N709UW

Service difficulty reports · 376

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 = 'N709UW' 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 USAA2010061591128Hinge Fitting · excess playSAL - S4 - MAJOR REPAIR - EXCESSIVE PLAY ON LEFT AFT NOSE LANDING GEAR DOOR POSITION NR 1 HINGE FITTING. REPLACED LEFT AFT NOSE LANDING GEAR DOOR POSITION NR 1 HINGE IAW A319 AMM 32-22-13.May 24, 2010 · N709UW · Airbus A319112 · Landing Gear DoorsSDR USAA2010061491121Seat Track · corrodedSAL - S4 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR41 TO FR46, Y1292. REPLACED SEAT TRACK BETWEEN FR41 TO FR46, Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53370500.May 24, 2010 · N709UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2010061491120Seat Track · corrodedSAL - S4 - MAJOR REPAIR - 230343 - CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, Y765. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112813.May 24, 2010 · N709UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2010061491119Seat Track · corrodedSAL - S4 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112815202.May 24, 2010 · N709UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2010061491118Seat Track · corrodedSAL - S4 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR41 TO FR47, -Y1292. REPLACED SEAT TRACK BETWEEN FR41 TO FR47, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53372500.May 24, 2010 · N709UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2010060791082Seat Track · corrodedSAL - S4 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112812.May 24, 2010 · N709UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2010060791081Seat Track · corrodedSAL - S4 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y765. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING 053112812.May 24, 2010 · N709UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2010060791080Seat Track · corrodedSAL - S4 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, -Y765. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, -Y765 IAW A319 SRM 51-72-11.May 24, 2010 · N709UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2010062491257Slide · bindsSAL - S4 - EES - SLIDE RAFT ON L-1 DOOR HITS FUSELAGE WHEN DOOR IS FULLY OPEN. REPLACED SLIDE RAFT ON L-1 DOOR IAW JOB CARD 26L00025011.May 23, 2010 · N709UW · Airbus A319112 · Escape SlideSDR USAA2010062291230Shear Plate · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23L. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23L IAW EA 132970.May 23, 2010 · N709UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2010061691149Coupling · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON UPPER OUTBOARD FLOORBEAM SPLICE AT FR68, -Y1292. REPLACED UPPER OUTBOARD FLOORBEAM COUPLING AT FR68, -Y1292 IAW A319 SRM 51-72-11.May 23, 2010 · N709UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2010060791078Washer · out of adjustSAL - S4 - MAJOR REPAIR - R-1 DOOR IS OUT OF ADJUSTMENT AT DIMENSION "A" & "B" BETWEEN FINGER & STRIKER LEVER DAMPER MECHANISM. PERFORMED ADJUSTMENT AT DIMENSION "A" (J2) & "B" (J1) BETWEEN STRIKER LEVER & FINGER LEVER DAMPER MECHANISM IAW A319 AMM 52-11-14-8May 23, 2010 · N709UW · Airbus A319112 · Service DoorsSDR USAA2010060791077Washer · out of adjustSAL - S4 - MAJOR REPAIR - R-2 DOOR IS OUT OF ADJUSTMENT AT DIMENSION "B" BETWEEN FINGER & STRIKER LEVER. PERFORMED ADJUSTMENT AT DIMENSION "B" (J1) BETWEEN FINGER & STRIKER LEVER IAW A319 AMM 52-13-14-820-002.May 23, 2010 · N709UW · Airbus A319112 · Service DoorsSDR USAA2010060791076Washer · out of adjustSAL - S4 - MAJOR REPAIR - L-2 DOOR IS OUT OF ADJUSTMENT AT DIMENSION "B" BETWEEN FINGER & STRIKER LEVER. PERFORMED ADJUSTMENT AT DIMENSION "B" (J1) BETWEEN FINGER & STRIKER LEVER IAW A319 AMM 52-11-14-820-002.May 23, 2010 · N709UW · Airbus A319112 · Passenger/Crew DoorsSDR USAA2010060791075Washer · out of adjustSAL - S4 - MAJOR REPAIR - L-1 DOOR IS OUT OF ADJUSTMENT AT DIMENSION "A" & "B" BETWEEN FINGER & STRIKER LEVER DAMPER MECHANISM. PERFORMED ADJUSTMENT AT DIMENSION "A" (J2) & B (J1) BETWEEN FINGER & FINGER LEVER DAMPER MECHANISM IAW A319 AMM 52-11-14-820-002.May 23, 2010 · N709UW · Airbus A319112 · Passenger/Crew DoorsSDR USAA2010062491258Reservoir · low pressureSAL - S4 - EES - GAUGE NEEDLE IS NOT IN GREEN "GO" BAND AT RESERVOIR INFLATION OFF WING LEFT SIDE AFT CARGO COMPARTMENT. REPLACED INFLATION RESERVOIR OFF WING LEFT SIDE AFT CARGO COMPARTMENT IAW A319 AMM 25-62-46.May 22, 2010 · N709UW · Airbus A319112 · Escape SlideSDR USAA2010061691148Coupling · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LOWER OUTBOARD FLOORBEAM SPLICE AT FR66, -Y1292. REPLACED LOWER OUTBOARD FLOORBEAM COUPLING AT FR66, -Y1292 IAW A319 SRM 51-72-11.May 22, 2010 · N709UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2010061691147Coupling · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON UPPER INBOARD FLOORBEAM SPLICE AT FR66, -Y1292. REPLACED UPPER INBOARD FLOORBEAM COUPLING AT FR66, -Y1292 IAW A319 SRM 51-72-11.May 22, 2010 · N709UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2010061491115Hinge Fitting · excess playSAL - S4 - MAJOR REPAIR - EXCESSIVE PLAY AT RUDDER HINGE NR 4 AT VERTICAL STAB STA 2632, RIB 6. REPLACED NR 4 RUDDER HINGE ASSEMBLY FITTING AT VERTICAL STAB STA 2632, RIB 6 IAW A319 AMM 55-36-41 & SRM 51-42-11.May 22, 2010 · N709UW · Airbus A319112 · Rudder StructureSDR USAA2010062191204Skin · saturatedSAL - S4 - MAJOR REPAIR - TRAPPED WATER IN RIGHT ELEVATOR UPPER SKIN IN HONEY COMB CORE STRUCTURE BETWEEN STAB STA 227 TO STAB STA 271. REPAIRED RIGHT ELEVATOR UPPER SKIN IAW A319 SRM 55-21-00 & 51-77-13.May 21, 2010 · N709UW · Airbus A319112 · Elevator, Plate/SkinSDR USAA2010061591134Skin · saturatedSAL - S4 - MAJOR REPAIR - TRAPPED WATER ON UPPER SURFACE OF LEFT ELEVATOR BETWEEN ELEV STA 342 TO 404, 227 TO 271, & AT ELEV STA 404 & 227. REPAIRED UPPER SURFACE OF LEFT ELEVATOR BETWEEN ELEV STA 342 TO 404, 227 TO 271, & AT ELEV STA 404 & 227 IAW A319 SRM 5May 21, 2010 · N709UW · Airbus A319112 · Elevator, Plate/SkinSDR USAA2010061691143Support Fitting · corrodedSAL - S4 - MAJOR REPAIR - CORROSION ON SUPPORT FITTING AT L-1 DOOR LOWER INTERNAL AREA. REPLACED SUPPORT FITTING AT L-1 DOOR LOWER INTERNAL AREA IAW A319 SRM 51-72-11 & AIRBUS DRAWING D52111550.May 20, 2010 · N709UW · Airbus A319112 · Passenger/Crew DoorsSDR USAA2010062191194Floorbeam · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67, -Y465. REPLACED FLOORBEAM BETWEEN FR64 TO FR67, -Y465 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472000.May 18, 2010 · N709UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2010062191193Floorbeam · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR16 TO FR18, Y254. REPLACED FLOORBEAM BETWEEN FR16 TO FR18, Y254 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112816.May 18, 2010 · N709UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2010062191192Floorbeam · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON UPPER INBOARD SPLICE OF FLOOR BEAM