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 USAA051526Floorbeam · corrodedFOUND FLOORBEAM CORRODED, -Y1160 BETWEEN FS 69-FS 70 FLOORBEAM. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72-11; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 2" X 10".SDR USAA051527Floorbeam · corrodedFOUND FLOORBEAM CORRODED, -Y1292 FS 66. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72-11; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 4" X 30".SDR USAA051528Floor Support · corrodedFOUND FLOORBEAM CORRODED, -Y1160 FS 66-67. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72-11; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 1" X 18".SDR USAA051529Seat Track · corrodedFOUND INBOARD SEAT TRACK CORRODED, FS 47 AFT. REMOVED AND REPLACED SECTION OF SEAT TRACK PER SRM 53-41-14; CORROSION LEVEL 2; TASK JA-220-25502, DEFECT SIZE: 1/2" X 1/4" AT THREE PLACES.SDR SA05123Bottle · lowPHL - PILOT REPORTED THE LEFT OVERWING EXIT SLIDE BOTTLE PRESSURE LOW. MAINTENANCE REMOVED AND REPLACED THE SLIDE BOTTLE. CHECKS OK PER TASK 25-62-49-020.SDR SA05122Battery Pack · dischargedTHE LT FORWARD EMERGENCY LIGHT BATTERY PACK FAILED TEST. MAINTENANCE REPLACED THE LT FORWARD BATTERY PACK. OPERATIONALLY CHECKS OK.SDR USAA051450Floorbeam · corrodedFOUND FLOORBEAM CORRODED, Y-1732 FROM 65-66. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11, DEFECT SIZE: 3" X 20".SDR USAA051449Floorbeam · corrodedLOCATION: BEAM Y1160 FRAME 67-68 ACTION: DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-43-00, 53-41-04; TASK JA-260-53500 DEFECT SIZE: 3" X 16"SDR USAA051448Shear Tie · corrodedFOUND SHEAR TIE CORRODED Y-1932 BETWEEN FRAME 69-70. DEFECRIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11; CORR TASK, JA-260-53500 DEFECT SIZE: 2" X 10".SDR USAA051447Floorbeam · corrodedLOCATION: BEAM Y1160 FR 68 ACTION: DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-43-00, 53-41-04; CORR TASK 260-53500-002 DEFECT SIZE: 3" X 20"SDR USAA051427Floorbeam · corrodedPAX FLOORBEAM AT Y765, FR 16, LT, REMOVED AND REPLACED FLOORBEAM; DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM 51-72-11; CORR. LEVEL 1, DEFECT SIZE: 1 SQ. IN.SDR USAA051428Floorbeam · corrodedPAX FLOORBEAM AT Y503, FR 14-16, REMOVED AND REPLACED FLOORBEAM IAW SRM 51-72-11; CORR. LEVEL 1; TASK JA-220-53500 DEFECT SIZE: 2 SQ. IN.SDR USAA051429Floorbeam · corrodedFLOORBEAM Y254 AT FR 21, DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM 51-72-11, DEFECT SIZE: 1 INCH DIA.SDR USAA051430Floorbeam · corrodedY765 BETWEEN FR 67-68 ON PAX COMPARTMENT FLOORBEAM REMOVED AND REPLACED FLOORBEAM IAW SRM 51-72-11; CORR. LEVEL 1; TASK JA-260-53500 DEFECT SIZE: 2 