N705UW

Service difficulty reports · 269

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 = 'N705UW' 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 USAA2012100400005Power Supply · inoperativeEMERGENCY LIGHTS INOPERATIVE AT FORWARD ENTRY, FORWARD GALLEY, AND FORWARD CABIN. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (10WL) PER AMM 33-51-38-044-001. OPS CHECKED GOOD.Oct 2, 2012 · N705UW · Airbus A319112 · Emergency LightingSDR USAA2012071100017Control Unit · faultyHYDRAULIC GREEN SYSTEM LOW PRESSURE FAULT. SYSTEM SHOWS 2950 PSI. BUT WE HAD AMBER ILLUMINATED ON GREEN SYSTEM. FLIGHT CONTROL PAGE SHOWED AMBER ON ALL GREEN ITEMS. BSCU-1 FAULT SHOWN. REMOVED AND REPLACED BSCU AS PER AMM 32-42-34-400-001-A , SYSTEM OPS CJul 8, 2012 · N705UW · Airbus A319112 · Landing Gear Brake SystemSDR USAA2012010900027Control Unit · faultyON LANDING GEAR RETRACTION AFTER TAKEOFF, LANDING GEAR REMAINED UNLOCKED. ECAM MESSAGE GENERATED AFTER APPROXIMATELY 3 MINUTES. LANDING GEAR RETRACTED. ECAM PROCEDURE HAD NOT YET BEEN ACCOMPLISHED. WHEN UNLOCKED, NOISE OF GEAR DOORS OPEN WAS HEARD. REMOVEJan 6, 2012 · N705UW · Airbus A319112 · Landing Gear Retraction/Extension SystemSDR USAA2011112800011Battery Pack · dischargedFORWARD LEFT EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER AMM 25-65-53. OPS CHECKED GOOD.Nov 22, 2011 · N705UW · Airbus A319112 · Emergency EquipmentSDR USAA2011060800005Wire · brokenFLT 2049 - BOS-DCA - EMERGENCY LIGHTS - SEAT 20 ABC HAS BROKEN WIRE AT CONNECTOR FOR EMERGENCY LIGHTNING. ACCOMPLISHED SERVICEABLE REPAIR PER ESPM 20-44-00. OPERATIONAL CHECK GOOD.Jun 7, 2011 · N705UW · Airbus A319112 · Light System WiringSDR USAA2010122093205Battery · dischargedDOOR R2 F/A FLASHLIGHT BATTERY BURNED OUT. R & R FLASHLIGHT BATTERY. OPS CHECK WAS GOOD.Dec 17, 2010 · N705UW · Airbus A319112 · Emergency EquipmentSDR USAA2010100792209Battery · dischargedFLT 1761 - BOS - EEL - AFT GALLEY EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY.Oct 13, 2010 · N705UW · Airbus A319112 · Emergency EquipmentSDR USAA2010020190247Stop Fitting · crackedPIT - S4 - MAJOR REPAIR - CRACK ON LEFT WING NR 3 SLAT NR 7 TRACK ANTI-ROTATION STOP OUTBOARD LUG. REPAIRED LEFT WING NR 3 SLAT NR 7 TRACK ANTI-ROTATION STOP IAW EA 114368.Jan 31, 2010 · N705UW · Airbus A319112 · Leading Edge DevicesSDR USAA2010012590185Floorbeam · corrodedPIT - S4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR23, Y1292. REPLACED FLOORBEAM AT FR23, Y1292 IAW A319 51-72-11.Jan 19, 2010 · N705UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2010011990142Floorbeam · corrodedLEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR20, -Y1292. REPLACED FLOORBEAM AT FR20, -Y1292 IAW A319 SRM 51-72-11.Jan 19, 2010 · N705UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2010011990141Floorbeam · corrodedLEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR 20 TO FR 21, -Y189. REPLACED FLOORBEAM BETWEEN FR 20 TO FR21, -Y189 IAW A319 SRM 51-72-11.Jan 17, 2010 · N705UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2010011990140Seat Track · corrodedLEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR 22, -Y765. REPLACED SEAT TRACK FLOORBEAM AT FR 22, -Y765 IAW A319 SRM 51-72-11.Jan 17, 2010 · N705UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2010011990143Seat Track · corrodedLEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR24, -Y1292. REPAIRED SEAT TRACK AT FR24, -Y1292 IAW A319 SRM 53-21-15.Jan 16, 2010 · N705UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2010012590186Floorbeam · corrodedPIT - S4 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM BETWEEN FR65 TO FR66, S23L, Y1732. REPLACED FLOORBEAM BETWEEN FR65 TO FR66, S23L, Y1732 IAW A319 SRM 51-72-11.Jan 14, 2010 · N705UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2010012090150Floorbeam · corrodedPIT - S4 - MAJOR REPAIR - NR 26C26053005/007 - LEVEL 2 CORROSION ON FLOORBEAM BETWEEN FR 65 TO FR 66, S23L, Y1732. REPLACED FLOORBEAM BETWEN FR 65 TO FR 66, S23L, Y1732 IAW A319 SRM 51-72-11.Jan 14, 2010 · N705UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2010012590184Floorbeam · corrodedPIT - S4 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM AT FR20, S23R, -Y254. REPAIRED FLOORBEAM AT FR20, S23R, -Y254 IAW A319 SRM 53-00-14.Jan 13, 2010 · N705UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2010011990137Floorbeam · corrodedLEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR 65 TO FR 69, Y1292. REPLACED FLOORBEAM BETWEEN FR 65 TO FR 69, Y1292 IAW A319 SRM 51-42-11.Jan 13, 2010 · N705UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2010011990136Floorbeam · corrodedLEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR 65 TO FR 69, Y1292. REPLACED FLOORBEAM BETWEEN FR 65 TO FR 69, Y1292 IAW A319 SRM 51-42-11.Jan 13, 2010 · N705UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2010020390271Floorbeam · corrodedPIT - S4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM SEGMENT BETWEEN FR66 TO FR68, & BETWEEN -Y1167 TO Y1292. REPLACED FLOORBEAM SEGMENT BETWEEN FR66 TO FR68, & BETWEEN -Y1167 TO Y1292 IAW A319 SRM 51-72-11 & 51-42-00.Jan 12, 2010 · N705UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2010011390096Floorbeam · corrodedPIT - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 TO FR67, -Y464. REPLACED FLOORBEAM BETWEEN FR66 TO FR67, -Y464 IAW A319 SRM 51-72-11.Jan 12, 2010 · N705UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2010011390095Floorbeam · corrodedPIT - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOOR BEAM BETWEEN FR66 TO FR67, Y512. REPLACED FLOORBEAM BETWEEN FR66 TO FR67, Y512 IAW A319 SRM 51-72-11.Jan 12, 2010 · N705UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2010011390092Floorbeam · corrodedPIT - S4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, -Y1292. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, -Y1292 IAW A319 SRM 51-72-11 & 51-42-00.Jan 12, 2010 · N705UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2010011990138Floorbeam · corrodedLEVEL 2 GALVANIC CORROSION ON R-2 DOOR SILL FLOORBEAM AT FR 66, S23R. REPLACED R-2 DOOR SILL FLOORBEAM AT FR 66, S23R IAW A319 SRM 53-41-14.Jan 11, 2010 · N705UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2010011990133Web · crackedSHEER WEB CRACKED BETWEEN FR 68 TO FR 69, -Y1162.5, S23R. REPLACED SHEER WEB BETWEEN FR 68 TO FR 69, -Y1162.5, S23R IAW A319 SRM 51-42-11.Jan 11, 2010 · N705UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2010011390097Web · corrodedPIT - S4 - MAJOR REPAIR - CORROSION ON SHEAR WEB BETWEEN FR68 TO FR69, -Y1162.5, S23L. REPAIRED SHEAR WEB BETWEEN FR68 TO FR69, -Y1162.5, S23L IAW A319 SRM 51-42-11.Jan 11, 2010 · N705UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2010011390094Beam · corrodedPIT - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SILL BEAM AT FR66, S23R. REPLACED SILL BEAM AT FR66, S23R IAW A319 SRM 53-41-14.Jan 11, 2010 · N705UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2010011290081Floor Panel · damagedCLT - S4 - MAJOR REPAIR - UPPER SURFACE OF CENTER CABIN FLOOR PANEL 232LF DAMAGED. REPLACED CENTER CABIN FLOOR PANEL 232LF.Jan 9, 2010 · N705UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2010010890055Floorbeam · corrodedPIT - S4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR20 TO FR21, Y254. REPLACED FLOORBEAM BETWEEN FR20 TO FR21, Y254 IAW A319 SRM 51-42-11.Jan 8, 2010 · N705UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2010011290082Skin · debondedCLT - S4 - MAJOR REPAIR - AREA DISBONDED ON RIGHT WING AILERON OUTBOARD LOWER SKIN AT TRAILING EDGE WEDGE. REPAIRED RIGHT WING AILERON OUTBOARD LOWER SKIN AT TRAILING EDGE WEDGE IAW A319 SRM 57-61-21.Jan 7, 2010 · N705UW · Airbus A319112 · AileronsSDR USAA2010011990134Plate · corrodedLEVEL 2 FILIFORM CORROSION ON SHEER PLATE BETWEEN FR 69 TO FR 70, -Y1162.5, S23R. REPLACED SHEER PLATE BETWEEN FR 69 TO FR 70, -Y1162.5, S23R IAW A319 SRM 51-22-00.Jan 6, 2010 · N705UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2010011390098Shear Plate · corrodedPIT - S4 - MAJOR REPAIR - LEVEL 2 FILIFORM CORROSION ON SHEER PLATE BETWEEN FR69 TO FR70, -Y1162.5. REPLACED SHEER PLATE BETWEEN FR69 TO FR70, -Y1162.5 IAW A319 SRM 51-22-00.Jan 6, 2010 · N705UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2010011190072Shear Plate · corrodedPIT - S2 - MAJOR REPAIR - LEVEL 2 FILIFORM CORROSION ON SHEAR PLATE AT FR70 RIGHT SIDE. REPLACED SHEAR PLATE AT FR70 RIGHT SIDE IAW A319 SRM 51-22-00.Jan 6, 2010 · N705UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2010011990135Floorbeam · corrodedLEVEL 2 CORROSION ON FLOORBEAM AT FR 16, Y505, S23L. REPLACED FLOORBEAM AT FR16, Y505, S23L IAW A319 SRM 51-72-11.Jan 3, 2010 · N705UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2009122493425Lens · missingFLT 880 - PHL-BOS - EMERGENCY LIGHTS - EXIT COVER LENS BY 2L DOOR MISSING. REPLACED EXIT COVER LENS AT 2L DOOR.Dec 22, 2009 · N705UW · Airbus A319112 · Emergency LightingSDR USAA2009111993170Battery · dischargedFLT 1692 - CLT - EEL - FORWARD GALLEY FLASHLIGHT NOT BLINKING. MAINTENANCE INSTALLED NEW BATTERY.Nov 18, 2009 · N705UW · Airbus A319112 · Emergency EquipmentSDR USAA2008112892155Windshield · crackedFLT 1660 - CLT-BNA - AIR TURNBACK - CAPTAIN WINDSHIELD ARCED AND THEN CRACKED SHORTLY AFTER TAKEOFF. WINDSHIELD SHATTERED IMMEDIATELY. REPLACED CAPTAIN WINDSHIELD. OPERATIONAL CHECK WAS GOOD.Nov 26, 2008 · N705UW · Airbus A319112 · Flight Compartment WindowsSDR SA07020Pin · bentDCA - THE TEST OF THE EMERGENCY EXIT LIGHT SYSTEM FAILED, FAULTING EPSU EXT LOAD L ON THE FORWARD CIDS PANEL. MAINTENANCE REPLACED THE AFT LEFT EMERGENCY POWER SUPPLY BATTERY, WHICH DID NOT FIX THE PROBLEM. THE AIRCRAFT WAS RELEASED ON MEL. SUBSEQUENTLY, MAMar 3, 2007 · N705UW · Airbus A319112 · Light System WiringSDR SA05036Window · crackedSAN - FLT 91 - EN-ROUTE PHL - SAN, THE RIGHT REAR COCKPIT WINDOW CRACKED DURING FLIGHT. THE AIRCRAFT CONTINUED TO SAN AND LANDED WITHOUT FURTHER INCIDENT.Mar 29, 2005 · N705UW · Airbus A319112 · Flight Compartment WindowsSDR