N114UW

Service difficulty reports · 270

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 = 'N114UW' 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 AALA201504089016Control Servo · faultyUNCOMMANDED ROLL TO LT WITH SPOILER DEPLOYMENT, FLAPS 2. AUTOPILOT ON & OFF, AILERONS SHOWED CORRECTION TO RT. REPLACED LT GREEN AILERON SERVO CONTROL & BLUE AILERON SERVO CONTROL IAW AMM 27-14-51. ACCOMPLISHED OPERATIONAL CHECKS WITH NO DEFECTS NOTED. SEEApr 7, 2015 · N114UW · Airbus A320214 · Aileron Control SystemSDR AALA201504089002Computer · malfunctionedWITH AP ON, OPEN DESCENT, SPEED BRAKES FULL, GOT 5' LT BANK GOING FROM FLAPS UP TO FLAPS 2 RT AT THE END OF FLAP MOVEMENT. R & R BOTH ELAC COMPUTERS IAW AMM 27-93-34-000-001A & 400-001-A. OPERATIONAL CHECK OF ELAC'S IAW AMM 27-93-00-710-001-A IS GOOD. SEE AApr 7, 2015 · N114UW · Airbus A320214 · Flight Control SystemSDR AALA201504089001Control Servo · malfunctionedUNCOMMANDED ROLL TO LEFT WITH SPOILER DEPLOYMENT, FLAPS 2. AUTOPILOT ON & OFF, AILERONS SHOWED CORRECTION TO RT. REPLACED LT GREEN AILERON SERVO CONTROL & BLUE AILERON SERVO CONTROL IAW AMM 27-14-51. ACCOMPLISHED OPERATIONAL CHECKS WITH NO DEFECTS NOTED.Apr 7, 2015 · N114UW · Airbus A320214 · Aileron Control SystemSDR USAA2015040500001Cover · detachedRIGHT FWD OVERWING EMER EXIT DOOR PLASTIC COVER OVER ESCAPE HANDLE CAME OFF. FLIGHT ATTENDANT REATTACHED IT. ECAM DOOR PROCEDURE CAME ON BUT CABIN STAYED AT RESET LEVEL. WENT AWAY AFTER FLIGHT ATTENDANT REATTACHED THE COVER. INSPECTED THE RT FWD OVERWINGApr 3, 2015 · N114UW · Airbus A320214 · Emergency ExitsSDR USAA2015033100015Rib · corrodedCORROSION FOUND ON FASTENER NUT ON RIB 5 AREA IN THE RT WING UNDER PANEL 674AB. REMOVED CORROSION & REPAIRED IAW EA 106551.Mar 28, 2015 · N114UW · Airbus A320214 · Wing, Rib/BulkheadSDR USAA2015033100014Rib · corrodedFOUND CORROSION AROUND FASTENERS AT FALSE SPAR BOX BETWEEN RIB 4 & 5 INSIDE LT WING ACCESS PANEL 574AB. REMOVED CORROSION & REPAIRED IAW EA 106552.Mar 28, 2015 · N114UW · Airbus A320214 · Wing, Rib/BulkheadSDR USAA2014111000008Lens · missingDOOR 2R EMER EXIT LENS LIGHT COVER MISSING. ACCOMPLISHED TEMPORARY REPAIR IAW EA 208931. FINAL REPAIR - INSTALLED LENS AT DOOR 2R EMERGENCY EXIT LIGHT IAW A320 AMM 33-51-13, P/B 0401.Nov 9, 2014 · N114UW · Airbus A320214 · Emergency LightingSDR USAA2014092500004Mechanism · dirtySLIDE ARM HANDLES AT DOORS L1 & R1 BOTH HAVE A GRINDING FEEL AS THEY ARE MOVED. SLIDE R1 HAD TO BE RECYCLED TO BE ARMED ON LOWER ECAM PAGE. CLEANED & LUBED BOTH L1 & R1 ENTRY DOOR SLIDE GIRT BAR HOLD DOWN & DOOR MECHANISM.Sep 24, 2014 · N114UW · Airbus A320214 · Passenger/Crew DoorsSDR USAA2014061700007Slide Raft · bulgedPERFORMING ORDER 2514Y110 FOUND CONTACT BETWEEN THE SLIDE RAFT COVER AT DOOR L2 & THE FUSELAGE. NO DAMAGE FOUND. REPLACED L2 DOOR SLIDE BUSTLE & ADJUSTED HOLD DOWN STRAPS AS REQUIRED. PROPER CLEARANCE ACHIEVED. OK FOR SERVICE.Jun 16, 2014 · N114UW · Airbus A320214 · Escape SlideSDR USAA2014040800004Flashlight · inoperativeFORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED FWD FLIGHT ATTENDANT FLASHLIGHT.Apr 7, 2014 · N114UW · Airbus A320214 · Emergency EquipmentSDR USAA2014030400002Lens · missingEMERGENCY LIGHT LENS AT SEAT 1C MISSING. REPLACED EMERGENCY LIGHT LENS AT SEAT 1C.Mar 3, 2014 · N114UW · Airbus A320214 · Emergency LightingSDR USAA2013123100006Selector Valve · inoperativeDURING TAXI PARKING BRAKE WAS SET & ACFT BEGAN TO ROLL. WHEN PARKING