N702UW

Service difficulty reports · 215

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 = 'N702UW' 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 AALA201602049002Warning System · false activationAIRCRAFT WAS NOT GNDE. FUEL CTR TANK PUMP 2 LOW PRESS LIGHT ON. COULD NOT DUPLICATE FAULT. DUE TO HISTORY, REPLACED RT CTR BOOST PUMP FOR TROUBLESHOOTING PURPOSES. ACCOMPLISHED A SATISFACTORY LEAK & OPERATIONAL CHECK IAW AMM 28-21-51. COMPONENT REPAIR VENFeb 2, 2016 · N702UW · Airbus A319112 · Fuel Indicating SystemSDR AALA201602039006Power Supply · defectiveAIRCRAFT WAS NOT GNDED. EMER POWER SUPPLY UNIT FAILED TEST ON WEEKLY CHECK. REPLACED LT POWER SUPPLY UNIT IAW AMM 33-50-00. INSPECTED THE POWER SUPPLY WITH SHOP BATTERY, NO DEFECTS WERE NOTED WITH A FULLY CHARGED BATTERY. THE POWER SUPPLY WAS RETURNED AS SFeb 2, 2016 · N702UW · Airbus A319112 · Emergency LightingSDR AALA201511299003Power Supply · failed3S CHECK, RT EPSU 12WL FAILED TEST. REPLACED POWER SUPPLY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38.Nov 28, 2015 · N702UW · Airbus A319112 · Emergency LightingSDR AALA201512019003Floor Panel · delaminated3S CHECK, FWD GALLEY FLOOR PANEL 221EF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.Nov 17, 2015 · N702UW · Airbus A319112 · Fuselage Floor PanelSDR AALA201511139005Hinge Pin · corroded3S CHECK, CORROSION INNER HINGE PIN INBD SIDE ON SPOILER 3, ON RT WING. REPLACED INNER HINGE PIN IAW 26C60057205.Nov 12, 2015 · N702UW · Airbus A319112 · SpoilersSDR AALA201511129008Hinge Pin · corroded3S CHECK, CORROSION INNER HINGE PIN INBD SIDE ON SPOILER 4 ON LT WING. REPLACED PIN IAW 26C50057205.Nov 11, 2015 · N702UW · Airbus A319112 · SpoilersSDR AALA201511129007Hinge Pin · corroded3S CHECK, CORROSION INNER HINGE PIN INBD SIDE ON SPOILER 1 ON LT WING. REPLACED PIN IAW 26C50057205.Nov 11, 2015 · N702UW · Airbus A319112 · SpoilersSDR AALA201511129006Hinge Pin · corroded3S CHECK, CORROSION INNER HINGE PINS ON SPOILER 2 ON RT WING. REPLACED PINS IAW 26C60057205.Nov 11, 2015 · N702UW · Airbus A319112 · SpoilersSDR AALA201511129003Flashlight · broken3S CHECK, BROKEN FLASHLIGHT ON SWIVEL SEAT IN PAX CABIN. REPLACED FLASHLIGHT.Nov 11, 2015 · N702UW · Airbus A319112 · Emergency EquipmentSDR AALA201511279011Bolt · corroded3S CHECK, LT WING OTBD FLAP NR 4 TRACK PIVOT BOLT HAS CORROSION & PROTECTIVE PLATING MISSING. REPLACED PIVOT BOLT IAW TASK CARD 26T53257001.Nov 9, 2015 · N702UW · Airbus A319112 · Trailing Edge FlapsSDR AALA201511209012Bolt · corroded3S CHECK, CORROSION & PLATING MISSING ON RT WING INBD FLAP NR 2 TRACK PIVOT BOLT. REPLACED PIVOT BOLT IAW 26T63157001.Nov 9, 2015 · N702UW · Airbus A319112 · Trailing Edge FlapsSDR AALA201511309007Plate · cracked3S CHECK, LT SIDE BOX BEAM FASTENER HOLE HAS CRACK INDICATION AT FRAME 43 & STRINGER 15. REPLACED PRESS PLATE IAW SRM 51-42-11 & 51-44-11.Nov 6, 2015 · N702UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR AALA201511309020Hinge Fitting · worn3S CHECK, RT WING NR 4 SPOILER, CTR HINGE FITTING BOLT STOP WORN. REPAIRED FITTING IAW SRM 57-70-00-201 PARAGRAPH 5 D FIGURE 201.Nov 4, 2015 · N702UW · Airbus A319112 · SpoilersSDR AALA201511279012Hinge Fitting · worn3S CHECK, LT WING NR 4 SPOILER, CTR HINGE FITTING BOLT STOP WORN. REPAIRED HINGE FITTING IAW SRM 57-70-00-201 PARAGRAPH 5 D FIGURE 201.Nov 1, 2015 · N702UW · Airbus A319112 · SpoilersSDR AALA201511309018Floor Panel · delaminated3S CHECK, AFT GALLEY FLOOR PANEL 261DF HAS DELAMINATION. REPLACED FLOOR PANEL IAW IRM 9701 REV G.Oct 30, 2015 · N702UW · Airbus A319112 · Fuselage Floor PanelSDR AALA201511309017Floor Panel · delaminated3S CHECK, AFT GALLEY FLOOR PANEL 262BG DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.Oct 30, 2015 · N702UW · Airbus A319112 · Fuselage Floor PanelSDR AALA201511169011Floor Panel · delaminated3S CHECK, AFT GALLEY FLOOR PANEL 261PF DELAMINATED. REPLACED IAW IRM 9701 REV G.Oct 30, 2015 · N702UW · Airbus A319112 · Fuselage Floor PanelSDR AALA201511309022Hinge Fitting · worn3S CHECK, RUDDER NR 5, HINGE FITTING HAS EXCESSIVE PLAY AT VERTICAL STABILIZER POSITION 2985, RIB 7. REPLACED HINGE FITTING IAW AMM 27-21-00-720-001-A.Oct 29, 2015 · N702UW · Airbus A319112 · Rudder StructureSDR AALA201511309019Seat Track · corroded3S CHECK, CORROSION ON SEAT TRACK BEAM, BETWEEN FRAME 12 & 24, AT -Y1292. REPLACED SEAT TRACK BEAM PER SRM 51-72-11 & DWG D53112812.Oct 29, 2015 · N702UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR AALA201511309006Skin · delaminated3S CHECK, RT ELEVATOR UPPER SKIN PANEL HAS DELAMINATION, BETWEEN STATION 1305 & 6009, RIB 4 & 14. REPLACED ELEVATOR IAW AMM 27-34-41.Oct 29, 2015 · N702UW · Airbus A319112 · Elevator, Plate/SkinSDR AALA201511119007Hinge Fitting · worn3S CHECK, RUDDER HINGE NR 2 HAS EXCESSIVE PLAY. REPLACED HINGE IAW AMM 55-36-41-400-001-A.Oct 29, 2015 · N702UW · Airbus A319112 · Rudder StructureSDR AALA201511119006Hinge Fitting · worn3S CHECK, RUDDER HINGE NR 4 HAS EXCESSIVE PLAY. REPLACED HINGE ARM FITTING IAW AMM 55-36-41-0401 & SRM 51-72-11.Oct 29, 2015 · N702UW · Airbus A319112 · Rudder StructureSDR AALA201511169012Floor Panel · delaminated3S CHECK, FWD CARGO COMPARTMENT FLOOR PANEL 131AF DELAMINATED. REPLACED IAW IRM 9701 REV G.Oct 27, 2015 · N702UW · Airbus A319112 · Fuselage Floor PanelSDR AALA201511169010Floor Panel · delaminated3S CHECK, AFT CARGO COMPARTMENT FLOOR PANEL 151VG DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.Oct 27, 2015 · N702UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2015022300003Slide · bulgedL2 DOOR SLIDE COVER IN CONTACT WITH FUSELAGE. REPLACED L2 DOOR EMER SLIDE IAW JC 26L00025011.Feb 21, 2015 · N702UW · Airbus A319112 · Escape SlideSDR USAA2015022000009Floorboard · damagedSY6 CHECK, AFT WET AREA FLOORBOARD 261AG HAS NUMEROUS AREAS OF SURFACE DAMAGE. INSTALLED NEW FLOORBOARD IAW JOB CARD 26C26053014.Feb 19, 2015 · N702UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2015021800004Plate · corrodedR2 DOOR SILL PLATE TOP SURFACE AT BOTTOM OF FRAME 68 HAS SEVERAL SPOTS OF CORROSION. REMOVED CORROSION & FOUND DAMAGE BEYOND LIMITS OF SRM 53-41-14 FIG 101. INSTALLED NEW DOOR SILL IAW DWGS D53480042, D53480043, D53480009 & IAW SRM 51-72-11 & 51-42-11.Feb 13, 2015 · N702UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2015021800003Floorbeam · corrodedBEAM AT FRAME 66 & AFT OF FRAME 64 HAS CORROSION & FOUND OUT OF LIMITS IAW SRM 53-41-00. R & R FLOORBEAM IAW DWGS D53472831, D53472815 & SRM 51-72-11.Feb 11, 2015 · N702UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2015021300004Web · corrodedSY6 CHECK, CORROSION ON WEB AT AFT END OF R1 DOOR AT BL Y-1584 & FRAME 20. R & R WEB IAW SRM 51-72-00.Feb 11, 2015 · N702UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2015021600006Floorbeam · corrodedSY6 CHECK, LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FRAME 66 - 70, Z-500, Y765. REPLACED FLOORBEAM IAW SRM 51-43-00 & DWG D53472831.Feb 11, 2015 · N702UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2015021600005Floorbeam · corrodedSY6 CHECK, LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FRAME 66 - 70, Z-500, Y765. REPLACED FLOORBEAM IAW SRM 51-43-00 & DWG D53472831.Feb 11, 2015 · N702UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2015021600004Floorbeam · corrodedSY6 CHECK, LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FRAME 66, Z-500, Y464.8. REPLACED FLOORBEAM IAW SRM 51-72-11.Feb 11, 2015 · N702UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2015021600003Floorbeam · corrodedSY6 CHECK, LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FRAME 66, Z-500, Y318. REPLACED FLOORBEAM AT FRAME 66, Z-500, Y318 IAW SRM 51-43-00.Feb 11, 2015 · N702UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2015021600002Floorbeam · corrodedSY6 CHECK, LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FRAME 66, Z-500, Y765. REPLACED FLOORBEAM IAW SRM 51-72-11.Feb 11, 2015 · N702UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2015021600001Door Sill · corrodedSYS 6 CHECK, LEVEL 2 EXFOLIATION CORROSION ON AFT SHAPE SILL FRAME 68, Z-500, Y1162.5. REPLACED AFT SHAPE SILL FRAME 68, Z-500, Y1162.5 IAW SRM 53-41-79.Feb 11, 2015 · N702UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2015021300005Shear Plate · crackedSY6 CHECK, L2 DOOR AREA, LT SHEAR PLATE BETWEEN FRAME 68 - 69 NEAR FLOORBEAM Y1162.5 HAS A 2 INCH CRACK. INSTALLED NEW SHEAR PLATE ASSEMBLY IN ACFT. ALL WORK ACCOMPLISHED IAW SRM 51-72-11 & DWG D53480019.Feb 10, 2015 · N702UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2014123000005Lens · missingSEAT 3C MISSING EMER LIGHT LENS. REPLACED SEAT MOUNTED EMER EXIT LIGHT LENS AT SEAT 3C IAW AMM 33-51-19 PB 401.Dec 29, 2014 · N702UW · Airbus A319112 · Emergency LightingSDR USAA2014100900012Unknown · malfunctionedUPON POWER APPLICATION ON TAKEOFF, THE ACFT MADE A SHARP LT TURN, RECOVERED WITH RUDDER APPLICATION TO NORMAL TAKEOFF. ON CLIMB OUT FLIGHT ATTENDANT REPORTED A LOUD CLUNK SOUND IN CABIN. NO ABNORMAL INDICATION ON ANY PAGES. FLIGHT CONTINUED & LANDED WITHOUTOct 8, 2014 · N702UW · Airbus A319112 · Engine (Turbine/Turboprop)SDR USAA2014080400011Light · inoperativeTHE EMER FLOOR LIGHTING AT SEAT 16A INOPERATIVE. R & R THE EMER SEAT LIGHT ASSEMBLY AT SEAT 16A IAW AMM 33-51-19-401.Aug 3, 2014 · N702UW · Airbus A319112 · Emergency LightingSDR USAA2014061600019Reservoir · low pressureTHE CIDS PANEL SYS INOPERATIVE RED LIGHT ON CIDS PANEL. SCREEN