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 USAA2013030400032Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL AT AFT LEFT PASSENGER DOOR WAY BETWEEN FR66 TO FR68, S23L. REPLACED LOWER SILL AT AFT LEFT PASSENGER DOOR WAY IAW A321 SRM 51-72-11, AIRBUS DRAWING D53480505 & EA 503875.SDR USAA2013030400031Plate · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FISH PLATE AT FR30+15 INCHES, S43L. REPLACED FISH PLATE AT FR30+15 INCHES, S43L IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53234615.SDR USAA2013022100022Cleat · corroded2S CHECK - GALVANIC CORROSION ON CLEAT AT FR33, BETWEEN S40R TO S41R. REPLACED CLEAT AT FR33, BETWEEN S40R TO S41R IAW A321 51-72-11 AND AIRBUS DRAWING D53234411.SDR USAA2013022100021Cleat · corroded2S CHECK - GALVANIC CORROSION ON CLEAT AT FR30, BETWEEN S40R TO S41R. REPLACED CLEAT AT FR30, BETWEEN S40R TO S41R IAW A321 SRM 51-72-11 AND AIRBUS DRAWING D53234411.SDR USAA2013022100018Beam · corroded2S CHECK - GALVANIC CORROSION ON BEAM ASSEMBLY BETWEEN FR65 TO FR66, AT Y1732. REPLACED BEAM ASSEMBLY BETWEEN FR65 TO FR66, AT Y1732 IAW A321 SRM 51-72-11 AND AIRBUS DRAWING D53474250.SDR USAA2013022600019Plate · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FISH PLATE AT FR30+15 INCH, S42L. REPLACED FISH PLATE AT FR30+15 INCH, S42L IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53234615.SDR USAA2013022600018Beam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON BEAM ASSEMBLY BETWEEN FR65 TO FR67, -Y318. REPLACED BEAM ASSEMBLY BETWEEN FR65 TO FR67, -Y318 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472814.SDR USAA2013022600008Beam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON BEAM ASSEMBLY AT FR66, -Y465. REPLACED BEAM ASSEMBLY AT FR66, -Y465 IAW A321 SRM 51-72-11 & AIRBUS DRAWING 53472816.SDR USAA2013022600007Beam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON BEAM ASSEMBLY BETWEEN FR64 TO FR67+10 INCHES, Y512. REPLACED BEAM ASSEMBLY BETWEEN FR64 TO FR67+10 INCHES, Y512 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472815.SDR USAA2013022600006Beam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON AUXILIARY BEAM ASSEMBLY BETWEEN FR64 TO FR66, Y512. REPLACED AUXILIARY BEAM ASSEMBLY BETWEEN FR64 TO FR66, Y512 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472815.SDR USAA2013022600005Cleat · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR34 BETWEEN S41R TO S42R. REPLACED CLEAT AT FR34 BETWEEN S41R TO S42R IAW A321 SRM 51-72-11 & AIRBUS DRAWING 53234411.SDR USAA2013022600004Cleat · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR35.1 BETWEEN S40R TO S41R. REPLACED CLEAT AT FR35.1 BETWEEN S40R TO S41R IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53235027.SDR USAA2013022100017Seat Track · corroded2S CHECK - GALVANIC CORROSION ON SEAT RAIL BETWEEN FR64 TO FR66, AT -Y1292. REPLACED SEAT RAIL BETWEEN FR64 TO FR66, AT -Y1292 IAW A321 SRM 51-72-11.SDR USAA2013022100011Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 151LF BETWEEN FR56 TO FR58, -Y765 TO Y765. REPLACED FLOOR PANEL 151LF IAW SRM 53-02-00 PARAGRAPH 8H, FIGURE 209 AND IRM 9701 REV G.SDR USAA2013022100010Floorbeam · corroded2S CHECK - CORROSION ON AFT PAX CABIN FLOORBEAM. REPLACED FLOORBEAM AND FASTENERS IAW A321 SRM 51-72-11 AND DRAWING D534 72816.SDR USAA2013022100009Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 151GF LOCATED BETWEEN FR 52 TO FR 56 AND BL Y-765 TO Y765. REPLACED FLOOR PANEL 151GF IN AFT CARGO COMPARTMENT IAW A321-211 SRM 53-02-00 PAR 8H FIGURE 209 AND IRM 9701 REV G.SDR USAA2013020800036Pump · failedAFTER ENGINE START, ECAM SHOWED NUMBER 2 ENGINE FAIL, ENGINE THEN SHUT DOWN. REMOVED AND REPLACED NR 2 ENGINE FUEL PUMP/FILTER, BLEED VALVE PRESSURE REGULATOR AND HYDROMECHANICAL UNIT. ENGINE FUEL PUMP DETERMINED TO BE CAUSE OF FAILURE.SDR USAA2013020600002Damper · out of adjust2S CHECK - OUT OF ADJUSTMENT DIMENSION "A" (J2) BETWEEN FINGER & STRIKER LEVER DAMPER MECHANISM AT DOOR 841. PERFORMED ADJUSTMENT DIMENSION "A" (J2) BETWEEN FINGER & STRINGER LEVER DAMPER MECHANISM AT DOOR 841 IAW A321 AMM 52-11-14-820-002-A. ADJUSTMENT IS OSDR USAA2013022600021Lever · damaged2S CHECK - ELONGATED HOLE ON LEFT INBOARD FLAP LEVER ASSEMBLY. REPLACED LEFT INBOARD FLAP LEVER ASSEMBLY IAW A321 CMM 57-52-23.SDR USAA2013022500034Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 151DF BETWEEN FR50 TO FR53 & BETWEEN -Y765 TO Y765. REPLACED FLOOR PANEL 151DF IAW A321 SRM 53-02-00, PAR 8H, FIG. 209 & IRM 9701 REV G.SDR USAA2013020400030Proximity Switch · faultyCREW REPORTED THE 4R DOOR SLIDE SHOWS DISARMED ON ECAM. ARMING HANDLE RECYCLED - STILL SHOWS DISARMED AND CABIN PRESSURE LIGHT ON DOOR FLASHING. SOMETIME DURING DESCENT DOOR SHOWED REARMED. MAINTENANCE REMOVED AND REPLACED PROXIMITY SWITCH (7WN2) ON 4R DOORSDR USAA2013021200002Stringer · corrodedS2 CHECK - CORROSION ON STRINGER 40L AT FR37.5. REPAIRED STRINGER 40L AT FR37.5 IAW A321 SRM 51-74-00 & EA 204147.SDR USAA2013021800025Stringer · corroded2S CHECK - CORROSION ON STRINGER BETWEEN FR34 TO FR35, S41R. REPAIRED STRINGER BETWEEN FR34 TO FR35, S41R IAW A321 SRM 53-21-13, FIG 202 (SHEET 2), PAGE 219.SDR USAA2013012800013Hydraulic Line · chafedCREW RECEIVED A GREEN HYDRAULIC LOW LEVEL ECAM WARNING IN CRUISE. FLIGHT CONTINUED TO CLT, CREW DECLARED AN EMERGENCY FOR LANDING, AND AIRCRAFT WAS TOWED OFF RUNWAY TO GATE. FOUND HYDRAULIC LINE CHAFED ON NR 1 ENGINE COMING FROM ENGINE DRIVEN PUMP PRESSURE SSDR USAA2013012900006Floor Panel · delaminatedS2 CHECK - DELAMINATION ON FLOOR PANEL 222EF BETWEEN FR16 TO FR20 & BETWEEN -Y1292 TO -Y520. REPLACED FLOOR PANEL 222EF IAW A321 SRM 51-10-02 & 51-40-02.SDR USAA2013012500011Floor Panel · delaminatedS2 CHECK - DELAMINATION ON FLOOR PANEL 261QF BETWEEN FR64 TO FR66 & BETWEEN Y254 TO Y-254. REPLACED FLOOR PANEL 261QF IAW IRM 9701 REV G.SDR USAA2013012500001Floor Panel · delaminatedS2 CHECK - DELAMINATION ON FLOOR PANEL 261DF BETWEEN FR66 TO FR68 & BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL 261DF IAW IRM 9701 REVISION G.SDR USAA2013021900010Stringer · corroded2S CHECK - CORROSION ON STRINGER AT FR35.5, S44. REPAIRED STRINGER AT FR35.5, S44 IAW EA 503797.SDR USAA2013012500002Lens · brokenSEAT 9D EMERGENCY EGRESS LIGHT COVER IS BROKEN. REPLACED SEAT 9D EMERGENCY EXIT LIGHT LENS COVER.SDR USAA2013020800012Crossbeam · elongated2S CHECK - ELONGATED HOLES ON SUPPORT CROSS BEAM AT FR67, Y1162. REPLACED SUPPORT CROSS BEAM AT FR67, Y1162 IAW A321 SRM 51-7-11 & AIRBUS DRAWING D53474250.SDR USAA2013020700028Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 241EF BETWEEN FR36 TO FR42 & BETWEEN Y254 TO -Y254. REPLACED FLOOR PANEL 241EF IAW A321 SRM 53-02-00-201 & IRM 9701 REV G.SDR USAA2013020500016Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 242FF BETWEEN FR36 TO FR42 & BETWEEN -Y765 TO -Y254. REPLACED FLOOR PANEL 242FF IAW A321 SRM 53-02-00-201 & IRM 9701 REV G.SDR USAA2013012200028Lens · brokenEXIT LIGHT COVER BY FORWARD FLIGHT ATTENDANT JUMPSEAT BROKEN OFF. REPLACED EXIT LIGHT LENS COVER AT L-1 DOOR AS REQUIRED.SDR USAA2013012200027Power Supply · failedEMERGENCY LIGHTING FAILS SYSTEM CHECK - INDICATES EPSU 10WL FAILURE. FOUND SEAT ROW 1L EMERGENCY LIGHT WIRING SHORTED. REMOVED AND REPLACED TWO DEFECTIVE SPLICES AT ROW 1L. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (EPSU) AND BATTERY IAW AIRBUS MAINTSDR USAA2013021300019Fitting · corroded2S CHECK - CORROSION ON FITTING AT FR56 BETWEEN S37R TO S38R. REPLACED FITTING AT FR56 BETWEEN S37R TO S38R IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53475500.SDR USAA2013020500018Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 251SF BETWEEN FR57 TO FR62 & BETWEEN Y254 TO Y765. REPLACED FLOOR PANEL 251SF IAW A321 SRM 53-02-00-201 & IRM 9701 REV G.SDR USAA2013020500017Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 252KF BETWEEN FR51 TO FR57 & BETWEEN -Y1732 TO -Y1292. REPLACED FLOOR PANEL 252KF IAW A321 SRM 53-02-00-201 & IRM 9701 REV G.SDR USAA2013012900008Support · damaged2S CHECK - ELONGATED HOLE ON CROSS BEAM SUPPORT AT FR67, -Y1292. REPLACED CROSS BEAM SUPPORT AT FR67, -Y1292 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53474250.SDR USAA2013021900009Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 251PG BETWEEN FR47 TO FR47.5 & BETWEEN -Y254 TO Y254. REPLACED FLOOR PANEL 251PG IAW A321 SRM 53-02-00, FIG 209 & IRM 9701, REV "G".SDR USAA2013021800022Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL NR 251AG BETWEEN FR47 TO FR47.5 & BETWEEN Y254 TO -Y254. REPLACED FLOOR PANEL 251AG IAW A321 SRM 53-02-00 & IRM 9701 REV G.SDR USAA2013021100011Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 251CG BETWEEN FR47 TO FR47.5, Y1292. REPLACED FLOOR PANEL 251CG IAW A321 SRM 51-72-11.SDR USAA2013020800013Web · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR STRUCTURE WEB AT FR20, Y1732. REPLACED FLOOR STRUCTURE WEB AT FR20, Y1732 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53110920.SDR USAA2013020700029Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 212EF BETWEEN FR6 TO FR12 & BETWEEN -Y254 TO -Y765. REPLACED FLOOR PANEL 212EF IAW A321 SRM 53-12-00, PAR 5.F, FIG 206 & IRM 9701 REV G.SDR USAA2013012200030Hydraulic Line · leakingFLIGHT CREW EXPERIENCED LOSS OF YELLOW HYDRAULIC PRESSURE ENROUTE FROM MBJ TO PHL AND REPORTED 'HYD Y LO LEVEL' FAULT. AN EMERGENCY WAS DECLARED FOR LANDING. MAINTENANCE FOUND NR 2 ENGINE HYDRAULIC TUBE LEAKING. REPLACED TUBE.SDR USAA2013020600014Skin Panel · cracked2S CHECK - CRACK ON FUSELAGE SKIN PANEL BETWEEN FR59 TO FR60 & BETWEEN S33L TO S34L. REPLACED LOWER INBOARD COUPLING AT FR66, S23L IAW A321 SRM 53-41-11, PARA 5L F.SDR USAA2013020500015Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 222EF BETWEEN FR24 TO FR20 & BETWEEN -Y254 TO -Y1292. REPLACED FLOOR PANEL 222EF IAW A321 SRM 53-12-00 & IRM 9701 REV G.SDR USAA2013020500014Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 221PF BETWEEN FR16 TO FR20 & BETWEEN -Y254 TO Y1292. REPLACED FLOOR PANEL 221PF IAW A321 SRM 53-12-00 & IRM 9701 REV G.SDR USAA2013020500013Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 221DF BETWEEN FR16 TO FR24 & BETWEEN -Y254 TO Y765. REPLACED FLOOR PANEL 221DF IAW A321 SRM 53-12-00 & IRM 9701 REV G.SDR USAA2013013100005Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 151GF BETWEEN FR52 TO FR56 & BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL 151GF IAW A321 SRM 53-02-00-201 & IRM 9701 REV G.SDR USAA2013021300020Hinge Pin · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT AILERON NR 4 HINGE PIN BETWEEN WS 1346 TO WS 1406 & BETWEEN WING RIB 26 TO RIB 25. REPLACED LEFT AILERON NR 4 HINGE PIN IAW A321 AMM 27-14-41.
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