N824AW

Service difficulty reports · 227

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 = 'N824AW' 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 USAA920081864Fan · failedFLT 440 PHX-DCA BURNING ODOR. DURING CRUISE, HEARD A LOUD RUMBLING NOISE ALONG WITH ELECTRICAL ODOR. SHUT OFF BLOWER FAN TO OVERRIDE. NOISE AND ODOR STOPPED. POPS BLOWER FAN CIRCUIT BREAKER BEHIND FIRST OFFICER. SWAPPED BLOWER FAN WITH EXTRACT FAN. R & Oct 10, 2008 · N824AW · Airbus A319132 · Air Distribution FanSDR USAA920070941Battery · dischargedPHX - EEL - FLT 210. MX REPORTED LT EPSU AT OVERWING HAS DEAD BATTERY. MX REPLACED THE LT EPSU BATTERY. OPERATIONAL CHECK WAS GOOD.Oct 12, 2007 · N824AW · Airbus A319132 · Emergency LightingSDR AWXA200601861Ballast · odorLAS - SMOKE - VERY STRONG SMELL OF ELECTRICAL BURNING WIRE SMELL NEAR AFT LAVATORY, NO SMOKE NOTED. MAINTENANCE REPLACED BALLAST ON ROWS 18-22R AND WINDOW LIGHTS. ALSO INSPECTED ELECTRICAL WIRING ON ROWS 18-22R NOTHING SHOWED ANY SIGNS OF SPARK OR SHORT PER Nov 2, 2006 · N824AW · Airbus A319132 · Passenger Compartment LightingSDR AWXA200601842Sill · corrodedSAL - MAJOR REPAIR - BC-4 CHECK - CORROSION ON R2 DOOR CUT OUT LOWER SILL , FS 66, -Y1472. REPAIRED R2 DOOR CUT OUT LOWER SILL , FS 66, -Y1472 IAW AWA ER 25-5341-06300-HF1.Oct 31, 2006 · N824AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601843Fitting · corrodedSAL - MAJOR REPAIR - BC-4 CHECK - CORROSION ON R1 DOOR CUT OUT LOWER THRESHOLD LOWER FITTING, FS 16+9" - FS 19, S23R. REPLACED R1 DOOR CUT OUT LOWER THRESHOLD LOWER FITTING, FS 16+9" - FS 19, S23R IAW A319 SRM 53-11-13 AND DRAWING D53112109.Oct 24, 2006 · N824AW · Airbus A319132 · Fuselage Main, Attach FittingsSDR AWXA200601794Seat Track · corrodedBC-4 CHECK - NR 5949426, CORROSION ON MAIN CABIN SEAT TRACK, FR 36 + 3 INCHES TO FR 41, -Y1292. REPLACED MAIN CABIN SEAT TRACK, FR 36 + 3 INCHES TO FR 41, -Y1292 IAW A319 SRM 51-42-11 AND 51-72-11.Oct 20, 2006 · N824AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200601792Floor Support · corrodedBC-4 CHECK - NR 5949853, CORROSION ON MAIN CABIN LONGITUDINAL BEAM, FR 67 - 1 INCH, +Y1292. REPLACED MAIN CABIN LONGITUDINAL BEAM, FR 67 - 1 INCH, +Y1292 IAW A319 SRM 51-42-11.Oct 20, 2006 · N824AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601791Floor Support · corrodedBC-4 CHECK - NR 5949844, CORROSION ON MAIN CABIN LONGITUDINAL BEAM, FR 68, -Y1292. REPLACED MAIN CABIN LONGITUDINAL BEAM, FR 68, -Y1292 IAW A319 SRM 51-72-11.Oct 20, 2006 · N824AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601847Skin · delaminatedMAJOR REPAIR - BC-4 CHECK -NR 5950024, DELAMINATION FOUND ON RUDDER RT SIDE PANEL, ABOVE BR 7 NEXT TO FASTENER ROW (FASTENER NR 31), DELAMINATED AREA APROX 81/4 X 5.0 INCHES. REPAIRED RUDDER RT SIDE PANEL ABOVE BR 7 IAW A319 SRM 55-41-00 PAR 9Q(9).Oct 