 COFFEEMAKER CIRCUIT BREAKER WAS PULLED. ARCSep 9, 2002 · N649AW · Airbus A320232 · Buffet/GalleysSDR AWXA200200691Solenoid Valve · leakingPHX - AIR TURNBACK - FLT 0081 - AFTER TAKEOFF FROM PHX EN ROUTE TO BWI DURING CLIMB ECAM INDICATED LOSS OF YELLOW HYDRAULIC PRESSURE AND FLUID. AIRCRAFT TURNED BACK TO PHX. MAINTENANCE FOUND THE 3150GP HYDRAULIC SOLENOID VALVE LEAKING AND REPLACED VALVE IAW Aug 4, 2002 · N649AW · Airbus A320232 · Hydraulic System, MainSDR AWXA200200562Fan · burnedFLT 175 - DURING FLT, PAX AND F/A REPORTED A STRONG ELECT BURNING ODOR AT OVER WING AREA, F/O VERIFIED BURNING ODOR AND A/C DIVERTED. ENGS WERE RUN TO T/O POWER AND PACKS WERE OPERATED BOTH SEPARATE AND TOGETHER IN BOTH THE HOT AND COLD MODE. HYD PUMPS WERE Jun 24, 2002 · N649AW · Airbus A320232 · Air Distribution Fan
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