AT FR64, -Y1292. REPLACED FLOORBEAM UPPER INBOARD COUPLING AT FR64, -Y1292 IAW A319 SRM 51-72-11.May 18, 2010 · N709UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2010062191191Floorbeam · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LOWER OUTBOARD SPLICE OF FLOORBEAM AT FR64, -Y1292. REPLACED FLOORBEAM LOWER OUTBOARD COUPLING AT FR64, -Y1292 IAW A319 SRM 51-72-11.May 18, 2010 · N709UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2010062191190Hinge Pin · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON AILERON HINGE PIN NR 5 RIGHT WING. REPLACED AILERON HINGE PIN NR 5 IAW A319 AMM 27-14-41.May 18, 2010 · N709UW · Airbus A319112 · AileronsSDR USAA2010062191189Sill · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING LOCATED AT LEVEL STR 23R BETWEEN FR66 TO FR68 LOWER SILL AREA OF AFT PASSENGER /CREW DOOR CUTOUT RT SIDE. REPLACED SHAPE SILL (CENTER FITTING) BETWEEN FR66 TO FR68, S23R LOWER SILL AREA OFMay 18, 2010 · N709UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2010030290480Cylinder · out of adjustFLT 1078 - UVF-PHL - EMERGENCY EQUIPMENT - L1 SLIDE REMOVED AFTER OPERATIONAL TEST OF L1 ESCAPE SLIDE FAILED PER TASK CARD 26L00025007. DOOR ASSIST BOTTLE FAILED TO DISCHARGE. FOUND BELL CRANK PERCUSSION FINGER TO BE OUT OF ADJUSTMENT. ADJUSTED BELL CRANK Feb 28, 2010 · N709UW · Airbus A319112 · Passenger/Crew DoorsSDR USAA2010030190465Slide · failedFLT 1078 - UVF-PHL - EMERGENCY EQUIPMENT - L1 SLIDE REMOVED AFTER OPERATIONAL TEST OF L1 ESCAPE SLIDE FAILED PER /C 26L00025007. DOOR ASSIST BOTTLE FAILED TO DISCHARGE. FOUND BELL CRANK PERCUSSION FINGER TO BE OUT OF ADJUSTMENT. ADJUSTED BELL CRANK FINGER PFeb 28, 2010 · N709UW · Airbus A319112 · Escape SlideSDR USAA2010020290256Receiver · malfunctionedBNA - CLT - ELECTRICAL ODOR - UPON AIRCRAFT ARRIVAL IN DCA, NOTICED ELECTRICAL ODOR IN COCKPIT AREA {ONLY COCKPIT AREA - CABIN OK}. BURN MARKS FOUND ON BOTTOM OF NR 2 MULTI-MODE RECEIVER (MMR). REMOVED AND REPLACED NR 2 MMR. LAND CAT 3 CAPABILITY TEST WAS SFeb 1, 2010 · N709UW · Airbus A319112 · Navigation SystemSDR USAA2009091192475Wire · brokenFLT 894- ATL-CLT - EMERGENCY LIGHTS - ROW 18 LEFT EMERGENCY LIGHT INOPERATIVE. FOUND WIRE BROKEN AT CONNECTOR AT ROW 18 LEFT. RE-PINNED CONNECTOR. OPERATIONAL CHECK WAS GOOD PER ESPM 20-48-12.Sep 8, 2009 · N709UW · Airbus A319112 · Light System WiringSDR USAA920080885Seat Track · corrodedPIT - MAJOR REPAIR - ULTIMATE BREAKING MODIFICATION - CORROSION ON CABIN SEAT TRACK, BS 808 / FR 20 - BS 950 / BS 24, -Y765. REPLACED CABIN SEAT TRACK, BS 808 / FR 20 - BS 950 / BS 24, -Y765 IAW A319 SRM 53-11-15.Apr 7, 2008 · N709UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR SA07007Girt Bar · detachedDEN - THE FORWARD LEFT MAIN ENTRY DOOR EMERGENCY ESCAPE SLIDE GIRT BAR WAS FOUND DETACHED. MAINTENANCE SECURED THE GIRT BAR. OPERATIONALLY CHECKED OK.Jan 30, 2007 · N709UW · Airbus A319112 · Escape SlideSDR USA2004F00089Skin · dentedFOUND DENT IN FUSELAGE SKIN, 1 INCH DIAMETER BY .050 INCH DEEP. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW SRM.Jun 17, 2004 · N709UW · Airbus A319112 · Fuselage Main, Plate/SkinSDR USA2004F00087Skin · dentedFOUND DENT IN FUSELAGE SKIN, 2.5 INCH DIAMETER BY .050 INCH DEEP. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW SRM.Jun 17, 2004 · N709UW · Airbus A319112 · Fuselage Main, Plate/SkinSDR USAA040320Seat Track · corrodedSEAT TRACK, 27 INCHES X .85 INCH X .047 INCH AREA, CORROSION; LEVEL 2; MAIN DECK FLOOR SUPPORT, FRAME 14-16, Y+503. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM.Jun 16, 2004 · N709UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA040327Sill · corrodedBFM - FOUND DOOR SILL CORRODED 1 INCH BY 1 INCH BY .068 INCH AREA, R2 DOOR SILL, -Y1732, FRAME 66-68, -Z240. REPLACED DOOR SILL PER SRM 53-41-14. (M)Jun 12, 2004 · N709UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040328Sill · corrodedBFM - FOUND SILL CORRODED 1 INCH BY 1 INCH BY .080 INCH AREA, L2 DOOR SILL, FRAME 66 TO 68 PLUS Y1732, -Z240. REPLACED DOOR SILL PER SRM 53-41-14. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)Jun 12, 2004 · N709UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA04345Seat Track · corrodedBFM - FOUND CORROSION ON SEAT TRACK, 2 INCHES BY 1 INCH BY .026 INCH. REPLACED SEAT TRACK. (M)Jun 10, 2004 · N709UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA04344Floor Support · corrodedBFM - FOUND CORROSION ON FLOOR SUPPORT, 1 INCH BY .90 INCH BY .040 INCH. REPLACED FLOOR SUPPORT. (M)Jun 10, 2004 · N709UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040322Frame · corrodedFOUND FRAME CORRODED 4.5 INCHES BY 2 INCHES BY .053 INCH AREA, FRAME 66-68, Y1292, Z-240. INSTALLED NEW FRAME PER SRM 53-00-14. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)Jun 10, 2004 · N709UW · Airbus A319112 · Fuselage Main, FrameSDR USAA040325Floorbeam · corrodedBFM - FOUND BEAM CORROED 1.5 INCHES BY 1 INCH BY .25 INCH CORRODED, BETWEEN FRAME 68 AND 69, BL -Y1292, -Z240. REPLACED WITH NEW PART PER SRM 53-00-14, FIG 102. (M)Jun 10, 2004 · N709UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA040326Floorbeam · corrodedBFM - FOUND BEAM CORRODED 1 INCH BY 1 INCH BY .20 INCH AREA, FS 66, BL -Y1292, -Z240. REPLACED WITH NEW PART PER SRM 53-00-14 FIG 102. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)Jun 10, 2004 · N709UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA040330Floor Support · corrodedBFM - FOUND FLOOR SUPPORT CORRODED 1 INCH BY .90 INCH BY .040 INCH AREA, FRAME 20, -Y254, Z-240. INSTALLED NEW FLOOR SUPPORT PER SRM 53-11-14, FIG 102. (M)Jun 10, 2004 · N709UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040334Seat Track · corrodedBFM - FOUND SEAT TRACK CORRODED 2 INCHES BY 1 INCH BY .026 INCH AREA, FS 24, BL -Y1292, -Z-240. REPLACED WITH NEW PART PER SRM 53-00-15. CORROSION LEVEL 2, TASK NR JA-220-53500. (M)Jun 10, 2004 · N709UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA040324Floorbeam · corrodedBFM - FOUND BEAM CORRODED 1 INCH BY .50 I NCH BY .20 INCH AREA, BETWEEN FRAME 66 AND 68 BL -Y1292. REPLACED WITH NEW PART PER SRM 53-00-10 FIG 102. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)Jun 10, 2004 · N709UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA040318Frame · corrodedFRAME , 3.0 INCH X 1.5 INCH X .040 INCH AREA, CORROSION, LEVEL 2; FR66, Y1292, Z240. INSTALLED NEW FRAME IAW SRM.Jun 10, 2004 · N709UW · Airbus A319112 · Fuselage Main, FrameSDR USAA040316Frame · corrodedFRAME, 4.5 INCH X 1.75 INCH X .064 INCH AREA, CORROSION; LEVEL 2; FR68, Y1292, Z240. INSTALLED NEW FRAME IAW SRM.Jun 10, 2004 · N709UW · Airbus A319112 · Fuselage Main, FrameSDR USAA040333Support · corrodedBFM - FOUND SUPPORT PLATE CORRODED 6 INCHES BY .5 INCH BY .020 INCH AREA, FRAME 66, -Y1975, -Z240. REMOVED AND REPLACED R2 DOOR FORWARD GIRT BAR FITTING SUPPORT PLATE PER SRM 51-74-00, SRM 53-12-00. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)Jun 9, 2004 · N709UW · Airbus A319112 · Fuselage Miscellaneous Structure
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