N747UW

Service difficulty reports · 195

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 = 'N747UW' 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 USAA2012010400013Floorbeam · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR67, Z-500, -Y1225. REPLACED FLOORBEAM BETWEEN FR66 TO FR67, Z-500, -Y1225 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472780.Jan 3, 2012 · N747UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012010400012Floorbeam · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR20, Z-500, -Y765. REPLACED FLOORBEAM AT FR20, Z-500, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D5311278220201.Jan 3, 2012 · N747UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012010400011Floorbeam · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, Z-500, Y1292. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, Z-500, Y1292 IAW A319 SRM 51-72-11.Jan 3, 2012 · N747UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012010400010Floorbeam · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, Z-500, Y1162. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, Z-500, Y1162 IAW A319 SRM 51-72-11 & AIRBUS DRAWING 10D534744250.Jan 3, 2012 · N747UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012010400009Floorbeam · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR69, Z-500, Y1225. REPLACED FLOORBEAM BETWEEN FR66 TO FR69, Z-500, Y1225 IAW A319 SRM 51-72-11.Jan 3, 2012 · N747UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012010400007Floorbeam · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR68, -Y1162. REPLACED FLOORBEAM AT FR68, -Y1162 IAW A319 SRM 53-41-15.Jan 3, 2012 · N747UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012010400006Floorbeam · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR BEAM AT FR64, -Y1225. REPLACED FLOORBEAM AT FR64, -Y1225 IAW A319 SRM 53-41-15.Jan 3, 2012 · N747UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012010400005Floorbeam · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR66, -Y1292. REPLACED FLOORBEAM AT FR66, -Y1292 IAW A319 SRM 51-42-11.Jan 3, 2012 · N747UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012010400004Floorbeam · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, Y765 IAW A319 SRM 53-41-15.Jan 3, 2012 · N747UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012010400003Floorbeam · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR68, Y765. REPLACED FLOORBEAM AT FR68, Y765 IAW A319 SRM 53-41-15.Jan 3, 2012 · N747UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012010400002Floorbeam · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR66, Y765. REPLACED FLOOR BEAM AT FR66, Y765 IAW A319 SRM 53-41-15.Jan 3, 2012 · N747UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012010400001Floorbeam · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR64, Y765. REPLACED FLOORBEAM AT FR64, Y765 IAW A319 SRM 53-41-15.Jan 3, 2012 · N747UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012010600021Shear Plate · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, Z-500, -Y1162.5. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, Z-500, -Y1162.5 IAW A319 SRM 51-72-11 & TYPICAL REPAIR TR320-2528-10-0011.Jan 2, 2012 · N747UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012010300007Floorbeam · corrodedS2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR66, Z-500, -Y466. REPLACED FLOORBEAM AT FR66, Z-500, -Y466 IAW A319 SRM 53-41-14.Dec 30, 2011 · N747UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012010300006Floorbeam · corrodedS2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR66, Z-500, -Y464.8. REPLACED FLOORBEAM AT FR66, Z-500, -Y464.8 IAW A319 SRM 53-41-14.Dec 30, 2011 · N747UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012010300005Floorbeam · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR66, -Y464.8, -Z500.REPLACED FLOORBEAM AT FR66, -Y464.8, -Z500 IAW A319 SRM 53-41-14.Dec 30, 2011 · N747UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012010300004Floorbeam · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR68, -Y464, -Z500. REPLACED FLOORBEAM AT FR68, -Y464, -Z500 IAW A319 SRM 53-41-14.Dec 30, 2011 · N747UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012010300003Sill · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON SILL PLATE AT L2 DOOR BETWEEN FR66 TO FR68, -Y1589, -Z500. REPLACED SILL PLATE AT L2 DOOR BETWEEN FR66 TO FR68, -Y1589, -Z500 IAW A319 SRM 51-72-11.Dec 30, 2011 · N747UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011123000006Door Frame · crackedS2 CHECK - CRACKS AT LEFT EMERGENCY EXIT DOOR 834 AT FRAME FORWARD SEGMENT. REPLACED FRAME FORWARD SEGMENT AT LEFT EMERGENCY EXIT DOOR 834 IAW EO 5210Y228.Dec 29, 2011 · N747UW · Airbus A319112 · Emergency ExitsSDR USAA2012012500020Panel · galledS2 CHECK - GALLING CLEAN-UP ON LEFT WING FUEL PANEL 540HB EXCEEDS MAXIMUM DIAMETER .3465 INCHES. REPLACED LEFT WING FUEL PANEL 540HB IAW A319 SRM 57-27-11.Dec 28, 2011 · N747UW · Airbus A319112 · Wing, Plate/SkinSDR USAA2012012500019Panel · galledS2 CHECK - GALLING CLEAN-UP ON LEFT WING FUEL PANEL 540JB EXCEEDS MAXIMUM DIAMETER .3465 INCHES. REPLACED LEFT WING FUEL PANEL 540JB IAW A319 SRM 57-27-11.Dec 28, 2011 · N747UW · Airbus A319112 · Wing, Plate/SkinSDR USAA2012012500018Panel · galledS2 CHECK - GALLING CLEAN-UP ON LEFT WING FUEL PANEL 540LB EXCEEDS MAXIMUM DIAMETER .3465 INCHES. REPLACED LEFT WING FUEL PANEL 540LB IAW A319 SRM 57-27-11.Dec 28, 2011 · N747UW · Airbus A319112 · Wing, Plate/SkinSDR USAA2011122900005Floor Support · corrodedS2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON AFT CARGO FLOOR SUPPORT BETWEEN FR53 TO FR54, S38L. REPLACED AFT CARGO FLOOR SUPPORT BETWEEN FR53 TO FR54, S38L IAW A319 SRM 51-72-11.Dec 23, 2011 · N747UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012011700006Skin · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FUSELAGE SKIN BETWEEN FR63 TO FR64, S41L. REPAIRED FUSELAGE SKIN BETWEEN FR63 TO FR64, S41L IAW EA 201629.Dec 22, 2011 · N747UW · Airbus A319112 · Fuselage Main, Plate/SkinSDR USAA2011053100006Fan · defectivePHL - BURNING SMELL - ECAM VENT EXTRACT FAULT - EXTRACT TO OVERRIDE - FAINT ELECTRICAL BURNING SMELL IN COCKPIT AND CABIN THAT CONTINUED FOR REMAINDER OF FLIGHT AND TAXI IN. MAINTENANCE REMOVED & REPLACED EXTRACT FAN IAW AIRBUS MAINTENANCE MANUAL 21-26-51-000May 27, 2011 · N747UW · Airbus A319112 · Air Distribution FanSDR USAA2011032291176Lens · missingFLT 1468 - BDL - EEL - RED LENS MISSING FROM WALL MOUNTED EMERGENCY LIGHT AT AFT LEFT LAV. MAINTENANCE REPLACED LENS IAW AIRBUS MAINTENANCE MANUAL 33-51-18-400-001.Mar 19, 2011 · N747UW · Airbus A319112 · Emergency LightingSDR USAA2010042890851Support Fitting · crackedPIT - TRIPLE GEAR CHANGE - MAJOR REPAIR - CRACK ON LEFT WING LEFT RIB 5 MAIN LANDING GEAR SUPPORT FITTING. REPLACED LEFT WING LEFT RIB 5 MAIN LANDING GEAR SUPPORT FITTING IAW EA 114913.Apr 21, 2010 · N747UW · Airbus A319112 · Wing, Landing Gear Attach FittingsSDR USAA2010042890850Stiffener · crackedPIT - TRIPLE GEAR CHANGE - MAJOR REPAIR - CRACK ON STIFFENER AT LEFT WING BETWEEN RIB 5 & 6 AFT OF AFT SPAR. REPLACED STIFFENER AT LEFT WING BETWEEN RIB 5 & 6 AFT OF AFT SPAR IAW A319 SRM 51-42-11.Apr 20, 2010 · N747UW · Airbus A319112 · Wing Miscellaneous StructureSDR USAA2010042190807Stiffener · crackedPIT - GEAR CHANGE - MAJOR REPAIR - CRACK ON LEFT WING STIFFENER BETWEEN WING RIB 5 TO RIB 6. REPLACED LEFT WING STIFFENER BETWEEN WING RIB 5 TO RIB 6 IAW A319 SRM 51-42-11.Apr 20, 2010 · N747UW · Airbus A319112 · Wing Miscellaneous StructureSDR USAA2010021290356Megaphone · unserviceableFLT 2178 - LGA-DCA - EMERGENCY EQUIPMENT - AFT MEGAPHONE MAINTENANCE DATE EXPIRED. REMOVED AND REPLACED AFT MEGAPHONE. OPERATIONAL CHECK WAS GOOD.Feb 11, 2010 · N747UW · Airbus A319112 · Emergency EquipmentSDR USAA2010011590114Battery · dischargedFLT NR 1869 - EMERGENCY EQUIPMENT - FLASHLIGHT FORWARD FLIGHT