N710UW

Service difficulty reports · 295

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 = 'N710UW' 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 USAA2010071991443Shear Plate · corrodedPIT - MAJOR REPAIR - S4 - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR 69-70, STR 23R. REPLACED SHEAR PLATE BETWEEN FR 69-70, STR 23R IAW A319 SRM 51-72-11-51-42-11.Jun 4, 2010 · N710UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2010071591425Seat Track · corrodedPIT - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR20, -Y1292. REPLACED SEAT TRACK AT FR20, -Y1292 IAW A319 SRM 51-42-11.Jun 4, 2010 · N710UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2010070891372Seat Track · corrodedPIT - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR20, -Y765. REPLACED SEAT TRACK AT FR20, -Y765 IAW A319 SRM 53-11-14.Jun 4, 2010 · N710UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2010070791362Shear Plate · corrodedPIT - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23R. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23R IAW A319 SRM 51-72-11 & 51-42-11.Jun 4, 2010 · N710UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2010070791361Shear Plate · corrodedPIT - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23L. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23L IAW A319 SRM 51-72-11 & 51-42-11.Jun 4, 2010 · N710UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2010070191315Sill · corrodedPIT - S4 - MAJOR REPAIR - LEVEL 2 CORROSION ON SILL PLATE BETWEEN FR66 TO FR68, -Y1162. REPLACED SILL PLATE BETWEEN FR66 TO FR68, -Y1162 IAW AIRBUS DRAWING D53448009.Jun 4, 2010 · N710UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2010062991304Angle · corrodedPIT - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON ANGLE AT FR16, Y50. REPLACED ANGLE AT FR16, Y50 IAW A319 SRM 51-75-12.Jun 4, 2010 · N710UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA920082018Connector · disconnectedLOGPAGE 8309802 FLT NR 954 FLL-PHL EMERGENCY EXIT SIGN OVER L2 DOOR INOPERATIVE. FOUND CANNON PLUG DISCONNECTED. RECONNECTED CONNECTOR. OPS CHECK WAS GOOD.Nov 7, 2008 · N710UW · Airbus A319112 · Light System WiringSDR USAA920081468Wire Harness · misroutedPIT-DROP-IN-EEL - L-1 DOOR SLIDE EMERGENCY WIRE HARNESS IMPROPERLY ROUTED. CORRECTED WIRE HARNESS ROUTING. (S)Jul 2, 2008 · N710UW · Airbus A319112 · Escape SlideSDR USAA920081443Survival Kit · out of positionPIT - DROP IN -EES - L2 DOOR SURVIVAL KIT LANYARD VELCRO PULLED APART AND DROPPED OUT OF TRIGGER ASSY. REROUTED LANYARD VELCRO END THRU TRIGGER ASSY PER - (JOB CARD JA-25-62-02). (A)Jul 2, 2008 · N710UW · Airbus A319112 · Emergency EquipmentSDR USAA920081311Stud · brokenPIT - NR 2 ENG - EMERGENCY EQUIPMENT - MOUNT STUD ASSEMBLY FOR SLIDE RAFT WIRE END BROKE OFF CAUSING STREAMER PULL HANDLE TO COME LOOSE ON THE L1 DOOR. REPLACED MOUNT STUD ASSEMBLY FOR SLIDE RAFT L-1 DOOR IAW TASK CARD 26L0025011 AND JA-900-09000-016. (S)Jul 2, 2008 · N710UW · Airbus A319112 · Escape SlideSDR USAA040315Plate · corrodedBFM - FOUND PLATE CORRODED .075 INCH BY .050 INCH BY .040 INCH DEEP, FS 16, Y1970, -Z40. REMOVED AND REPLACED