N119US

Service difficulty reports · 340

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 = 'N119US' 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 USAA2011122200001Lens · broken2S CHECK - RIGHT EMERGENCY EXIT DOOR EXIT SIGN LENS BROKEN. REPLACED BROKEN RIGHT EMERGENCY EXIT DOOR EXIT SIGN LENS IAW A320 AMM 33-51-16-0401.Dec 21, 2011 · N119US · Airbus A320214 · Emergency LightingSDR USAA2011122200012Bolt · worn2S CHECK - NR 2 SPOILER CENTER HINGE FITTING BOLT IS WORN. REPLACED NR 2 SPOILER CENTER HINGE FITTING BOLT IAW A320 AMM 20-22-0.Dec 19, 2011 · N119US · Airbus A320214 · SpoilersSDR USAA2011122700006Slide Raft · defective2S CHECK - OVER INFLATED SLIDE RAFT AT DOOR 832. REPACKED SLIDE RAFT AT DOOR 832 IAW A320 CMM 25-61-20 REV 16, PAGE 309 AND SECC DISASSEMBLY AND FOLDING PROCEDURE P-11915.Dec 16, 2011 · N119US · Airbus A320214 · Escape SlideSDR USAA2011121500001Damper · damaged2S CHECK - DURING OPERATIONAL TEST OF DAMPING FUNCTION & EMERGENCY OPERATION BUFFER HARD IMPACT ON A/C STRUCTURE AT DOOR 841. REPLACED DOOR-DAMPER & EMERGENCY-OPERATION CYLINDER AT DOOR 841 IAW A320 AMM 52-11-14 & 52-10-00.Dec 14, 2011 · N119US · Airbus A320214 · Passenger/Crew DoorsSDR USAA2011121300001Damper · damaged2S CHECK - MISSING PROTECTIVE CAP ON GAUGE INDICATOR AT DOOR DAMPER & EMERGENCY OPERATION CYLINDER DOOR 831. REPLACED DOOR-DAMPER & EMERGENCY OPERATION CYLINDER AT DOOR 831 IAW A320 AMM 52-11-14 & PERFORMED ADJUSTMENT OF THE PERCUSSION BELLCRANK FINGER, ADJUSDec 12, 2011 · N119US · Airbus A320214 · Passenger/Crew DoorsSDR USAA2011121200018Damper · damaged2S CHECK - MISSING CAP PROTECTIVE ON GAUGE INDICATION AT DOOR DAMPER & EMERGENCY OPERATION CYLINDER DOOR 832. REPLACED DOOR-DAMPER & EMERGENCY OPERATION CYLINDER AT DOOR 832 IAW A320 AMM 52-11-14 & PERFORMED ADJUSTMENT OF THE PERCUSSION BELLCRANK FINGER, ADJUDec 10, 2011 · N119US · Airbus A320214 · Passenger/Crew DoorsSDR USAA2011121200019Door · out of adjust2S CHECK - OUT ADJUSTMENT DIM "A" BETWEEN FINGER & STRIKER LEVER AT DOOR 841. PERFORMED ADJUSTMENT DIM "A"(J2) BETWEEN FINGER AND STRIKER LEVER OF THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT DOOR 841, ADJUSTMENT IS OK IAW AMM 52-11-14-820-002.Dec 9, 2011 · N119US · Airbus A320214 · Passenger/Crew DoorsSDR USAA2011122800012Support · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SUPPORT FRAME BETWEEN FR69 TO FR70, S23R. REPLACED SUPPORT FRAME BETWEEN FR69 TO FR70, S23R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53474180.Dec 6, 2011 · N119US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2011121200040Fuel Door · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING LOWER FUEL DOOR 640KB BETWEEN WS 8268 TO WS 8744 & BETWEEN WING RIB 15 TO RIB 16. REPLACED RIGHT WING LOWER FUEL DOOR 640KB IAW A320 SRM 57-27-11.Dec 2, 2011 · N119US · Airbus A320214 · Wing, Plate/SkinSDR USAA2011121200039Fuel Door · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING LOWER FUEL DOOR 640PB BETWEEN WS 10204 TO WS 10729 & BETWEEN WING RIB 19 TO RIB 20. REPLACED RIGHT WING LOWER FUEL DOOR 640PB IAW A320 SRM 57-27-11.Dec 2, 2011 · N119US · Airbus A320214 · Wing, Plate/SkinSDR USAA2011121200038Fuel Door · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING LOWER FUEL DOOR 640JB BETWEEN WS 7792 TO WS 8268 & BETWEEN WING RIB 14 TO RIB 15. REPLACED RIGHT WING LOWER FUEL DOOR 640JB IAW A320 SRM 57-27-11.Dec 2, 2011 · N119US · Airbus A320214 · Wing, Plate/SkinSDR USAA2011121200037Fuel Door · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING LOWER FUEL DOOR 540KB AT WS 8268, WING RIB 