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 USAA2013040800032Seat Track · corrodedS2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR16, -Y765. REPLACED SEAT TRACK AT FR16, -Y765 IAW A321 SRM 51-42-11, 53-11-15, 51-44-11 & 51-75-12.Apr 3, 2013 · N171US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013040800031Seat Track · corrodedS2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR20, Y765. REPLACED SEAT TRACK AT FR20, Y765 IAW A321 SRM 51-42-11 & 51-75-12.Apr 3, 2013 · N171US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013040800035Seat Track · corrodedS2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR16 TO FR24, -Y1292. REPLACED SEAT TRACK BETWEEN FR16 TO FR24, -Y1292 IAW A321 SRM 51-42-11 & 51-75-12.Apr 3, 2013 · N171US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013040800002Support Fitting · corroded2S CHECK - CORROSION ON FITTING AT RIGHT AFT PASS/CREW DOOR OF SLIDE SUPPORT. REPLACED SLIDE SUPPORT FITTING AT RIGHT AFT PASS/CREW DOOR IAW A321 CMM 52-13-15-400.Apr 3, 2013 · N173US · Airbus A321211 · Passenger/Crew DoorsSDR USAA2013040400004Power Supply · faultyWHILE TESTING EMERGENCY LIGHTING SYSTEM. RECEIVED EMERGENCY POWER SUPPLY UNIT FAULT. REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT, IAW AIRBUS MAINTENANCE MANUAL 33-51-38-000-001-A.Apr 3, 2013 · N179UW · Airbus A321211 · Emergency LightingSDR USAA2013040800004Fitting · corroded2S CHECK - GALVANIC CORROSION ON CENTER FITTING LOCATED BETWEEN FR 66 TO FR 68 STR 23L (SHAPE, SILL). REPLACED CENTER FITTING (SHAPE SILL) LOCATED BETWEEN FR 66 TO FR 68, STR 23L IAW A321 SRM A321 51-72-11 PAGE 1-2 AND DRAWING D53480505.Apr 2, 2013 · N173US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013040900022Floor Support · corrodedS2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR16 TO FR23, Y254. REPLACED FLOOR SUPPORT BETWEEN FR16 TO FR23, Y254 IAW A321 SRM 51-42-11, 51-44-11, 51-73-00 & 53-11-14.Apr 2, 2013 · N171US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013040900020Sill · corrodedS2 CHECK - LEVEL 2 GALVANIC CORROSION ON SILL BETWEEN FR66 TO FR68, -Y1732. REPLACED SILL BETWEEN FR66 TO FR68, -Y1732 IAW A321 SRM 51-74-00, 53-41-14 & 51-42-11.Apr 2, 2013 · N171US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013040800047Floor Panel · delaminatedS2 CHECK - DELAMINATION ON FLOOR PANEL 151PF BETWEEN FR58 TO FR59 & BETWEEN S38L TO S38R. REPLACED FLOOR PANEL 151PF IAW A321 SRM 53-02-00.Apr 2, 2013 · N171US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013040800046Floor Panel · delaminatedS2 CHECK - DELAMINATION ON FLOOR PANEL 151LF BETWEEN FR56 TO FR58 & BETWEEN S38L TO S38R. REPLACED FLOOR PANEL 151LF IAW A321 SRM 53-02-00.Apr 2, 2013 · N171US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013040800045Floor Panel · delaminatedS2 CHECK - DELAMINATION ON FLOOR PANEL 151GF BETWEEN FR53 TO FR56 & BETWEEN S38L TO S38R. REPLACED FLOOR PANEL 151GF IAW A321 SRM 53-02-00.Apr 2, 2013 · N171US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013040800044Floor Panel · delaminatedS2 CHECK - DELAMINATION ON FLOOR PANEL 222CF BETWEEN FR16 TO FR20 & BETWEEN Y1292 TO -Y254. REPLACED FLOOR PANEL 222CF IAW A321 SRM 53-02-00.Apr 2, 2013 · N171US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013040800043Floor Panel · delaminatedS2 CHECK - DELAMINATION