SHOWS SLIDES LOW PRESS & EMER RT WHEN SELECTED. REPLACED RT OFF WING ESCAPE SLIDE INFLATION RESERVOIR IAW AMM 25-62-46-400-001-A. OPERATIONS CHECKED NORMAL.Jun 14, 2014 · N702UW · Airbus A319112 · Escape SlideSDR USAA2014060200006Slide Raft · defectiveL1 DOOR SLIDE COVER CONTACTS FUSELAGE WHEN DOOR IS FULLY OPEN. REPLACED L1 SLIDE & RAFT IAW JOB CARD 26L00025011.May 30, 2014 · N702UW · Airbus A319112 · Escape SlideSDR USAA2014042800013Lens · missingEMERGENCY EXIT 2R EXIT LIGHT LENS COVER MISSING. REPLACED EMERGENCY EXIT LIGHT LENS AT 2R.Apr 27, 2014 · N702UW · Airbus A319112 · Emergency LightingSDR USAA2014040700006Panel · dislodgedRECEIVED A 1R DOOR RED PRESS & A DOOR DISARMED WARNING IN FLIGHT. FOUND 1R SLIDE ARMING LEVER FAILING TO ENGAGE FULLY DUE TO DISLODGED LINING PANEL INTERFERENCE. CORRECTED LINING INSTALLATION IAW 25-23-46-400-001-A. ADJUSTED 1R SLIDE ARM PROX SENSOR 4WN2 IAApr 5, 2014 · N702UW · Airbus A319112 · Passenger Compartment EquipmentSDR USAA2014032400019Window · crackedFLIGHT ATTENDANT NOTICED CRACK IN WINDOW ON 2R DOOR. VERIFIED CRACK IN 2R DOOR OUTER PANE. R & R 2R DOOR OUTER PANE, INNER PANE & SEAL IAW AMM 56-31-13-400-002-A.Mar 23, 2014 · N702UW · Airbus A319112 · Door WindowsSDR USAA2014012400012Computer · inoperativeEN ROUTE FROM PHL TO CUN, CREW REPORTED THE NR 1 FMGC INOPERATIVE. FLIGHT DIVERTED TO CLT & LANDED WITHOUT INCIDENT. MX R & R THE NR 1 FMGC IAW AMM 22-96-00-0501 & 22-97-00-0501.Jan 23, 2014 · N702UW · Airbus A319112 · Flight Management Computing Hardware SystemSDR USAA2014010700008Computer · faultyEN ROUTE FROM CLE TO CLT, CREW RECEIVED ECAM, ENG 2 REVERSER FAULT. FLIGHT DIVERTED TO PIT & LANDED WITHOUT INCIDENT. R & R LGCIU IAW AMM 32-31-71. OPERATIONS CHECKED GOOD. OPERATIONS CHECK NR 2 T/R IAW AMM 78-30-00 CHECKED GOOD.Jan 6, 2014 · N702UW · Airbus A319112 · Engine Thrust ReverserSDR USAA2013120400011Display · faultyCREW REPORTED THE FIRST OFFICER'S ND FLICKERS, HAS FLASHES OF LIGHT & AUTO TRANSFERRED ITSELF WITH THE PFD. FIRST OFFICER ALSO STATES HE COULD SMELL ELEC FUMES. R & R FIRST OFFICER'S ND, 3WT2, IAW AMM 31-63-22-401.Dec 3, 2013 · N702UW · Airbus A319112 · Central DisplaySDR USAA2013120200015Seal · leakingTHE NR 1 ENG OIL QTY REDUCED SLOWLY TO ZERO DURING CRUISE OF LAST TWENTY MINUTES, PRESS WAS GOOD. CREW DECLARED AN EMERGENCY & MADE A NORMAL LANDING, ACFT TAXIED TO GATE. REPLACED THE NR 1 ENG STARTER SEAL OIL SEAL IAW AMM 72-63-00-300-002-A6. SYS LEAK CHECNov 28, 2013 · N702UW · Airbus A319112 · Turbine Engine Oil SystemSDR USAA2013092300014Outflow Valve · failedDURING CLIMBOUT, CREW REPORTED VENT SKIN ANNOUNCED ON ECAM. ACFT WOULD NOT PRESSURIZE. AFTER PERFORMING ECAM ACTIONS, FLIGHT DIVERTED AND LANDED WITHOUT INCIDENT. MX R & R SKIN AIR OUTLET VALVE IAW AMM 21-26-53. OPS CHECKED OK IAW AMM 21-26-00-710-001A.Sep 22, 2013 · N702UW · Airbus A319112 · Pressure Regulator/Outflow ValveSDR USAA2013060700006Lens · brokenCREW REPORTED THE FLOOR EMERGENCY LIGHTS AT 1C BROKEN. MX REPLACED LENS AT 1C EMERGENCY LIGHT. OPS OK.Jun 6, 2013 · N702UW · Airbus A319112 · Emergency Lighting
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