N188US

Service difficulty reports · 285

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 = 'N188US' 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 USAA2014080100004Lens · missingTHE SEAT MOUNTED EXIT RED LENS MISSING AT SEAT 9D. REPLACED SEAT MOUNTED EXIT RED LENS AT SEAT 9D. LIGHTS OPERATIONS CHECKED GOOD. OK FOR SERVICE.Jul 31, 2014 · N188US · Airbus A321211 · Emergency LightingSDR USAA2014072100025Cover · missingTHE EXIT SIGN COVER BY DOOR 2R MISSING. INSTALLED MISSING EXIT COVER AT 2R DOOR IAW AMM 33-50-00.Jul 21, 2014 · N188US · Airbus A321211 · Emergency LightingSDR USAA2014072100021Cover · missingEMER LIGHT COVER 1C MISSING. REPLACED MISSING EMER LIGHT COVER AT 1C, GOOD TO GO.Jul 19, 2014 · N188US · Airbus A321211 · Emergency LightingSDR USAA2014070300003Placard · missingTHE ARMED & DISARMED PLACARDS MISSING ON R1 DOOR. INSTALLED TEMPORARY PLACARDS WITH A RECHECK EVERY 7 DAYS & PROGRAMMED FOR PERMANENT INSTALLATION OF PLACARDS WITHIN 60 DAYS.Jun 29, 2014 · N188US · Airbus A321211 · Placards and MarkingsSDR USAA2014061100002Actuator Valve · faultyEN ROUTE FROM PHL TO SFO, CREW REPORTED AN ACT 1 FUEL FAULT TRAPPING 5,200 POUNDS OF FUEL IN THE TANK. FLIGHT DESCENDED TO FL260 IAW QRH. FUEL WAS NOT ENOUGH TO CONTINUE TO SFO, SO THE FLIGHT WAS DIVERTED TO ORD. FLIGHT LANDED WITHOUT INCIDENT. R & R THE 5Jun 9, 2014 · N188US · Airbus A321211 · Aircraft Fuel Distribution SystemSDR USAA2014060600012Actuator · faultyEN ROUTE FROM LAX TO PHL, CREW RECEIVED A FUEL ACT NR 1 XFERED FAULT. THERE WAS 5,300 LBS IN NR 1 ACT. FLIGHT DIVERTED TO DFW & LANDED WITHOUT INCIDENT. INSTALLED NEW ACT TRANSFER VLV ACTUATOR IAW AMM 28-28-28-53-400-001-A. ACCOMPLISHED SUCCESSFUL OPERATIOJun 4, 2014 · N188US · Airbus A321211 · Fuel Transfer ValveSDR USAA2014052900012Fire Bottle · failedAPU FIRE EXTINGUISHER BOTTLE FAILED HYDROSTATIC CHECK. REPLACED APU FIRE EXTINGUISHER IAW ROUTINE JOB CARD 26C31026002 & OPERATIONAL CHECK IAW JOB CARD 26C31026003.May 28, 2014 · N188US · Airbus A321211 · Fire Bottle, FixedSDR USAA2014052700029Floor Panel · delaminatedS2 CHECK DELAMINATION ON FLOOR PANEL 232ZH AT FRAME 35.3, Z-500, -Y509.5. REPLACED FLOOR PANEL 232ZH IAW IRM 9701, REV G.May 25, 2014 · N188US · Airbus A321211 · Fuselage Floor PanelSDR USAA2014052700028Floor Panel · delaminatedS2 CHECK DELAMINATION ON FLOOR PANEL 231ZH AT FRAME 35.3, Z-500, Y509.5. REPLACED FLOOR PANEL 231ZH IAW IRM 9701, REV G.May 25, 2014 · N188US · Airbus A321211 · Fuselage Floor PanelSDR USAA2014052700027Floor Panel · delaminatedS2 CHECK DELAMINATION ON FLOOR PANEL 241EF AT FRAME 39, Z-500, Y=0. REPLACED FLOOR PANEL 241EF IAW IRM 9701, REV G.May 25, 2014 · N188US · Airbus A321211 · Fuselage Floor PanelSDR USAA2014052700026Floor Panel · delaminatedS2 CHECK DELAMINATION ON FLOOR PANEL 231NG AT FRAME 37.5, Z-500, Y=0. REPLACED FLOOR PANEL 231NG IAW IRM 9701, REV G.May 25, 2014 · N188US · Airbus A321211 · Fuselage Floor PanelSDR USAA2014052700025Floor Panel · delaminatedS2 CHECK DELAMINATION ON CABIN FLOOR PANEL 261DF AT FRAME 67, Z-500, Y=0. REPLACED CABIN FLOOR PANEL 261DF IAW IRM 9701, REV G.May 25, 2014 · N188US · Airbus A321211 · Fuselage Floor PanelSDR USAA2014052700024Floor Panel · delaminatedS2 CHECK DELAMINATION ON CABIN FLOOR PANEL 261CG AT