ON FLOOR PANEL 261FG BETWEEN FR64 TO FR66 & BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL 261FG IAW A321 SRM 53-02-00.Apr 2, 2013 · N171US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013040800042Floor Panel · delaminatedS2 CHECK - DELAMINATION ON FLOOR PANEL 261QF BETWEEN FR64 TO FR66 & BETWEEN Y765 TO -Y254. REPLACED FLOOR PANEL 261QF IAW A321 SRM 53-02-00.Apr 2, 2013 · N171US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013040800041Floor Panel · delaminatedS2 CHECK - DELAMINATION ON FLOOR PANEL 262HG BETWEEN FR64 TO FR66 & BETWEEN Y254 TO -Y1732. REPLACED FLOOR PANEL 262HG IAW A321 SRM 53-02-00.Apr 2, 2013 · N171US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013040800040Floor Panel · delaminatedS2 CHECK - DELAMINATION ON FLOOR PANEL 261PF BETWEEN FR68 TO FR70 & BETWEEN Y1292 TO -Y1292. REPLACED FLOOR PANEL 261PF IAW A321 SRM 53-02-00.Apr 2, 2013 · N171US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013040800039Floor Panel · delaminatedS2 CHECK - DELAMINATION ON FLOOR PANEL 261DF BETWEEN FR66 TO FR68 & BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL 261DF IAW A321 SRM 53-02-00.Apr 2, 2013 · N171US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013040800022Floorbeam · corrodedS2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, Y765 IAW A321 SRM 51-42-11, 51-74-00 & 51-21-11.Apr 2, 2013 · N171US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA2013040900026Fitting · corrodedS2 CHECK - LEVEL 2 GALVANIC CORROSION ON FITTING BETWEEN FR16 TO FR20, -Y1732. REPLACED FITTING BETWEEN FR16 TO FR20, -Y1732 IAW A321 SRM 51-42-11 & 53-11-14.Apr 1, 2013 · N171US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013040900019Sill · corrodedS2 CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT AFT PASSENGER DOOR MIDDLE SHAPE SILL BETWEEN FR66 TO FR68, Y1732. REPLACED SHAPE SILL BETWEEN FR66 TO FR68, Y1732 IAW A321 SRM 51-42-11, 51-44-11 & 51-21-11.Apr 1, 2013 · N171US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013040800030Dummy Rail · corrodedS2 CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY AT FR16, Y503.2. REPLACED RAIL DUMMY AT FR16, Y503.2 IAW A321 SRM 51-74-00, 53-11-14 & 51-42-11.Apr 1, 2013 · N171US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013040800029Dummy Rail · corrodedS2 CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY AT FR16, -Y81. REPLACED RAIL DUMMY AT FR16, -Y81 IAW A321 SRM 51-22-00, 53-11-12 & 51-42-11.Apr 1, 2013 · N171US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013040800028Seat Track · corrodedS2 CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL/TRACK BETWEEN FR20 TO FR24, -Y189. REPLACED RAIL/TRACK BETWEEN FR20 TO FR24, -Y189 IAW A321 SRM 51-74-00, 53-11-14 & 51-42-11.Apr 1, 2013 · N171US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013040300008Floor Panel · delaminatedS2 CHECK - DELAMINATION ON FLOOR PANEL 221LF BETWEEN FR12 TO FR16, Z-500 & BETWEEN Y510 TO Y=0. REPLACED FLOOR PANEL 221LF IAW IRM, 9701, REV G.Mar 30, 2013 · N172US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013040100032Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 231EF BETWEEN FR20 TO FR24 & BETWEEN Y1292 TO Y765. REPLACED FLOOR PANEL 231EF IAW A321 IRM 9701, REV G.Mar 30, 2013 · N172US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013040100031Floor