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 = 'T210N' 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 = 'T210N' 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 2004FA0000536Wire · chafedFOUND BEACON CIRCUIT WIRING RUNNING UP THROUGH THE VERTICAL STABILIZER CHAFED IN 3 PLACES WHERE THE WIRES WERE ROUTED THROUGH 3 RIBS. REPLACED THE WIRES AND INSTALLED THE NEW WIRES IN A FIBERGLASS LOOM TO PREVENT FURTHER CHAFING. OPERATOR STATED THE BEACON CISDR CRJ2004F00000Ground Wire · dirtyWHEN PITOT HEAT IS ENGAGED, IT RENDERS THE STALL WARNING HORN INOPERABLE. STALL WARNING RESUMES WORKING PROPERLY WITH PITOT HEAT DISENGAGED. THE GROUND ON THE STALL WARNING UNIT WAS CLEANED. ALL OPERATIONS WORK PROPERLY. NOTE: THIS IS THE THIRD FINDING COMSDR 2004FA0000558Attach Bracket · misinstalledWHEN PN 1232041 ARE INSTALLED, INCORRECT FIT UNLESS SK210-125 ALSO INSTALLED ON STA 209.0 BULKHEAD. NO CORRELATING REFERENCE IN MFG PARTS OR SERVICE. TOOK 2 WEEKS WITH MFG TECH TO WORK OUT. IMPROPER FIT CAUSES STRESS AND BINDING ON PARTS THAT COULD LEAD TO SDR FIP2004F00000Flange · crackedTOP MOUNT EAR AND IB BAFFLE FLANGE CRACKED UNDER NORMAL OPERATING CONDITIONS.SDR FPI2004F00002Crankcase · crackedRT CASE CRACKED AT CYLINDER NR 1. 7TH STUD LOWER RECESS IN CASE.SDR 2004FA0000819Reinforcement · brokenFOUND REINFORCEMENT BROKEN AT ANNUAL INSPECTION. BREAK IS AT LOWER OB BOLT HOLE. PROBABLE CAUSE UNKNOWN. RECOMMEND CAREFUL INSPECTION OF AFT HORIZONTAL STABILIZER SPAR REINFORCEMENTS AT EACH 100 HOUR/ ANNUAL INSP.SDR 2004FA0000204Autopilot Sys · malfunctionedONCE ESTABLISHED IN CRUISE FLIGHT WITH ALTITUDE HOLD ENGAGED, THE S-TEC SYSTEM 55X AUTOPILOT FREQUENTLY BEGINS TO GENTLY PORPOISE IN PITCH. THIS GETS PROGRESSIVELY WORSE UNTIL THE AUTOPILOT CAUSES SERIOUS PITCH EXCURSIONS OF SEVERAL HUNDRED FEET PER MINUTE UPSDR 2004FA0000208Cylinder · unserviceableINSPECTED NEW CYLINDER AS RECEIVED. FOUND EXHAUST VALVE GUIDE INSIDE DIAMETER TO BE BELOW MINIMUM SPECIFICATIONS, AND VALVE SEAT MACHINING NOT CONCENTRIC.SDR 2004FA0000205Cylinder · mismanufacturedINSPECTED NEW CYLINDER AS RECEIVED. FOUND INSIDE DIAMETER OF EXHAUST VALVE GUIDE DID NOT MEET MINIMUM SIZE DIMENSIONS AND VALVE SEAT MACHINING NOT CONCENTRIC.SDR 2004FA0000207Cylinder · unserviceableINSPECTED NEW CYLINDER ASSY TISN 71.2BCA AS RECEIVED. FOUND VALVE SEAT MACHINING NOT CONCENTRIC AND EXHAUST VALVE SEAT DIAMETER CUT TO APPX. 1.847 INCH WHEN IT SHOULD BE APPX. 1.781 INCH ACCORDING TO PRINT DIMENSIONS IN OVERHAUL MANUAL.SDR 2004FA0000214Cylinder · unserviceableINSPECTED NEW CYLINDER ASSY. AS RECEIVED. FOUND INSIDE DIAMETER OF EXHAUST VALVE GUIDE TO BE BELOW MINIMUM MFG. SPECS. AND VALVE SEAT