N181UW

Service difficulty reports · 364

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 = 'N181UW' 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 USAA2013071600051Fitting · corroded2S CHECK - CORROSION ON CENTER SHAPE SILL FITTING BETWEEN FR66 TO FR68, S23L. REPLACED CENTER SHAPE SILL FITTING IAW SRM 51-72-11 & DWG D53480505.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013071600050Fitting · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON CORNER FITTING AT FR20, S20R. REPLACED CORNER FITTING IAW SRM 51-72-11 & DWG D53112109.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013071600048Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL FITTING BETWEEN FR16 TO FR20, S23R, -Y1758. REPLACED LOWER SILL FITTING IAW SRM 51-72-11 & DWG D53110339.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013071600044Fitting · corroded2S CHECK, CORROSION ON CENTER FITTING BETWEEN FR16 TO FR20, S23R. REPLACED CENTER FITTING IAW SRM 51-72-11 & DWG D53112109.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013071600043Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON ANGLE FITTING AT FR20, S23L. REPLACED ANGLE FITTING AT FR20, S23L IAW SRM 51-72-11 & DWG D53112784.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013071600038Structure · corroded2S CHECK - CORROSION ON COUPLING AT FR67+16", -Y1292. REPLACED COUPLING IAW SRM 51-72-11 & DWG 53472780.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013071600037Structure · corroded2S CHECK - CORROSION ON COUPLING AT FR67+6", Y1162. REPLACED COUPLING IAW SRM 51-72-11 & DWG 53472780.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013071600036Structure · elongated2S CHECK - 1.007" ELONGATED HOLE ON COUPLING AT FR66, S23L. REPLACED COUPLING IAW SRM 51-72-11 AND DWG D53474250.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013071600035Structure · elongated2S CHECK - .215" ELONGATED HOLE ON COUPLING AT FR66, S23L. REPLACED COUPLING IAW SRM 51-72-11 DWG D53474250.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013071600034Structure · elongated2S CHECK - .249" ELONGATED HOLE ON COUPLING AT FR66, S23R. REPLACED COUPLING IAW SRM 51-72-11, DWG D53480505 AND D53474250.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013071600033Structure · damaged2S CHECK - .244" ELONGATED HOLE ON COUPLING AT FR66, S23R. REPLACED COUPLING AT FR66, S23R IAW SRM 51-72-11, DWG D53480505 AND D53474250.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013071600026Seat Track · corroded2S CHECK - CORROSION ON DUMMY RAIL BETWEEN FRAMES 12 - 16, -Y81. REPLACED DUMMY RAIL IAW SRM 51-72-11 & DWG D53112828.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013071600024Plate · corroded2S CHECK - CORROSION ON SHEAR PLATE BETWEEN FRAMES 69 - 70, S23L. REPLACED SHEAR PLATE IAW SRM 51-72-11 & DWG D53474180.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013071600023Floor Support · corroded2S CHECK - CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 12 - 24, -Y254. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 & DWG D53111462.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013071600022Floor Support · corroded2S CHECK - CORROSION ON FLOOR SUPPORT BETWEEN FR 66+5" TO FR 70, -Y765. REPLACED FLOOR SUPPORT IAW SRM 51-72-11, DWG D53472816 AND D53472093.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013071100043Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR24, -Y765. REPLACED SEAT TRACK AT FR24, -Y765 IAW SRM 51-72-11, DWG D53112812 AND D53115054.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013071100040Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR20 TO FR24, -Y189. REPLACED SEAT TRACK BETWEEN FR20 TO FR24, -Y189 IAW SRM 51-72-11 AND DWG D53111406.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013071100039Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, Y1292 IAW SRM 51-72-11, DWG D53112812 & D53115054.