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 = '210' 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 = '210' 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 2025FA0000251Panel · crackedOUTBOARD RIGHT LANDING GEAR WELL STRUCTURAL PANEL CRACKED FROM LOWER FORWARD EDGE OF PANEL. THE CRACK EXTENDED UPWARD UNDERNEATH A DOUBLER BRACKET THROUGH THE PANEL AND A PREVIOUS REPAIR DOUBLER, THROUGH A FUEL LINE PENETRATION HOLE IN THE PANEL. THE PREVIOUS SDR 2025FA0000250Panel · crackedOUTBOARD LEFT LANDING GEAR WELL STRUCTURAL PANEL CRACKED FROM LOWER FORWARD EDGE OF PANEL. THE CRACK EXTENDED UPWARD THROUGH THE PANEL AND A DOUBLER BRACKET TO THE FUEL LINE PENETRATION HOLE IN THE PANEL. NO PREVIOUS REPAIR ON THIS PANEL.SDR 2020FA0000094Collar · missingSWITCH PIN GUIDE COLLAR FOUND MISSING. ALLOWS SWITCH PIN TO WOBBLE IN SWITCH HOUSING. HARD TO SEE UPON INSPECTION.SDR 2017FA0000410Alternator · failedREBUILT ALTERNATOR WAS INSTALLED. DURING A 50/100 HOUR INSPECTION FOR A NORMAL TBO REPLACEMENT, IT WAS REMOVED FROM THE ACFT DUE TO FAILURE AT AIRCRAFT TT 6680.0 ALTERNATOR FAILED AFTER 44.5 HOURS.SDR 2014FA0000047Attach Bracket · corrodedDURING SCHEDULED ANNUAL INSPECTION, FOUND MOVEMENT IN THE RT WING SPAR FITTINGS, BETWEEN THE RT WING MAIN SPAR ATTACH BRACKETS AND THE FUSELAGE CARRY-THROUGH SPAR ATTACH BRACKETS. REMOVED RT WING FROM AIRCRAFT, FOUND SIGNIFICANT PITTING AND CORROSION IN BORESSDR BSYR201309130001Actuator · malfunctionedAFTER TAKEOFF, PUMP CONTINUED TO RUN AFTER GEAR RETRACTION. PILOT RETURNED AND LANDED SAFELY WITHOUT INCIDENT. MX ADJUSTED GEAR ACTUATOR, OPS CHECK NORMAL.SDR BSYR20120913060Alternator · failedAFTER DEPARTURE, PILOT DISCOVERED ALTERNATOR FAILURE. PILOT RETURNED AND LANDED SAFELY AT DEPARTURE. OPENSDR BSYR20120913059Pitot Tube · obstructedPILOT ABORTED TAKEOFF, DUE TO INOPERATIVE AIRSPEED INDICATION. PILOT TAXIED BACK TO RAMP WITHOUT INCIDENT. MX REMOVED OBSTUCTION FROM PITOT TUBE.SDR BSYR201309092058Pump · failed20 MINUTES AFTER DEPARTURE, VACUUM PUMP FAILED. PILOT RETURNED AND LANDED SAFELY AT BUY WITHOUT INCIDENT.SDR BSYR201307020001Engine · power lossDURING FLIGHT, ENGINE STARTED RUNNING ROUGH. DIVERTED AND LANDED SAFELY WITHOUT INCIDENT. OPEN.SDR CA060307005Motor · erratic(CAN) GEAR MOTOR CHANGED DUE TO ERATIC GEAR OPERATION. GEAR MOTOR WAS SPRAYING SOLDER. PRESSURE SWITCH ADJUSTED TO SPEC FOR GEAR OPEARTION. (TC NR 20060307005)SDR 2005FA0001261Line · mismanufacturedFERRULE ON NLG DOOR OPEN LINE CRACKED ALONG STRESS RISER