N111US

Service difficulty reports · 274

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 = 'N111US' 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 USAA2011110700022Flex Line · leakingCLIMBING OUT OF FL220 GREEN HYDRO QUANTITY WENT TO ZERO; RESERVOIR SYSTEM LOW AND LOSS OF GREEN HYDRAULICS. EMERGENCY LANDING GEAR EXTENDED, PINNED GEAR AND TOWED TO GATE AFTER LANDING. RIGHT MLG DOOR ACTUATOR FLEX LINE FAILED - LEAKING. REMOVED AND REPLACENov 5, 2011 · N111US · Airbus A320214 · Hydraulic System, MainSDR USAA2011101000026Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL AT FR68, S23L. REPAIRED LOWER SILL AT FR68, S23L IAW A320 SRM 53-41-14.Oct 3, 2011 · N111US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2011100400018Door · out of adjust2S CHECK - OUT OF ADJUSTMENT DIMENSION "B" BETWEEN STRIKER LEVER & FINGER DAMPER MECHANISM AT DOOR 831. PERFORMED ADJUSMENT DIM "B" (J1) BETWEEN STRIKER LEVER & FINGER DOOR DAMPER & EMERGENCY OPERATION CYLINDER AT DOOR 831, ADJUSTMENT IS OK IAW AMM 52-11-14-8Oct 3, 2011 · N111US · Airbus A320214 · Passenger/Crew DoorsSDR USAA2011100300039Door · out of adjust2S CHECK - OUT OF ADJUSTMENT DIMENSION "B" BETWEEN STRIKER LEVER AND FINGER DAMPER MECHANISM AT DOOR 841. PERFORMED ADJUSTMENT DIM "B" (J1) BETWEEN STRIKER LEVER & FINGER OF THE DOOR DAMPER & EMERGENCY OPERATION CYLINDER AT DOOR 841, ADJUSTMENT IS OK IAW AMM Oct 2, 2011 · N111US · Airbus A320214 · Passenger/Crew DoorsSDR USAA2011101700042Fairing · eroded2S CHECK - EROSION ON LEFT WING NR 1 SLAT INBOARD FAIRING BETWEEN WS0 TO WS700, BETWEEN RIB 1 TO RIB 2. REPAIRED FAIRING BETWEEN WS0 TO WS700, BETWEEN RIB 1 TO RIB 2 IAW EA 133834.Sep 28, 2011 · N111US · Airbus A320214 · Leading Edge DevicesSDR USAA2011101700041Fairing · eroded2S CHECK - EROSION ON RIGHT WING NR 1 SLAT INBOARD FAIRING BETWEEN WS0 TO WS700, BETWEEN RIB 1 TO RIB 2. REPAIRED FAIRING BETWEEN WS0 TO WS700, BETWEEN RIB 1 TO RIB 2 IAW EA 133834.Sep 28, 2011 · N111US · Airbus A320214 · Leading Edge DevicesSDR USAA2011100500044Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL AT FR48, -Y765. REPAIRED SEAT RAIL AT FR48, -Y765 IAW A320 SRM 53-00-15.Sep 27, 2011 · N111US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011092600016Power Supply · inoperativeS2 CHECK - DURING OPERATIONAL TEST OF EMERGENCY LIGHTING SYSTEM WAS SHOWN THE MESSAGE "EPSU COMM EMER R". REPLACED THE 1CT CABIN EMERGENCY POWER SUPPLY UNIT.Sep 25, 2011 · N111US · Airbus A320214 · Emergency LightingSDR USAA2011092600015Power Supply · inoperativeS2 CHECK - DURING OPERATIONAL TEST OF EMERGENCY LIGHTING SYSTEM WAS SHOWN THE MESSAGE "EPSU INT LOAD EMER L". REPLACED THE AFT CABIN EMERGENCY POWER SUPPLY UNIT.Sep 25, 2011 · N111US · Airbus A320214 · Emergency LightingSDR USAA2011092600014Slide Raft · misinstalled2S CHECK - SLIDE/RAFT AT DOOR 842 HITS FUSELAGE WHEN DOOR IS