15. REPLACED LEFT WING LOWER FUEL DOOR 540KB IAW A320 SRM 57-27-11.Dec 2, 2011 · N119US · Airbus A320214 · Wing, Plate/SkinSDR USAA2012010300008Angle · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON AFT CURVED EDGE SEGMENT OF EMERGENCY EXIT DOOR 843 BETWEEN FR38 TO FR39, BEAM 4. REPLACED AFT CURVED EDGE SEGMENT OF EMERGENCY EXIT DOOR 843 BETWEEN FR38 TO FR39, BEAM 4 IAW A320 SRM 51-42-11, 51-72-11 & AIRBUS DRAWINGNov 30, 2011 · N119US · Airbus A320214 · Emergency ExitsSDR USAA2011122800016Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR61+13 INCHES TO FR64, Y765. REPLACED SEAT RAIL BETWEEN FR61+13 INCHES TO FR64, Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472770.Nov 30, 2011 · N119US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011122200013Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 262BG. REPLACED FLOOR PANEL 262BG IAW A320 SRM 53-02-00, IRM 9701 REV G & EA 133919.Nov 30, 2011 · N119US · Airbus A320214 · Fuselage Floor PanelSDR USAA2011121900022Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 261PF BETWEEN FR68 TO FR70 & BETWEEN -Y1292 TO Y1292. REPLACED FLOOR PANEL 261PF IAW A320 SRM 53-02-00 & IRM 9701 REV G.Nov 30, 2011 · N119US · Airbus A320214 · Fuselage Floor PanelSDR USAA2011121300011Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 241EF BETWEEN FR36 TO FR42, BETWEEN -Y254 TO Y254. REPLACED FLOOR PANEL 241EF IAW A320 SRM 53-02-00, IRM 9701 REV G.Nov 30, 2011 · N119US · Airbus A320214 · Fuselage Floor PanelSDR USAA2011121300010Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 242HF BETWEEN FR36 TO FR42, BETWEEN -Y1732 TO Y1292. REPLACED FLOOR PANEL 242HF IAW A320 SRM 53-02-00, IRM 9701 REV G.Nov 30, 2011 · N119US · Airbus A320214 · Fuselage Floor PanelSDR USAA2011121300009Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 222EF BETWEEN FR16 TO FR20, BETWEEN -Y254 TO -Y1292. REPLACED FLOOR PANEL 222EF IAW A320 SRM 53-12-00, IRM 9701 REV G.Nov 30, 2011 · N119US · Airbus A320214 · Fuselage Floor PanelSDR USAA2011121200029Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 231LF BETWEEN FR24 TO FR28, BETWEEN Y254 TO Y765. REPLACED FLOOR PANEL 231LF IAW A320 SRM 53-02-0, IRM 9701 REV G.Nov 30, 2011 · N119US · Airbus A320214 · Fuselage Floor PanelSDR USAA2011121200028Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 231YF BETWEEN FR32 TO FR35, BETWEEN Y1292 TO Y1732. REPLACED FLOOR PANEL 231YF IAW A320 SRM 53-02-00, IRM 9701 REV G.Nov 30, 2011 · N119US · Airbus A320214 · Fuselage Floor PanelSDR USAA2011121200027Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 221DF BETWEEN FR16 TO FR24, BETWEEN -Y254 TO Y254. REPLACED FLOOR PANEL 221DF IAW A320 SRM 53-12-00 AND MCGILL IRM 9701 REV G.Nov 30, 2011 · N119US · Airbus A320214 · Fuselage Floor PanelSDR USAA2011121200010Floor Panel · corroded2S CHECK - CORROSION ON FLOOR PANEL 262FF BETWEEN FR66 TO FR68, S23R. REPLACED FLOOR PANEL 262FF IAW JOB CARD 26C26053014 AND TYPICAL REPAIR 320-2528-10-0011.Nov 30, 2011 · N119US · Airbus A320214 · Fuselage Floor PanelSDR USAA2011121200008Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 232FF BETWEEN FR22 TO FR24, BETWEEN -Y1732 TO -Y1292. REPLACED FLOOR PANEL 232FF IAW A320 SRM 53-12-00 AND MCGILL IRM 9701 REV G.Nov 30, 2011 · N119US · Airbus A320214 · Fuselage Floor PanelSDR USAA2011121200007Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 261AG BETWEEN FR64 TO FR66, BETWEEN -Y254 TO Y254. REPLACED FLOOR PANEL 261AG IAW A320 SRM 53-02-00 AND MCGILL IRM 9701 REV G.Nov 30, 2011 · N119US · Airbus A320214 · Fuselage Floor PanelSDR