CREATED BY FLARING TOOL VISE. RESULTED IN LOSS OF HYDRAULIC FLUID TO OPERATE LANDING GEAR. AIRCRAFT LANDED WITH MAIN LANDING GEAR UP. (K)SDR 2005FA0001096Pin · missingNOSE GEAR UPLOCK PIN FELL OUT AFTER RETAINING COTTER PIN FAILED, NOT ALLOWING UPLOCK ACTUATOR TO RELEASE GEAR RESLULTING IN NOSE GEAR UP LANDING, ALSO FOUND NOSE GEAR UPLOCK SPRING ATTACH BRACKETT SEVERLY WORN. (SW09200511362)SDR CA050420002Support · cracked(CAN) OUTBOARD AFT WEB OF LEFT OUTBOARD LANDING GEAR SUPPORT FOUND CRACKED WHILE REPLACING LANDING GEAR PIVOT ASSEMBLY.SDR 2005FA0000566Pump · wrong partSUSPECT PUMP IS INCORRECT BY PN 4760876 FOR INSTALLATION AC. INTERFERED WITH NOSE LANDING GEAR UPLOCK OPERATION. (K)SDR N210TM1Clevis Pin · failedNOSE GEAR FAILED TO EXTEND DUE TO BROKEN CLEVIS PIN IN NOSE GEAR UPLOCK SYSTEM.SDR 2003FA0000132Crankshaft · brokenAIRCRAFT MADE EMERGENCY LANDING AFTER ENGINE FAILURE. INVESTIGATION FOUND THAT THE ENGINE CRANKSHAFT HAD BROKEN BETWEEN CYLINDERS TWO AND THREE.SDR 2003FA0000056Saddle · brokenCOMPLIANCE WITH AD 76-14-07 R2 FOUND LT MAIN GEAR SADDLE BROKEN.SDR 20001207SH014Tab · brokenMOUNTING TABS BROKE OFF ON BOTH SIDES OF THE STARTER SOLENOID BREAKING GROUND CONNECTION SO STARTER WAS INOP. SOLENOID IS MOUNTED DIRECTLY ON THE STARTER. MOUNTING BRACKET IS SPOT WELDED TO SOLENOID HOUSING. FAILURE POSSIBLY DUE TO VIBRATION. REPLACED SOLESDR 20001109SH037Tube · brokenTHE TUBE WELDED ASSY WHICH STEERS NOSE GEAR, ARM BROKE THE WELD ON THE TUBE WHICH ALOWED THE NOSE WHEEL TO SWIVEL AND COLLAPSED THE NOSE WHEEL ON LANDING. (X)SDR EY2R57093ANut · corrodedTHREADS ON BLADE RETENTION NUT CORRODED. REPLACED. (X)SDR EY2R57093Pin · corrodedACTUATING PIN CORRODED ON SURFACE OF PIN. REPLACED. (X)SDR 20000814SH006Shock Mount · mismanufacturedPART LABELED/MANUFACTURED WRONG. PART LABELED ''''TOP FORWARD MOUNTING'''', BUT AT INSTALLATION, DID NOT HAVE REQUIRED REINFORCEMENT WASHER PUT IN AT MANUFACTURE. PART CURE DATE: 3/99. (X)SDR CA000824026Rod End · separated(CAN) PILOT REPORTED LACK OF THROTTLE RESPONSE. THE AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND THROTTLE ROD END SEPARATED FROM BALL AT THROTTLE ARM ON THE FUEL CONTROL. A NEW ROD ENDSDR 20000413SH050Piston Rod · failedTHREADED END OF ACTUATOAR ROD BROKE ALLOWING NOSE GEAR TO UNLOCK AND RETRACT. (X)SDR 98ZZZX555Channel · crackedELEVATOR CHANNEL HAS 7 LOCATIONS WHERE BUCKING BAR SLIPPED OFF OF RIVET TAIL AND INDENTED STRUCTURE. CRACKS HAVE FORMED AT ALL 7 LOCATIONS. THIS DEFECT IS ORIGINAL FROM