FULLY OPEN. REPACKED SLIDE RAFT AT DOOR 842 IAW CMM 25-61-20 REV 16 PAGE 309 SECC, DISASSEMBLY AND FOLDING PROCEDURE P-11915 REV AC.Sep 24, 2011 · N111US · Airbus A320214 · Escape SlideSDR USAA2011101700046Stringer · damaged2S CHECK - ELONGATED HOLE ON STRINGER BETWEEN FR34 TO FR35, S35L. REPAIRED STRINGER BETWEEN FR34 TO FR35, S35L IAW SRM A320 53-00-13 FIGURE 201.Sep 23, 2011 · N111US · Airbus A320214 · Fuselage Main, Longeron/StringerSDR USAA2011101700045Skin · corroded2S CHECK - CORROSION ON FUSELAGE SKIN PLATE BETWEEN FR63 TO FR64, BETWEEN S41R TO S42R. REPAIRED SKIN PLATE BETWEEN FR63 TO FR64, BETWEEN S41R TO S42R IAW EA 133805.Sep 22, 2011 · N111US · Airbus A320214 · Fuselage Main, Plate/SkinSDR USAA2011101400005Skin Panel · corroded2S CHECK - CORROSION ON FUSELAGE SKIN PANEL AT FR63 + 8 INCHES & BETWEEN S41L TO S42L. REPAIRED FUSELAGE SKIN PANEL AT FR63 + 8 INCHES & BETWEEN S41L TO S42L IAW EA 133806.Sep 22, 2011 · N111US · Airbus A320214 · Fuselage Main, Plate/SkinSDR USAA2011101000023Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL SEAT AT FR55, Y1292. REPAIRED RAIL SEAT AT FR55, Y1292 IAW A320 SRM 53-00-15.Sep 19, 2011 · N111US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011092900020Fuel Door · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING LOWER FUEL DOOR ASSY 640MB BETWEEN WS9235 TO WS9704 & BETWEEN RIB 17 TO RIB 18. REPLACED RIGHT WING LOWER FUEL DOOR ASSY 640MB IAW JOB CARD 26C60057091.Sep 18, 2011 · N111US · Airbus A320214 · Wing, Plate/SkinSDR USAA2011101400033Door Frame · cracked2S CHECK - CRACK INDICATION WAS FOUND IN THE EMERGENCY EXIT HATCH DOOR 834 INNER FRAME SEGMENTS BETWEEN FR40 TO FR41. REPLACED INNER FRAME SEGMENTS ON EMERGENCY EXIT HATCH DOOR 834 IAW EO 5210Y228.Sep 17, 2011 · N111US · Airbus A320214 · Emergency ExitsSDR USAA2011101400032Door Frame · cracked2S CHECK - CRACK INDICATION WAS FOUND IN THE EMERGENCY EXIT HATCH DOOR 833 INNER FRAME SEGMENTS BETWEEN FR38 TO FR39. REPLACED INNER FRAME SEGMENTS ON EMERGENCY EXIT HATCH DOOR 833 IAW EO 5210Y228.Sep 17, 2011 · N111US · Airbus A320214 · Emergency ExitsSDR USAA2011101400031Door Frame · cracked2S CHECK - CRACK INDICATION WAS FOUND IN THE EMERGENCY EXIT HATCH DOOR 844 INNER FRAME SEGMENTS BETWEEN FR40 TO FR41. REPLACED INNER FRAME SEGMENTS ON EMERGENCY EXIT HATCH DOOR 844 IAW EO 5210Y228.Sep 17, 2011 · N111US · Airbus A320214 · Emergency ExitsSDR USAA2011101400030Door Frame · cracked2S CHECK - CRACK INDICATION WAS FOUND IN THE EMERGENCY EXIT HATCH DOOR 843 INNER FRAME SEGMENTS BETWEEN FR38 TO FR39. REPLACED INNER FRAME SEGMENTS ON EMERGENCY EXIT HATCH DOOR 843 IAW EO 5210Y228.Sep 17, 2011 · N111US · Airbus A320214 · Emergency ExitsSDR USAA2011093000018Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR25+6 INCHES, Y765. REPAIRED SEAT TRACK AT FR25+6 INCHES, Y765 IAW A320 SRM 53-21-15.Sep 17, 2011 · N111US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011101700043Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT PYLON RECEPTACLE FITTING AT S679, BETWEEN RIB 4 TO RIB 5. REPAIRED RECEPTACLE FITTING AT S679, BETWEEN RIB 4 TO RIB 5 IAW A320 SRM 54-51-12, FIGURE 201.Sep 16, 2011 · N111US · Airbus A320214 · Nacelle/Pylon, Attach FittingsSDR USAA2011101400006Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL SEAT BETWEEN FR61+12 INCHES, -Y1192. REPAIRED RAIL SEAT BETWEEN FR61+12" TO FR64, -Y1292 IAW A320 SRM 53-41-15 & BOEING DRAWING D53472770 & D53472831.Sep 16, 2011 · N111US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011092800007Attach Bracket · worn2S CHECK - WEAR ON LEFT WING INTERCONNECTING STRUT ATTACHMENT BRACKET AT RIB 14 REAR SPAR OUTBOARD FLAPS. REPLACED LEFT WING INTERCONNECTING STRUT ATTACHMENT BRACKET IAW A320 SRM 51-72-11 & AIRBUS DRAWING D57570280.Sep 16, 2011 · N111US · Airbus A320214 · Wing Miscellaneous StructureSDR USAA2011092700021Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR BEAM BETWEEN FR68 TO FR70, Y160. REPLACED FLOORBEAM BETWEEN FR68 TO FR70, Y160 IAW A320 SRM 51-72-11.Sep 16, 2011 · N111US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2011092600003Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON HINGE FITTING ASSEMBY AT HORIZONTAL STABILIZER STATION 1305, RIB 4 RIGHT ELEVATOR. REPLACED HINGE FITTING ASSEMBY AT HORIZONTAL STABILIZER STATION 1305, RIB 4 RIGHT ELEVATOR IAW A320 AMM 55-16-42.Sep 16, 2011 · N111US · Airbus A320214 · Elevator StructureSDR USAA2011092300010Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON NR 2 HINGE FITTING ASSEMBLY AT HORIZONTAL STABILIZER STATION 1809, RIB 5 RIGHT ELEVATOR. REPLACED NR 2 HINGE FITTING ASSEMBLY AT HORIZONTAL STABILIZER STATION 1809, RIB 5 RIGHT ELEVATOR IAW A320 AMM 55-16-42.Sep 16, 2011 · N111US · Airbus A320214 · Elevator StructureSDR USAA2011092300009Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON RIGHT ELEVATOR NR 6 HINGE FITTING AT HORIZONTAL STABILIZER STATION 5894, RIB 13. REPLACED RIGHT ELEVATOR NR 6 HINGE FITTING AT HORIZONTAL STABILIZER STATION 5894, RIB 13 IAW A320 AMM 55-16-42.Sep 16, 2011 · N111US · Airbus A320214 · Elevator StructureSDR USAA2011092200024Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON LEFT ELEVATOR HINGE FITTING NR 6 AT HORIZONTAL STAB STA5894/RIB 13. REPLACED LEFT ELEVATOR HINGE FITTING NR 6 IAW A320 AMM 55-16-42.Sep 16, 2011 · N111US · Airbus A320214 · Elevator StructureSDR USAA2011100500042Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON AFT LOWER CORNER FITTING AT R2 DOOR ENTRY WAY AT FR68, S23R. REPLACED AFT LOWER CORNER FITTING AT R2 DOOR ENTRY WAY IAW A320 SRM 51-72-11 & BOEING DRAWING D53480505.Sep 15, 2011 · N111US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2011101400004Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 