USAA040094Floor Panel · corrodedBFM - FOUND FLOOR PANEL CORRODED 3 INCHES LONG BY 2 INCHES WIDE BY .02 INCH DEEP, MAIN DECK FLOOR PANEL 262FF. REMOVED AND REPLACED FLOOR PANEL PER SRM 51-72-11 AND 51-42-11. (M)Apr 1, 2004 · N705UW · Airbus A319112 · Fuselage Floor PanelSDR USAA040093Floor Panel · corrodedBFM - FOUND FLOOR PANEL CORRODED 5 INCHES LONG BY 3 INCHES WIDE BY .02 INCH DEEP AREA, MAIN CABIN 261FF. REMOVED AND REPLACED FLOOR PANEL PER SRM 51-72-11 AND 51-42-11. (M)Apr 1, 2004 · N705UW · Airbus A319112 · Fuselage Floor PanelSDR USAA040114Angle · crackedMAIN DECK SEAL ANGLES AT PNL 262GF AND 262EG CRACKED AT WELDS. REMOVED AND REPLACED SEAL ANGLES PER SRM 51-72-11 AND 51-42-11. (M)Apr 1, 2004 · N705UW · Airbus A319112 · Fuselage Floor PanelSDR USAA040086Plate · corrodedBFM - FOUND PLATE ASSEMBLY CORRODED 5 INCHES BY 1.6 INCHES BY .020 INCH AREA, FRAME 20, -Z240, -Y765. REMOVED AND REPLACED PLATE ASSEMBLY PER SRM 53-11-14 AND 51-72-11. CORROSION LEVEL 2, TASK NR JA-220-53500. (M)Mar 31, 2004 · N705UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040091Floor Panel · corrodedBFM - FOUND FLOOR PANEL CORRODED 1 INCH WIDE BY .015 DEEP ENTIRE LENGTH, MAIN CABIN, PNI 222FF. REPLACED WITH NEW PANEL PER SRM 51-72-11. (M)Mar 31, 2004 · N705UW · Airbus A319112 · Fuselage Floor PanelSDR USAA040090Floorbeam · corrodedBFM - FOUND BEAM CORRODED 1 INCH BY 1 INCH BY .039 INCH DEEP, FRAME 68, Y1162, -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)Mar 31, 2004 · N705UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA040092Floor Panel · corrodedBFM - FOUND FLOOR PANEL CORRODED 1 INCH BY 1 INCH WIDE BY .02 INCHES DEEP AREA, MAIN CABIN, PANEL 221FF. REPLACED WITH NEW PANEL PER SRM 51-72-11. (M)Mar 31, 2004 · N705UW · Airbus A319112 · Fuselage Floor PanelSDR USAA040088Floorbeam · corrodedBFM - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH BY .02 AND .03, TWO AREAS, FS 66-68, Y1292, -Z240. REMOVED AND REPLACED FLOORBEAM PER SRM 53-00-14, 51-74-00 AND 51-42-11. REMOVED AND REPLACED BEAM PER SRM 53-00-14, 51-74-00 AND 51-42-11. CORROSION LEVEL 2, Mar 31, 2004 · N705UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA040087Floorbeam · corrodedBFM - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH BY .048D AREA, FRAME 68 Y 1292 -Z240. REMOVED AND REPLACED FLOORBEAM PER SRM 51-74-00, 53-00-14 AND 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)Mar 31, 2004 · N705UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA040089Sill · corrodedBFM - FOUND SILL CORRODED .110 INCH BY .190 INCH BY .070 INCH DEEP, FRAME 68, Y1420, -Z240. REMOVED AND REPLACED SILL PER SRM 51-41-14. CORRODED LEVEL 2, TASK NR JA 260-53500. (M)Mar 30, 2004 · N705UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040085Sill · corrodedBFM - FOUND SILL CORRODED 2 INCHES BY 1.3 INCHES BY .070 INCH DEEP, FRAME 66, Y 1502, -Z240. REMOVED AND REPLACED SILL PER SRM 53-41-14. CORROSION LEVEL 2, TASK NR JA 260-53500. (M)Mar 30, 2004 · N705UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040083Floorbeam · corrodedBFM - FOUND FLOORBEAM CORRODED 3 INCHES BY 1 INCH BY .050 INCH AREA, FRAME 68-69, -Y1210, -Z2240. REMOVED AND REPLACED FLOORBEAM PER SRM 53-00-14, 51-74-00, 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)Mar 30, 2004 · N705UW · Airbus A319112 · Fuselage Main, Floor Beam
Back to N705UW