FACTORY. SUBMITTER STATED THIS IS THE 2ND PART WITH THE SAME DEFECT FOUND.SDR 97ZZZX4949Bypass Spring · failedOIL FILTER BYPASS SPRING FOUND BROKEN AND DISC FOUND UNDER ENGINE OIL PRESSURE VALVE. ENGINE HAD NO OIL PRESSURE AFTER START-UP. BYPASS DISC FOUND UNDER ENGINE OIL PRESSURE RELIEF VALVE PREVENTING ENGINE FROM DEVELOPING ANY PRESSURE.SDR EY2R9601285Hub · corrodedHUB FOUND CORRODED.SDR EY2R9601284Blade · corrodedBLADE, SN BH500, FOUND CORRODED.SDR EY2R9601283Blade · corrodedBLADE, SN BH489, FOUND CORRODED.SDR EY2R9601282Blade · corrodedBLADE, SN BH469, FOUND CORRODED.SDR EY2R9600187Hub · crackedHUB ASSY CRACKED IN NR1 SOCKETSDR EY2R9600180Retain Nut · crackedPROP ASSY RETAIN NUT CRACKED THREADSSDR 97ZZZX151Propeller Assy · crackedINSPECTION FOUND PROPELLER ASSY P/N C1976 CRACKED.SDR 97ZZZX150Blade · below specINSPECTION FOUND BLADE P/N S90M8 BELOW MINIMUM.SDR 97ZZZX149Blade · below specINSPECTION FOUND PROPELLER BLADE P/N S90M8 BELOW MINIMUM.SDR 97ZZZX148Propeller Assy · crackedINSPECTION FOUND PROPELLER ASSY C2715/C33 NR 1 SOCKET CRACKED.SDR EY2R9601038Hub · corrodedHUB CORRODED.SDR EY2R9601037Cylinder · corrodedCYLINDER CORRODED.SDR EY2R9601036Blade · corrodedBLADE, SN B98523, FOUND CORRODED.SDR EY2R9601035Blade · corrodedBLADE, SN B09515, FOUND CORRODED.SDR EY2R9601034Blade · corrodedBLADE, SN B136412, FOUND CORRODED.SDR EY2R9600147Hub · crackedHUB CRACKED IN NR1 SOCKETSDR EY2R9600146Retain Nut · crackedPROP ASSY RETAIN NUT CRACKEDSDR EY2R9601062Cylinder · corrodedCYLINDER CORRODED.SDR EY2R9601061Piston · corrodedPISTON CORRODED.SDR EY2R9601060Link · corrodedCORROSION FOUND ON LINK.SDR 96ZZZX4764Air Box · defectiveFLAPPER VALVE IN AIR BOX WAS IN CLOSED POSITION CAUSING INDUCTION HEAT TO BE SUPPLIED TO ENGINE WITH CONTROL IN THE INDUCTION HEAT OFF POSITION. SUSPECT CAUSE, CONTROL CABLE SLIPPAGE ALLOWING INDUCTION AIR TO BE CLOSED OFF AND INDUCTION HEA T TO BE SUPPLIED TSDR 96ZZZX4039Placard · improperAIRCRAFT MADE AN EMERGENCY RETURN TO AIRPORT LANDING (GEAR UP) DUE TO ENGINE POWER LOSS ON TAKEOFF/CLIMB. INVESTIGATION FOUND INDUCTION AIR FLAPPER IN 'HOT' POSITION. THIS IS AN INJECTED ENGINE. AIRCRAFT PLACARD FOR TAKEOFF LANDING CHECK LIST IMPROPERLY WORSDR 96ZZZX3768Elt · malfunctionCESSNA PART NR C589510-0290. MANUFACTURED TO TSO-C91, WOULD NOT PASS G-SWITCH OPERATIONAL CHECK PER FAR 91.207(D) EVEN AFTER SLAMMING ELT INTO GROUND IN DIRECTION OF FLIGHT. ELT WOULD PUT OUT SIGNAL WHEN MANUALLY SWITCHED TO ON.
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