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 USAA070257Sill · corrodedFR 66 SILL BEAM UPPER SURFACE HAS CORROSION. INSTALLED TWO BATH TUB FITTINGS PER SRM 53-41-14, DEFECT SIZE: 2"W X .075"D.Apr 3, 2007 · N174US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USA2007F00003Skin · corrodedCORRODED RIVET TAILS ON FUSELAGE FORWARD CARGO COMARTMENT BETWEEN FRM 24-35 STRINGER 38L AND 38R. APPROXIMATELY 500 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD PAINT FLAKING OFF THE RIVET TAILS THAT WEREMar 27, 2007 · N173US · Airbus A321211 · Fuselage Main, Plate/SkinSDR USAA070250Fitting · corrodedFR 66 AT Y1732 HAS CORROSION. INSTALLED FILLER/DOUBLER PER SRM 53-41-14; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1 SQ INCH.Mar 27, 2007 · N173US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USA2007F00002Skin · corrodedCORRODED RIVET TAILS ON FUSELAGE FORWARD CARGO COMPARTMENT BETWEEN FRAME 24 TO 35, STRINGER 38L AND 38R. APPROXIMATELY 100 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD PAINT FLAKING OFF THE RIVET TAILS THMar 26, 2007 · N172US · Airbus A321211 · Fuselage Main, Plate/SkinSDR USAA070231Floorbeam · corrodedRIGHT FLOORBEAM TOP FLANGE FROM FR 64-69, -Y1160-Y1292 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM PER SRM 51-72-11; CORR TASK JA-260-53500, LEVEL 1, DEFECT SIZE: 1.5 SQ INCH.Mar 23, 2007 · N163US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA070232Floorbeam · corrodedRIGHT FLOORBEAM TOP FLANGE FROM FR 64-FR 69, -Y1160 TO -Y1192 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM PER SRM 51-72-11; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1.5 SQ INCH.Mar 23, 2007 · N163US · Airbus A321211 · Fuselage Main, Floor BeamSDR SA07024Seal · leakingABQ FLT 1596 EN ROUTE. WHILE IN CRUISE FLIGHT, THE NR 1 ENGINE BEGAN TO LOOSE OIL PRESSURE. THE CREW SHUTDOWN THE NR 1 ENGINE AND THE FLIGHT DIVERTED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. THERE WAS 20 MINUTES OF SINGLE ENGINE TIME. MAINTENANCE REPMar 21, 2007 · N189UW · Airbus A321211 · Turbine Engine Oil SystemSDR USAA070229Floorbeam · corrodedY1732 FR 66 - FR 65, CORROSION AROUND SCREW HOLE CORRODED. CUT OUT DAMAGE & INSTALLED REPAIR ANGLES & FILLER PER SRM 53-41-14; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1 INCH DIA.Mar 20, 2007 · N172US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA070230Floorbeam · corrodedY-1732 BETWEEN FR 65 & 66 CORRODED. CUT OUT DAMAGE, INSTALLED REPAIR ANGLES & FILLER PER SRM 53-41-14; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1 INCH DIA.Mar 20, 2007 · N172US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA070179Sill · corrodedAFT RIGHT DOOR SILL AT FR 66 HAS CORROSION. REMOVED CORROSION, INSTALLED REPAIR ANGLES PER SRM 53-41-14; CORR LEVEL 1; TSK JA-260-53500, DEFECT SIZE: .5 X .5 INCH.Mar 13, 2007 · N171US · Airbus A321211 · Fuselage Miscellaneous StructureSDR SA07022Girt Bar · out of adjustPHL - THE CABIN CREW STATED THAT THE EMERGENCY ESCAPE SLIDE ARMING LEVER AT DOOR 4L KEEPS POPPING OUT. MAINTENANCE ADJUSTED THE GIRT BAR FITTING. OK FOR SERVICE.Mar 12, 2007 · N163US · Airbus A321211 · Escape SlideSDR USAA070174Floorbeam · corrodedRIGHT FLOORBEAM TO FLANGE FROM FR 64-68; -Y1160 TO -Y1292 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM PER SRM 51-72-11; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1 SQ INCH.Mar 9, 2007 · N163US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA070170Floorbeam · corrodedRIGHT FLOORBEAM -Y1732 AT FR 66 AT NUT PLATE HOLE HAS CORROSION. INSTALLED NEW REPAIR ANGLES & FILLER PER SRM 53-41-14; CORR TASK JA-260-53500, LEVEL 1, DEFECT SIZE: 0.750 X 0.750 INCH.Mar 9, 2007 · N167US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA070171Floorbeam · corrodedSEVERAL AREAS, FLOORBEAM AT Y254 BETWEEN FR C14 & C23 HAS CORROSION. REMOVED & REPLACED BEAM PER SRM 51-72-11; CORR TASK JA-220-53500, DEFECT SIZE: 1 X 1 INCH.Mar 9, 2007 · N167US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA070172Floorbeam · corrodedFLOORBEAM AT Y505 HAS CORROSION. REMOVED & REPLACED BEAM PER SRM 51-72-11; CORR TASK JA-220-53500; LEVEL 1, DEFECT SIZE: 1 X 8 INCHES.Mar 9, 2007 · N167US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA070173Shear Tie · corrodedLEFT SHEAR TIE FR 70, Y1292 HAS CORROSION. REMOVED AND REPLACED SHEAR TIE PER SRM 51-72-11, CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 2 SQ INCHES.Mar 9, 2007 · N167US · Airbus A321211 · Fuselage Internal Mounting StructureSDR USAA070175Floor Support · corrodedLEFT FLOOR SUPPORT Y1292 FR 67-68 HAS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-72-11; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 3 SQ INCHES.Mar 9, 2007 · N167US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA070176Seat Track · corrodedRIGHT O/B SEAT TRACK 2 INCHES FWD OF FR 23 2 GALLEY MOUNT HAS CORROSION. REMOVED & REPLACED PER SRM 53-11-15, DEFECT SIZE: 6 X 4 INCHES.Mar 9, 2007 · N167US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA070177Floor Panel · delaminatedSEPARATION OF COMPOSITE, AFT EDGE OF COCKPIT FLOOR PANEL 211FF. FABRICATED NEW BOARD PER MCGILL IRM 979 REV F, DEFECT SIZE: 1 X 3 INCHES.Mar 9, 2007 · N167US · Airbus A321211 · Fuselage Floor PanelSDR USA2007F00001Skin · corrodedCORRODED RIVET TAILS WERE FOUND IN FUSELAGE FORWARD CARGO COMPARTMENT BETWEEN FRAME 35 TO AFT PRESSURE BULKHEAD FROM S38L TO 38R. APPROXIMATELY 100 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD THE PAINT FFeb 28, 2007 · N167US · Airbus A321211 · Fuselage Main, Plate/SkinSDR USAA070167Floor Panel · damagedPANEL 251 AG FRAME 47-47.5 DAMAGED. MANUFACTURED NEW PANEL PER MCGILL IRM 9701 REV F, DEFECT SIZE: 2 X 1 INCH.Feb 28, 2007 · N163US · Airbus A321211 · Fuselage Floor PanelSDR USAA070166Floor Panel · crackedFLOOR PANEL 262 HG CRACKED. MANUFACTURED REPLACEMENT PART PER MCGILL IRM 9701, REV F, DEFECT SIZE: 6 INCHES.Feb 27, 2007 · N167US · Airbus A321211 · Fuselage Floor PanelSDR SA07015Hmu · failedCLT FLT 1408 EN-ROUTE SFO - CLT. DURING DESCENT, AT APPROXIMATELY FL 290, A RUMBLING SOUND DEVELOPED WITH A COINCIDING RISE IN EGT TO THE REDLINE LIMIT OF THE NUMBER 1 ENGINE. PASSENGERS REPORTED SEEING FLAMES COMING OUT OF THE NUMBER ONE ENGINE TO THE CABFeb 26, 2007 · N181UW · Airbus A321211 · Fuel Control/Reciprocating EnginesSDR SA07014Battery Pack · faultyTPA - A BATTERY FAULT LIGHT CAME ON FOR THE EMERGENCY LIGHTS SYSTEM. MAINTENANCE REPLACED THE BATTERY PACK IN THE FORWARD LEFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.Feb 26, 2007 · N191UW · Airbus A321211 · Emergency LightingSDR USAA070112Floorbeam · corrodedLEFT FLOORBEAM ON TOP FLANGE FROM FR 65-69 AT Y1160 - 1292 HAS CORROSION. REMOVED AND REPLACED 3 FLOORBEAMS PER DWG D53472815, SRM 51-74-12; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 8 INCHES