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 = '206B' 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 = '206B' 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 CA120905009Governor · malfunctioned(CAN) GOVERNOR WILL NOT RECOVER FROM OVERSPEED WHEN COLLECTIVE DECREASED.SDR Z0AL20120809001Bulkhead · crackedTAIL ROTOR GEARBOX SUPPORT BULKHEAD CRACKED, AT RIGHT REAR MOUNTING HOLE TO 2ND RIVET INBOARD TO GB SUPPORT.SDR CA120807001Bearing · failed(CAN) DURING 100HR INSPECTION, METAL FOUND ON ALL 3 M/R TRANSMISSION MAGNETIC CHIP DETECTORS. NOT ENOUGH METAL FOR A COCKPIT CHIP INDICATION. METAL ALSO FOUND IN M/R GEARBOX OIL FILTER. TRANSMISSION ASSY AND MAST ASSY REMOVED FOR INSPECTION, M/R MAST BEARINSDR CA120727011Bearing · failed(CAN) DURING APPROACH TO A LANDING SITE, THE PILOT HEARD AN INCREASE IN NOISE FROM THE TURBINE AND EXPERIENCED A SLIGHT YAW TO THE RT. THE NR GUAGE WAS INDICATING 112 PERCENT. THE PILOT LOWERED THE COLLECTIVE AND TRIED TO CONTROL THE RPM WITH THE THROTTLE TOSDR CA120727009Governor · slow(CAN) PILOT REPORTED THAT GOVENOR WAS SLOW TO RESPOND. GOVENOR REPLACED.SDR CA120813016Blade · fractured(CAN) DURING LANDING, THE PILOT NOTICED POWER LOSS OF THE NR 2 ENGINE. THE ACFT MADE AN UNEVENTFUL LANDING. A VISUAL INSPECTION OF THE ENGINE SHOWED THE EXHAUST DUCT INNER CRACKED WITH MATERIAL MISSING. THERE WAS NO INDICATION OF FRACTURED PT BLADES. THE POWSDR CA120727010Friction Pad · worn(CAN) DURING 100/300 HR INSPECTION OF THE HELICOPTER THE STARTER GENERATOR FRICTION PADS WERE FOUND TO BE WORN. STARTER GENERATOR REPLACED.SDR CA120906011Blade · wrong part(CAN) IT HAS BEEN REPORTED THAT ACFT HAS HAD THE WRONG TAIL ROTOR BLADES FITTED. IT HAS BEEN FLOWN WITH 206-011-810-135 BLADES, LONG SHAFT, FITTED ON A -103 GEARBOX, SMALL SHAFT, FOR APPROXIMATELY 100 HOURS IN THIS CONFIGURATION. THE TAILBOOM HAS NOT BEEN CSDR 2012FA0000459Fuel Cell · contaminatedRECEIVING FUEL CELLS FROM MFG WITH CONTAMINATES REMAINING IN FUEL CELL.SDR CA120523006Seal · failed(CAN) AIRCRAFT WAS ON A FERRY FLIGHT WHEN IT HAD A SUDDEN YAW AND A DECREASE OF APPROXIMATELY LO PERCENT TORQUE AND AN INCREASE IN ENGINE TOT OF APPROXIMATELY 70 DEGREES C. THE PILOT HAD NO FAILURE INDICATIONS AND THE ACFT APPREARED TO BE OPERATING NORMALLY OSDR CA120517006Servo · leaking(CAN) LEFT HYDRAULIC SERVO FOUND LEAKING DURING 100 HR AIRFRAME INSPECTION. HYDRAULIC SERVO REPLACED.SDR CA120417007Seal · separated(CAN) PILOT WAS PERFORMING DAILY PRE-FLIGHT INSPECTION. HE FOUND GREASE LEAKAGE FROM THE FORWARD PART OF THE MAIN ROTOR DRIVE SHAFT AT THE TRANSMISSION