MACHINING NOT CONCENTRIC.SDR 2004FA0000209Cylinder · mismanufacturedINSPECTED NEW CYLINDER ASSY. AS RECEIVED. FOUND INSIDE DIAMETER OF EXHAUST VALVE GUIDE TO BE BELOW MINIMUM MFG. SPECS. AND VALVE SEAT MACHING NOT CONCENTRIC.SDR 2004FA0000213Cylinder · unserviceableINSPECTED NEW CYLINDER ASSY. AS RECEIVED. FOUND INSIDE DIAMETER OF EXHAUST VALVE GUIDE TO BE BELOW MFG. MINIMUM SPECS. AND VALVE SEAT MACHINING NOT CONCENTRIC.SDR 2004FA0000212Cylinder · unserviceableINSPECTED NEW CYLINDER ASSY. AS RECEIVED. FOUND INSIDE DIAMETER OF EXHAUST VALVE GUIDE TO BE BELOW MINIMUM MFG. SPECS. AND VALVE SEAT MACHINING NOT CONCENTRIC. PRE-SIZED GUIDES ARE USED ON THIS UNIT AND 5 OTHERS IN THIS BATCH INSPECTED. ALL UNAIRWORTHY. ALLSDR 2004FA0000211Cylinder · mismanufacturedINSPECTED NEW CYLINDER ASSY AS RECEIVED. FOUND INSIDE DIAMETER OF EXHAUST VALVE GUIDE TO BE BELOW MINIMUM MFG SPECS., AND VALVE SEAT MACHINING NOT CONCENTRIC.SDR 2004FA0000210Cylinder · mismanufacturedINSPECTED NEW CYLINDER ASSY AS RECEIVED. FOUND INSIDE DIAMETER OF EXHAUST VALVE GUIDE DID NOT MEET MINIMUM MFG. DIMENSIONS, AND VALVE SEAT MACHINING NOT CONCENTRIC.SDR 2004FA0000199Inlet · mismanufacturedUPON INSPECTION OF NEW PARTS DEFECTS WERE FOUND WITH THE TURBO INLET COMPONENT. DAMAGE WAS NOTED ON THE TURBOCHARGER MOUNTING FLANGE AND THE WELDING HAD VERY POOR PENETRATION. PART REJECTED AND SENT BACK TO O/H FACILITY. UPON RECEIVING PARTS, FACILITY WAS NSDR FPI2004F00000Oil Cooler · crackedBOTTOM COOLER TO ENGINE MOUNT EAR CRACKED. OCCURRED UNDER NORMAL OPERATION.SDR 2004F00256Trunnion · crackedNOSE GEAR COLLAPSED DURING LANDING ROLLOUT. DETERMINED TO BE CAUSED BY FAILURE OF THE UPPER TRUNNION ASSY NR 1243009-7. THE DRAG BRACE FAILED AT THE COLLAR AROUND THE STRUT TUBE. INDICATIONS OF INTERGRANULAR CORROSION ARE APPARENT AND PROBABLY CAUSED BY AN USDR IPMA854FTrunnion · failedNOSE GEAR COLLAPSED DURING LANDING ROLLOUT. DETERMINED TO BE CAUSED BY FAILURE OF THE UPPER TRUNNION ASSY (NR 12430097) THE DRAG BRACE FAILED AT THE COLLAR AROUND THE STRUT TUBE. INDICATIONS OF INTERGRANULAR CORROSION ARE APPARENT AND PROBABLY CAUSED BY AN SDR 2003FA0001175Spar · crackedCRACKED WING SPAR WEB AT ATTACHMENT FOR RECIPROCATING FUEL PUMP ASSOCIATED WITH FLINT WING TIP AUXILIARY FUEL SYSTEM. VIBRATION ASSOCIATED WITH FUEL PUMP OPERATION CAUSES THIN SPAR WEB (.025 INCH) TO FLEX AND CRACK AT OUTSIDE RADIUS OF ATTACHMENT HARDWARE.SDR FPI2003F00013Oil Cooler · crackedBOTTOM COOLER TO ENGINE MOUNT EAR CRACKED. OCCURRED UNDER NORMAL OPERATION.SDR FPI2003F00012Oil Cooler · crackedTOP AND BOTTOM COOLER TO TO ENGINE MOUNTING EARS CRACKED. OCCURRED UNDER NORMAL OPERATION.SDR FPI2003F00011Oil Cooler · crackedOIL