Airbus A321-211

Service difficulty reports · 12,330

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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 USAA920080776Floor Support · corrodedPIT - MAJOR REPAIR - S3 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 709 / FR 16, +Y254. REPLACED CABIN FLOOR SUPPORT, BS 709 / FR 16, +Y254 IAW A321 SRM 53-11-14.Mar 27, 2008 · N187US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA920080782Shear Plate · corrodedPIT - MAJOR REPAIR - S3 CHECK - LEVEL 2 CORROSION ON SHEAR PLATE, BS 3523 / FR 60 - BS 4059 / FR 70, S23L. REPLACED SHEAR PLATE, BS 3523 / FR 60 - BS 4059 / FR 70, S23L IAW A321 SRM 51-72-11.Mar 26, 2008 · N187US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA920080780Floor Support · corrodedPIT - MAJOR REPAIR - S3 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 3851 / FR 66 - BS 3950 / FR 68, +Y1162. REPLACED CABIN FLOOR SUPPORT, BS 3851 / FR 66 - BS 3950 / FR 68, +Y1162 IAW A321 SRM 51-72-11.Mar 26, 2008 · N187US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA920080778Floor Support · corrodedPIT - MAJOR REPAIR - S3 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 3950 / FR 68 - BS 4059 / FR 70, -Y1050 TO -Y1162. REPLACED CABIN FLOOR SUPPORT, BS 3950 / FR 68 - BS 4059 / FR 70, -Y1050 TO -Y1162 IAW A321 SRM 51-72-11.Mar 26, 2008 · N187US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA920080777Floor Support · corrodedPIT - MAJOR REPAIR - S3 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 3950 / FR 68 - BS 4059 / FR 70, -Y1050 TO -Y1162. REPLACED CABIN FLOOR SUPPORT, BS 3950 / FR 68 - BS 4059 / FR 70, -Y1050 TO -Y1162 IAW A321 SRM 51-72-11.Mar 26, 2008 · N187US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA920080779Floor Support · corrodedPIT - MAJOR REPAIR - S3 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 3950 / FR 68 - BS 4003 / FR 69, +Y1050. REPLACED CABIN FLOOR SUPPORT, BS 3950 / FR 68 - BS 4003 / FR 69, +Y1050 IAW A321 SRM 51-72-11.Mar 25, 2008 · N187US · Airbus A321211 · Fuselage Miscellaneous StructureSDR CA080222007Bolt · corroded(CAN) CORRODED FAIL SAFE BOLTS THAT SECURE MAIN LANDING GEAR SIDE STAY ATTACH PINS TO UPPER AND LOWER CARDAN PINS. BOLTS ARE ITEMS 290 AND 296 IN A321 IPC 32-11-18-02E. ITEM 290 IS AN AN6-56A AND ITEM 295 IS AN AN6-62. THE LOWER BOLT ITEM 295 IS HEAVILY CORRODFeb 15, 2008 · Airbus A321211 · Main Landing Gear Attach SectionSDR USAA920080280Computer · defectiveFLT 921 - PHL-MJB - BURNING SMELL - AVIONICS SMOKE ECAM MESSAGE, SMELL OF LIGHT SMOKE IN COCKPIT. CLT MAINTENANCE REMOVED AND REPLACED THE AVIONICS EQUIPMENT VENTILATION COMPUTER AND SMOKE DETECTOR. ECAM MESSAGE CLEARED AND NO FURTHER SMELL OF SMOKE IN THE CJan 27, 2008 · N174US · Airbus A321211 · Air Distribution SystemSDR USAA920080271Pin · misalignedFLT 9172 - PIT-CLT - EMERGENCY LIGHTING - AFT EMERGENCY POWER SUPPLY UNIT SHOWS EXTERIOR LIGHTS FAULT. CIDS TEST SHOWS EPSU EXTERNAL LOAD LEFT AFT. MAINTENANCE ACCOMPLISHED TSM TASK 33-51-00. REALIGNED PIN IN RIGHT AFT ESCAPE SLIDE CONNECTOR. OPERATIONAL CJan 26, 2008 · N182UW · Airbus A321211 · Equipment/Furnishings WiringSDR USAA920080187Computer · odorFLT NR 1650, COCKPIT GLARESHIELD LIGHTING PANEL HAD AND ODOR OF ELECTRICAL HEAT AFTER ADJUSTING RHEOSTATS AREA FOR GLARESHIELD LIGHTING AND PULLED CB Z234 AND Y2345. FLIGHT LANDED WITHOUT INCIDENT AND NO EMERGENCY WAS DECLARED. CLT MAINTENANCE REMOVED AND RJan 15, 2008 · N165US · Airbus A321211 · Autopilot SystemSDR USAA920071375Disk · brokenFLT 1433 - CLT - LAX - ATB - CREW REPORTED DURING CLIMB, EXPERIENCED A FUEL TRANSFER PROBLEM WITH THE