262HG BETWEEN FR64 TO FR66 & BETWEEN -Y1732 TO -Y765. REPLACED FLOOR PANEL 262HG IAW A320 SRM 53-02-00 TABLE 103 & IRM 9701 REV G.Sep 14, 2011 · N111US · Airbus A320214 · Fuselage Floor PanelSDR USAA2011101400003Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 261DF BETWEEN FR66 TO FR68, & BETWEEN -Y765 TO Y765. REPLACED FLOOR PANEL 261DF IAW A320 SRM 53-02-00 TABLE 103 & IRM 9701 REV G.Sep 14, 2011 · N111US · Airbus A320214 · Fuselage Floor PanelSDR USAA2011101100047Floor Panel · corroded2S CHECK - CORROSION ON FLOOR PANEL 222FF BETWEEN FR16 TO FR20, S23R. REPLACED FLOOR PANEL 222FF IAW EA 133781.Sep 14, 2011 · N111US · Airbus A320214 · Fuselage Floor PanelSDR USAA2011100500047Shear Tie · corroded2S CHECK - LEVEL 2 FILIFORM CORROSION ON SHEAR TIE AT FR28 BETWEEN S41R TO S43R. REPLACED SHEAR TIE AT FR28 BETWEEN S41R TO S43R IAW A320 SRM 51-72-11.Sep 14, 2011 · N111US · Airbus A320214 · Fuselage Internal Mounting StructureSDR USAA2011100500046Cleat · corroded2S CHECK - LEVEL 2 FILIFORM CORROSION ON CLEAT AT FR26 BETWEEN S42R TO S43R. REPLACED CLEAT AT FR26 BETWEEN S42R TO S43R IAW A320 SRM 51-72-11 & BOEING DRAWING D53231712.Sep 14, 2011 · N111US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2011092900019Floor Panel · delaminated2S CHECK - DELAMINATION FLOOR PANEL 261PF IN AFT CARGO COMPARTMENT BETWEEN FR68 TO FR70 & BETWEEN -Y765 TO Y765. REPLACED FLOOR PANEL 261PF IAW A320 SRM 53-02-00 & IRM 9701 REV G.Sep 14, 2011 · N111US · Airbus A320214 · Fuselage Floor PanelSDR USAA2011092700012Floor Panel · corroded2S CHECK - CORROSION ON FLOOR PANEL BETWEEN FR16 TO FR20, S23L. REPLACED FLOOR PANEL BETWEEN FR16 TO FR20, S23L IAW JOB CARD 26C22053014.Sep 14, 2011 · N111US · Airbus A320214 · Fuselage Floor PanelSDR USAA2011092700011Floor Panel · corroded2S CHECK - CORROSION ON FLOOR PANEL BETWEEN FR66 TO FR68, S23L. REPLACED FLOOR PANEL BETWEEN FR66 TO FR68, S23L IAW JOB CARD 26C26053014.Sep 14, 2011 · N111US · Airbus A320214 · Fuselage Floor PanelSDR USAA2011092700010Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 221PF BETWEEN FR12 TO FR24, BETWEEN Y254 TO Y1292. REPLACED FLOOR PANEL 221PF BETWEEN FR12 TO FR24, BETWEEN Y254 TO Y1292 IAW SRM 53-12-00, IRM 9701 REV G.Sep 14, 2011 · N111US · Airbus A320214 · Fuselage Floor PanelSDR USAA2011092200025Floor Panel · corroded2S CHECK - CORROSION ON FLOOR PANEL 262FF BETWEEN FR66 TO FR68, S23R. REPLACED FLOOR PANEL 262FF BETWEEN FR66 TO FR68, S23R IAW JOB CARD NR 26C26053014.Sep 14, 2011 · N111US · Airbus A320214 · Fuselage Floor PanelSDR USAA2011101700044Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON L2 DOOR LOWER SILL AT FR68, S23L. REPLACED L2 DOOR LOWER SILL AT FR68, S23L IAW A320 SRM 51-72-11.Sep 13, 2011 · N111US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2011101100012Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL AT FR67 PLUS 