USAA2011121200006Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 261BG BETWEEN FR64 TO FR66, BETWEEN Y765 TO Y1732. REPLACED FLOOR PANEL 261BG IAW A320 SRM 53-02-00 AND MCGILL IRM 9701 REV G.Nov 30, 2011 · N119US · Airbus A320214 · Fuselage Floor PanelSDR USAA2011121200005Floor Panel · corroded2S CHECK - CORROSION ON FLOOR PANEL 261FF BETWEEN FR66 TO FR68, S23L. REPLACED FLOOR PANEL 261FF IAW JOB CARD 26C26053014 AND TYPICAL REPAIR 320-2528-10-0011.Nov 30, 2011 · N119US · Airbus A320214 · Fuselage Floor PanelSDR USAA2012010500011Angle · cracked2S CHECK - CRACK ON SEGMENT ANGLE AT EMERGENCY EXIT DOOR 843 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3. REPLACED SEGMENT ANGLE AT EMERGENCY EXIT DOOR 843 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3 IAW EO 5210Y228.Nov 29, 2011 · N119US · Airbus A320214 · Emergency ExitsSDR USAA2012010300011Angle · cracked2S CHECK - CRACKS ON SEGMENT ANGLE AT LEFT EMERGENCY EXIT DOOR 833 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 4. REPLACED SEGMENT ANGLE AT LEFT EMERGENCY EXIT DOOR 833 IAW EO 5210Y228.Nov 29, 2011 · N119US · Airbus A320214 · Emergency ExitsSDR USAA2012010300010Door Frame · cracked2S CHECK - CRACK ON FRAME SEGMENT EMERGENCY EXIT HATCH DOOR 834 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. REPLACED FRAME SEGMENT EMERGENCY EXIT HATCH DOOR 834 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3 IAW EO 5210Y228.Nov 29, 2011 · N119US · Airbus A320214 · Emergency ExitsSDR USAA2011121500016Floor Panel · corroded2S CHECK - CORROSION ON FLOOR PANEL 221FF BETWEEN FR16 TO FR20, S23L. REPLACED FLOOR PANEL 221FF IAW JOB CARD 26C22053014.Nov 29, 2011 · N119US · Airbus A320214 · Fuselage Floor PanelSDR USAA2011121300013Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 251RF BETWEEN FR58 TO FR62, BETWEEN -Y254 TO Y254. REPLACED FLOOR PANEL 251RF IAW A320 SRM 53-02-00, IRM 9701 REV G.Nov 29, 2011 · N119US · Airbus A320214 · Fuselage Floor PanelSDR USAA2011121300012Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 251AF BETWEEN FR47 TO FR51, BETWEEN -Y254 TO Y254. REPLACED FLOOR PANEL 251AF IAW A320 SRM 53-02-00, IRM 9701 REV G.Nov 29, 2011 · N119US · Airbus A320214 · Fuselage Floor PanelSDR USAA2011121200031Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM ASSEMBLY BETWEEN FR65 TO FR66, Y1732. REPLACED FLOORBEAM ASSEMBLY BETWEEN FR65 TO FR66, Y1732 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472750.Nov 29, 2011 · N119US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2011121200009Floor Panel · corroded2S CHECK - CORROSION ON FLOOR PANEL 222FF BETWEEN FR16 TO FR20, S23R. REPLACED FLOOR PANEL 222FF IAW JOB CARD 26C22053014.Nov 29, 2011 · N119US · Airbus A320214 · Fuselage Floor PanelSDR USAA2012010600003Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR41 TO FR47, -Y1292. REPLACED SEAT TRACK BETWEEN FR41 TO FR47, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53370500.Nov 28, 2011 · N119US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012010500012Stringer · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON STRINGER BETWEEN FR33+11 INCHES TO FR34+6 INCHES, S41R. REPAIRED STRINGER BETWEEN FR33+11 INCHES TO FR34+6 INCHES, S41R IAW A320 SRM 53-21-13 FIG 203 SHEET 2.Nov 28, 2011 · N119US · Airbus A320214 · Fuselage Main, Longeron/StringerSDR USAA2012010400018Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL AT L2 DOORWAY BETWEEN FR66 TO FR68, S23L. REPAIRED LOWER SILL AT L2 DOORWAY BETWEEN FR66 TO FR68, S23L IAW EA 133932.Nov 28, 2011 · N119US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012010300009Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, -Y765. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, -Y765 IAW A320 SRM 51-72-11, AIRBUS DRAWING D53370500, D57130300 & D53371000.Nov 28, 2011 · N119US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011122800011Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON AFT CORNER FITTING AT LOWER SILL OF R2 DOOR AT FR68, S23R. REPLACED AFT CORNER FITTING AT LOWER SILL OF R2 DOOR AT FR68, S23R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53480505.Nov 28, 2011 · N119US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2011122700014Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FORWARD CORNER FITTING OF L2 DOOR LOWER SILL AT FR66, S23L. REPLACED AFT CORNER FITTING OF L2 DOOR LOWER SILL AT FR66, S23L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53480505.Nov 28, 2011 · N119US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2011122700013Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON AFT CORNER FITTING OF L2 DOOR LOWER SILL AT FR68, S23L. REPLACED AFT CORNER FITTING OF L2 DOOR LOWER SILL AT FR68, S23L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53480505.Nov 28, 2011 · N119US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2011122100004Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR52+9 INCHES, -Y765. REPLACED SEAT TRACK AT FR52+9 INCHES, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472770.Nov 28, 2011 · N119US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011122000024Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, -Y1292. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53370500.Nov 28, 2011 · N119US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011122000023Seat Track · corroded2S CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, Y1292. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D57130300.Nov 28, 2011 · N119US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011122000022Seat Track · corroded2S CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SEAT TRACK BETWEEN FR41 TO FR47, Y1292. REPLACED SEAT TRACK BETWEEN FR41 TO FR47, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D57130300.Nov 28, 2011 · N119US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011122000020Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHAPE SILL BETWEEN FR66 TO FR68, S23L. REPLACED SHAPE SILL BETWEEN FR66 TO FR68, S23L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53480505.Nov 28, 2011 · N119US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2011121400015Fitting · corrodedS2 CHECK - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING AT LEFT FORWARD DOOR CUTOUT BETWEEN FR16 TO FR20. REPLACED CENTER FITTING AT LEFT FORWARD DOOR CUTOUT BETWEEN FR16 TO FR20 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112109.Nov 28, 2011 · N119US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2011121400014Fitting · corrodedS2 CHECK - LEVEL 2 GALVANIC CORROSION ON FITTING AT RIGHT FORWARD DOOR CUTOUT BETWEEN FR16 TO FR20. REPLACED FITTING AT RIGHT FORWARD DOOR CUTOUT BETWEEN FR16 TO FR20 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112109.Nov 28, 2011 · N119US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012010500010Panel · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON TOP AFT PANEL UPPER SURFACE AT CENTER WING BOX AT FR42, Y1292. REPAIRED TOP AFT PANEL UPPER SURFACE AT CENTER WING BOX AT FR42, Y1292 IAW EA 133908.Nov 27, 2011 · N119US · Airbus A320214 · Wing, Center Box
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