Airbus A321-211

Service difficulty reports · 12,330

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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 aircraft_model_key = 'A321211'
  ORDER BY difficulty_date DESC"

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SDR USAA2013052800033Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 261HG BETWEEN FR64 TO FR66 & BETWEEN Y765 TO Y1732. REPLACED FLOOR PANEL 261HG IAW SRM 53-02-00, FIG. 209.May 23, 2013 · N170US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013052800032Floor Panel · delaminated2S CHECK, DELAMINATION ON FLOOR PANEL 251RF BETWEEN FR57 TO FR62 & BETWEEN Y254 TO Y765. REPLACED FLOOR PANEL 251RF IAW SRM 53-02-00, FIG. 209.May 23, 2013 · N170US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013052800031Floor Panel · delaminated2S CHECK, DELAMINATION ON FLOOR PANEL, 251LF BETWEEN FR54 TO FR58 & BETWEEN Y254 TO Y765. REPLACED FLOOR PANEL 251LF IAW SRM 53-02-00, FIG. 209.May 23, 2013 · N170US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013052800030Floor Panel · delaminated2S CHECK, DELAMINATION ON FLOOR PANEL 241LF BETWEEN FR42 TO FR47 & BETWEEN Y765 TO Y1292. REPLACED FLOOR PANEL 241LF IAW SRM 53-02-00, FIG. 209.May 23, 2013 · N170US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013052800028Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 232RF BETWEEN FR28 TO FR32 & BETWEEN Y254 TO Y765. REPLACED FLOOR PANEL 232RF IAW SRM 53-02-00, FIG. 209.May 23, 2013 · N170US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013052800027Floor Panel · delaminated2S CHECK, DELAMINATION ON FLOOR PANEL 231KF BETWEEN FR24 TO FR28 & BETWEEN Y254 TO Y254. REPLACED FLOOR PANEL 231KF IAW A321, SRM 53-02-00, FIG. 209.May 23, 2013 · N170US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013052800025Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL NR 231FF BETWEEN FR20 TO FR24 & BETWEEN Y1232 TO Y1732. REPLACED FLOOR PANEL NR 231FF IAW SRM 53-02-00, FIG. 209.May 23, 2013 · N170US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013062000013Stringer · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON STRINGER 39R AT FR35.2+18". REPAIRED STRINGER 39R AT FR35.2+18" IAW EA 504107.May 22, 2013 · N179UW · Airbus A321211 · Fuselage Main, Longeron/StringerSDR USAA2013062000012Stringer · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON STRINGER 40R AT FR35.3. REPAIRED STRINGER 40R AT FR35.3 IAW EA 504104.May 22, 2013 · N179UW · Airbus A321211 · Fuselage Main, Longeron/StringerSDR USAA2013052300033Mechanism · dirty2S CHECK-RIGHT AFT EMERGENCY EXIT DOOR GUST LOCK MECHANISM IS NOT LOCKING IN THE OPEN POSITION AND STIFF. CLEANED RT AFT EMERGENCY EXIT DOOR STAY LOCK MECHANISM IAW AMM 52-10-00. OPS CHECK GOOD.May 22, 2013 · N170US · Airbus A321211 · Emergency ExitsSDR USAA2013062000011Stringer · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON STRINGER 41R AT FR35.1+2". REPAIRED STRINGER 41R AT FR35.1+2" IAW EA NR 504103.May 21, 2013 · N179UW · Airbus A321211 · Fuselage Main, Longeron/StringerSDR USAA2013062000010Stringer · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON STRINGER 42L AT FR35.1. REPAIRED STRINGER 42L AT FR35.1 IAW EA NR 504105.May 21, 2013 · N179UW · Airbus A321211 · Fuselage Main, Longeron/StringerSDR USAA2013061700004Structure · corroded2S CHECK - CORROSION ON CORNER SEALING ASSY AT FR56, S38R. REPLACED CORNER