SQ. IN.SDR USAA051431Sill · corrodedBETWEEN FR 67-68 Y1160, REPLACED SILL IAW SRM 51-72-11 DWG. 53480505; LEVEL 1; TASK JA-260-53500 DEFECT SIZE: .5 INCH X .5 INCH.SDR USAA051432Sill · corrodedAFT SERVICE DOOR, DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM 51-22-11; LEVEL 1; TASK JA-260-53500 DEFECT SIZE: 4 INCHES X 24 INCHES.SDR USAA051416Floorbeam · corrodedBEAM Y254 FWD CABIN, DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-72-11; CORROSION LEVEL 2; TASK JA-220-53500. DEFECT SIZE: .5 INCH X .5 INCH.SDR USAA051417Sill · corrodedRIGHT AFT DOOR SILL FR 66; CORROSION LEVEL 2; TASK JA-260-53500. SPLICE ANGLE REPAIR IAW SRM 53-41-14. DEFECT SIZE: 10 INCHES X .846 INCH.SDR USAA051418Beam · corrodedBEAM - Y1292 FROM FRAME 66 THRU FRAME 68; CORROSION LEVEL 1; TASK JA-260-53500. REMOVED AND REPLACED IAW SRM 51-72-11. DEFECT SIZE: 2 INCHES X 6 INCHES.SDR USAA051419Beam · corrodedBEAM Y1292 FROM FRAME 66-68; CORROSION LEVEL 1; TASK JA-260-53500. REMOVED AND REPLACED IAW SRM 51-72-11. DEFECT SIZE: 2 INCHES X 4 INCHES.SDR USAA051420Beam · corrodedBEAM - Y1292 AT FRAME 16; CORROSION LEVEL 1; TASK JA-220-53500. REMOVED AND REPLACED IAW SRM 51-72-11. DEFECT SIZE: 2 INCHES X 1 INCH.SDR USAA051421Floorboard · crackedAT 41 INCHES FROM END, 64 INCHES FROM OPP END, 4 INCHES FROM EDGE, 15 INCHES FROM OPP EDGE CRACKED. FILLED AND INSTALLED PRECURED DOUBLER IAW SRM 53-02-00 FIG 203. DEFECT SIZE: 5 INCHES.SDR SA05118Battery · dischargedTPA - THE MID CABIN, RIGHT SIDE EMERGENCY POWER SUPPLY UNIT FAILED THE OPERATIONAL TEST. MAINTENANCE REPLACED THE BATTERY IN THE MID CABIN, RIGHT SIDE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.SDR SA05110Epsu · faultyDCA - THE EMERGENCY POWER SUPPLY UNIT AT THE MID LEFT POSITION FAILED THE SYSTEM TEST. MAINTENANCE REPLACED THE MID LEFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY TESTED OK.SDR SA05109Bottle · faultyBOS - A SLIDE BOTTLE PRESSURE CAUTION LIGHT CAME ON THE CABIN INTERCOMMUNICATION DATA SYSTEM PANEL DURING DOOR CLOSURE. MAINTENANCE RELEASED THE AIRCRAFT ON MEL. REPLACED THE L3 DOOR SLIDE BOTTLE. OK FOR SERVICE.SDR SA05105Battery · faultyTPA - THE L2 DOOR SLIDE EMERGENCY ESCAPE LIGHTS INDICATE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IN EMERGENCY POWER SUPPLY UNIT 15WL.SDR SA05102Disc · puncturedLGA - MAINTENANCE REPORTED THE CIDS PANEL INDICATES MID LEFT ENTRY DOOR ASSIST BOTTLE PRESSURE LOW. LGA MAINTENANCE SERVICED THE MID LEFT DOOR ASSIST BOTTLE PER MM. LEAK CHECK GOOD. ALSO, ACTION FROM A MAINTENANCE TECH SERVICE ITEM REVEALED A PUNCTURED BLOWSDR SA05101Bottle · lowTPA PILOT REPORTED THE CIDS PANEL CAUTION LIGHTS KEEP ILLUMINATING DURING FLIGHT. LIGHTS