Airbus A321-211

Service difficulty reports · 12,330

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = 'A321211'
  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 USAA2013080600016Shear Plate · crackedDURING 2S CHECK - A CRACK WAS FOUND ON SHEAR PLATE BETWEEN FR68 TO FR69, Y1732. REPLACED SHEAR PLATE IAW SRM 51-44-11 & 51-42-11.Jul 31, 2013 · N183UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013080600015Shear Plate · crackedDURING 2S CHECK, A CRACK FOUND ON SHEAR PLATE BETWEEN FR68 TO FR69, -Y1732. REPLACED SHEAR PLATE IAW SRM 53-41-14, 51-44-11 & 51-42-11.Jul 31, 2013 · N183UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013080100001Battery · inoperativeF/A REPORTS EXIT SIGN L3 DOOR DOES NOT ILLUMINATE. R & R EMERGENCY BATTERY AT L3 DOOR.Jul 31, 2013 · N176UW · Airbus A321211 · Emergency LightingSDR USAA2013080500034Floor Panel · cracked2S CHECK - CRACK ON FLOOR PANEL NR 152NG BETWEEN FR48 TO FR50 & BETWEEN -Y765 TO -Y970.8. REPLACED FLOOR PANEL IAW SRM 53-02-00, PAR 8.H, FIG. 209 &IRM 9701, REV G.Jul 30, 2013 · N182UW · Airbus A321211 · Fuselage Floor PanelSDR USAA2013080500027Hinge Fitting · wornDURING 2S CHECK - WEAR ON RT WING NR 3 SPOILER CENTER HINGE STOP FITTING BETWEEN WS 732 - 874 & BETWEEN RIB 13 TO RIB 16. REPAIRED RT WING NR 3 SPOILER CENTER HINGE STOP FITTING IAW SRM 57-70-00, FIG 201, (SHEET 2) PAGE 208.Jul 30, 2013 · N182UW · Airbus A321211 · SpoilersSDR USAA2013080500026Hinge Fitting · wornDURING 2S CHECK, WEAR ON LT WING NR 2 SPOILER CENTER HINGE STOP FITTING BETWEEN WS 551 - 732 & BETWEEN RIB 10 TO RIB 13. REPAIRED LT WING NR 2 SPOILER CENTER HINGE STOP FITTING IAW SRM 57-70-00, FIG 201, (SHEET 2) PAGE 208.Jul 30, 2013 · N182UW · Airbus A321211 · SpoilersSDR USAA2013073100015Light · malfunctionedEMERGENCY EXIT LIGHT OVER R2 DOOR APPEARS TO BE INOPERATIVE. RESET MID EMERGENCY POWER SUPPLY UNIT AND PERFOMRED BITE TEST, NO FAULTS FOUND.Jul 30, 2013 · N173US · Airbus A321211 · Emergency LightingSDR USAA2013073000023Floor Support · corrodedDURING 2S CHECK, FOUND CORROSION ON FLOOR SUPPORT AT FR66, -Y765. REPLACED FLOOR SUPPORT IAW SRM 53-00-14, 51-44-11 AND 51-42-11.Jul 29, 2013 · N183UW · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013073000022Floor Support · corrodedDURING 2S CHECK, FOUND CORROSION ON FLOOR SUPPORT AT FR66, Y765. REPLACED FLOOR SUPPORT IAW SRM 53-00-14, 51-44-11 AND 51-42-11.Jul 29, 2013 · N183UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013073000021Floor Support · corrodedDURING 2S CHECK, FOUND CORROSION ON FLOOR SUPPORT AT FR68, Y765. REPLACED FLOOR SUPPORT IAW SRM 53-00-14, 51-44-11 AND 51-42-11.Jul 29, 2013 · N183UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013073000020Floor Support · corrodedDURING 2S CHECK, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FR65 TO FR67, -Y318. REPLACED FLOOR SUPPORT IAW SRM 53-00-14, 51-44-11 AND 51-42-11.Jul 29, 2013 · N183UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013073000019Seat Track · corrodedDURING 2S CHECK, FOUND CORROSION ON SEAT TRACK BETWEEN FR19 TO FR20, -Y254. REPLACED SEAT TRACK IAW SRM 53-11-14, 51-42-11 AND 51-75-12.Jul 29, 2013 · N183UW · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013073000018Seat Track · corrodedDURING 2S CHECK, FOUND CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, Y254. REPLACED SEAT TRACK IAW SRM 53-11-14, 51-42-11 AND 51-75-12.Jul 29, 2013 · N183UW · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013073000017Seat Track · corrodedDURING 2S CHECK, FOUND CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y765. REPLACED SEAT TRACK IAW SRM 51-74-00, 53-00-15, AND 51-42-11.Jul 29, 2013 · N183UW · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013073000016Seat Track · corrodedDURING 2S CHECK, FOUND CORROSION ON SEAT TRACK BETWEEN FR20 TO FR24, -Y189. REPLACED SEAT TRACK IAW SRM 53-11-14, 51-44-11 & 51-42-11.Jul 29, 2013 · N183UW · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013073000015Shear Plate · corrodedDURING 2S CHECK, FOUND CORROSION ON SHEAR PLATE FRAMES 69 TO 70, Y1732. REPLACED SHEAR