BRAKE WAS RELEASED MAX BRAKING OCCURRED. RETURNED TO GATE WITH NORMAL BRAKING UNTIL NR 2 ENG SHUTDOWN, LOSS OF ALL BRAKING FOR ABOUT 2 SECONDS. AFTER ACFT WAS CHOCKED & ENG NR 1 SHUTDOWN LDec 30, 2013 · N114UW · Airbus A320214 · Landing Gear Brake SystemSDR USAA2013032100004Battery · dischargedEMERGENCY FLASHLIGHT BATTERY DEAD. REPLACED BATTERY IN AFT EMERGENCY FLASHLIGHT, OPERATIONAL CHECK GOOD.Mar 20, 2013 · N114UW · Airbus A320214 · Emergency EquipmentSDR USAA2013020500032Seal · deterioratedCREW REPORTED NR 1 ENGINE LOW OIL QUANTITY DROPPED TO ZERO FOLLOWED BY "OIL LO PR" ECAM MESSAGE. OIL PRESSURE INDICATED < 13 PSI ON ECAM ENG PAGE. THE NR 1 ENGINE WAS SHUT DOWN AND FLIGHT WAS DIVERTED TO CLT. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE ANDFeb 3, 2013 · N114UW · Airbus A320214 · Turbine Engine Oil SystemSDR USAA2013020400019Manifold · leakingAFTER TAKEOFF, CREW REPORTED STRONG FUMES IN FLIGHT DECK AND CABIN. FLIGHT RETURNED TO FIELD AT CLT. MAINTENANCE ACCOMPLISHED J/C 26L00021001 (CABIN ODO T/S). DETERMINED ODOR FROM APU DUE TO HYDRAULIC INGESTION FROM LEFT BRAKE MANIFOLD LEAKING. REMOVED ANDJan 31, 2013 · N114UW · Airbus A320214 · Landing Gear Brake SystemSDR USAA2013020100016Manifold · leakingCREW REPORTED FUMES AND SMOKE IN CABIN AFTER DEPARTING CLT. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND ODOR CAUSED BY INGESTION OF HYDRAULIC FLUID FROM LEAKING BRAKE MANIFOLD. REMOVED AND REPLACED LEFT NORMAL BRAKE MANIFOLD IAJan 30, 2013 · N114UW · Airbus A320214 · Landing Gear Brake SystemSDR USAA2012040200028Chiller · faultyFLIGHT ATTENDANTS REPORTED AN ELECTRICAL ODOR EN ROUTE. TURNED OFF CHILLERS AS A PRECAUTION AND ODOR DISSIPATED TEMPORARILY, RETURNED SHORTLY BEFORE LANDING. REMOVED AND REPLACED AFT CHILLER IAW MM 25-34-51.Mar 31, 2012 · N114UW · Airbus A320214 · Buffet/GalleysSDR USAA2011112800004Plate · corroded2S CHECK, CORROSION ON PROFILE PLATE BETWEEN FR 28 AND FR 34 AT S38R AND Z-500. REPLACED PROFILE PLATE BETWEEN FR 28 AND FR 34 AT S38R AND Z-500 IAW A320 SRM 51-23-11.Nov 27, 2011 · N114UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2011112400003Floor Panel · delaminated2S CHECK, FLOOR PANEL 231KF BETWEEN FR 24 AND FR 28 AT Y000 AND Z-500 HAS DELAMINATION. REPLACED FLOOR PANEL 231KF BETWEEN FR 24 AND FR 28 AT Y000 AND Z-500 IAW MCGILL IRM 9701 REV G.Nov 23, 2011 · N114UW · Airbus A320214 · Fuselage Floor PanelSDR USAA2011111800010Floor Panel · debonded2S CHECK - DEBONDED ON FLOOR PANEL 232LF BETWEEN FR24 TO FR28, -Y510, -Z500. REPLACED FLOOR PANEL 232LF IAW MCGILL IRM 9701 REV G.Nov 17, 2011 · N114UW · Airbus A320214 · Fuselage Floor PanelSDR USAA2011111800008Floor Panel · damaged2S CHECK - DAMAGE ON FLOOR PANEL 221PF BETWEEN FR12 TO FR16, Y1028, -Z500. REPLACED FLOOR PANEL 221PF IAW MCGILL IRM 9701 REV G.Nov 17, 2011 · N114UW · Airbus A320214 · Fuselage Floor PanelSDR USAA2011111800007Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 251RF BETWEEN FR58 TO FR62, Y=0, -Z500. REPLACED FLOOR PANEL 251RF IAW MCGILL IRM 9701 REV G.Nov 17, 2011 · N114UW · Airbus A320214 · Fuselage Floor PanelSDR USAA2011111800006Floor Panel · peeling2S CHECK - PEELING ON FLOOR PANEL 262BF BETWEEN FR64 TO FR66, -Y1028, -Z500. REPLACED FLOOR PANEL 262BF IAW MCGILL IRM 9701 REV G.Nov 17, 2011 · N114UW · Airbus A320214 · Fuselage Floor PanelSDR USAA2011111800005Floor Panel · peeling2S CHECK - PEELING ON FLOOR PANEL 231QF BETWEEN FR28 TO FR32, Y=0, -Z500. REPLACED