COUPLING. THE GREASE LEAKED OUT OF THE SPLIT/SEPARATED SEAL/BOOT. THE INDICATOR HAS FLASHED OFF ON THE RESDR CA120404005Line · cracked(CAN) WHILE MAINTENANCE WAS CARRYING OUT POWER ASSURANCE CHECK IT WAS NOTED THAT THE TORQUE WAS LOW. TROUBLESHOOTING WAS ACCOMPLISHED BY MAINTENANCE AND FOUND A DEFECTIVE ANTI-ICE VALVE. THE ANTI-ICE VALVE FOUND TO HAVE CRACKED WHERE IT ATTACHES TO THE COMPRSDR 2012FA0000218Indicator · failedDURING ROUTINE INSPECTION, DISCOVERED THAT AFTER MAIN ROTOR TRANSMISSION OIL WAS DRAINED, OIL LEVEL INDICATED FULL. OIL LEVEL SIGHT GLASS REMOVED. INSPECTION OF THE OIL LEVEL INDICATOR REVEALED COATING WITH LEVEL MARKINGS HAD SEPARATED FROM THE METALLIC BACSDR CA120229001Blower · failed(CAN) BLOWER MOTOR BLEED AIR HEATER FAILED IN FLIGHT. BLOWER MOTOR REPLACED.SDR CA120305006Case · cracked(CAN) WHEN ELT WAS REMOVED FOR ANNUAL INSPECTION NUMEROUS CRACKS WERE NOTED AROUND THE CASE SCREWS. A SMALL AMOUNT OF FLUID, POSSIBLY HYDRAULIC, WAS FOUND ON THE ELT. CASE SCREW HAVE NOT BEEN ADJUSTED BY THE OPERATOR SINCE THE ELT WAS PURCHASED. POSSIBLY OVSDR CA120229002Seal · leaking(CAN) DURING 24 MONTH INSPECTION THE MAIN ROTOR TRANSMISSION WAS FOUND TO HAVE AN INPUT SEAL LEAK. TRANSMISSION REPLACED.SDR CA120113009Blade · delaminated(CAN) BEST DESCRIBE THIS DEFECT AS A CONVEX BUBBLE DELAMINATION IN THE SKIN OF THE BLADE. DEFECT IS FOUND ON BOTH TOP AND BOTTOM OF BLADE, SAME SIZE AND SHAPE FOR BOTH. DEFECT LOCATION IS FOUND 9.5" INBD FROM THE BLADE TIP, AND 2" FORWARD FROM THE T/E. THE SDR CA120105004Gearbox · leaking(CAN) INTERMITTENT REDUCTION GEARBOX OIL VENTING AND ERRATIC OIL PRESSURE DROP OUT TO ZERO FOR 15 SECONDS. SUSPECT INTERNAL DEFECT.SDR CA120104010Fcu · failed(CAN) PILOT WAS APPROACHING LANDING AREA, NOTICED N2 WAS INCREASING, SO USED THE LINEAR ACTUATOR TO REDUCE N2 SPEED. N2 ADJUSTMENT FAILED TO REDUCE N2 SPEED WHILE IN THE AIR, SO PILOT CONTINUED TO ATTEMPT TO SLOW N2 SPEED THROUGH LINEAR ACTUATOR ADJUSTMENT UNSDR CA120104001Actuator · binding(CAN) PILOT NOTED STICKY TAIL ROTOR PEDALS ON FINAL APPROACH. TAIL ROTOR SERVO ACTUATOR REPLACED.SDR CA111129011Bushing · elongated(CAN) M/R BLADE INSPECTED FOR INSTALLATION ONTO A BELL 206B. THE BLADE WAS PURCHASED THRU A BHT APPROVED SUPPLIER IN THE USA, STERLING HELICOPTERS IN A USED SERVICEABLE CONDITION. THE MAIN BLADE HAD BEEN REPAIRED 37 HOURS EARLIER WITH A REPLACEMENT BLADE BOLSDR YTRA11320Starter Gen · damagedAIRCRAFT WOULD NOT START. WHEN PILOT ENGAGED STARTER THE STARTER WOULD SPIN BUT NOT TURN THE ENGINE. ON INSPECTION NOTED THE SPLINES BETWEEN THE