LEFT TANK CAUSING A FUEL IMBALANCE CONDITION THE LEFT ENGINE WAS REDUCED TO IDLE, CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD. THE CABIN WAS NOT PREPPEDDec 22, 2007 · N174US · Airbus A321211 · Fuel StorageSDR USAA920071153Smoke Detector · defectiveFLT NR 1521 - CLT-DEN - EMERGENCY EQUIPMENT, SMOKE LAV + CRG DET FAULT DURING PREFLIGHT. MAINTENANCE REPLACED FORWARD LAV SMOKE DETECTOR. BITE CHECK SMOKE DETECTOR CONTROL UNIT. SYSTEM OPS NORMAL. MESSAGE CLEARED.Nov 15, 2007 · N161UW · Airbus A321211 · Smoke DetectionSDR USAA920071117Connector · unsecureTPA - EEL - AFT LEFT EMERGENCY EXIT POWER SUPPLY FAILED DURING SYSTEM TEST DURING WEEKLY CHECK. MAINTENANCE RESECURED MISALIGNED PIN IN ATTACH CONNECTOR AT AFT EPSU. TEST SEVERAL TIMES, SHOWED "TEST OK" MESSAGE EACH TIME.Nov 12, 2007 · N173US · Airbus A321211 · Light System WiringSDR SA07069A/C Pack · inoperativePHX FLT 700 EN ROUTE PHX TO PHL. AT APPROXIMATELY 100 MILES EAST OF ABQ, AT FL310, THE CABIN ALTITUDE HAD CLIMBED TO 13,000 FT. THE CREW REPORTED A PACK ONE FAULT WITH THE NUMBER TWO PACK ON MEL AT THE TIME. THE FLIGHT DESCENDED TO 10,000 FEET AND RETURNED Oct 20, 2007 · N181UW · Airbus A321211 · Cabin Cooling SystemSDR SA07067Epsu · faultyTPA - SEVERAL EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE RIGHT HAND, CENTER EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.Oct 19, 2007 · N162UW · Airbus A321211 · Emergency LightingSDR USAA070725Seat Track · corrodedINBOARD SEAT TRACK Y765 FRAME 47.1 & 47.2 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK PER SR 53-00-15, DEFECT SIZE: 1" X 4" X .090".Oct 18, 2007 · N186US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR SA07065Engine · stalledMCI FLT 1167 EN ROUTE CLT TO MCI. AT FL 320, THE RIGHT ENGINE HAD A COMPRESSOR STALL AND WENT TO IDLE. THE FLIGHT DESCENDED TO FL 180 AND PERFORMED AN IN-FLIGHT START OF THE ENGINE. THE ENGINE REMAINED AT MINIMUM POWER. THE FLIGHT DIVERTED TO MCI. UPON TOct 11, 2007 · N172US · Airbus A321211 · Engine (Turbine/Turboprop)SDR SA07063Epsu · dischargedTPA - THE EMERGENCY LIGHTS FAILED TEST WITH -R MID (R2) FAULT-. MAINTENANCE REPLACED THE RIGHT SIDE, MID-CABIN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.Oct 8, 2007 · N169UW · Airbus A321211 · Emergency LightingSDR USAA070716Floor Support · corrodedPAX FLOOR SUPPORT AT FR 20 40 INCHES RIGHT OF BL 0. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-72-11; CORR TASK JA-220-53500, CORR LEVEL 1, DEFECT SIZE: 2 SQ INCHES.Oct 5, 2007 · N186US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA070717Floor Support · corrodedFLOOR SUPPORT - Y1292 BETWEEN FR 64-69 HAS CORROSION. REMOVED AND REPLACED PAX FLOOR SUPPORT PER SRM 51-72-11; CORR TASK JA-260-53500; CORR LEVEL 1, DEFECT SIZE: 2.5 SQ INCH.Oct 5, 2007 · N186US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA070718Floor Support · corrodedFLOOR SUPPORT -Y1292 BETWEEN FR 64-69 HAS CORROSION. REMOVED AND REPLACED PAX FLOOR SUPPORT PER SRM 51-72-11; CORR TASK JA-260-53500; CORR LEVEL 1, DEFECT SIZE: 1 SQ INCH.Oct 5, 2007 · N186US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA070719Floor Support · corrodedFLOOR SUPPORT -Y1292 BETWEEN FR 64-69 HAS CORROSION. REMOVED AND REPLACED PAX FLOOR SUPORT PER SRM 51-72-11, DEFECT SIZE: 2 INCHES.Oct 5, 2007 · N186US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA070720Floor Support · corrodedFLOOR SUPORT Y1292 BETWEEN FRAMES C69-C65 HAS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 53-00-14; CORR TASK JA-160-53500; LEVEL 1, DEFECT SIZE: 1 X 2 INCHES AT 3 AREAS.Oct 5, 2007 · N186US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA070721Floor Support · corrodedFLOORBEAM Y1292 BETWEEN FRAMES C69-C65 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM PER SR 53-00-14, DEFECT SIZE: 1 X 2 INCHES AT 2 AREAS.Oct 5, 2007 · N186US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA070722Shear Tie · corrodedSHEAR PLATE AT SIDE BETWEEN FRAME 69-70 S-23R HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72-11, DEFECT SIZE: 2 SQ INCHES.Oct 5, 2007 · N186US · Airbus A321211 · Fuselage Internal Mounting StructureSDR USAA070723Floor Support · corrodedY254 FLOOR SUPPORT BETWEEN FRAMES 16-20 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72-11, DEFECT SIZE: 1 INCH DIA AT 3 SPOTS.Oct 5, 2007 · N186US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA070724Seat Track · corrodedFWD WET AREA FR 12-14 BL 10L HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SR 51-72-11; CORR TASK JA-220-53500; LEVEL 1. DEFECT SIZE: 3 X 24 INCHES.Oct 5, 2007 · N186US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USA2008F00000Rivet · corrodedCORRODED RIVET TAILS WERE FOUND IN THE FUSELAGE FWD CARGO COMPARTMENT BETWEEN FR 24 TO 35.8, STRINGER 39L TO 39R. APPROXIMATELY 1492 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD THE PAINT FLAKING OFF THE RSep 26, 2007 · N186US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA070713Floorbeam · corrodedTOPSIDE OF FLOORBEAM HAS CORROSION. REMOVED CORRODED FLOORBEAM & INSTALLED NEW BEAM PER SRM 51-72-11; CORR TASK JA-220-53500; DEFECT SIZE: 1 X 1 INCH.Sep 21, 2007 · N184US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA070714Floorbeam · corrodedTOPSIDE OF FLOORBEAM Y1292 HAS CORROSION. INSTALLED FILLER WITH ANGLE SPLICES ON BOTH SIDES PER SRM 53-00-14; CORR TASK JA-220-53500, DEFECT SIZE: 1.5 X 1.5 INCH.Sep 21, 2007 · N184US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA070715Angle · corrodedFR 66 JUST FWD OF RT AFT DOOR IN SILL PLATE UPPER ANGLE AT NUT CLIP HOLE CORRODED. INSTALLED ANGLE (BATHRUB) REPAIR PER SRM 53-41-14; CORR TASK JA-260-53500-14, DEFECT SIZE: 1 X 1 INCH.Sep 21, 2007 · N184US · Airbus A321211 · Fuselage Miscellaneous StructureSDR SA07061Epsu · failedPIT - THE LEFT, MID-CABIN EMERGENCY POWER SUPPLY UNIT FAILED THE OPERATIONAL CHECK. MAINTENANCE REPLACED THE LEFT, MID-CABIN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.Sep 17, 2007 · N187US · Airbus A321211 · Emergency LightingSDR SA07059Engine · overtempPHX - FLT 1540 EN ROUTE PHX TO CLT. AFTER ROTATION, CREW RECEIVED A NUMBER 2 ENGINE OVERTEMP WARNING. THE EGT WAS 972 DEGREES FOR 22 SECONDS. THE CREW SHUT DOWN THE NUMBER 2 ENGINE. THE FLIGHT RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. SINGLE ESep 16, 2007 · N165US · Airbus A321211 · Engine (Turbine/Turboprop)SDR SA07058Slide · faultyCLT - RECEIVED A RIGHT EMERGENCY EXIT SLIDE ECAM MESSAGE DOOR 2R. MAINTENANCE ACCOMPLISHED A CHECK OF THE DOOR SLIDE ARMING/DISARMING SYSTEM, AND CHECKED WIRING AND LINKAGE. NO FAULTS FOUND. REPLACED THE RIGHT SIDE, POSITION 2, EMERGENCY DOOR ESCAPE SLIDE ASep 10, 2007 · N169UW · Airbus A321211 · Escape SlideSDR USA2007F00013Skin · corrodedCORRODED RIVET TAILS WERE FOUND IN THE FUSELAGE FORWARD CARGO COMPARTMENT BETWEEN FRAME 26 TO 35.7 STRINGER 38R TO 38L. APPROXIMATELY 217 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD THE PAINT FLAKING OFFSep 6, 2007 · N184US · Airbus A321211 · Fuselage Main, Plate/SkinSDR USAA070709Beam · corrodedTHE 1162/1292 BEAM SEGMENT BETWEEN FR C66 & 68 HAS CORROSION. PART REPLACED WITH LIKE PART PER SRM 53-41-14; CORR TASK JA-260-53500, DEFECT SIZE: 1 INCH SQ (2 EA).Aug 30, 2007 · N185UW · Airbus