FLOOR PANEL 231QF IAW MCGILL IRM 9701 REV G.Nov 17, 2011 · N114UW · Airbus A320214 · Fuselage Floor PanelSDR USAA2011111700015Floor Panel · debondedS2 CHECK - AREA OF DISBOND ON FLOOR PANEL 222EF BETWEEN FR16 TO FR20 & BETWEEN -Y200 TO -Y1292. REPLACED FLOOR PANEL 222EF IAW MCGILL IRM 9701 REV G.Nov 16, 2011 · N114UW · Airbus A320214 · Fuselage Floor PanelSDR USAA2011111700006Floor Panel · delaminatedS2 CHECK - DELAMINATION ON FLOOR PANEL 261DF AT BETWEEN FR66 TO FR68 & BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL 261DF IAW MCGILL IRM 9701 REVISION G.Nov 16, 2011 · N114UW · Airbus A320214 · Fuselage Floor PanelSDR USAA2011111700005Panel · corrodedS2 CHECK - LEVEL 2 SURFACE CORROSION ON FUEL PANEL 540HB AT WS 7792 BETWEEN S8L TO S11L, ALSO BETWEEN RIBS 13 TO 14. REPLACED FUEL PANEL 540HB IAW A320 SRM 57-27-11.Nov 6, 2011 · N114UW · Airbus A320214 · Wing, Plate/SkinSDR USAA2011111500011Floor Support · corrodedS2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT BETWEEN FR12 TO FR24, -Y254. REPLACED FLOOR SUPPORT BETWEEN FR12 TO FR24, -Y254 IAW A320 SRM 51-72-11.Nov 4, 2011 · N114UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2011111000023Panel · corrodedS2 CHECK - LEVEL 2 SURFACE CORROSION ON RIGHT WING FUEL PANEL 640NB, BETWEEN RIB 18 TO RIB 19. REPLACED RIGHT WING FUEL PANEL 640NB IAW A320 SRM 57-27-11 PAGE 103.Nov 4, 2011 · N114UW · Airbus A320214 · Wing, Plate/SkinSDR USAA2011112300012Mount Fitting · corroded2S CHECK - LEVEL 2 CORROSION ON R2 DOOR MOUNT FITTING. REPLACED R2 DOOR MOUNT FITTING IAW A320 SRM 51-72-11.Nov 1, 2011 · N114UW · Airbus A320214 · Service DoorsSDR USAA2011112300011Mount Fitting · corroded2S CHECK - LEVEL 2 CORROSION ON L2 DOOR MOUNT FITTING. REPLACED L2 DOOR MOUNT FITTING IAW A320 SRM 51-72-11.Nov 1, 2011 · N114UW · Airbus A320214 · Passenger/Crew DoorsSDR USAA2011111100011Sill · corroded2S CHECK - LEVEL 2 EXFOLIATION ON SILL PLATE AT FR68, S23R, -Y1500. REPLACED SILL PLATE AT FR68, S23R, -Y1500 IAW A320 SRM 51-72-11.Oct 31, 2011 · N114UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2011111500023Floorbeam · corrodedS2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, Y512.5. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, Y512.5 IAW A320 SRM 51-72-11.Oct 29, 2011 · N114UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2011111500021Floorbeam · corrodedS2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, Y512.5. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, Y512.5 IAW A320 SRM 51-72-11.Oct 29, 2011 · N114UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2011111500017Shear Plate · corrodedS2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON LEFT SHEAR PLATE BETWEEN FR69 TO FR70, Y1160. REPLACED LEFT SHEAR PLATE BETWEEN FR69 TO FR70, Y1160 IAW A320 SRM 51-72-11 & AIRBUS DRAWING 18D53474180.Oct 29, 2011 · N114UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2011111500016Floorbeam · corrodedS2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR Z-BEAM BETWEEN FR68 TO FR70, Y1162.5. REPLACED FLOOR Z-BEAM BETWEEN FR68 TO FR70, Y1162.5 IAW A320 SRM 51-72-11.Oct 29, 2011 · N114UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2011111500015Floorbeam · corrodedS2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR Z-BEAM BETWEEN FR66 TO FR68, Y1162.5. REPLACED FLOOR Z-BEAM BETWEEN FR66 TO FR68, Y1162.5 IAW A320 SRM 51-42-11.Oct 29, 2011 · N114UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2011111500014Floorbeam · corrodedS2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR Z-BEAM BETWEEN FR64 TO FR66, Y1292. REPLACED FLOOR Z-BEAM BETWEEN FR64 TO FR66, Y1292 IAW A320 SRM 51-42-11.Oct 29, 2011 · N114UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2011110900004Shear Plate · cracked2S CHECK - CRACK ON SHEAR PLATE AT FR68, S23L, Y1160. REPLACED SHEAR PLATE AT FR68, S23L, Y1160 IAW A320 SRM 51-31-00, PAGE 22 TABLE 4.Oct 29, 2011 · N114UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2011110700005Floorbeam · corrodedS2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON UPPER SURFACE OF FLOORBEAM AT FR65+22", S23L, Y765. REPLACED FLOORBEAM AT FR65+22", S23L, Y765 IAW A320 SRM 51-42-00.Oct 29, 2011 · N114UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2011110700004Floorbeam · corrodedS2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON UPPER SURFACE OF FLOORBEAM AT FR70, S23L, Y765. REPLACED FLOORBEAM AT FR70, S23L, Y765 IAW A320 SRM 51-42-00.Oct 29, 2011 · N114UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2011111500020Floorbeam · corrodedS2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR66, -Y1292. REPLACED FLOORBEAM AT FR66, -Y1292 IAW A320 SRM 51-42-11.Oct 28, 2011 · N114UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2011111500019Floorbeam · corrodedS2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, -Y1162.5. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, -Y1162.5 IAW A320 SRM 51-42-11 & 51-72-11.Oct 28, 2011 · N114UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2011111500018Floorbeam · corrodedS2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR68 TO FR70, -Y1162.5. REPLACED FLOORBEAM BETWEEN FR68 TO FR70, -Y1162.5 IAW A320 SRM 51-42-11.Oct 28, 2011 · N114UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2011111500013Floorbeam · corrodedS2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR66 TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR66 TO FR70, -Y765 IAW A320 SRM 51-42-11.Oct 28, 2011 · N114UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2011110500002Shear Plate · corroded2S CHECK - LEVEL 2 INTERGRANULAR CORROSION ON AFT SHEAR PLATE BETWEEN FR69 TO FR70, -Y1160. REPLACED AFT SHEAR PLATE BETWEEN FR69 TO FR70, -Y1160 IAW A320 SRM 51-74-00 AND AIRBUS DRAWING 18D53474180.Oct 28, 2011 · N114UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2011111500012Floor Support · corrodedS2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT BETWEEN FR20 TO FR24, -Y189. REPLACED FLOOR SUPPORT BETWEEN FR20 TO FR24, -Y189 IAW A320 SRM 51-72-11.Oct 27, 2011 · N114UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2011111100010Floorbeam · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR12 TO FR16, -Y81. REPLACED FLOORBEAM BETWEEN FR12 TO FR16, -Y81 IAW A320 SRM 51-72-11.Oct 27, 2011 · N114UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2011111000003Floorbeam · corrodedS2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR16 TO FR24, -Y765. REPLACED FLOORBEAM BETWEEN FR16 TO FR24, -Y765 IAW A320 SRM 51-72-11.Oct 27, 2011 · N114UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2011110800011Seat Track · corrodedS2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, Y765. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, Y765 IAW A320 SRM 51-72-11.Oct 27, 2011 · N114UW · Airbus A320214 · Fuselage, Seat/Cargo Attach Fittings
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