COOLER CRACKED AT UPPER FOREMOUNTING FLANGE.SDR 2003FA0001162Switch · intermittentCONDITION OCCURRED APPROX 3 TIMES UNTIL OPERATOR WOULD NOT FLY UNTIL REPAIRED. AFTER RUN UP A LT TURN WAS NEGOTIATED, DOWN INDICATOR LIGHT WENT (OUT) AND HORN SOUNDED. MAINT DID INITIAL CHECK FOR BROKEN WIRES. SUPPORTED AC, POWER APPLIED, SHORT RUN OF GEAR SDR B3OR20033016Strut · corrodedDURING AN ANNUAL INSPECTION, THE LEFT MAIN LANDING GEAR SPRING HAD BUBBLING PAINT IN THE AREA WHERE THE SPRING CONNECTS TO THE AXEL ASSEMBLY. THE SPRING WAS REMOVED AND THE AXEL ASSEMBLY WAS REMOVED. THE SPRING WAS FOUND TO HAVE SEVERE PITTING CORROSION ON THESDR B3OR20033015Strut · corrodedDURING AN ANNUAL INSPECTION, THE RT MAIN LANDING GEAR SPRING HAD BUBBLING PAINT IN THE AREA WHERE THE SPRING CONNECTS TO THE AXEL ASSEMBLY. THE SPRING WAS REMOVED AND THE AXEL ASSEMBLY WAS REMOVED. THE SPRING WAS FOUND TO HAVE SEVERE PITTING CORROSION ON THE BSDR B3OR2003002Dipstick · brokenAFTER THE SECOND GROUND RUN, AND DURING A PRE-RUN CHECK FOR A THIRD GROUND RUN, A MECHANIC REMOVED THE OIL FILLER CAP/DIPSTICK AND DISCOVERED THAT THE DIPSTICK HAD BROKEN OFF FROM THE OIL FILLER CAP. THE OIL WAS DRAINED FROM THE ENGINE, AND A BORESCOPE WAS USESDR CTU2003F00005O-Ring · leakingO-RING FAILED TO SEAL PROPERLY ALLOWING OIL TO LEAK AT THE OIL FILTER ADAPTER TO ENGINE ATTACHMENT. CAUSE OF THE FAILURE COULD BE ATTRIBUTED TO O-RING TOTAL TIME. ALL WORK WAS DOEN IAW MM AND INSTRUCTIONS CONTAINED IN AD 96-12-22.SDR B3OR20030001Alt Air Door · separatedON CLIMB OUT, ENG BEGAN TO RUN ROUGH, DROPPING 300 RPM. DURING GROUND RUN UP, MAG CHECK AT 1700 RPM SHOWED NO PROBLEM. RUN UP TO PWR AND ENG RAN FINE, THEN DROPPED 300 RPM AND RAN ROUGH. MAINT REMOVED ALL SPARK PLUGS AND FOUND LEAD FOULED. CLEANED AND FIRE CHESDR 2003FA0000222Trunnion · brokenNOSE GEAR COLLAPSED DURING TAXI, AFTER LANDING, TOOK PLACE AFT NORMAL LANDING. COLLAR BROKE WHERE TRUNION ATTACHES TO NOSE GEAR BARREL, PREVIOUS CRACK EXISTED.SDR 2003FA0000152Hose · restrictedTHE CESSNA 210 LANDED WITH THE NOSE LANDING GEAR STILL IN THE NOSE WHEEL WELL. UPON TROUBLESHOOTING THE NOSE GEAR HYDRAULC SYSTEM, FOUND ONE OF THE NOSE GEAR ACTUATOR HOSES RESTRICTED AND KINKED. CESSNA SERVICE BULLETIN SEB92-8 RELATES TO THE CHANGING OF CERSDR FPI2003F00005Actuator · crackedC/W SEB 01-2, INSPECTED ACTUATORS FOR CRACKS, FOUND CRACKS, REMOVED FROM SERVICE.SDR FPI2002F00010Actuator · crackedBOTH MAIN GEAR ACTUATORS FOUND CRACKED. IAW SB ACTUATOR INSPECTION.SDR GFV2002F00006Rocker Cover · damagedDAMAGE TO ROCKER COVER MATING SURFACE. GRIT IN ROCKER SHAFT BOLT THREADS.SDR GFV2002F00005Fuel Nozzle · damagedROCKER COVER MATING SURFACE UN-EVEN AT WELD. FUEL