18, 2006 · N824AW · Airbus A319132 · Rudder, Plate/SkinSDR AWXA200601846Floor Panel · corrodedMAJOR REPAIR - BC-4 CHECK - NR 5949849, CORROSION ON L2 DOOR WAY THRESHOLD FLOOR PANEL 261FF, FR66 TO FR68. REPLACED L2 DOOR WAY THRESHOLD FLOOR PANEL 261FF, FR66 TO FR68 IAW AWA CARD C1D25318.Oct 17, 2006 · N824AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601841Floor Support · corrodedSAL - MAJOR REPAIR - BC-4 CHECK - CORROSION ON MAIN CABIN LONGITUDINAL BEAM, FS 66 + 5" - FS 68 -5", -Y1292. REPLACED MAIN CABIN LONGITUDINAL BEAM, FS 66 + 5" - FS 68 -5", -Y1292 IAW A319 SRM 51-72-11.Oct 17, 2006 · N824AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601839Floorbeam · corrodedSAL - MAJOR REPAIR - CORROSION ON MAIN CABIN LONGITUDINAL FLOORBEAM, FS 66, -Y1292. REPLACED MAIN CABIN LONGITUDINAL FLOORBEAM, FS 66, -Y1292 IAW A319 SRM 51-72-11.Oct 17, 2006 · N824AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200601793Seat Track · corrodedBC-4 CHECK - NR 5949834, CORROSION ON MAIN CABIN DUMMY RAIL/SEAT TRACK, FR16, -Y765. REPAIRED MAIN CABIN DUMMY RAIL/SEAT TRACK, FR16, -Y765 IAW A319 SRM 53-11-14.Oct 17, 2006 · N824AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200601787Floor Support · corrodedBC-4 CHECK - NR 5949838, CORROSION ON MAIN CABIN DUMMY RAIL (FLOOR SUPPORT), FR16, +Y254. REPAIRED MAIN CABIN DUMMY RAIL (FLOOR SUPPORT), FR16, +Y254 IAW A319 SRM 53-00-14, FIG NR 204 (SHEET 2).Oct 17, 2006 · N824AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601785Floor Support · corrodedBC-4 CHECK - NR 5949846, CORROSION ON MAIN CABIN LONGITUDINAL BEAM, FR 68, -Y765. REPLACED MAIN CABIN LONGITUDINAL BEAM, FR 68, -Y765 IAW A319 SRM 51-42-11 AND 51-72-11.Oct 17, 2006 · N824AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601784Floor Support · corrodedBC-4 CHECK - NR 5949841, CORROSION ON MAIN CABIN DUMMY RAIL (FLOOR SUPPORT), FR21, -Y189. REPLACED MAIN CABIN DUMMY RAIL (FLOOR SUPPORT), FR21, -Y189 IAW A319 SRM 51-72-11.Oct 17, 2006 · N824AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601783Floor Support · corrodedBC-4 CHECK - NR 5949839, CORROSION ON MAIN CABIN DUMMY RAIL (FLOOR SUPPORT), FR14+7 INCHES - FR16, +Y503.2. REPLACED MAIN CABIN DUMMY RAIL (FLOOR SUPPORT), FR14+7 INCHES -FR16, +Y503.2 IAW A319 SRM 51-72-11, 51-42-11 AND DRAWING NR D531-12826.Oct 17, 2006 · N824AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601782Floor Support · corrodedMAJOR REPAIR - BC-4 CHECK - NR 5949835, CORROSION ON MAIN CABIN DUMMY RAIL (FLOOR SUPPORT), FR20, -Y254. REPAIRED MAIN CABIN DUMMY RAIL (FLOOR SUPPORT), FR20, -Y254 IAW A319 SRM 53 -00-14 FIG 204 SHEET 2.Oct 17, 2006 · N824AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601845Wire · damagedSAL - EEL - BC-4 CHECK - NR 5949617, DAMAGED EMERGENCY LIGHT PATH CABLE, SEAT ROW 6 LT. REPLACED EMERGENCY