ATTENDANT STATION INOPERATIVE. REMOVED AND REPLACED BATTERY AND STRAP. OPERATIONAL CHECK WAS GOOD.Jan 14, 2010 · N747UW · Airbus A319112 · Emergency EquipmentSDR USAA2009110693049Connector · damagedRON - CLT - EEL - FLIGHT ATTENDANT PANEL EMERGENCY POWER SUPPLY UNIT 'INT LOAD EMER L' FAULTS. EMERGENCY LIGHTING SYSTEM WILL NOT TEST. FOUND HIGH RESISTANCE BATTERY CONNECTION AT EPSU. MAINTENANCE REPAIRED CONNECTION AND ACCOMPLISHED SATISFACTORY OPERATIONNov 5, 2009 · N747UW · Airbus A319112 · Light System WiringSDR USAA2009043091041Proximity Switch · out of adjustFLT 1724 - TPA-DCA - EMERGENCY EQUIPMENT - 2L SLIDE SHOWED DISARM WARNING ON CIDS PANEL. REMOVED DEBRIS FROM AFT GIRT BAR FLOOR FITTING AND VERIFIED ADJUSTMENT OF PROXIMITY SWITCH 7WN1 (L2 SLIDE ARMING SENSOR) PER MAINTENANCE MANUAL TASK 52-71-00-05-820-002. Apr 29, 2009 · N747UW · Airbus A319112 · Door Warning SystemSDR USAA2009011690088Torque Link · corrodedPIT- C11 - MAJOR REPAIR - NR 5031290 - PITTING CORROSION IN BORE OF LT MLG UPPER TORQUE LINK. REPLACED LT MLG UPPER TORQUE LINK IAW TASK CARD NR 26C73032002.Jan 7, 2009 · N747UW · Airbus A319112 · Landing Gear Retraction/Extension SystemSDR USAA920081435Battery Pack · malfunctionedFLT 1137 PHL-DFW - EEL - FLIGHT ATTENDANT REPORTED THAT THE CABIN EMERGENCY LIGHTS WERE FLASHING ON AND OFF DURING DESCENT AND LANDING. MAINTENANCE PERFORMED A BITE TEST WHICH FAULTED THE LT AND RT BATTERY PACKS. RESET BATTERY PACKS. OPERATIONAL CHECKS WEREJul 29, 2008 · N747UW · Airbus A319112 · Emergency LightingSDR SA07030Epsu · dischargedTPA - THE EMERGENCY LIGHT AT SEAT 18A WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.May 18, 2007 · N747UW · Airbus A319112 · Emergency LightingSDR USAA060393Seat Track · corrodedFOUND RAIL Y-1292 AT FS 20 CORROSION NOTED. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11; CORR TASK JA-220-53500, DEFECT SIZE: 0.5".Mar 2, 2006 · N747UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA060394Seat Track · corrodedFOUND RAIL Y-81 FS 17 CORROSION NOTED; CORR TASK JA-220-53500. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11, DEFECT SIZE: 0.5" DIA.Mar 2, 2006 · N747UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA060391Floorbeam · corrodedTOP SIDE OF FLOORBEAM Y254 AT FR 17 CORRODED. INSTALLED FILLER PER SRM 53-00-14; CORROSION LEVEL 1; TASK JA-220-53500, DEFECT SIZE: 1 X 1 INCH.Mar 2, 2006 · N747UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA060392Floorbeam · corrodedTOP FLANGE OF FLOORBEAM AT Y - 254 FRAME 19; CORROSION TASK JA-220-53500. CUT OUT DAMAGED AREA, MANUFACTURED NEW FILLER AND ANGLE & INSTALLED PER SRM 53-00-14, DEFECT SIZE: .25 X .5 INCH.Mar 2, 2006 · N747UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA060395Beam · corrodedFRAME C-66 - C-70; CORROSION TASK JA-260-53100. REMOVED & REPLACED PER DWG D53480009, DEFECT SIZE: 4IN X 6FT.Mar 2, 2006 · N747UW · Airbus A319112 · Fuselage Main, StructureSDR USAA060396Floorbeam · corrodedFOUND FLOORBEAM CORRODED. REMOVED AND REPLACED PER DWG, 53480009, DEFECT SIZE: 4" X 8'.Mar 2, 2006 · N747UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA060370Floorbeam · corrodedFLOORBEAM AT Y303.2, FR 12-14; CORROSION LEVEL 1; TASK JA-160-53500. REMOVED AND REPLACED FLOORBEAM PER SRM 51-72-11.Feb 27, 2006 · N747UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAASA02013Smoke · detectedCLT - FLT 53 - EN ROUTE CLT-JAX - AFTER TAKEOFF, THICK SMOKE FILLED THE CABIN, BUT NOT THE COCKPIT. FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIR CONDITIONING PACKS AND RAN THE ENGINES AT VARIOUS POWER SETTINGS. NO SMOKE Jan 19, 2002 · N747UW · Airbus A319112 · Air Distribution SystemSDR USAASA02009Cable Fitting · brokenDCA - THE LEFT OVERWING SLIDE INFLATION BOTTLE SIDE CABLE END WAS FOUND BROKEN. MAINTENANCE INSTALLED A NEW INFLATION BOTTLE ASSEMBLY AND CABLE END. OK FOR SERVICE. (M)Jan 16, 2001 · N747UW · Airbus A319112 · Escape Slide
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