FRAME 65, Z-500, Y=0. REPLACED CABIN FLOOR PANEL 261CG IAW IRM 9701, REV G.May 25, 2014 · N188US · Airbus A321211 · Fuselage Floor PanelSDR USAA2014052700023Floor Support · crackedS2 CHECK CRACK IN FLOOR SUPPORT BEAM AT FRAME 35.1, STRINGER 35R. REPLACED FLOOR SUPPORT BEAM AT FRAME 35.1, STRINGER 35R IAW SRM 51-42-11 & DWG C4 D53235151.May 23, 2014 · N188US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2014052200013Slide · faulty2S CHECK UPON INSTALLATION OF LT AFT PAX CREW DOOR SLIDE FOUND SLIDE CONNECTOR WOULD NOT ATTACH TO DOOR CONNECTOR RECEPTACLE. INSTALLED NEW SLIDE IAW JOB CARD 6C83252020.May 21, 2014 · N188US · Airbus A321211 · Escape SlideSDR USAA2014052100008Floor Support · crackedS2 CHECK CRACK IN FWD CARGO FLOOR PANEL SUPPORT BETWEEN FRAME 32 TO FRAME 33, STRINGER 38L, Z-1900. REPAIRED FWD CARGO FLOOR PANEL SUPPORT BETWEEN FRAME 32 TO FRAME 33, STRINGER 38L, Z-1900 IAW EA 207558.May 20, 2014 · N188US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2014051900027Floorbeam · corrodedS2 CHECK CORROSION ON FLOORBEAM AT FRAME 47.4, Z-500, -Y1589. REPLACED FLOORBEAM AT FRAME 47.4, Z-500, -Y1589 IAW SRM 51-72-11.May 16, 2014 · N188US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA2014051200035Floorbeam · corrodedS2 CHECK, LEVEL 2 INTERGRANULAR CORROSION ON UPPER SURFACE OF FLOORBEAM AT FRAME 66, Y1292. REPLACED FLOORBEAM AT FRAME 66, Y1292 IAW SRM 51-42-11.May 10, 2014 · N188US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA2014051300009Door Sill · corrodedS2 CHECK LEVEL 2 EXFOLIATION CORROSION ON L4 DOOR SILL AT FRAME 68, Z -500. REPAIRED L4 DOOR SILL AT FRAME 68, Z -500 IAW SRM 53-41-14-001 & EA 207421.May 9, 2014 · N188US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2014051200017Tray · crackedS2 CHECK, CRACK IN TRAY BETWEEN FRAME 68 TO FRAME 69, STRINGER 23R, Z-500, -Y1162.5. REPLACED TRAY BETWEEN FRAME 68 TO FRAME 69, STRINGER 23R, Z-500, -Y1162.5 IAW SRM 51-72-11.May 8, 2014 · N188US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2014050800005Floorbeam · corrodedS2 CHECK LEVEL 2 EXFOLIATION CORROSION ON CABIN FLOORBEAM AT FRAME 16, Z-500, Y503. REPLACED CABIN FLOORBEAM AT FRAME 16, Z-500, Y503 IAW SRM 51-72-11.May 7, 2014 · N188US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA2014050600022Floorbeam · corrodedS2 CHECK LEVEL 2 SURFACE CORROSION ON CABIN FLOORBEAM AT FRAME 66, Z-500, Y765. REPLACED CABIN FLOORBEAM AT FRAME 66, Z-500, Y765 IAW SRM 51-42-11, 51-72-11 & DWG D53472831 & D53472815.May 4, 2014 · N188US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA2014050600020Shear Plate · corrodedS2 CHECK LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FRAME 69 TO FRAME 70 & BETWEEN STRINGER 23L TO STRINGER 24L, Z-500. REPLACED SHEAR PLATE BETWEEN FRAME 69 TO FRAME 70 & BETWEEN STRINGER 23L TO STRINGER 24L, Z-500 IAW SRM 51-72-11.May 3, 2014 · N188US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2014051500006Fitting · corrodedS2 CHECK LEVEL 2 EXFOLIATION CORROSION ON FWD CARGO SKIN CLIP AT FRAME 32, STRINGER 43L. REPLACED FWD CARGO SKIN CLIP AT FRAME 32, STRINGER 43L IAW SRM 51-42-11.Apr 30, 2014 · N188US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2014060200024Access Panel · corrodedS2 CHECK LEVEL 2 FRETTING CORROSION ON LT WING