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 USAA070645Floorbeam · corrodedFR 12 - FR 16 -Y81 (FLOORBEAM) HAS CORROSION. REMOVED AND REPLACED FLOORBEAMS PER SRM 51-72-11; CORR TASK JA-220-53500, DEFECT SIZE: 2 SQ INCHES.SDR USAA070646Floorbeam · corrodedAROUND FASTENER HOLES & TOPSIDE OF FLOORBEAM, FR 66-69 HAS CORROSION. INSTALLED NEW FLOORBEAM PER SRM 51-72-11; CORR TASK JA-260-53500, DEFECT SIZE: 1.5 X 1.5 INCH.SDR USAA070647Floorbeam · corrodedAROUND FASTENER HOLES & TOPSIDE OF FLOORBEAM, FR 66-69 HAS CORROSION. INSTALLED NEW FLOORBEAM PER SR 51-72-11; CORR TASK JA-260-53500, DEFECT SIZE: 1.5 X 1.5 INCH.SDR USAA070648Floorbeam · corrodedAROUND FASTENER HOLES & TOPSIDE OF FLOORBEAM, FR 66-69 HAS CORROSION. INSTALLED NEW FLOORBEAM PER SRM 51-72-11; CORR TASK JA-260-53500, DEFECT SIZE: 1.5 X 1.5 INCH.SDR SA07049Epsu · failedPIT - THE EMERGENCY LIGHTS TEST PRODUCED FAILURE MESSAGE -EMER POWER SUPPLY EXIT R-. MAINTENANCE REPLACED THE MID-CABIN, RIGHT SIDE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.SDR USA2007F00011Structure · corrodedCORRODED RIVET TAILS WERE FOUND IN FUSELAGE CARGO COMPARTMENT BETWEEN FRAME 26 TO 35.8 STRINGER 38R TO 38L. APPROX 1500 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD THE PAINT FLAKING OFF THE RIVET TAILS TSDR USAA070576Floorbeam · corrodedDOOR R4 SILL BEAM FWD END ABOVE FRAME 66; CORRODED TASK JA-260-53500. CUT OUT AREA, FAB'D & INSTALLED FILLER & SPLICE ANGLES PER SRM 53-41-14, DEFECT SIZE: .5 X .5 INCH.SDR USAA070577Floor Support · corrodedFLOOR SUPPORT Y254 AT CROSSBEAM C23 HAS CORROSION. INSTALLED DOUBLER IAW SRM 53-00-14; CORR TASK JA-220-53500, DEFECT SIZE: .5 INCH DIA.SDR USAA070578Floorboard · delaminatedFWD CABIN FLOOR HAS DELAMINATION. FABRICATED PER MCGILL IRM 970 REV F PER MCGILL MANUAL; CORR TASK JA-220-53500, DEFECT SIZE: 6 X 12 INCHES.SDR USAA070579Floorbeam · corrodedFLOORBEAM Y254 AT FRAME 16 HAS CORROSION. FABRICATED FILLER AND REPAIR ANGLES, INSTALLED WITH LOCK FASTENERS; CORR TASK JA-220-53500; LEVEL 1, DEFECT SIZE: 1 X 1 INCH.SDR SA07048Sense Line · crackedFLIGHT 1522, SFO-CLT: AFTER TAKEOFF, POWER ON NUMBER 1 ENGINE ROLLED BACK. NO SHUTDOWN OCCURRED. FLIGHT RETURNED TO SFO. MAINTENANCE REPLACED THE NUMBER ONE ENGINE HMU AND FUEL PUMP - NO HELP. FOUND THE NUMBER ONE ENGINE PS3 SENSE LINE DAMAGED. REPLACED SDR USAA0000000Skin · corrodedCORRODED RIVET TAILS WERE FOUND IN FUSELAGE CARGO COMPARTMENT BETWEEN FRAME 24 TO 35.6 STRINGER 38R TO 38L. APPROXIMATELY 1350 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD THE PAINT FLAKING OFF THE RIVET SDR USAA070520Floor Support · corrodedTOPSIDE