SEALING ASSY AT FR56, S38R IAW SRM 51-72-11 & D53475500.May 21, 2013 · N179UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013061400005Cleat · corroded2S CHECK, LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR35.1 BETWEEN S39R TO S40R. REPLACED CLEAT AT FR35.1 BETWEEN S39R TO S40R IAW SRM 51-72-11 & DWG D53235031.May 21, 2013 · N179UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013061300009Cleat · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR35.1 BETWEEN S42R TO S43R. REPLACED CLEAT AT FR35.1 BETWEEN S42R TO S43R IAW SRM 51-72-11 & DWG D53235030, D53235008.May 21, 2013 · N179UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013052800056Beam · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON LONGITUDINAL BEAM BETWEEN FR67 TO FR69, Y1292. REPLACED LONGITUDINAL BEAM BETWEEN FR67 TO FR69, Y1292 IAW SRM 53-00-14, FIG. 102 & 51-42-11.May 21, 2013 · N170US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013052800054Beam · corroded2S CHECK, LEVEL 2 EXFOLIATION CORROSION ON LONGITUDINAL BEAM BETWEEN FR66 TO FR68, Y1292. REPLACED LONGITUDINAL BEAM BETWEEN FR66 TO FR68, Y1292 IAW SRM 53-00-14, FIG. 102 & 51-42-11.May 21, 2013 · N170US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013052800052Beam · corroded2S CHECK - LEVEL 2, EXFOLIATION CORROSION ON LONGITUDINAL BEAM BETWEEN FR65 TO FR66, Y765. REPLACED LONGITUDINAL BEAM BETWEEN FR65 TO FR66, Y765 IAW SRM 53-00-14, FIG. 102 & 51-42-11.May 21, 2013 · N170US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013052800048Beam · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON LONGITUDINAL BEAM BETWEEN FR64 TO FR66, Y1292. REPLACED LONGITUDINAL BEAM BETWEEN FR64 TO FR66, Y1292 IAW SRM 53-00-14, FIG. 102 & 51-42-11.May 21, 2013 · N170US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013052800045Seat Track · corroded2S CHECK, LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR63 TO FR64, Y1292. REPLACED SEAT TRACK BETWEEN FR63 TO FR64, Y1292 IAW SRM 53-41-15, FIG. 102 & 51-42-11.May 21, 2013 · N170US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013052800044Seat Track · corroded2S CHECK, LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR20 TO FR23, Y765. REPLACED SEAT TRACK BETWEEN FR20 TO FR23, Y765 IAW SRM 53-00-15, FIG. 101 & 51-42-11.May 21, 2013 · N170US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013052800043Seat Track · corroded2S CHECK, LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR19 TO FR23, Y1292. REPLACED SEAT TRACK BETWEEN FR19 TO FR23, Y1292 IAW SRM SRM 53-11-15, FIG 101 & 51-42-11.May 21, 2013 · N170US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013052900015Fitting · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON CORNER FITTING AT FR68, Y1732. REPLACED CORNER FITTING AT FR68, Y1732 IAW A321 SRM 53-41-14, FIG. 101 & 51-42-11.May 20, 2013 · N170US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013052800041Seat Track · corroded2S CHECK, LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR18 TO FR21, Y1292. REPLACED SEAT TRACK BETWEEN FR18 TO FR21, Y1292 IAW SRM 53-11-14, FIG. 103 & 51-42-11.May 20, 2013 · N170US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013052300032Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, -Y1292. REPLACED SEAT TRACK BETWEEN FR24 TO FR35, -Y1292 IAW SRM 51-74-00, 53-00-15 AND 51-42-11.May 20, 2013 · N176UW · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013052300029Seat Track · corroded2S CHECK-LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR47.2, Y1292. REPLACED SEAT TRACK AT FR47.2, Y1292 IAW SRM 51-74-00, 53-00-14 AND 51-42-11.May 20, 2013 · N176UW · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013052100006Shear Pin · shearedSHEAR PIN IS SHEARED ON R1 DOOR ASSIST BOTTLE ASSY STRIKER MECHANISM. SLIDE IS ALSO FROZEN. R & R SHEAR PIN ON R1 DOOR ASSEMBLY STRIKER IAW MM 52-10-00-610-001-A AND CLEANED SLIDER AS REQUIRED.May 20, 2013 · N180US · Airbus A321211 · Passenger/Crew DoorsSDR USAA2013052100005Lens · missingCEILING MOUNTED EMERGENCY LIGHT LENS MISSING NEAR SEAT ROW 10 IAW EA 204921. REPLACED LENS.May 20, 2013 · N193UW · Airbus A321211 · Emergency LightingSDR USAA2013061100015Fuel Door · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RT WING FUEL DOOR 640LB BETWEEN WS874 TO WS924 & BETWEEN RIB 16 TO RIB 17. REPLACED RT WING FUEL DOOR 640LB IAW SRM 51-72-11.May 19, 2013 · N179UW · Airbus A321211 · Wing, Plate/SkinSDR USAA2013061100014Fuel Door · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RT WING FUEL DOOR NR 640MB BETWEEN WS924 TO WS970 & BETWEEN RIB 17 TO RIB 18. REPLACED T WING FUEL DOOR NR 640MB IAW SRM 51-72-11.May 19, 2013 · N179UW · Airbus A321211 · Wing, Plate/SkinSDR USAA2013060500026Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL NR 232RF BETWEEN FR28 TO FR32 & BETWEEN Y254 TO Y765. REPLACED FLOOR PANEL NR 232RF IAW A321 SRM 53-20-00 & IRM 9701, REV G.May 19, 2013 · N179UW · Airbus A321211 · Fuselage Floor PanelSDR USAA2013060500025Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL NR 232MF BETWEEN FR24 TO FR28 & BETWEEN Y765 TO Y1292. REPLACED FLOOR PANEL 232MF IAW SRM 53-20-00 & IRM 9701, REV G.May 19, 2013 · N179UW · Airbus A321211 · Fuselage Floor PanelSDR USAA2013052900020Shear Plate · cracked2S CHECK -CRACK ON SHEAR PLATE BETWEEN FR68 TO FR69, S23L. REPLACED SHEAR PLATE BETWEEN FR68 TO FR69, S23L IAW SRM 51-42-11.May 19, 2013 · N170US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013052900018Web · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON WEB SUPPORT BETWEEN FR69 TO FR70, S23R. REPLACED WEB SUPPORT BETWEEN FR69 TO FR70, S23R IAW SRM 51-74-00 & 51-42-11.May 19, 2013 · N170US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013052900017Support · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON WEB SUPPORT BETWEEN FR69 TO FR70, S23L. REPLACED WEB SUPPORT BETWEEN FR69 TO FR70, S23L IAW A321 SRM 51-74-00 & 51-42-11.May 19, 2013 · N170US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013052800055Beam · corroded2S CHECK, LEVEL 2 EXFOLIATION CORROSION ON LONGITUDINAL BEAM BETWEEN FR67 TO FR68, Y1292. REPLACED LONGITUDINAL BEAM BETWEEN FR67 TO FR68, Y1292 IAW SRM 53-00-14, FIG. 102 & 51-42-11.May 19, 2013 · N170US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013052800053Beam · corroded2S CHECK, LEVEL 2 EXFOLIATION CORROSION ON LONGITUDINAL BEAM BETWEEN FR66 TO FR67, Y1292. REPLACED LONGITUDINAL BEAM BETWEEN FR66 TO FR67, Y1292 IAW SRM 53-00-14, FIG. 102 & 51-42-11.May 19, 2013 · N170US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013052800049Beam · corroded2S CHECK, LEVEL 2 EXFOLIATION CORROSION ON LONGITUDINAL BEAM BETWEEN FR64 TO FR66, Y1292. REPLACED LONGITUDINAL BEAM BETWEEN FR64 TO FR66, Y1292 IAW SRM 53-00-14, FIG. 102 & 51-42-11.May 19, 2013 · N170US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013061400014Fitting · missing2S CHECK - DAMAGE AREA, MISSING MATERIAL ON LT ELEVATOR FITTING 2 OTBD ACTUATOR FITTING BETWEEN RIB 4 TO RIB 5 AT FRONT SPAR. REPAIRED OTBD ACTUATOR FITTINGS BETWEEN RIB 4 TO RIB 5 AT FRONT SPAR IAW SRM 55-26-47, PAR. 5A, FIG. 201.May 18, 2013 · N179UW · Airbus A321211 · Elevator Miscellaneous StructureSDR USAA2013061300005Cleat · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR28 BETWEEN S42R AND S43R. REPLACED CLEAT AT FR28 BETWEEN S42R AND S43R IAW A321 SRM 51-72-11 & DWG D53234615.May 18, 2013 · N179UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013061300004Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR47.2 TO FR47.4, S23L, Y1600. REPLACED FLOORBEAM BETWEEN FR47.2 TO FR47.4, S23L, Y1600 IAW SRM 51-72-11 & DWG D53259000.May 18, 2013 · N179UW · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA2013061300003Coupling · damaged2S CHECK - ELONGATED HOLE ON FLOORBEAM "Z" COUPLING AT FR47.4", S23L, Y1600. REPLACED FLOORBEAM "Z" COUPLING AT FR47.4", S23L, Y1600 IAW SRM 51-72-11 & DWG D53456807.May 18, 2013 · N179UW · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA2013061000033Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON NR 4 HINGE FITTING OF LEFT ELEVATOR AT HORIZONTAL STABILIZER STA 342, RIB 9. REPLACED NR 4 HINGE ARM FITTING OF LT ELEVATOR IAW AMM 55-16-42-400-001-A.May 18, 2013 · N179UW · Airbus A321211 · Elevator StructureSDR USAA2013061000032Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON NR 3 HINGE FITTING OF RT ELEVATOR AT HORIZONTAL STABILIZER STA. 297, RIB 8. REPLACED NR 3 HINGE ARM FITTING OF RT ELEVATOR IAW AMM 55-16-42-400-001-A.May 18, 2013 · N179UW · Airbus A321211 · Elevator StructureSDR USAA2013061000031Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON NR 5 HINGE FITTING OF RT ELEVATOR AT HORIZONTAL STABILIZER STA. 466, RIB 11. REPLACED NR 5 HINGE ARM FITTING OF RT ELEVATOR IAW AMM 55-16-42-400-001-A.May 18, 2013 · N179UW · Airbus A321211 · Elevator StructureSDR USAA2013061000029Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON NR 2 HINGE FITTING ASSY OF RT ELEVATOR AT HORIZONTAL STABILIZER STA. 227, RIB 6. REPLACED NR 2 HINGE ARM FITTING OF RT ELEVATOR IAW AMM 55-16-42-400-001-A.May 18, 2013 · N179UW · Airbus A321211 · Elevator StructureSDR USAA2013061200013Floor Panel · corroded2S CHECK - CORROSION ON FLOOR PANEL 222FF BETWEEN FR16 TO FR20, S23R, -Y1732. REPLACED FLOOR PANEL 222FF IAW AMM 53-12-12.May 17, 2013 · N179UW · Airbus A321211 · Fuselage Floor PanelSDR USAA2013061100011Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL NR 221LF BETWEEN FR12 TO FR16 & BETWEEN Y254 TO Y765. REPLACED FLOOR PANEL NR 221LF IAW SRM 53-12-00, PAR. 4C(1), FIG. 101 & IRM 9701, REV G.May 17, 2013 · N179UW · Airbus A321211 · Fuselage Floor PanelSDR USAA2013060600008Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL NR 232EF BETWEEN FR20 TO FR24 & BETWEEN Y765 TO Y1292. REPLACED FLOOR PANEL 232EF IAW SRM 53-12-00 & IRM 9701, REV G.May 17, 2013 · N179UW · Airbus A321211 · Fuselage Floor PanelSDR USAA2013060600007Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL, NR 261AG BETWEEN FR64 TO FR66 & BETWEEN Y765 TO Y765. REPLACED FLOOR PANEL NR 261AG IAW SRM 53-02-00 & IRM 9701, REV.G.May 17, 2013 · N179UW · Airbus A321211 · Fuselage Floor Panel
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