SQ.Feb 22, 2007 · N163US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA070113Floorbeam · corrodedFLOORBEAM AT Y765 AT LAV D AFT MOUNT NEAR FRAME 66 HAS CORROSION. REMOVED & REPLACED WITH IDENTICAL PART PER SRM 53-00-14 FIG 102, DEFECT SIZE: 2 SQ INCHES.Feb 22, 2007 · N163US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA070114Floorbeam · corrodedRIGHT FLOORBEAM TOP FLANGE FROM FR 64-69, -Y1160-1292 HAS CORROSION. REMOVED AND REPLACED 3 FLOORBEAMS PER SRM 51-72-11; CORR TASK JA-260-53500, LEVEL 1, DEFECT SIZE: 4 SQ INCHES.Feb 22, 2007 · N163US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA070115Floorbeam · corrodedY254 AT FRAME 16 HAS CORROSION. REMOVED AND REPLACED BEAM PER SRM 53-00-14; CORR TASK JA-220-53500; LEVEL 1, DEFECT SIZE: 5 X 5 INCHES.Feb 22, 2007 · N163US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA070116Floorbeam · corrodedFLOORBEAM Y-254 FR 17-19 HAS CORROSION. REMOVED AND REPLACED BEAM PER SRM 53-00-14; CORR TASK JA-220-53500; LEVEL 1, DEFECT SIZE: .5 X 4 INCHES.Feb 22, 2007 · N163US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA07099Floorbeam · corrodedTWO AREAS, 13 INCHES LEFT OF CENTER FLOORBEAM C16 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-14-14; CORR LEVEL 1; CORR TASK: JA-220-25503, DEFECT SIZE: 1 X 1 INCH.Feb 14, 2007 · N169UW · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA070100Floorbeam · corrodedFLOORBEAM -Y1292 BETWEEN FRAMES 66 & 68, SEVERAL SPOTS CORRODED. DEFECTIVE PART REPLACED WITH IDENTICAL PART; CORR LEVEL 1; TASK JA-260-53500, DEFECT SIZE: .5 X .5 INCH.Feb 14, 2007 · N169UW · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA070101Floor Support · corrodedAFT END OF FLOOR SUPPORT AT C16 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72-11; CORR TASK JA-220-25503; LEVEL 1, DEFECT SIZE: 1 X 1 INCH.Feb 14, 2007 · N169UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA070102Floorbeam · corrodedTOP OF BEAM, FWD END OF SEAT TRACK I/B LEFT BEAM HAS CORROSION. REMOVED & REPLACED BEAM PER SRM 51-72-11; CORR LEVEL 1; TASK JA-220-25503, DEFECT SIZE: .5 INCH.Feb 14, 2007 · N169UW · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA070103Shear Tie · corrodedFROM 69 TO 70 AT Y1162.5 HAS CORROSION. REPLACED SHEAR TIE WITH IDENT PART PER SRM 51-72-11; CORR LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 4 SQ INCHES.Feb 14, 2007 · N169UW · Airbus A321211 · Fuselage Internal Mounting StructureSDR USAA070104Track · corrodedAT 21 INCHES LEFT OF CENTER FROM COCKPIT DOOR TO FLOORBEAM C16, FR 12-16 HAS CORROSION. REMOVED & REPLACED PER AIRBUS SRM 51-72-11; CORR TASK JA-220-25503; LEVEL 1, DEFECT SIZE: 1 X 21 INCHES.Feb 14, 2007 · N169UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA070096Floorbeam · corrodedFOUND FLOORBEAM CORRODED, -Y1732 BNTH TAB FITTING AFT RT DOOR. MODIFIED PART INSTALLED PER SRM 53-41-14; CORROSION LEVEL 1; TASK NR JA-260-53500 DEFECT SIZE: 1" BY 1".Feb 13, 2007 · N169UW · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA070097Fitting · corrodedFOUND Y1732 LT BATH TUB FITTING AFT LT DOOR. REMOVED AND REPLACED MODIFIED PART INSTALLED PER SRM 53-41-14; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 1" BY 1".Feb 13, 2007 · N169UW · Airbus A321211 · Fuselage Main, Attach FittingsSDR USAA070098Floorbeam · corrodedFOUND 2 AREAS, TOP SIDE OF FLOORBEAM Y1292 FR 64-49. INSTALLED NEW BEAMS PER SRM 