DRIVESHAFT AND ARMATURE WERE COMPLETELY ERODED.SDR CA111109010Freewheel Unit · making metal(CAN) METAL SLIVERS FOUND ON CHIP PLUG DURING DAILY INSPECTION. REMOVED FREEWHEEL UINT AND SEVERAL MORE SLIVERS WERE FOUND IN THE FREEWHEEL HSG. FREEWHEEL UNIT SENT TO MFG SERVICE CENTER FOR DISASSEMBLY AND INVESTIGATION. METAL SLIVERS WERE MAX .5" BY .005".SDR CA111020004Bulkhead · cracked(CAN) DISCOVERED DURING A REGULAR INSPECTION, A .2500" CRACK COMING FROM THE AFT LT STUD HOLD FOR THE TAIL ROTOR GEARBOX MOUNTING ON THE TAIL BOOM.SDR CA110923001Line · leaking(CAN) HYDRAULIC FAILURE ON FINAL TO AIRPORT BASE. FOUND HYDRAULIC PRESSURE LINE WORN THROUGH WHERE CLAMPED TO DECK. CLAMP WAS IN GOOD CONDITION, BUT THE RUBBER CUSHION HAD TURNED VERY SLIGHTLY LEAVING VERY SMALL GAP THAT HOSE RUBBED THROUGH ON. HOSE REPLACESDR 2011FA0000599Counterweight · departedAT APPROXIMATELY 21:15 THE EVENING OF 31 AUG 2011, DEPARTED THE COUNTY RAMP IN FOR A NIGHT VISION GOGGLE TRAINING MISSION WITH A CONTRACT INSTRUCTOR PILOT. WEATHER AT THE TIME WAS VFR. ALL PRE-FLIGHT CHECKS WERE NORMAL, AS WAS TAKEOFF AND CLIMB HEADING SOUTSDR CA110928016Servo · leaking(CAN) HYDRAULIC SERVO FOUND LEAKING DURING ACFT INSPECTION. HYDRAULIC SERVO REPLACED.SDR CA110808006Bearing · failedTHE TRANSMISSION HAS BEEN INSPECTED FOR "MAKING METAL", UPON FURTHER INSP THE BEARING, PN 206-040-038-101 SN MB 4790, WAS DEEMED TO BE THE SOURCE. THE BEARING WAS INSTALLED CORRECTLY AS INDICATED, HOWEVER THE BEARING ITSELF WAS ASSEMBLED INCORRECTLY WITH THE ISDR CA110803025Fcu · failedACFT EXPERIENCED COMPRESSOR STALLING. FCU REPLACED.SDR CA110727006Fcu · failedFCU INSTALLED IN ACFT WITH 585.2 HRS TSO AND 0.0 HRS TSI. FCU WOULD NOT SPOOL UP FROM GROUND IDLE TO FLIGHT IDLE.SDR CA110727002Compressor · failedENGINE FAILURE OCCURED. PRELIMINARY INSPECTION REVEAL COMPRESSOR FAILURE.SDR CA110803026Governor · malfunctionedROTOR DROOPING TO 94 PERCENT AND WOULD NOT RECOVER. GOVERNOR REPLACED.SDR CA110714008Brush Block · failedUNIDENTIFIED METAL PARTICLES FOUND IN ENGINE COMPARTMENT. DURING A ROUTINE BRUSH INSP OF THE STARTER GENERATOR, PN 23032-018, SN 14011, A SCREW WAS FOUND TO HAVE BEEN MAKING CONTACT WITH WHAT LOOKED TO BE AN IMPROPER OR IMPROPERLY INSTALLED SPRING WHICH IS USESDR CA110719002Turbine · making metal(CAN) ENGINE CHIP WARNING LIGHT CAME ON DURING FINAL APPROACH. TURBINE ASSY REPLACED.SDR CA110720007Governor · malfunctioned(CAN) ROTOR RPM DROOPING TO 94 PERCENT. GOVENOR REPLACED.SDR CA111006003Tube · chafed(CAN) TUBE ASSY WAS FOUND TO HAVE CHAFING DAMAGE. CLAMP SETUP FOUND ON ADJACENT