NOZZLE THREADS, GRITTY.SDR GFV2002F00004Fuel Nozzle · damagedFUEL NOZZLE THREADS, NO GOOD. ROCKER SHAFT BOLTS GRITTY.SDR GFV2002F00003Fuel Nozzle · dirtyFUEL NOZZLE THREADS AND ROCKER SHAFT BOLT GRITTY.SDR GFV2002F00002Fuel Nozzle · strippedFUEL NOZZLE THREADS NO GOOD. ROCKER SHAFT BOLTS STRIPPED.SDR GFV2002F00001Fuel Nozzle · dirtyFUEL NOZZLE THREADS AND ROCKER SHAFT BOLTS GRITTY.SDR 2002FA0000790Bracket · brokenAIRCRAFT UNDERGOING ANNUAL INSPECTION. HORIZONTAL STABILIZER FOUND LOOSE. INSPECTED AND FOUND REAR MOUNTING REINFORCEMENT BRACKET BOTH SIDES BROKEN AND THE FORWARD ATTACHMENT FITTINGS LOOSE. INSTALLED REAR BRACKETS AND PN SK210-126.SDR H792002F00001Control Cable · failedTHIS AIRCRAFT, ENROUTE, ON TAKEOFF THE PILOT NOTICED A ROUGHNESS IN THE ENGINE OPERATION. THE PILOT ELECTED TO LAND AT AIRPORT TO HAVE MAINTENANCE TROUBLESHOOT ROUGHNESS. MAINTENANCE DISCOVERED THAT THE MIXTURE CONTROL CABLE HAD FAILED AT THE CRIMP SWIVEL JOSDR 2002FA0000686Trunnion · collapsedWHILE RETRIEVING AIRCRAFT FROM NOSE GEAR COLLAPSE, FOUND LOWER TRUNNION ASSEMBLY. BROKEN AT AFT SIDE WHERE COLLAR WRAPS AROUND GEAR. APPEARS THERE WERE CRACKS AT LEFT AND RIGHT TOP CORNERS JUST FORWARD OF THE BRACE SUPPORT MOUNTS. THEY ARE IN A VERY DIFFICSDR H792002F00000Bracket · crackedDURING ANNUAL INSPECTION NOTICED CRACKS IN THE LEFT AFT HORIZONTAL STABILIZER ATTACH BRACKET. IF BRACKET IS CRACKED, REPLACE WITH IMPROVED BRACKET.SDR FPI2002F00003Actuator · brokenACTUATOR PISTON SERVES AS A RACK WITH GEAR TEETH CUT INTO THE BOTTOM PART OF THE PISTON. THE RACK DRIVES A PINION GEAR ATTACHED TO THE GEAR LEG. THE RACK PISTON IS HELD IN ENGAGEMENT WITH THE PINION BY A HARDENED STEEL ROLLER ON TOP OF THE RACK. THE ROLLER SDR 2002FA0000535Wire · cutAIRCRAFT HAD THE LEFT GEAR COLLAPSE ON ROLLOUT. PLACED AIRCRAFT ON JACKS AND CHECKED RETRACT SYSTEM. FOUND POWER PACK NOT RUNNING DUE TO A CUT WIRE IN THE NOSE WHEEL WELL. THE WIRING TO THE NOSE DOWN LOCK SWITCH WAS MISROUTED AND WAS CUT IN THE DOWN LOCK ASSDR FPI2002F00001Switch · inoperativeSWITCH USED TO ACTUATE LANDING GEAR WARNING HORN. SWITCH MOUNTED TO THROTTLE CABLE.SDR 2001FA0000552Connector · looseAIRCRAFT LOST ELECTRICAL POWER IN FLIGHT. PLUG THAT CONNECTED VOLTAGE REGULATOR/ WARNING INDICATOR TO ALTERNATOR DID NOT LOCK AND VIBRATED LOOSE. BECAUSE THE LOW VOLTAGE INDICATOR DIE NOT ILLUMINATE AND THE AMMETER IS ON THE FAR RIGHT SIDE OF CABIN, PILOT WASDR 2001FA0000526Spar · crackedELEVATOR FRONT SPAR, DOUBLERS, AND ATTACHMENT CRACKED.AIRCRAFT USED IN PIPELINE PATROL.SDR 2001FA0000525Spar · crackedELEVATOR SPAR CRACKED,ATTACHMENT BRACKET, AND DOUBLERS ALSO CRACKED.
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