51-42-11; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 1.5" BY 1.5".Feb 13, 2007 · N169UW · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA070092Shear Tie · corrodedFR 69 - 70 AT Y1162.5 HAS CORROSION. REPLACED SHEAR TIE PER SRM 51-72-11; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 3 SQ INCHES.Feb 9, 2007 · N169UW · Airbus A321211 · Fuselage Internal Mounting StructureSDR USAA070093Shear Tie · corrodedFR 69 - 70 AT Y1162.5 HAS CORROSION. REPLACED SHEAR TIE PER SRM 51-72-11; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 4 SQ INCHES.Feb 9, 2007 · N169UW · Airbus A321211 · Fuselage Internal Mounting StructureSDR USAA070041Beam · corrodedDOOR SEAL BEAM Y1290 & 5 INCHES FWD OF FR 68 CORRODED. CUT OUT DAMAGED AREA, INSTALLED FILLER & DOUBLER PER SRM 53-41-14; CORR TASK JA-260-53500, LEVEL 1, DEFECT SIZE: .5 X .625 INCH.Jan 17, 2007 · N168US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA070034Galley Track · corrodedFWD GALLEY SEAT TRACK Y-1292 FR 23 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK PER SRM 51-42-11; CORR TASK JA-220-53500; CORR LEVEL 2, DEFECT SIZE: 6 X 2 INCHES.Jan 11, 2007 · N165US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA070029Seat Track · corrodedY765 FR 23 SEAT TRACK FWD GALLEY HAS CORROSION. REMOVED AND REPLACED SEAT TRACK PER SRM 51-42-11; CORR TASK JA-220-53500; CORR LEVEL 2, DEFECT SIZE: 4 X 2 INCHES.Jan 11, 2007 · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA070035Threshold · corrodedLEFT AFT PAX DOOR THRESHOLD FRAME 67 HAS CORROSION. INSTALLED DOUBLER REPAIR AND FILLER PER SRM 53-41-14; CORR TASK JA-260-25500; LEVEL 1, DEFECT SIZE: .75 INCH DIA.Jan 11, 2007 · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA070036Threshold · corrodedRIGHT AFT PAX DOOR THRESHOLD FWD CORNER HAS CORROSION. CORRODED AREA WAS CUT OUT & REPAIRED PER SRM 53-41-14, FIG 201; CORR TASK JA-260-25500; LEVEL 1.Jan 11, 2007 · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA070037Strut · corrodedNOSE LANDING GEAR UPPER STRUT TORQUE LINK LUGS HAS CORROSION. INSTALLED OVERSIZED BUSHINGS, REAMED HOLES & REMOVED CORROSION PER TYP REPAIR 32-20-01, DEFECT SIZE: .125 INCH.Jan 11, 2007 · Airbus A321211 · Main Landing Gear Strut/Axle/TruckSDR USAA070038Floorbeam · corrodedTOPSIDE OF FLOORBEAM Y1732 AT FR 66 HAS CORROSION. ACCOMPLISHED REPAIR PER SRM 53-41-14; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 2 X 2 INCHES.Jan 11, 2007 · N168US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAASA07003Slide · faultyPHL - AFTER AN ACCIDENTAL SLIDE DEPLOYMENT OF THE L3 DOOR, THE SLIDE DID NOT RELEASE WHEN THE DITCH HANDLE WAS PULLED AND THE DOOR ASSIST BOTTLE DID NOT DISCHARGE DURING DOOR OPENING. MAINTENANCE REPLACED THE SLIDE AND THE DOOR ASSIST BOTTLE. OK FOR SERVICE.Dec 31, 2006 · N169UW · Airbus A321211 · Escape SlideSDR USAA061455Floorbeam · corrodedCORROSION THRU HOLE, FLOORBEAM AT Y-254 & FRAME C16. REMOVED & REPLACED FLOORBEAM PER SRM 51-72-11; CORR TASK JA-220-53500; LEVEL 1, DEFECT SIZE: .5 INCH.Dec 29, 2006 · N166US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA061456Seat Track · corrodedRIGHT O/B SEAT TRACK TOP SURFACE 5 INCHES FWD OF FRAME C24 HAS CORROSION. REMOVED SEAT TRACK AND REPLACED WITH NEW PER SRM 53-11-01; CORR TASK JA-220-53500; LEVEL 1 DEFECT SIZE: 1 INCH DIA.Dec 29, 2006 · N166US · Airbus A321211 · Fuselage, Seat/Cargo Attach Fittings
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