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013071100038Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y1292 IAW SRM 51-72-11, DWG D53110984 & D53112812.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013071100031Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR66+5" TO FR64, -Y1292. REPLACED SEAT RAIL BETWEEN FR66+5" TO FR64, -Y1292 IAW SRM 51-72-11 & DWG D53472816.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013071100019Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR65 TO FR67, -Y318. REPLACED FLOORBEAM BETWEEN FR65 TO FR67, -Y318 IAW SRM 51-72-11 AND DWG 53472814.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA2013071100018Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+5" TO FR70, Y765. REPLACED FLOORBEAM BETWEEN FR66+5" TO FR70, Y765 IAW SRM 51-72-11, DWG D53472780 AND D53472815.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA2013071100017Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+5" TO FR67+16", -Y1292. REPLACED FLOORBEAM BETWEEN FR66+5" TO FR67+16", -Y1292 IAW SRM 51-72-11 AND DWG D53474250.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA2013071100016Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67+16" TO FR69+3",-Y1162. REPLACED FLOORBEAM BETWEEN FR67+16" TO FR69+3", -Y1162 IAW SRM 51-72-11 AND DWG D53472780.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA2013071100015Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67+16" TO FR69+3", Y1162. REPLACED FLOORBEAM BETWEEN FR67+16" TO FR69+3", Y1162 IAW SRM 51-72-11 & DWG D53472780.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA2013071100014Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+5" TO FR67+16" & Y1292 TO Y1162. REPLACED FLOORBEAM BETWEEN FR66+5" TO FR67+16" & Y1292 TO Y1162 IAW SRM 51-72-11 & DWG D53472815.Jun 20, 2013 · N181UW · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA2013072200035Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY AT RUDDER HINGE ARM FITTING NR 4 AT RUDDER STA 263, RIB 6. REPLACED RUDDER HINGE ARM FITTING IAW SRM 51-72-11 & AMM 55-36-41 & EA 504179A.Jun 19, 2013 · N181UW · Airbus A321211 · Rudder StructureSDR USAA2013072200020Hinge Fitting · worn2S CHECK - EXCESSIVE PLAY AT RUDDER HINGE ARM FITTING NR 3 AT RUDDER STA 228, RIB 5. REPLACED RUDDER HINGE ARM FITTING NR 3 AT RUDDER STA 228, RIB 5 IAW SRM 51-72-11 & AMM 55-36-41-400-001-A.Jun 19, 2013 · N181UW · Airbus A321211 · Rudder StructureSDR USAA2013072200019Skin · worn2S CHECK - WEAR AREA ON LEFT WING NR 1 SLAT NOSE SKIN AT TRACK NR 2 CLOSING PLATE AREA. REPAIRED LT WING NR 1 SLAT NOSE SKIN AT TRACK NR 2 CLOSING PLATE AREA IAW EA 504176.Jun 19, 2013 · N181UW · Airbus A321211 · Leading Edge DevicesSDR USAA2013071100029Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 151GF BETWEEN FR52 TO FR56 & BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL 151GF IAW SRM 53-02-00, PAR. 8H, FIG 209 AND IRM 9701, REV G.Jun 19, 2013 · N181UW · Airbus A321211 · Fuselage Floor PanelSDR USAA2013071100026Floor Panel · cracked2S CHECK - CRACK ON FLOOR PANEL 151HF BETWEEN FR52 TO FR56 & BETWEEN Y970.8 TO Y1353. REPLACED FLOOR PANEL 151HF IAW SRM 53-02-00, PAR.8H, FIG 209 AND IRM 9701, REV G.Jun 19, 2013 · N181UW · Airbus A321211 · Fuselage Floor PanelSDR USAA2013062600006Floor Panel · delaminated2S CHECK. CABIN FLOOR PANEL FROM FR 56 TO FR 58 AND Y765 TO Y -765 DELAMINATED. R & R PANEL IAW SRM 53-02-00, FIG 209 AND IRM 9701, REV G.Jun 19, 2013 · N181UW · Airbus A321211 · Fuselage Floor PanelSDR USAA2013061200026O-Ring · damagedSTRONG ODOR DETECTED IN CABIN AND COCKPIT. F/A`S COMPLAINED OF SMELL. PARAMEDICS MET CREW AT THE GATE AND ONE F/A WAS ADMINISTERED OXYGEN. ALL 4 CREW MEMBERS WERE PHYSICALLY DEEMED OK. ACCOMPLISHED TROUBLESHOOTING AIR QUALITY JOB CARDS, FOUND ENGINE NR 2 WJun 9, 2013 · N181UW · Airbus A321211 · Turbine Engine Oil SystemSDR USAA2013053000009Bracket · brokenSEAT 9D EMERGENCY EXIT LIGHT BRACKET BROKEN. REPLACED EMERGENCY EXIT LIGHT BRACKET.May 29, 2013 · N181UW · Airbus A321211 · Emergency LightingSDR USAA2013051000007Battery · inoperativeAFT LEFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT.May 9, 2013 · N181UW · Airbus A321211 · Emergency EquipmentSDR USAA2013041500007Line · damagedON APPROACH TO CLT GOT "G HYD RSVR LO LVL" ECAM MESSAGE, AN EMERGENCY WAS DECLARED AND CAPTAIN REQUESTED EMERGENCY EQUIPMENT AT THE RUNWAY. FLIGHT LANDED WITHOUT INCIDENT AND WAS ABLE TO TAXI TO THE GATE. REPLACED NORMAL BRAKE LINE IN AFT CARGO COMPARTMENT IApr 13, 2013 · N181UW · Airbus A321211 · Landing Gear Brake SystemSDR USAA2012081600013Smoke Detector · false activationECAM MESSAGE FOR LAV SMOKE WHICH DISAPPEARED WITHIN 5 SECONDS. FLIGHT ATTENDANT ALSO REPORTED ALARM FROM AFT RIGHT LAV. THERE WAS NO OBVIOUS EXPLANATION FOR ALARM, NO DEFECTS NOTED AND NO REPEAT EVENTS TO DATE.Aug 15, 2012 · N181UW · Airbus A321211 · Smoke DetectionSDR USAA2012081000013Fan · faultyELECTRICAL SMELL IN CABIN AFTER TURNING ON EXTERNAL POWER. FORWARD CABIN RECIRCULATION FAN INOPERATIVE. REMOVED AND REPLACED FAN 15HG IAW AIRBUS MAINTENANCE MANUAL 21-21-51-400-001-A.Aug 7, 2012 · N181UW · Airbus A321211 · Air Distribution FanSDR USAA2011120600024Lens · missingRED COVER PLATE (EMERGENCY EXIT) MISSING 8D (AISLE). INSTALLED RED EMERGENCY LIGHT LENS SEAT 8D.Dec 5, 2011 · N181UW · Airbus A321211 · Emergency LightingSDR USAA2011100300016Arming Lever · looseDOOR 2R SLIDE ARMING LEVER IS LOOSE. MAINTENANCE TIGHTENED AND SECURED 2R DOOR ARMING HANDLE.Sep 30, 2011 · N181UW · Airbus A321211 · Service DoorsSDR USAA2011061500018Rib · crackedPIT - GEAR CHANGE - CRACK IN LEFT MAIN LANDING GEAR RIB 5 SUPPORT FITTING FORWARD LUG BORE. REMOVED CRACK IN THE LEFT MAIN LANDING GEAR RIB 5 SUPPORT FITTING FORWARD LUG BY OVERSIZING THE BORE IAW EA 200035.Jun 11, 2011 · N181UW · Airbus A321211 · Wing, Rib/BulkheadSDR USAA2011061500017Floor Panel · delaminatedPIT - GEAR CHANGE - DELAMINATION ON FLOOR PANEL 261DF BETWEEN FR66 TO FR68 & BETWEEN Y515 TO -Y465. REPLACED FLOOR PANEL 261DF IAW MCGILL IRM 9701 REV G.Jun 9, 2011 · N181UW · Airbus A321211 · Fuselage Floor PanelSDR USAA2011031091019Bottle · low pressureFLT 1433 - CLT - EES - CIDS CAUTION LIGHT FOR R3 DOOR. MAINTENANCE SERVICED R3 DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.Mar 9, 2011 · N181UW · Airbus A321211 · Emergency ExitsSDR USAA2011011390191Lens · missingMX - LAX - EEL - DOOR 4R EMERGENCY LIGHT MISSING LENS. MAINTENANCE REPLACED DOOR EMERGENCY LIGHT COVER AS REQUIRED.Jan 12, 2011 · N181UW · Airbus A321211 · Emergency LightingSDR USAA2011010390001Reservoir · low pressureFLT 1511 - LGA-CLT - EMERGENCY EGRESS SYSTEM - CIDS CAUTION LIGHT ILLUMINATED - L3 EXIT SLIDE PRESSURE. REMOVED AND REPLACED L3 DOOR ESCAPE SLIDE INFLATION PER AMM 25-62-49. PRESSURE CHECKED GOOD.Dec 31, 2010 · N181UW · Airbus A321211 · Escape SlideSDR USAA2010101892307Bottle · low pressureFLT 1498 - LAX - EES - 3-L SLIDE RESERVOIR BOTTLE LOW PRESSURE. MAINTENANCE REPLACED SLIDE RESERVOIR ASSEMBLY IAW AIRBUS MAINTENANCE MANUAL 25-62-49.Oct 15, 2010 · N181UW · Airbus A321211 · Escape SlideSDR USAA2010061091098Lens · missingFLT 122 - CLT - EEL - EMERGENCY LIGHTS (FLOOR LEVEL) LENS MISSING AT SEAT 9-D. MAINTENANCE REPLACED THE EMERGENCY LIGHT LENS AT SEAT 9-D.Jun 9, 2010 · N181UW · Airbus A321211 · Emergency LightingSDR USAA2010021190341Lens · brokenFLT 932 - PHX - EEL - EMERGENCY EXIT SIGN 4L NEEDS REPAIR. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT LENS AT DOOR 4L.Feb 10, 2010 · N181UW · Airbus A321211 · Emergency LightingSDR USAA2010012290161Actuator · low pressureFLT 1624 - ORD - EES - CIDS CAUTION LIGHT ON FAULTING DOOR MID L. SERVICED LT FORWARD MID EXIT DOOR PER AIRBUS MAINTENANCE MANUAL 52-22-00-03-614-002.Jan 21, 2010 · N181UW · Airbus A321211 · Emergency ExitsSDR USAA2010011990118Cylinder · lowFLT NR 9205- R-2 DOOR LOW DOOR ASSIST BOTTLE PRESSURE. MAINTENANCE SERVICED DOOR ASSIST BOTTLE.Jan 15, 2010 · N181UW · Airbus A321211 · Service Doors
Back to N181UW