19 INCHES, S23R, Y-1732. REPLACED SILL AT FR67 PLUS 19 INCHES, S23R, Y-1732 IAW A320 SRM 51-72-11 AND EA 133827.Sep 13, 2011 · N111US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2011101100011Coupling · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR66, S23R, Y-1450. REPLACED COUPLING AT FR66, S23R, Y-1450 IAW A320 SRM 51-72-11 AND EA 133827.Sep 13, 2011 · N111US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2011101000020Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CORNER FITTING AT FR66, S23L. REPLACED CORNER FITTING AT FR66, S23L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53480505.Sep 13, 2011 · N111US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2011101000019Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, -Y1292. REPLACED SEAT TRACK BETWEEN FR24 TO FR35, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231730.Sep 13, 2011 · N111US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011101000018Skin · saturated2S CHECK - TRAPPED WATER INDICATION ON RIGHT ELEVATOR UPPER SURFACE BETWEEN THS STA 271 TO STA 297 & RIB 7 TO RIB 8 APPROX 3 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR UPPER SURFACE IAW A320 SRM 55-21-11 PARA 5D.Sep 13, 2011 · N111US · Airbus A320214 · Elevator, Plate/SkinSDR USAA2011101000017Skin · saturated2S CHECK - TRAPPED WATER INDICATION ON RIGHT ELEVATOR UPPER SURFACE BETWEEN THS STA 466 TO STA 527 & RIB 11 TO RIB 12 APPROX 5 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR UPPER SURFACE IAW A320 SRM 55-21-11 PARA 5D.Sep 13, 2011 · N111US · Airbus A320214 · Elevator, Plate/SkinSDR USAA2011100500051Skin · saturated2S CHECK - TRAPPED WATER INDICATION IN LEFT ELEVATOR UPPER SURFACE BETWEEN THS STA 131 TO STA 227 & BETWEEN RIB 5 TO RIB 6 APPROX 5.5 INCHES FROM TRAILING EDGE. REPAIRED LT ELEVATOR UPPER SKIN IAW A320 SRM 55-21-11, PARA 5D (2).Sep 13, 2011 · N111US · Airbus A320214 · Elevator, Plate/SkinSDR USAA2011100500050Skin · saturated2S CHECK - TRAPPED WATER INDICATION IN LEFT ELEVATOR UPPER SURFACE AT THS STA 527, RIB 12 APPROX 3.5 INCHES FROM TRAILING EDGE. REPAIRED LT ELEVATOR UPPER SKIN IAW A320 SRM 55-21-11, PARA 5D (2).Sep 13, 2011 · N111US · Airbus A320214 · Elevator, Plate/SkinSDR USAA2011100500049Skin · saturated2S CHECK - TRAPPED WATER INDICATION IN LEFT ELEVATOR UPPER SURFACE BETWEEN THS STA 466 TO STA 527 & RIB 11 & RIB 13 OF THE THS APPROX 3 INCHES FROM TRAILING EDGE. REPAIRED LT ELEVATOR UPPER SKIN IAW A320 SRM 55-21-11, PARA 5D (2).Sep 13, 2011 · N111US · Airbus A320214 · Elevator, Plate/SkinSDR USAA2011100500048Skin · saturated2S CHECK - TRAPPED WATER INDICATION IN LEFT ELEVATOR UPPER SURFACE AT STAB STA 589, RIB 13 OF THE THS. REPAIRED LT ELEVATOR UPPER SKIN IAW A320 SRM 55-21-11 PAR 5E (2).Sep 13, 2011 · N111US · Airbus A320214 · Elevator, Plate/Skin
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