TUBE ASSY MIGRATED ALONG THEIR TUBES AND CAME IN CONTACT WITH THE SUBJECT TUBE ASSY. CONTACT CAUSED CHAFING TO OCCUR. CLAMPS ON THE ADJACENT TUBE HAD LOST THE CLAMPUP, WHICH ALLOSDR CA110719011Governor · malfunctioned(CAN) RPM DROOP NOT RECOVERING. GOVENOR REPLACED.SDR 2011F00140Oil Filter · unknownSCAVENGE OIL FILTER END CAP REMAINED IN FILTER HOUSING DURING ROUTINE SCHEDULED FILTER CHANGE. FILTER PN P1050.SDR CA110603007Battery · dischargedDURING ANNUAL ELT PERFORMANCE TEST IT WAS FOUND THAT THE BATTERY VOLTAGE WOULD DOP BELOW MFG SPEC DURING TRANSMIT. UNDER TEST THE BATTERY VOLTAGE DROPPED TO 7.7 V WHILE THE CMM INDICATES 8.0 V AS THE MINIMUM. BATTERY WAS MARKED WITH EXPIRATION DATE OF FEBRUASDR CA110530007Fuel Nozzle · wornSLOW STARTING, ENGINE HANGING AT 48-50 PERCENT N1. FUEL NOZZLE REPLACED.SDR CA100528001Governor · failed(CAN) GOVERNOR WOULD NOT STABILIZE THE RPM AT 1005, PT GOVERNOR REPLACED.SDR CA080519001Drive Shaft · damaged(CAN) THE INTERNAL SPRING INSIDE THE DRIVE SHAFT COUPLING GEAR WAS FOUND TO HAVE BEEN DAMAGED DUE TO IMPROPER INSTALLATION DURING LAST CALENDAR INSPECTION. DAMAGE BEYOND LIMITS SHAFT REPLACED.SDR CA110516012Brushes · wornTHIS STARTER/GENERATOR WAS INSTALLED ON THE ACFT AT THE TIME OF PURCHASE. STARTER BRUSHES WORN.SDR CA110603003Elt · crackedDURING ANNUAL ELT INSPECTION, UNIT WAS FOUND TO HAVE 28 CRACKS IN THE HOUSING. THE UNIT WAS FOUND TO HAVE SOME OIL CONTAMINATION ON THE HOUSING. ALL CRACKS WERE FOUND NEAR THE COVER SCREWS SUGGESTING THAT THE SCREWS MAY HAVE BEEN OVER-TORQUED. THE COVER SCREWSDR CA100512005Bearing · failed(CAN) DURING PIPELINE PATROL LOW LEVEL OPERATIONS: AN OVERSPEED WAS EXPERIENCED UP TO 107-110 PERCENT. GOVERNOR WAS BEEPED DOWN TO CONTROL OVERSPEED AND THROTTLE HAD TO BE REDUCED AS WELL TO CONTROL ENGINE RPM. ACFT WAS LANDED SUCCESSFULLY AT THE NEXT AVAILASDR CA110509012Blade · crackedDURING AN AFTER LAST FLIGHT CHECK, A CRACK WAS FOUND ON THE TAIL ROTOR BLADE RUNNING PARALLEL WITH THE T/E, ADJACENT TO THE CHORDWISE BALANCE WEIGHT.SDR CA110503008Bulkhead · cracked2 CRACKS FOUND ON TAILBOOM BULKHEAD. CRACKS GENERATED FROM THE HOLES FOR T/R GEARBOX STUDS, FOUND DURING TAIL ROTOR GEAR BOX ATTACHMENT CHECK ON 300 HOUR AIRFRAME INSPECTION.SDR CA110511006Transponder · intermittentATC TRANSPONDER INTERMITTENTLY TRANSMITTING WRONG MODE A CODE. MODE A CODE SELECTOR SWITCHES INTERMITTENT. TRANSPONDER IN SERVICE FOR 5 DAYS SINCE LAST RECERTIFICATION. TRANSPONDER REPLACED.SDR CA110426006Disc Pack · cracked(CAN) CRACKED DISC SEGMENT.
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