WILL RESET IN FLIGHT BUT ONCE ON GROUND THE CAUTION LIGHTS ILLUMINATE AGAIN. MAINTENANCE SERVICED THE LEFT MID DOOR ASSIST BOTTLE TO CORRECT PRESSURE.SDR SA05099Bottle · reads lowPIT - THE SLIDE BOTTLE PRESSURE AT DOOR R3 WAS LOW. MAINTENANCE REPLACED THE SLIDE BOTTLE AT DOOR R3. OK FOR SERVICE.SDR SA05097Battery · dischargedTHE EMERGENCY LIGHTS TEST FAILED IN THE MID LT POSITION OF THE CABIN. MAINTENANCE REPLACED THE 15WL BATTERY. SYSTEM TESTS OK.SDR SA05096Epsu · failedCLT - DURING TEST, RECEIVED FAULT MESSAGE, EPSU INT LOAD FWD L. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT AT THE FORWARD LOCATION. OPERATIONALLY CHECKS OK.SDR GTIA050223Proximity Switch · out of adjustR1 DOOR NOT SHOWING CLOSED INFLIGHT ON ECAM. RECYCLED EMERGENCY LIGHT TEST SWITCH ON FAP AND DOOR LIGHTS WORKED NORMALLY. PERFORMED ADJUSTMENT OF R1 DOOR PROX SWITCH PER AMM. SYSTEM OPS CHECK GOOD, LP NR 179708-3. (M)SDR GTIA050216Slide · deployedFLT 507 - FLL - FOUND FORWARD SLIDE ACCIDENTALLY DEPLOYED AT THE GATE, SLIDE PACK DID NOT FULLY INFLATE DUE TO A RUPTURED LINE ON THE CHARGE BOTTLE. (M)SDR SA05083Light · inoperativeDURING EMERGENCY LIGHT TEST, GREEN LIGHT WOULD NOT ILLUMINATE ON PROGRAMMING AND TEST PANEL. MAINTENANCE REPLACED THE LEFT HAND, AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.SDR SA05076Wire Harness · misroutedDURING INSPECTION OF RT AFT DOOR ESCAPE SLIDE, LIGHT WIRE HARNESS FOUND MIS-ROUTED. MAINTENANCE CORRECTLY ROUTED LIGHT WIRE HARNESS. OK FOR SERVICE.SDR SA05074Bottle · dischargedCIDS PANEL CAUTION LIGHT ILLUMINATED IN FLIGHT AND ON LANDING. MAINTENANCE FOUND L-2 DOOR SLIDE INFLATION BOTTLE PRESSURE LOW. MAINTENANCE REPLACED L-2 DOOR SLIDE INFLATION BOTTLE. OK FOR SERVICE.SDR GTIA050157Lamp · burned outSEVERAL LIGHTS BURNED OUT IN EMERGENCY EXITS SIGNS ABOVE L1, R1 AND R4 DOORS, AIRCRAFT TAIL SWAP WITH N825NK. RELAMPED EMERGENCY EXIT SIGNS IN CABIN AS REQUIRED, OPS CHECK GOOD. (M)SDR SA05046Landing Gear · malfunctionedLAX FLT 1 EN-ROUTE PIT TO LAX, DURING APROACH, THE LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. THE FLT PERFORMED A GO-AROUND, AND THEN MANUALLY EXTENDED THE LANDING GEAR. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED TROUBLESHOOTINSDR SA05042Computer · failedMCI - FLT 201 - ENROUTE PHL - SFO, DURING CRUISE, ECAM MESSAGE F/CTL ELAC 2 PITCH FAULT GENERATED, FOLLOWED BY AN A/P 2 DISC MESSAGE. AFTERWARDS, CREW FURTHER RECEIVED ECAM MESSAGES F/CTL STABILIZER JAM AND F/CTL ALTN LAW. DURING THIS TIME, STATUS ITEMS THATSDR CA050401002Landing Gear · inoperative(CAN) LANDING GEAR WOULD NOT EXTEND ON FIRST ATTEMPT. GEAR HANDLE RECYCLED, NO FIX ALTERNATE GEAR EXTENTION OPERATE