OF FLOOR SUPPORT Y1732 AT NUT PLATE HOLE HAS CORROSION. ACCOMPLISHED BATH TUB REPAIR PER SRM 53-41-14; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1 X 1 INCH.SDR USAA070521Beam · corrodedFWD END OF RIGHT (R4) SILL BEAM ABOVE FR C66. DAMAGED AREA CUTOUT AND REPAIRED PER SRM REPAIR, SRM 53-41-14; CORR TASK JA-260-53500, LEVEL 1, DEFECT SIZE: 1 X 1.25 INCH.SDR SA07045Light · inoperativeTPA - THE EMERGENCY BATTERY TEST LIGHTS WAS FOUND INOPERATIVE AT THE CIDS PANEL.SDR USA2007F00009Structure · corrodedCORRODED RIVET TAILS WERE FOUND IN FUSELAGE CARGO COMPARTMENT BETWEEN FRAME 24 TO 35.7 STRINGER 38L TO 38R. APPROXIMATELY 1070 RIVETS WERE REPLACED. 25 RIVETS WERE REPLACED AT S38 OB. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS SDR SA07043Unknown · odorPHX FLT 732 EN-ROUTE, LAX TO CLT. AFTER TAKEOFF, A STRONG ODOR WAS NOTICED IN THE AFT CABIN. THE FLIGHT CREW ELECTED TO DIVERT TO PHX FOR MAINTENANCE. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING.SDR USAA070471Sill · corrodedR4 DOOR SILL AT FRAME C66 HAS CORROSION. INSTALLED DOUBLER REPAIR IAW TYP REP 53-41-01, DEFECT SIZE: 1 INCH.SDR USAA070472Floorbeam · corrodedFLOORBEAM -Y254 AT FRAME 20 HAS CORROSION. INSTALLED NESTED ANGLE REPAIR & FILLER PER SRM 53-00-14, DEFECT SIZE: .75 INCH.SDR USAA070469Profile · crackedFR 48 STR 38 LEFT, FLOOR CORNER PROFILE HAS CRACK. INSTALLED DOUBLER PER EA 84652, DEFECT SIZE: 2 INCHES.SDR USA2007F00010Structure · corrodedCORRODED RIVET TAILS WERE FOUND IN FUSELAGE CARGO COMPARTMENT BETWEEN FRAME 25 TO 35.6 STRINGER 31L TO 31R. APPROXIMATELY A TOTAL OF 600 RIVETS WERE REPLACED. 7 RIVETS WERE REPLACED AT S31L AND 3 S32L FOR A TOTAL OF 22 RIVETS THAT WERE REPLACED ABOVE STRINGESDR USA2007F00008Structure · corrodedCORRODED RIVET TAILS WERE FOUND IN FUSELAGE CARGO COMPARTMENT BETWEEN FRAME 24 TO 35.7 STRINGER 38L TO 39R OB (UPPER). APPROXIMATELY A TOTAL OF 2,500 RIVETS WERE REPLACED. APPROXIMATELY 700 WERE REPLACED ON OB (UPPER) SIDE OF STRINGER 38. A RESIDUE OF SODIUSDR USAA070462Frame · corrodedFRAME 66 HAS CORROSION. INSTALLED BATH TUB FITTING PER TR 53-41-01, DEFECT SIZE: 1" X 1" X .067".SDR USAA070463Floorbeam · corrodedFR 66 BATH TUB AREA HAS CORROSION. INSTALLED BATH TUB FITTING PER SRM 53-41-14, DEFECT SIZE: 1" X 1" X .056".SDR SA07032Epsu · faultedTPA - THE MID-CABIN EMERGENCY LIGHT POWER SUPPLY UNIT FAULTED DURING THE EMERGENCY LIGHTS OPERATIONAL CHECK. MAINTENANCE REPLACED THE MID-CABIN EMERGENCY POWER SUPPLY UNIT. OK FOR SERVICE.SDR USAA070414Floorbeam · corrodedEXFOLIATION AT FR 16 ON TOP OF FLOORBEAM Y254. FLOORBEAM REMOVED & REPLACED PER SRM 51-72-11; CORR