PLATE ASSEMBLY. (M)Jun 8, 2004 · N710UW · Airbus A319112 · Fuselage Main, Plate/SkinSDR USAA040268Seat Track · corrodedBFM - FOUND TRACK CORRODED .150 INCH BY .045 INCH BY .025 INCH AREA, SEAT TRACK, FRAME 23,Y-1292. REMOVED AND REPLACED TRACK PER SRM 53-00-15. CORROSION LEVEL 2, TASK NR JA-220-53500. (M)Jun 8, 2004 · N710UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA040284Floor Panel · delaminatedFLOOR PANEL, GREATER THAN 10 PERCENT OF AREA, DELAMINATION, MAIN DELAMINATION, MAIN DECK FLOOR PANEL, 221PF. FABRICATED NEW PANEL IAW SRM.Jun 8, 2004 · N710UW · Airbus A319112 · Fuselage Floor PanelSDR USAA040269Plate · corrodedPLATE ASSY, 6 INCHES X 4 INCHES X 0.060 INCH DEEP, CORROSION; LEVEL 2; FR68, Y1732, Z240. REPLACED WITH NEW PART IAW SRM.Jun 8, 2004 · N710UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040313Sill · corrodedBFM - FOUND SILL ASSEMBLY CORRODED 1 INCH BY .8 INCH BY .061 INCH AREA, FRAME 66, -Y1732, -Z240. INSTALLED NEW ILL ASSEMLBY PER SRM 53-41-14, PAGE 103 FIG 101. (M0Jun 7, 2004 · N710UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040283Floor Panel · delaminatedBFM - FOUND FLOOR PANEL DELAMINATED MORE THAN 10 PERCENT MAIN DECK FLOOR PANEL, 231 CF. FABRICATED NEW PANEL PER SRM 53-02-00, FIG 209. (M)Jun 4, 2004 · N710UW · Airbus A319112 · Fuselage Floor PanelSDR USAA040261Floorbeam · corrodedBFM - FOUND BEAM CORRODED 1 INCH BY 1 INCH BY .032 INCH DEEP, FS 66, Y765, Z240. REMOVED AND REPLACED BEAM PER SRM 53-00-14. CORROSION LEVEL 2, TASK NR JA 260 53500. (M)Jun 4, 2004 · N710UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA040314Plate · corrodedBFM - FOUND PLATE ASSEMBLY CORRODED 1 INCH LONG BY .075 INCH WIDE BY .040 INCH DEEP AREA, L7 DOOR 9R, -Z240, FRAME 68. REMOVED AND REPLACED PARTS PER SRM 51-72-11. (M)Jun 3, 2004 · N710UW · Airbus A319112 · Fuselage Main, Plate/SkinSDR USAA040277Floor Support · corrodedBFM - FOUND FLOOR SUPPORT RAIL CORRODED 1.4 INCH LONG BY .098 INCH WIDE BY .023 INCH DEEP, FRAME 64-66, -Y1292. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-74-00, 53-00-14, 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. DEFECTIVE PART REPLACEDJun 3, 2004 · N710UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040274Floor Support · corrodedBFM - FOUND FLOOR SUPPORT FRAME CORRODED, 2 INCHES LONG BY .900 INCH WIDE BY.032 INCH DEEP, FRAME 66-68, -Y1192 TO -Y1292, -Z240. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-14. CORROSION LEVEL 2, TASK NR JA-260-5300. (M)Jun 3, 2004 · N710UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040275Floor Support · corrodedBFM - FOUND FLOOR SUPPORT RAIL CORRODED 1.60 INCH BY .900 INCH WIDE BY .023 INCH DEEP, FRAME 68-69, -Y1192, -Z240. REMOVED AND REPLACED BEAM PER SRM 53-00-14. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)Jun 3, 2004 · N710UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040312Seat Track · corrodedBFM - FOUND SEAT TRACK CORRODED .135 INCH LONG BY .060 INCH WIDE BY .017 INCH DEEP AREA, BETWEEN FRAME 21 AND 23, BL Y-965, -Z240. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-15 FIG 101. (M)Jun 2, 2004 · N710UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA040271Seat Track · corrodedBFM - FOUND TRACK CORRODED .85 INCH BY .75 INCH BY .36 INCH DEEP, MAIN DECK FLOOR SUPPORT, FRAME 16, Y 1292. REMOVED AND REPLACED TRACKS PER SRM 53-11-14. CORROSION LEVEL 2, TASK NR JA-220-53500. (M)Jun 2, 2004 · N710UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA040276Seat Track · corrodedBFM - FOUND BEAM ASSEMBLY SEAT TRACK 2 INCHES BY 1.6 INCH BY .070 IND DEEP AREA, FRAME 64-66, -Y765, -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11, 51-21-11, 51-23-11. (M)Jun 2, 2004 · N710UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA040267Web · crackedBFM - FOUND WEB CRACKED 5 INCHES BY .0003 INCH BY .063 INCH, FS 68-59, Y 1192, -Z240. REPLACED WITH NEW PART PER SRM 51-72-11, PAGE 1, 51-42-11, 51-44-11. (M)Jun 2, 2004 · N710UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040272Web · corrodedBFM - FOUND WEB CORRODED 2.2 INCHES BY 1.7 INCHES BY .45 INCH AND 1.4 INCH BY 1.65 INCH BY .04 INCH, MAIN DECK FLOOR WEB AFT LEFT CORNER FRAME 69-70, Y1192-Y1292. REMOVED AND REPLACED WEB PER SRM 53-41-17. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)Jun 2, 2004 · N710UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040263Floorbeam · corrodedBFM - FOUND FLOORBEAM CORRODED 1.5 INCH BY 1 INCH BY .075 INCH AREA, FS 66-68M Y1192 TO Y1292, -Z240. REPLACED FLOORBEAM PER SRM 53-00-14. CORRODED LEVEL 2, TASK NR JA-160-53500. (M)Jun 1, 2004 · N710UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA040273Web · corrodedBFM - FOUND WEB CRACKED 2.5 INCHES BY 1.35 INCH BY .040 INCH, AFT OF FRME 69, -Y1192, -Y1292. REPLACED WEB PER SRM 51-41-17. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)Jun 1, 2004 · N710UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040270Floor Support · corrodedBFM - FOUND FLOOR SUPPORT CORRODED 2 INCHES BY 1.5 INCH BY .060 INCH DEEP, FRAME 68-69, Y1192, -Z240. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 53-00-14. CORROSION LEVEL 2, TASK NR JA-260-535. (M)Jun 1, 2004 · N710UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040264Floor Support · corrodedFLOOR SUPPORT/ RAIL, 2.25 INCH X 1.0 INCH X .088 INCH D, CORROSION; LEVEL 2; MAIN DECK, FRAME 68 AT +765. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM.Jun 1, 2004 · N710UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040265Beam · corrodedBFM - FOUND BEAM CORRODED 2 INCHES BY 1 INCH BY .068 INCH AREA, FLOOR SUPPORT, FRAME 64-66, Y1292, -Z240. REMOVED AND REPLACED BEAM PER SRM 53-00-15. (M)May 30, 2004 · N710UW · Airbus A319112 · Fuselage Main, StructureSDR USAA040266Seat Track · corrodedBFM - FOUND SEAT TRACK CORRODED .750 INCH LONG BY .600 INCH WIDE BY .077 INCH DEEP, SEAT TRACK FRAME 16 AT Y + 765, -Z240. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-42-11, SRM 53-11-14. CORROSION LEVEL 2, TASK NR JA-220-53500. (M)May 29, 2004 · N710UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA040262Beam · corrodedBFM - FOUND BEAM CORRODED 4.8 INCH LONG BY 1.8 INCH WIDE BY .051 INCH DEEP, Z240 BETWEEN FS 13 AND FS 18 BL +Y503.2. INSTALLED NEW BEAM PER SRM 53-11-14, FIG 103. (M)May 28, 2004 · N710UW · Airbus A319112 · Fuselage Main, StructureSDR USAASA04050Lanyard · missingTHE ESCAPE SLIDE RELEASE LANYARD AND SURVIVAL KIT LANYARD WERE FOUND NOT INSTALLED, ON THE SLIDE IN THE L1 DOOR POSITION, WHEN SLIDE WAS REMOVED FOR ACCESS DURING THE HEAVY MAINTENANCE VISIT. MAINTENANCE REPLACED THE SLIDE ASSEMBLY. OK FOR SERVICE. THE SHOP May 25, 2004 · N710UW · Airbus A319112 · Escape SlideSDR USAASA04060Lanyard · misroutedBFM - THE FORWARD RIGHT SERVICE DOOR, AFT LEFT ENTRY DOOR, AND THE AFT RIGHT SERVICE DOOR ESCAPE SLIDES SURVIVAL KIT LANYARDS WERE FOUND ROUTED INCORRECTLY WHEN THE SLIDES WERE REMOVED FROM THE AIRCRAFT FOR HEAVY MAINTENANCE. MAINTENANCE CORRECTLY ROUTED THE May 25, 2004 · N710UW · Airbus A319112 · Escape SlideSDR USA2004F00060Lanyard · missingTHE ESCAPE SLIDE RELEASE LANYARD WAS FOUND NOT INSTALLED WHEN SLIDE WAS REMOVED FOR ACESS DURING THE HEAVY MAINTENANCE VISIT. MAINTENANCE ACTION PENDING.May 25, 2004 · N710UW · Airbus A319112 · Escape SlideSDR USA2004F00034Odor · detectedENROUTE, DURING DESCENT, THE CABIN CREW REPORTED A PUNGENT ODOR IN THE CABIN. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE CABIN, CARGO, AND AVIONICS COMPARTMENTS. NO ABNORMALITIES FOUND. OK FOR SERVICE.May 8, 2004 · N710UW · Airbus A319112 · Air Distribution SystemSDR USAASA03052Slide · malfunctionedTHE LT FORWARD ENTRY DOOR SLIDE WILL NOT ARM. THE ARMING LEVER SPRINGS BACKUP AFTER ARMING. MAINTENANCE REMOVED, INSPECTED, THEN INSTALLED THE SAME SLIDE BACK ONTO THE LEFT FORWARD ENTRY DOOR. NO DEFECTS WERE NOTED. THE GIRT BAR AREA AT DOOR FRAME CORNERS May 24, 2003 · N710UW · Airbus A319112 · Escape SlideSDR USAASA03051Slide · dislodgedTHE FORWARD LEFT ENTRY DOOR ESCAPE SLIDE/RAFT WAS FOUND SEPARATING FROM THE MOUNTING. MAINTENANCE REPLACED THE ESCAPE SLIDE. OK FOR SERVICE. THE REPAIR SHOP FOUND THAT THE SLIDE REQUIRED REPACKING. THE SLIDE WAS REPACKED AND RETURNED TO SERVICE. (M)May 24, 2003 · N710UW · Airbus A319112 · Escape SlideSDR USAASA03041Girt Bar · inoperativeCLT - DURING INSPECTION, THE L2 DOOR WAS FOUND TO HAVE IMPROPER CLEARANCE BETWEEN DOUBLER/STOP AND GIRT BAR. MAINTENANCE REPLACED THE GIRT BAR. INSPECTED INSTALLATION AND FOUND SERVICEABLE. (M)May 14, 2003 · N710UW · Airbus A319112 · Escape SlideSDR USAASA01020Wire · brokenDCA - THE ESCAPE LIGHT ON SEAT ROW 13 WAS INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRES. OPS CHECKED OK. (M)May 18, 2001 · N710UW · Airbus A319112 · Light System WiringSDR USAASA00010Power Supply · dischargedRDU - FOUND EMERGENCY LIGHT SYSTEM FAILING TEST. MAINTENANCE REPLACED AFT EPSU AND REPAIRED SEAT WIRING. LIGHT SYSTEM OPS CHECKED OK. (M)Feb 24, 2000 · N710UW · Airbus A319112 · Emergency LightingSDR USAASA99009Power Supply · dischargedRDU - FOUND EMERGENCY LIGHT SYSTEM FAILED OPERATIONAL TEST. MAINTENANCE REPLACED THE AFT EPSU. OPS CHECKED OKAY. (X)Nov 22, 1999 · N710UW · Airbus A319112 · Emergency LightingSDR USAASA99006Battery Pack · dischargedSFO - THE AFT EXIT EMERGENCY LIGHTS FOR SEAT 21 WERE INOPERATIVE. MAINTENANCE REPLACED THE EXIT LIGHT BATTERY PACK. (X)Sep 23, 1999 · N710UW · Airbus A319112 · Emergency Lighting
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