LIGHT PATH CABLE, SEAT ROW 6 LT IAW A319 AMM 33-51-18 AND 33-51-00.Oct 16, 2006 · N824AW · Airbus A319132 · Light System WiringSDR AWXA200600797Bypass Valve · malfunctionedLAS - AIR TURN BACK - FLT 837 - DURING CLIMB-OUT CREW RECEIVED NR 1 PACK FAULT WITH THE NR 2 PACK BEING DEFERRED. CREW CYCLED THE NR 1 PACK SWITCH TWICE WITH NO HELP. CREW DECIDED TO RETURN TO LAS. REPORTED THAT ON DOWN WIND, TIRED THE NR 1 PACK AGAIN AND IMay 10, 2006 · N824AW · Airbus A319132 · Cabin Cooling SystemSDR AWXA200500323Battery · dischargedDEN - EEL - DURING 4-DAY CHECK OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM RECEIVED A LT OVERWING EMERGENCY POWER SUPPLY UNIT BATTERY FAULT. MAINTENANCE REMOVED AND REPLACED BATTERY PACK IN THE LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK Mar 10, 2005 · N824AW · Airbus A319132 · Emergency LightingSDR AWXA200400343Slide · leakingR-2 DOOR EMERGENCY ESCAPE SLIDE RESERVOIR PRESSURE WAS BELOW SERVICEABLE LIMITS. MAINTENANCE REMOVED AND REPLACED R-2 DOOR EMERGENCY ESCAPE SLIDE ASSEMBLY IAW T/C R1C25305. VENDORS CONFIRMED FAILURE OF EMERGENCY ESCAPE SLIDE ASSEMBLY S/N A9584, SLIDE WAS OVEApr 2, 2004 · N824AW · Airbus A319132 · Escape SlideSDR AWXA200400288Adc · faultyJFK - ABORTED TAKEOFF - FLT 0411 - ON TAKEOFF AT JFK EN ROUTE TO SFO RECEIVED NR 1 IR FAULT, REJECTED TAKEOFF AT 90 KTS. MAINTENANCE ISSUED MEL 34-10-01, COND 2 IRS NR 1 NAV MODE INOP. ON 03/15/2004 MAINTENANCE REMOVED AND REPLACED THE NR 1 AIR DATA INERTIALMar 13, 2004 · N824AW · Airbus A319132 · Air Data ComputerSDR AWXA200301560Wire · chafedJFK - EEL - DURING INSPECTION EMERGENCY ESCAPE PATH LIGHTS WERE INOPERATIVE AT FORWARD & OVERWING AREA. MAINTENANCE REMOVED AND REPLACED LT & RT OVERWING EMERGENCY POWER SUPPLY UNITS (11WL & 12WL), REPAIRED DAMAGED WIRE AT SEAT ROW 6 LT, OPERATIONAL CHECK WASDec 17, 2003 · N824AW · Airbus A319132 · Light System WiringSDR AWXA200301464Cable · brokenPHX - EES - DURING P-09 CHECK THE CABLE END WAS FOUND BROKEN ON THE RT OVERWING SLIDE BOTTLE. MAINTENANCE REMOVED AND REPLACED RT OVERWING SLIDE RESERVOIR ASSEMBLY IAW AMM 25-62-46.Nov 2, 2003 · N824AW · Airbus A319132 · Escape SlideSDR AWXA200301463Cable · brokenPHX - EES - DURING P-09 CHECK THE CABLE END WAS FOUND BROKEN ON THE LT OVER WING SLIDE BOTTLE. MAINTENANCE REMOVED AND REPLACED LT OVERWING SLIDE RESERVOIR ASSEMBLY IAW AMM 25-62-46.Nov 2, 2003 · N824AW · Airbus A319132 · Escape SlideSDR AWXA200301121Pump · leakingEN ROUTE FROM IAD TO PHX FLIGHT CREW OBSERVED A LOSS OF THE GREEN SYSTEM HYDRAULICS, DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND THE PLUG ON TOP THE NR 1 ENGINE DRIVEN PUMP LEAKING. REMOVED AND REPLACED THE NR 1 ENGINE DRIVEN HYDRAULOct 1, 2003 · N824AW · Airbus A319132 · Hydraulic Pump (Electric/Engine), Main
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