LOWER FUEL PANEL 540KB BETWEEN RIB 15 TO 16 & BETWEEN STRINGER 8L TO 11L. REPLACED LT WING LOWER FUEL PANEL 540KB IAW SRM 57-27-11.Apr 29, 2014 · N188US · Airbus A321211 · Wing, Plate/SkinSDR USAA2014050700003Access Panel · corroded2S CHECK LT WING FUEL ACCESS PANEL 550BB CORRODED AT FASTENER HOLES. R & R ACCESS PANEL IAW SRM 57-27-11.Apr 29, 2014 · N188US · Airbus A321211 · Wing, Plate/SkinSDR USAA2014051300014Seat Track · corrodedS2 CHECK LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK AT FRAME 24, Z -500, -Y1292. REPAIRED SEAT TRACK AT FRAME 24, Z -500, -Y1292 IAW SRM 53-11-01-05.Apr 26, 2014 · N188US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2014051200034Floorbeam · corrodedS2 CHECK, LEVEL 2 INTERGRANULAR CORROSION ON UPPER SURFACE OF FLOORBEAM AT FRAME 66, Y1292. REPLACED FLOORBEAM AT FRAME 66, Y1292 IAW SRM 51-42-11.Apr 26, 2014 · N188US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA2014051200019Floorbeam · corrodedS2 CHECK, LEVEL 2 INTERGRANULAR CORROSION ON AFT SECTION OF FLOORBEAM AT FRAME 68, Z-500, -Y1160. REPLACED FLOORBEAM AT FRAME 68, Z-500, -Y1160 IAW SRM 51-72-11 & IPC 53-41-04-21.Apr 26, 2014 · N188US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA2014051200018Floorbeam · corrodedS2 CHECK, LEVEL 2 INTERGRANULAR CORROSION UPPER SURFACE OF FLOORBEAM BETWEEN FRAME 66 TO FRAME 67, Z-500, -Y1292. REPLACED FLOORBEAM BETWEEN FRAME 66 TO FRAME 67, Z-500, -Y1292 IAW SRM 51-42-11.Apr 26, 2014 · N188US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA2014050900001Door Sill · corrodedS2 CHECK, LEVEL 2 SURFACE CORROSION ON R4 DOOR SILL AT FRAME 68, Z-500, -Y1589. REPAIRED R4 DOOR SILL AT FRAME 68, Z-500, -Y1589 IAW SRM 53-41-14-201, REPAIR PRINCIPLE 5 & EA 207457.Apr 26, 2014 · N188US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2014050800004Door Sill · corrodedS2 CHECK LEVEL 2 EXFOLIATION CORROSION ON R1 DOOR SILL BETWEEN FRAME 16 TO FRAME 20, Z-500, -Y1584. REPLACED R1 DOOR SILL BETWEEN FRAME 16 TO FRAME 20, Z-500, -Y1584 IAW SRM 51-72-11 & 51-75-12.Apr 26, 2014 · N188US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2014050700002Floorbeam · corroded2S CHECK CABIN FLOORBEAM CORRODED AT FRAME 16, W -500 & Y -81. R & R FLOORBEAM IAW SRM 51-72-11 & DWG D53112828.Apr 26, 2014 · N188US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA2014050600021Door Sill · corrodedS2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON L4 DOOR WAY CTR SHAPE SILL BETWEEN FRAME 66 TO FRAME 68 & BETWEEN Z-500, Y1292. REPLACED L4 DOOR WAY CTR SHAPE SILL BETWEEN FRAME 66 TO FRAME 68 & BETWEEN Z-500, Y1292 IAW SRM 51-72-11 & DWG D53480048.Apr 26, 2014 · N188US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2014050600019Seat Track · corrodedS2 CHECK LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FRAME 21 TO FRAME 23, Z-500, -Y 765. REPLACED SEAT TRACK BETWEEN FRAME 21 TO FRAME 23, Z-500, -Y765 IAW SRM 51-27-11.Apr 26, 2014 · N188US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013121000001Floor Panel · damagedSPONGY FLOOR PANEL 261EF AT FR 67, STRINGER 23L. REPLACED FLOOR PANEL 261EF IAW A321 AMM 53-42-12-0401.Dec 9, 2013 · N188US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013120900013Wire Harness · failedMAINTENANCE REPORTED ROW 34ABC SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. FOUND SEAT HARNESS TO HAVE FAILED. INSTALLED SERVICEABLE ELEC HARNESS FOR SEAT 34ABC IAW EO 2512E103. LIGHT OPERATIONS CHECKED GOOD.Dec 6, 2013 · N188US · Airbus A321211 · Light System WiringSDR USAA2013103100002Smoke Detector · faultedDURING TAXI OUT, CREW RECEIVED STATUS MESSAGE FOR SMOKE DETECTOR. MAINTENANCE REPLACED LAVATORY "D" SMOKE DETECTOR IAW 26-17-15-400-001-A. OPS CHECKED NORMAL.Oct 30, 2013 · N188US · Airbus A321211 · Smoke DetectionSDR USAA2013090900028Light · dislodged9D EMERGENCY EXIT LIGHT FELL OFF. SECURED EMERGENCY EXIT LIGHT AT 9D.Sep 6, 2013 · N188US · Airbus A321211 · Emergency LightingSDR USAA2013082300008Light · missingLAV L EMERGENCY LIGHT MODULE MISSING. INSTALLED EMERGENCY LIGHT MODULE AT LAV L.Aug 22, 2013 · N188US · Airbus A321211 · Emergency LightingSDR USAA2013082200010Light · bentEMERGENCY EXIT LIGHT AT SEAT 9D BENT AND PARTIALLY DETACHED. STRAIGHTENED AND SECURED EMERGENCY LIGHT.Aug 21, 2013 · N188US · Airbus A321211 · Emergency LightingSDR USAA2013072900011Fire Bottle · dischargedAFT RIGHT LAV WASTE CONTAINER FIRE BOTTLE FLAT. R & R AFT RT LAV FIRE BOTTLE IAW AMM 26-25-41.Jul 27, 2013 · N188US · Airbus A321211 · Extinguishing SystemSDR USAA2013050300002Unknown · hazeELECTRICAL ODOR OF FIRE OR FUMES UPON LANDING. FLIGHT ATTENDANT REPORTED HAZE AND ODOR WHICH CONTINUED TO INTENSIFY TO THE POINT FLIGHT ATTENDANTS AND PASSENGERS WERE EXPERIENCING DIFFICULTY WITH EYES AND BREATHING. PERFORMED SATIFACTORY CHECK OF NR 2 PACK IMay 2, 2013 · N188US · Airbus A321211 · Air Distribution SystemSDR USAA2013031100019Lens · missingEMERGENCY EXIT LIGHT LENS MISSING OVER 4L DOOR. REPLACED MISSING EMERGENCY EXIT LIGHT LENS AT 4L DOOR.Mar 8, 2013 · N188US · Airbus A321211 · Emergency LightingSDR USAA2013021800008Lens · missingROW 9D EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED EMERGENCY LIGHT LENS AT SEAT 9D.Feb 17, 2013 · N188US · Airbus A321211 · Emergency LightingSDR USAA2013012200030Hydraulic Line · leakingFLIGHT CREW EXPERIENCED LOSS OF YELLOW HYDRAULIC PRESSURE ENROUTE FROM MBJ TO PHL AND REPORTED 'HYD Y LO LEVEL' FAULT. AN EMERGENCY WAS DECLARED FOR LANDING. MAINTENANCE FOUND NR 2 ENGINE HYDRAULIC TUBE LEAKING. REPLACED TUBE.Jan 19, 2013 · N188US · Airbus A321211 · Hydraulic System, MainSDR USAA2013010800005Proximity Switch · defectiveDOOR 4R DISARMED ITSELF ON DESCENT INTO KBOS - INDICATION LIGHT NEVER CAME BACK ON. MAINTENANCE REMOVED AND REPLACED ARM HANDLE PROXIMITY SWITCH (7WN2) IAW AIRBUS MAINTENANCE MANUAL 52-73-11-400-002-A.Jan 4, 2013 · N188US · Airbus A321211 · Door Warning SystemSDR USAA2012120700015Stringer · corrodedIFE (GOGO) INSTALLATION. FUSELAGE STRINGER 43L CORRODED BETWEEN FR 55 AND FR 58. REPAIRED STRINGER IAW EA 203929.Dec 6, 2012 · N188US · Airbus A321211 · Fuselage Main, Longeron/StringerSDR USAA2012102200023Light · brokenEMERGENCY LIGHT ON SEAT 8D BROKEN / MISSING. MAINTENANCE REPLACED / SECURED LIGHT ASSEMBLY.Oct 19, 2012 · N188US · Airbus A321211 · Emergency LightingSDR USAA2012082000006Light · brokenEMERGENCY EXIT LIGHT AT SEAT 9D BROKEN. RE-INSTALLED EMERGENCY EXIT LIGHT AT SEAT ROW 9D.Aug 18, 2012 · N188US · Airbus A321211 · Emergency Lighting
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