Panel · cracked2S CHECK - CRACK ON FLOOR PANEL 251UF BETWEEN FR58 TO FR62 & BETWEEN Y1732 TO Y1292. REPLACED FLOOR PANEL 251UF IAW A321 IRM 9701, REV G.Mar 30, 2013 · N172US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013040100006Unknown · odorDURING CRUISE, FLIGHT ATTENDANTS REPORTED AN ACRID ODOR IN THE CABIN IN THE AREA OF ROW 8 TO 16. SEVERAL PASSENGERS REPORTED AN ODOR SIMILAR TO NAIL POLISH OR MARKERS. FLIGHT ATTENDANT "A" AND "F" REPORTED HAVING A DULL HEADACHE AND NOSE IRRITATION. MAINTENMar 30, 2013 · N165US · Airbus A321211 · Air Distribution SystemSDR USAA2013032900023Lens · missingTHE 14C EMERGENCY LIGHT LENS MISSING. REPLACED EMERGENCY LIGHT LENS AT SEAT 14C.Mar 28, 2013 · N180US · Airbus A321211 · Emergency LightingSDR USAA2013032800012Lens · missingEMERGENCY LIGHT COVER MISSING AT L4 DOOR. REPLACED EMERGENCY LIGHT COVER AT L4 DOOR.Mar 27, 2013 · N170US · Airbus A321211 · Emergency LightingSDR USAA2013042300008Rib · cracked2S CHECK - CRACK IN LEFT WING SLAT NR 2, TRACK RIB 5. REPAIRED ATTACH FITTING OF LEFT WING SLAT NR 2 TRACK RIB 5 IAW A321 SRM 57-40-00.Mar 26, 2013 · N173US · Airbus A321211 · Leading Edge DevicesSDR USAA2013042200016Fuel Door · elongated2S CHECK - ELONGATED HOLE ON LOWER LEFT WING FUEL DOOR 540HB BETWEEN RIB 13 TO RIB 14 & BETWEEN S8L TO S11L. REPLACED LEFT WING FUEL DOOR 540HB IAW A321 SRM 57-27-11.Mar 26, 2013 · N173US · Airbus A321211 · Wing, Plate/SkinSDR USAA2013042200015Fuel Door · elongated2S CHECK - ELONGATED HOLE ON LOWER RIGHT WING FUEL DOOR 640KB BETWEEN RIB 15 TO RIB 16 AND BETWEEN S8R TO S11R. REPLACED RIGHT WING FUEL DOOR 640KB IAW A321 SRM 57-27-11.Mar 26, 2013 · N173US · Airbus A321211 · Wing, Plate/SkinSDR USAA2013041700031Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, S23R, -Y765. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, S23R, -Y765 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53372500.Mar 26, 2013 · N173US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013042300012Stringer · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON STRINGER BETWEEN FR28 TO FR29, S42L. REPAIRED STRINGER 42L BETWEEN FR28 TO FR29 IAW A321 SRM 53-21-13.Mar 25, 2013 · N173US · Airbus A321211 · Fuselage Main, Longeron/StringerSDR USAA2013042200013Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 151LF BETWEEN FR56 TO FR58 & BETWEEN -Y765 TO Y765. REPLACED FLOOR PANEL 151LF IAW A321 SRM 53-02-00 FIGURE 209 & IRM 9701 REV G.Mar 25, 2013 · N173US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013042200011Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 261DF BETWEEN FR66 TO FR68 & BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL 261DF IAW A321 SRM 53-02-00 FIG 209, IRM 9701 REV G & EA 503993.Mar 25, 2013 · N173US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013042200010Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 232DF BETWEEN FR20 TO FR24 & BETWEEN -Y765 TO -Y254. REPLACED FLOOR PANEL 232DF IAW A321 AMM 53-12-12.Mar 25, 2013 · N173US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013041800016Seat Track · corroded2S CHECK - CABIN SEAT TRACK CORRODED FROM FR 41 TO FR 47 AT Y -1292. REMOVED AND REPLACED SEAT TRACK IAW A321 SRM 51-72-11, AIRBUS DRAWING D53371112 AND EA 503994.Mar 25, 2013 · N173US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013041800015Seat