TASK JA-220-53500; LEVEL 1, DEFECT SIZE: 1 X 2 INCHES.SDR USAA070415Shear Plate · corrodedLEFT SHEAR TIE PLATE FRAMES 69 - 70 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL. CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 5 X 17 INCHES.SDR USAA200705U12Beam · corrodedA 1.125 X 2 INCH CORROSION FOUND AT RIGHT AFT SILL BEAM. REPAIRED PER SRM 53-41-14. CORROSION TASK JA-260-53500, CORR LEVEL 1.SDR USAA070389Seat Track · corrodedFRAME 23, RIGHT OUTBOARD SEAT TRACK -Y760 HAS CORROSION. SPLICED IN NEW SECTION IAW SRM 53-00-15 FIG 201, DEFECT SIZE: 1 INCH DIA.SDR USA2007F00000Structure · corrodedCORRODED RIVET TAILS WERE FOUND IN FUSELAGE CARGO COMPARTMENT BETWEEN FRAME 35.1 TO 35.7, STRINGER 39L TO 39R. APPROXIMATELY 1,000 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD THE PAINT FLAKING OFF THE RISDR SA07029Valve · malfunctionedLGA FLT 938, EN ROUTE CLT TO LGA. AFTER TAKEOFF, A -HOT AIR- ODOR WAS NOTICED IN BOTH THE CABIN AND COCKPIT. THE APU WAS OFF AT THE TIME. WHEN THE LEFT AIR PACK WAS TURNED OFF, THE ODOR BECAME WORSE. THE PACKS WERE RECONFIGURED AND THE FLIGHT CONTINUED TOSDR USAA070388Floorbeam · corrodedFLOORBEAM Y254 HAS CORROSION. REMOVED & REPLACED BEAM PER SRM 51-72-11; CORR TASK JA-220-53500, LEVEL 1, DEFECT SIZE: 2.5 X 3.5 INCHES.SDR USA2007F00007Skin · corrodedCORRODED RIVET TAILS ON FUSELAGE FORWARD CARGO COMPARTMENT BETWEEN FRM 28-35, STRINGER 38L. APPROXIMATELY 900 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD PAINT FLAKING OFF THE RIVET TAILS THAT WERE CLEANSDR USA2007F00006Skin · corrodedCORRODED RIVET TAILS WERE FOUND IN FUSELAGE FWD CARGO COMPARTMENT BETWEEN FRM 24-35, STRINGER 38L AND 38R. APPROXIMATELY 50 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD PAINT FLAKING OFF THE RIVET TAILS TSDR USAA070338Sill · corrodedLT AFT DOOR SILL AT FWD END FR 66. REPAIRED PER EA 84449 & SRM 53-41-14 PRIN NR 6. DEFECT SIZE: 5/8" DIA.SDR USA2007F00005Skin · corrodedCORRODED RIVET TAILS WERE FOUND IN FUSELAGE FORWARD CARGO COMPARTMENT BETWEEN FRM 26-35, STRINGER 40L AND 42R. APPROXIMATELY 500 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD PAIN FLAKING OFF THE RIVET TAISDR USAA070325Floorbeam · corrodedFOUND CORROSION FLOORBEAM -Y254 BETWEEN FR 19 AND 20. REMOVED CORROSION AND INSTALLED FILLER AND DOUBLER PER SRM 53-00-14, FIG 204, CORROSION TASK JA-220-53500, DEFECT SIZE: 1" BY 1".SDR USAA070326Floorbeam · corrodedFOUND CORROSION AROUND SCREW HOLE, FRAME 66, Y-1292. CUT OUT DAMAGE, INSTALLED FILLER AND REPAIR ANGLES PER SRM 53-41-14, PRINCIPLE 6; CORROSION TASK JA-260-535, DEFECT SIZE: 1".SDR USAA070309Floor Support · corrodedFLOOR SUPPORT -Y1292 AT FRAME 69 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-42-00, 51-44-11; CORR TASK JA-260-53500, DEFECT SIZE: 1 INCH.SDR USAA070308Floor Support · corrodedFLOOR SUPPORT -Y1292 AT FRAME 67 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-42-00, 51-44-11, CORR TASK JA-260-53500, DEFECT SIZE: 1 INCH.SDR USAA070307Floorbeam · corrodedAROUND SCREW HOLE, FRAME 66, Y-1292 HAS CORROSION. CUT OUT DAMAGE, INSTALLED FILLER & REPAIR ANGLES PER SRM 53-41-14,; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1 INCH.SDR SA07028Hmu · leakingDTW FLT 902 EN ROUTE CLT TO DTW, DURING DESCENT, BELOW FL 290, ENGINE 1 BEGAN TO RUMBLE AND VIBRATE. THE AUTOTHROTTLE WAS DISCONNECTED AND THE NUMBER 1 ENGINE WAS BROUGHT BACK IDLE AND THE VIBRATIONS STOPPED. AT 7,000 FEET AND 210 KNOTS, THE AUTOTHROTTLES WESDR USAA070283Floorbeam · corrodedFOUND CORROSION FWD OF L4 DOOR SILL AT FRAME 66. CUT OUT DAMAGED AREA AND FABRICATED FILLER PER SRM 53-41-14; CORROSION TASK JA-260-53500; LEVEL 1 DEFECT SIZE: 1/2" DIA.SDR USAA070282Frame · corrodedFOUND CORROSION FR 66 - Y1732. INSTALLED DOUBLER PER SRM 53-41-14; CORROSION TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1/2 SQ IN.SDR USAA070270Seat Track · corrodedCORROSION AT 3 PLACES AT LEFT I/B SEAT TRACK FROM FRAME 47-47.2. CUT OFF DAMAGED SECTION, SPLICED IN NEW SECTION PER SRM 53-41-15 FIG 202; CORROSION TASK JA-220-25502, DEFECT SIZE: 1 INCH.SDR SA07025Engine · malfunctionedTPA FLT 1945 EN ROUTE CLT TO RSW. OVER THE VICINITY OF GNV, THE NUMBER ONE ENGINE N1 SPEED DROPPED TO 50 PERCENT. A PASSENGER REPORTED TO HAVE SEEN FIRE AND SMOKE COME FROM THE NUMBER ONE ENGINE. THE FLIGHT DIVERTED TO TPA, AND DURING DESCENT, REGAINED POWESDR USAA070269Floorbeam · corrodedFLOORBEAM AT Y476.4 FR 16 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM PER SRM 51-72-11; CORR LEVEL 1; TASK JA-220-53500, DEFECT SIZE: 2 SQ INCHES.SDR USAA070261Floorbeam · corrodedAROUND SCREW HOLE, FRAME 66, RIGHT SIDE Y -1292 HAS CORROSION. CUT OUT DAMAGE, INSTALLED REPAIR ANGLES & FILLER PER SRM 53-41-14; CORR TASK JA-260-53500, LEVEL 1, DEFECT SIZE: .75 INCH DIA.SDR USA2007F00004Skin · corrodedCORODED RIVET TAILS WERE FOUND IN FUSELAGE FORWARD CARGO COMARTMENT BETWEEN FRM 32-35.5, STRINGER 44L AND 42R. APPROXIMATELY 500 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD PAINT FLAKING OFF THE RIVET TASDR USAA070256Shear Web · crackedSHEAR WEB TRAY FR 68 & 69 ATTACHING TO Y -1162 HAS CRACK. FABRICATED TRAY & INSTALLED PER SRM 51-31-00 & 51-72-11, DEFECT SIZE: 2 INCHES.
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