A321211 · Fuselage Main, StructureSDR USAA070708Shear Plate · corrodedRIGHT LATERAL SHEAR PLATE BETWEEN FR 69 & 70 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART; CORR TASK JA-260-53500, DEFECT SIZE: 2" X 3".Aug 30, 2007 · N185UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA070707Skin · damagedFR 76 - 77 BETWEEN STRINGERS R36-37 HAS CREASE. CUT OUT DAMAGE & INSTALLED DOUBLER PER SRM 53-00-11 FIG 203, DEFECT SIZE: 2.5" X 1" X .125".Aug 30, 2007 · N185UW · Airbus A321211 · Fuselage Main, Plate/SkinSDR USAA070710Beam · corrodedY1292 BEAM BETWEEN FR C68 & 69 HAS CORROSION.Aug 30, 2007 · N185UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA070650Seat Track · corrodedSEAT TRACK AT FR 24 - Y1292 CORRODED. CUT OUT CORRODED PORTION & SPLICED IN NEW PER SRM 53-00-15 FIG 202; CORR TASK JA-900-0900-137, LEVEL 1, DEFECT SIZE: 2 INCH SQ.Aug 23, 2007 · N177US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USA2007F00012Skin · corrodedCORRODED RIVET TAILS WERE FOUND IN THE FUSELAGE FORWARD CARGO COMPARTMENT BETWEEN FRAME28 TO 35.5 STRINGER 38R TO 38L. APPROX 450 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD THE PAINT FLAKING OFF THE RIVAug 18, 2007 · N185UW · Airbus A321211 · Fuselage Main, Plate/SkinSDR SA07051Epsu · dischargedLAX - THE 3L DOOR EXIT SIGN APPEARED INOPERATIVE. MAINTENANCE REPLACED THE RIGHT SIDE, MID-CABIN EMERGENCY POWER SUPPLY UNIT, FIN 14WL. OPERATIONALLY CHECKS OK.Aug 13, 2007 · N183UW · Airbus A321211 · Emergency LightingSDR USAA070637Seat Track · corrodedSEAT TRACK Y1292 JUST FWD OF FR 23 HAS CORROSION. CUT OUT BAD SECTION, SPLICED IN NEW PER SRM 51-72; CORR TASK JA-900-09000, DEFECT SIZE: .25 INCH DIA X .030 INCH DEEP.Aug 10, 2007 · N177US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA070638Shear Tie · corrodedLEFT REAR SHEAR TIE BETWEEN FRAMES F69 AND F70 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72-11, DEFECT SIZE: 2 INCH SQ.Aug 10, 2007 · N177US · Airbus A321211 · Fuselage Internal Mounting StructureSDR USAA070639Floorbeam · corrodedFLOORBEAM Y495 BETWEEN FR 14-16 HAS CORROSION. REMOVED AND REPLACED PAX FLOORBEAM PER SRM 51-72-11; CORR TASK JA-220-53500, DEFECT SIZE: 3 INCH SQ ON SURFACE.Aug 10, 2007 · N177US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA070640Floorbeam · corrodedFASTENER HOLE AT FR 66 FOORBEAM (-Y1732) HAS CORROSION. REMOVED CORRODED SECTION & INSTALLED FILLER & DOUBLERS PER SRM 53-41-14; CORR TASK JA-260-53500, DEFECT SIZE: 1 X 1 INCH.Aug 10, 2007 · N177US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA070641Sill · corrodedFR 66 Y1732 (LEFT DOOR SILL) HAS CORROSION. OVERSIZED FASTENER HOLE, TRIMMED, INSTALLED FILLER & REPAIR ANGLES PER SRM 53-41-14; CORR TASK JA-26, DEFECT SIZE: .25 INCH.Aug 10, 2007 · N177US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA070642Seat Track · corrodedLEFT INBOARD SEAT TRACK FRAME 46 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PER SRM 51-72-11, DEFECT SIZE: 1 INCH DIA.Aug 10, 2007 · N177US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA070643Seat Track · corrodedY765 ABOVE FR C47.2, BEAM (SEAT TRACK) HAS CORROSION. SEAT TRACK SPLICE REPAIR 4.25 INCH SECTION PER SRM 53-00-15; CORR TASK JA-251-53500, DEFECT SIZE: 2 X 3 INCHES.Aug 10, 2007 · N177US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA070644Beam · corrodedY254 BEAM ABOVE FRS C16, C18, C21 HAS CORROSION. PART REPLACED WITH LIKE PART PER SRM 51-72-00; CORR TASK JA-220-53500, DEFECT SIZE: 3 EA, 1.5 X 1.5 INCH.Aug 10, 2007 · N177US · Airbus A321211 · Fuselage Miscellaneous Structure
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