PLATE IAW SRM 51-42-11, 51-44-11, & TR 320-2528-10-0011G.Jul 29, 2013 · N183UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR 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 USAA2013072900009Power Supply · failedSEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. R & R POWER SUPPLY IAW AMM 33-51-38.Jul 26, 2013 · N191UW · Airbus A321211 · Emergency LightingSDR USAA2013072900010Lens · missingEXIT SIGN LIGHTING LENS COVER MISSING AT SEAT 5C LOCATION. REPLACED MISSING LIGHT COVER AT SEAT 5C.Jul 26, 2013 · N177US · Airbus A321211 · Emergency LightingSDR USAA2013072900012Web · corrodedDURING 2S CHECK, CORROSION WAS FOUND ON WEB BETWEEN FR53 TO FR54, S38R. REPLACED WEB IAW SRM 51-74-00, 51-11-14 AND 51-42-11.Jul 25, 2013 · N180US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013072400015Sill · corroded2S CHECK - CORROSION ON R4 DOOR SILL BETWEEN FRAMES 66 TO 68, S23R. REPLACED DOOR SILL IAW SRM 51-74-00, 53-41-14, 51-42-11 & EA 505491.Jul 23, 2013 · N180US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013072400014Sill · corroded2S CHECK - CORROSION ON L4 DOOR SILL BETWEEN FRAMES 66 TO 68, S23L. REPLACED DOOR SILL IAW SRM 51-74-00, 53-41-14, 51-42-11 & EA 505491.Jul 23, 2013 · N180US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013072300004Gust Lock · out of adjust2S CHECK - RT FWD EMERGENCY EXIT DOOR GUST LOCK HOOK WON`T ENGAGED PROPERLY. CLEANED AND LUBE RT FWD EMERGENCY EXIT DOOR GUST LOCK HOOK IAW MM 12-21-60, OPS CHECKED GOOD IAW MM 52-22-00-710-001-A.Jul 22, 2013 · N180US · Airbus A321211 · Emergency ExitsSDR USAA2013072300015Light · inoperativeSEAT 25C EMERGENCY LIGHT INOPERATIVE. R & R SEAT 25C EMERGENCY LIGHT IAW AMM 33-51-18.Jul 22, 2013 · N194UW · Airbus A321211 · Emergency LightingSDR USAA2013072300006Cylinder · lowR4 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED R4 DOOR EMERGENCY CYLINDER TO PROPER PRESSURE IAW AMM 52-10-00-614-001A.Jul 22, 2013 · N161UW · Airbus A321211 · Service DoorsSDR USAA2013072600005Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 232FF BETWEEN FRAMES 20 TO 24 & -Y1292 TO -Y1732. REPLACED FLOOR PANEL IAW SRM 53-12-00, FIG 206 & IRM 9701, REV G.Jul 21, 2013 · N182UW · Airbus A321211 · Fuselage Floor PanelSDR USAA2013072600004Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 221LF BETWEEN FRAMES 12 TO 16 & -Y254 TO Y765. REPLACED FLOOR PANEL IAW SRM 53-12-00, FIG 206 & IRM 9701 REV. G.Jul 21, 2013 · N182UW · Airbus A321211 · Fuselage Floor PanelSDR USAA2013072300012Cylinder · lowFORWARD CIDS PANEL HAS "CAUTION" BUTTON MESSAGE. SERVICED EMERGENCY EXIT DOOR DAMPER AT R4 IAW AMM 52-22-00-614-002-A.Jul 21, 2013 · N173US · Airbus A321211 · Service DoorsSDR USAA2013072400013Fitting · corroded2S CHECK -CORROSION ON RT AFT SILL BEAM FITTING AT FR20, Z-520. REPAIRED SILL BEAM FITTING IAW SRM 53-11-14, SHEET 1 TO SHEET 5.Jul 18, 2013 · N180US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013072400012Fitting · corroded2S CHECK - CORROSION ON LT AFT SILL BEAM FITTING AT FR20, Z-520. REPAIRED SILL BEAM FITTING IAW SRM 53-11-14, SHEET 1 TO SHEET 5.Jul 18, 2013 · N180US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013072400011Fitting · corroded2S CHECK - CORROSION ON LT FORWARD SILL BEAM FITTING AT FR16, Z-520. REPAIRED LT FORWARD SILL BEAM FITTING AT FR16, Z-520 IAW SRM 53-11-14, SHEET 1 TO SHEET 5.Jul 18, 2013 · N180US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013072400010Fitting · corroded2S CHECK, CORROSION ON RT FWD SILL BEAM FITTING AT FR16, Z-520. REPAIRED RT FORWARD SILL BEAM FITTING AT FR16, Z-520 IAW SRM 53-11-14, SHEET 1 TO SHEET 5.Jul 18, 2013 · N180US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013080600006Fitting · corroded2S CHECK - FOUND CORROSION ON CORNER FITTING AT FR68, S23R, -Y1313. REPLACED WEB IAW SRM 51-72-11 & DWG D53112571.Jul 17, 2013 · N182UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013073000008Fitting · elongatedDURING 2S CHECK, FOUND AN ELONGATED HOLE ON L2 DOORWAY CORNER FITTING AT FR66, S23L. REPLACED FITTING IAW SRM 51-72-11 DWG D53480505.Jul 17, 2013 · N182UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013073000007Sill · corrodedDURING 2S CHECK, FOUND CORROSION ON CENTER SILL BETWEEN FR66 TO FR68, S23L. REPLACED SILL IAW SRM 51-72-11.Jul 17, 2013 · N182UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013072300034Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL AFT OF CENTER CONSOLE IN COCKPIT BETWEEN FRAMES 6 - 12 & BETWEEN Y765 & Y254. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jul 17, 2013 · N180US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013072300033Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL UNDER CO-PILOTS SEAT IN COCKPIT BETWEEN FRAMES 6 - 12 & BETWEEN Y254 & -Y254. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jul 17, 2013 · N180US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013072300027Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 261FG BETWEEN FR64 TO FR66 & BETWEEN Y1292 TO Y254. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG. 209.Jul 17, 2013 · N180US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013072300026Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 261QF BETWEEN FR64 TO FR66 & BETWEEN -Y254 TO Y254. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG. 209.Jul 17, 2013 · N180US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013072300025Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 262BG BETWEEN FR64 TO FR66 & BETWEEN -Y1292 TO -Y764. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG. 209.Jul 17, 2013 · N180US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013072300024Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 261PF BETWEEN FR68 TO FR70 & BETWEEN Y1292 TO -Y1292. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG. 209.Jul 17, 2013 · N180US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013072300023Floor Panel · corroded2S CHECK - CORROSION ON FLOOR PANEL NR 222FF BETWEEN FR16 TO FR20, -Y1292. REPLACED FLOOR PANEL IAW SRM 51-74-00 & AMM 53-12-12.Jul 17, 2013 · N180US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013072300022Floor Panel · corroded2S CHECK - CORROSION ON FLOOR PANEL NR 221FF BETWEEN FR16 TO FR20, Y1292. REPLACED FLOOR PANEL IAW SRM 51-74-00 & AMM 53-12-12.Jul 17, 2013 · N180US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013071600008Power Supply · inoperativeEMERGENCY EXIT LIGHTS ABOVE 4L AND 5R DOORS AND ABOVE DIRECT VIEW JUMPSEAT FAILED TO ILLUMINATE WHEN PED SWITCH ON. R & R EMERGENCY POWER SUPPLY UNIT IAW AMM 33-51-38-400-001-A. TEARDOWN CONFIRMED FAILURE OF EPSU.Jul 15, 2013 · N177US · Airbus A321211 · Emergency LightingSDR USAA2013080100014Seat Track · worn2S CHECK - WEAR ON SEAT TRACK AT FR35.5+6", -Y765. REPAIRED SEAT TRACK IAW SRM 53-00-15; FIG 201.Jul 15, 2013 · N182UW · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013072500001Bearing · corroded2S CHECK - CORROSION ON NR 2 PYLON SPIGOT BEARING AT PYLON STATION 7063, RIB 5. REPLACED 2 PYLON SPIGOT BEARING IAW AMM 54-51-41-400-001-A.Jul 15, 2013 · N180US · Airbus A321211 · Nacelle/Pylon, Main FrameSDR USAA2013072300028Floorbeam · corroded2S CHECK - CORROSION ON FLOORBEAM AT FRAME 20, -Y254. REPLACED FLOORBEAM IAW SRM 53-11-15, FIG 102 & 51-42-11.Jul 15, 2013 · N180US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA2013071900041Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL NR 242BF BETWEEN FR35.8 TO FR36 & BETWEEN -Y765 TO -Y1292. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG. 209.Jul 14, 2013 · N180US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013071900040Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 241AF BETWEEN FR35.8 TO FR36 & BETWEEN Y254 TO -Y254. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG. 209.Jul 14, 2013 · N180US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013071900039Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL NR 231FF BETWEEN FR24 TO FR28 & BETWEEN Y765 TO Y1292. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG. 209.Jul 14, 2013 · N180US · Airbus A321211 · Fuselage Floor Panel
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