Track · corroded2S CHECK - CABIN SEAT TRACK CORRODED FROM FR 36 TO FR 41 AT Y 765. REMOVED AND REPLACED SEAT TRACK IAW A321 SRM 51-72-11 AND AIRBUS DRAWING D53372500.Mar 25, 2013 · N173US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013041700032Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR41 TO FR46+15 INCHES, S23L, Y1292. REPLACED SEAT TRACK BETWEEN FR41 TO FR46+15 INCHES, S23L, Y1292 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53372500.Mar 25, 2013 · N173US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013041600023Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 261BG BETWEEN FR64 TO FR66 & BETWEEN Y1732 TO Y765. REPLACED FLOOR PANEL 261BG IAW A321 SRM 53-02-00, FIGURE 209 & IRM 9701 REV G.Mar 25, 2013 · N173US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013041600022Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 151PF BETWEEN FR58 TO FR59 & BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL 151PF IAW A321 SRM 53-02-00, FIGURE 209 & IRM 9701 REV G.Mar 25, 2013 · N173US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013041600021Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 152MF BETWEEN FR56 TO FR58 & BETWEEN -Y970.8 TO -Y765. REPLACED FLOOR PANEL 152MF IAW A321 SRM 53-02-00, FIGURE 209 & IRM 9701 REV G.Mar 25, 2013 · N173US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013041600020Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 231BF BETWEEN FR20 TO FR24 & BETWEEN Y765 TO -Y254. REPLACED FLOOR PANEL 231BF IAW A321 SRM 53-12-00, FIGURE 206 & IRM 9701 REV G.Mar 25, 2013 · N173US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013041600019Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 222CF BETWEEN FR12 TO FR16 & BETWEEN -Y1732 TO -Y254. REPLACED FLOOR PANEL 222CF IAW A321 SRM 53-12-00, FIGURE 206 & IRM 9701 REV G.Mar 25, 2013 · N173US · Airbus A321211 · Fuselage Floor PanelSDR USAA2013040300021Hinge Fitting · corroded2S CHECK - EXCESSIVE PLAY ON NR 6 LEFT ELEVATOR HINGE ARM FITTING AT HORIZONTAL STABILIZER STA 589, RIB 13. REPLACED NR 6 LEFT ELEVATOR HINGE ARM FITTING IAW A321 AMM 55-16-42.Mar 25, 2013 · N173US · Airbus A321211 · Elevator StructureSDR USAA2013032900003Skin Panel · crackedS2 CHECK - CRACK IN RIGHT WING UPPER SKIN PANEL OF FIXED LEADING EDGE AT SLAT TRACK NR 2 CUTOUT SURROUNDING AREA BETWEEN RIB 2 THRU RIB 3. REPAIRED RIGHT WING UPPER SKIN PANEL OF FIXED LEADING EDGE AT SLAT TRACK NR 2 CUTOUT IAW EA 204449.Mar 25, 2013 · N172US · Airbus A321211 · Wing, Plate/SkinSDR USAA2013032600010Light · inoperativeFLOOR LEVEL EMERGENCY EXIT LIGHT AT SEAT 9D IS INOPERATIVE. RE-INSTALLED LIGHT ASSEMBLY.Mar 25, 2013 · N169UW · Airbus A321211 · Emergency LightingSDR USAA2013042900012Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, Y765. REPLACED SEAT TRACK BETWEEN FR24 TO FR35, Y765 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53234930.Mar 24, 2013 · N173US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013042300009Angle · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON ANGLE BETWEEN FR47.2 TO FR47.4, S28R. REPLACED ANGLE BETWEEN FR47.2 TO FR47.4, S28R IAW A321 SRM 51-72-11, AIRBUS DRAWING D53456593 & D53456593.Mar 24, 2013 · N173US · Airbus A321211 · Fuselage Miscellaneous Structure
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