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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR USAA2013012300002Web · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON WEB AT FR16, S23R. REPLACED WEB AT FR16, S23R IAW A321 SRM 51-42-11 & 51-72-11.SDR USAA2013012300001Floor 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.SDR USAA2013012200015Shear Plate · cracked2S CHECK - CRACK ON SHEAR PLATE BETWEEN FR47.2A TO FR47.4, S28R. REPLACED SHEAR PLATE BETWEEN FR47.2A TO FR47.4, S28R IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53475333.SDR USAA2013012200014Floor 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 FIG 209, IRM 9701 REV G & EA 503673.SDR USAA2013012200013Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 262BG BETWEEN FR64 TO FR66 & BETWEEN -Y1732 TO -Y765. REPLACED FLOOR PANEL 262BG IAW A321 SRM 53-02-00 FIG 209, IRM 9701 REV G & EA 503674.SDR USAA2013011700031Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y765. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y765 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53112812.SDR USAA2013011700030Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR16 TO FR24, -Y1292. REPLACED SEAT TRACK BETWEEN FR16 TO FR24, -Y1292 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53112812.SDR USAA2013011500028Support Bracket · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CABIN SUPPORT ANGLE BETWEEN FR12+4 INCHES TO FR16, S23R. REPLACED CABIN SUPPORT ANGLE BETWEEN FR12+4 INCHES TO FR16, S23R IAW A321 SRM 51-72-11.SDR USAA2013011500027Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 261AG BETWEEN FR64 TO FR66 & BETWEEN -Y765 TO Y765. REPLACED FLOOR PANEL 261AG IAW A321 SRM 53-02-00 & IRM 9701 REV G.SDR USAA2013011500023Coupling · damaged2S CHECK - ELONGATED HOLE ON COUPLING AT FR66, S23L. REPLACED COUPLING AT FR66, S23L IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53474250.SDR USAA2013011500022Coupling · damaged2S CHECK - ELONGATED HOLE ON COUPLING AT FR66, S23L. REPLACED COUPLING AT FR66, S23L IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53474250.SDR USAA2013011500021Coupling · damaged2S CHECK - ELONGATED HOLE ON COUPLING AT FR66, S23R. REPLACED COUPLING AT FR66, S23R IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53474250.SDR USAA2013011500020Coupling · damaged2S CHECK - ELONGATED HOLE ON COUPLING AT FR66, S23R. REPLACED COUPLING AT FR66, S23R IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53474250.SDR USAA2013011500019Coupling · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR67+19 INCHES, Y1132. REPLACED COUPLING AT FR67+19 INCHES, Y1132 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472780.SDR USAA2013011500015Cleat · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR32 BETWEEN S40R TO S41R. REPLACED CLEAT AT FR32 BETWEEN S40R TO S41R IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53234411.SDR USAA2013011000033Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR65+19 INCHES, -Y1732. REPLACED FLOORBEAM AT FR65+19 INCHES, -Y1732 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53474250 & D53472750.SDR USAA2013011000032Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR67+11 INCHES, Y1132. REPLACED FLOORBEAM AT FR67+11 INCHES, Y1132 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53472815 & D53472780.SDR USAA2013011000029Fitting · damaged2S CHECK - ELONGATED HOLE ON FITTING AT FR12, Y503. REPLACED FITTING AT FR12, Y503 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53112758.SDR USAA2013011100008Seat Track · corroded2S CHECK - SEAT TRACK CORRODED AT Y765 BETWEEN FR 12 AND FR 24. REMOVED AND REPLACED SEAT TRACK IAW A321 SRM 51-72-11 AND AIRBUS DRAWINGS D53112812 AND D53110984.SDR USAA2013011100007Stiffener · corroded2S CHECK - STIFFENER CORRODED BETWEEN FR 12 AND FR 13 FROM -Y254 TO -Y1292. REMOVED AND REPLACED STIFFENER IAW A321 SRM 51-72-11.SDR USAA2013011100006Floor Support · corroded2S CHECK - LONGITUDINAL FLOOR SUPPORT CORRODED AT -Y254 BETWEEN FR 12 AND FR 24. REMOVED AND REPLACED SUPPORT IAW A321 SRM 51-72-11 AND AIRBUS DRAWING D53111462.SDR USAA2013011000014Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 241AF BETWEEN FR35.8 TO FR36 & BETWEEN -Y254 TO Y254. REPLACED FLOOR PANEL 241AF IAW A321 SRM 53-02-00 PARA 8H FIG 209 & IRM 9701 REV G.SDR USAA2013011000012Dummy Rail · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY BETWEEN FR12 TO FR16, Y503. REPLACED RAIL DUMMY BETWEEN FR12 TO FR16, Y503 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53112825 & D53110984.SDR USAA2013011000011Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER DOOR SILL BETWEEN FR66 TO FR68, S23L. REPLACED LOWER DOOR SILL BETWEEN FR66 TO FR68, S23L IAW A321 SRM 51-72-11, EA 503645 & AIRBUS DRAWING D53480505.SDR USAA2013011000010Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER DOOR SILL BETWEEN FR66 TO FR68, S23R. REPLACED LOWER DOOR SILL BETWEEN FR66 TO FR68, S23R IAW A321 SRM 51-72-11, EA 503646 & AIRBUS DRAWING D53480505.SDR USAA2013010800030Web · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON WEB BETWEEN FR20 TO FR24, S23L. REPLACED WEB BETWEEN FR20 TO FR24, S23L IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53114392.SDR USAA2013010800029Web · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON WEB BETWEEN FR20 TO FR24, S23R. REPLACED WEB BETWEEN FR20 TO FR24, S23R IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53114392.SDR USAA2013010800028Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR20 TO FR24, -Y189. REPLACED SEAT TRACK BETWEEN FR20 TO FR24, -Y189 IAW A321 SRM 51-72-11, 51-42-11 & AIRBUS DRAWING D53111406.SDR USAA2013010400019Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR64 TO FR66, -Y1292. REPLACED SEAT RAIL BETWEEN FR64 TO FR66, -Y1292 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472816.SDR USAA2013010400017Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BEAM AT FR64+10 INCHES, -Y765. REPLACED SEAT RAIL BEAM AT FR64+10 INCHES, -Y765 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472816.SDR USAA2013010400016Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR66 TO FR70, -Y765 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472780.SDR USAA2013010400015Dummy Rail · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY BETWEEN FR12 TO FR16, -Y81. REPLACED RAIL DUMMY BETWEEN FR12 TO FR16, -Y81 IAW A321 SRM 51-72-11.SDR USAA2013010400014Floor Support · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SUPPORT FLOOR BETWEEN FR12 TO FR24, Y254. REPLACED SUPPORT FLOOR BETWEEN FR12 TO FR24, Y254 IAW A321 SRM 51-42-11, AIRBUS DRAWING D53112816 & D53110920.SDR USAA2012122600014Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 221EF BETWEEN FR16 TO FR20 & BETWEEN Y254 TO Y1292. REPLACED FLOOR PANEL 221EF IAW A321 SRM 53-12-00 FIG 206 & IRM 9701 REV G.SDR USAA2012122600013Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 261PF BETWEEN FR68 TO FR70 & BETWEEN -Y1292 TO Y1292. REPLACED FLOOR PANEL 261PF IAW A321 SRM 53-02-00 FIG 209 & IRM 9701 REV G.SDR USAA2013010800033Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON NR 4 RUDDER HINGE FITTING AT VERTICAL STABILIZER STA 2632, RIB 6. REPLACED NR 4 RUDDER HINGE FITTING AT VERTICAL STABILIZER STA 2632, RIB 6 IAW A321 SRM 51-72-11.SDR USAA2013010800032Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON NR 3 RUDDER HINGE FITTING AT VERTICAL STABILIZER STA 2279, RIB 5. REPLACED NR 3 RUDDER HINGE FITTING AT VERTICAL STABILIZER STA 2279, RIB 5 IAW A321 SRM 51-72-11.SDR USAA2013010800031Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON NR 2 RUDDER HINGE FITTING AT VERTICAL STABILIZER STA 1926, RIB 4. REPLACED NR 2 RUDDER HINGE FITTING AT VERTICAL STABILIZER STA 1926, RIB 4 IAW A321 SRM 51-42-11.SDR USAA2012120700015Stringer · corrodedIFE (GOGO) INSTALLATION. FUSELAGE STRINGER 43L CORRODED BETWEEN FR 55 AND FR 58. REPAIRED STRINGER IAW EA 203929.SDR USAA2012120700014Target · out of adjustL4 DOOR DISARMED ITSELF DURING CLIMBOUT. AIRCRAFT PRESSURIZED NORMALLY BUT ECAM SHOWED DOOR DISARMED AND RED LIGHTS WERE FLASHING ON FLIGHT ATTENDANT PANEL. ADJUSTED TARGET FOR SLIDE ARM SWITCH IAW AIRBUS MAINTENANCE MANUAL 52-13-22.SDR USAA2012120700013Lens · detachedEMERGENCY LIGHT COVER FOR 4L FELL OFF. REINSTALLED LIGHT LENS COVER AT 4L.SDR USAA2012120500011Lens · brokenPLASTIC EXIT LIGHT COVER AT 4L DOOR BROKEN. INSTALLED SERVICEABLE EMERGENCY EXIT LIGHT COVER AT 4L DOOR.SDR USAA2012120400014Power Supply · inoperativeEXIT SIGN LIGHT OVER AFT TWO DOORS INOPERATIVE USING THE "PED"SWITCH. REMOVED AND REPLACED AFT EMERGENCY POWER SUPPLY UNIT IAW AIRBUS MAINTENANCE MANUAL 33-51-38-400-001-A.SDR USAA2012120300042Cylinder · low pressureR2 DOOR EMERGENCY OPERATION CYLINDER PRESSURE IS IN YELLOW BAND. SERVICED R2 DOOR EMERGENCY OPERATION CYLINDER IAW AMM 52-22-00-014-002.SDR USAA2012120300028Lens · crackedEMERGENCY LIGHT LENS COVER CRACKED ROW 9D. REMOVED AND REPLACED EMERGENCY LIGHT LENS COVER ROW 9D.SDR USAA2012112800022Extinguisher · dischargedLAV D FIRE EXTINGUISHER EMPTY FOR WASTE BIN. REMOVED AND REPLACED LAV D WASTE CONTAINER FIRE EXTINGUISHER BOTTLE.SDR USAA2012112700031Power Supply · inoperativeEXIT 3R EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT IAW AIRBUS MAINTENANCE MANUAL 33-51-38-000-002A.SDR USAA2012112700033Proximity Switch · faultyON GROUND DOOR 4R SLIDE ARMED. IN-FLIGHT AT ALTITUDE 4R DOOR SLIDE NOT ARMED. REPLACED DOOR 4R PROXIMITY SWITCH IAW AIRBUS MAINTENANCE MANUAL 52-71-11-000-001A.SDR USAA2012112600006Lens · detachedEMERGENCY EXIT LIGHT COVER OFF AT DOOR 4R. RE-INSTALLED LENS.SDR USAA2012112600001Connector · unsecureECAM MESSAGE "WHEEL, N/W STEER FAULT" ON APPROACH AFTER GEAR WAS SELECTED DOWN. CREW FOLLOWED ECAM PROCEDURES, CONTACTED MOC AND CYCLED NOSE WHEEL STEERING SWITCH AS INSTRUCTED WITH NO SUCCESS. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS
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