NORMALLY. BITE TEST ALL CHECKED OK. LG CIU 1 AND 2 INTERCHANGED NO FIX. MTCE ADVISED AND TROUBLESHOT THE SNAG, ACFT ON JACKS.SDR SA05034Switch · leakingEN ROUTE, PHL TO LAX. AFTER TAKEOFF, AND FOR SEVERAL THOUSAND FEET, A STRONG OILY ODOR WAS NOTICED COMING FROM THE AIR CONDITIONING SYSTEM. ODOR DISSIPATED. FLIGHT CONTINUED TO LAX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND OIL LEAK IN APU. MASDR GTIA050042Compressor · stalledNR2 ENGINE COMPRESSOR STALL AT 10,000 LEVEL FLIGHT, PERFORMED QRH REST ENGINE TO MATCH NR1 AND ENGINE STALLED AGAIN, DIVERTED. REMOVED AND REPLACED NR2 ENGINE, PERFORMED IDLE LEAK CHECK, OPS CHECK GOOD. (K)SDR SA05017Epsu · faultyTPA - THE AFT EMERGENCY POWER SUPPLY UNIT REQUIRED REPLACEMENT. MAINTENANCE REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.SDR SA05018Light · inoperativeFOUND THE EMERGENCY LIGHT TEST SYSTEM INOPERATIVE. MAINTENANCE RESET THE CIDS SYSTEM. TEST PERFORMED SATISFACTORILY.SDR SA05008Epsu · dischargedDCA - THE EMERGENCY LIGHT SYSTEM FAILED THE SYSTEM TEST. MAINTENANCE REPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT BATTERY. OPERATIONALLY CHECKS OK.SDR SA05005Fairing · missingDCA - DURING OVERNIGHT SERVICE WALK AROUND INSPECTION, MAINTENANCE FOUND THE LEFT WING FLAP TRACK 3A FAIRING ASSEMBLY MISSING THE FORWARD FAIRING AND DAMAGE TO THE AFT FAIRING. MAINTENANCE REMOVED THE AFT FAIRING. ENGINEERING AUTHORIZATION WAS OBTAINED TO OPSDR CA041214006Interface Unit · malfunctioned(CAN) ENG 1 IGN 'A' FAULT, ENG 2 IGN 'A' FAULT. 1&2 IGN A C/B POPPED. ENG 1 CTLC/B POPPED. STRONG SMELL OF ELECTRICAL BURNING. CONNECTOR 473VC SHORTED, CONNECTOR REPLACED. BMC NR 1 DAMAGED, REPLACED PER MM 36-11-34-400. EIU NR 2 CAUSING INTFC PROBLEMS WITH AEVSDR CA041209002Engine · malfunctioned(CAN) THE CREW REJECTED TAKE-OFF AT A SPEED GREATER THAN 100 KNOTS. THE DECISION TO REJECT WAS A RESULT OF A NR 2 ENGINE ROLL BACK AFTER A N2 OVERSPEED. ACRFT RETURNED TO GATE. A/C OFFLINE FOR INVESTIGATION, DFDR REMOVED FOR READOUT. NOTE: MORE INFO WILL FOLSDR CA041206002Transmitter · fluctuates(CAN) IN CRUISE WE HAD TO SLOW DOWN OIL PRESS NR 2 FLASHED GREEN 14 PSI. HAD SOME POWER THE PRESSURE FLUCTUATED BETWEEN 18-19 PSI WHEN POWER WAS SELECTED TOWARD IDLE OIL PRESSURE WENT TO 10 PSI (RED). WE KEPT THE POWER UP DURING DECENT AND APPROACH. REPLACED OSDR GTIA040829Compressor · stalledLP NR 2907041; SHUTDOWN RT ENGINE, AIR RETURN. RT ENGINE COMPRESSOR STALL ON T/O AFTER V1, PULLED THROTTLE TO IDLE. TRIED ADVANCING POWER AGAIN ANOTER COMPRESSOR STALL AT ABOUT 1.3 EPR, FLEW SINGLE ENGINE APPROACH AND LANDING. REMOVED AND REPLACED RT ENGINE
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