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 2005FA0000122Engine · making metalPILOT REPORTED HEARING A GRINDING NOISE FROM THE ENGINE WHICH WAS FOLLOWED BY AN ENGINE CHIP LIGHT INDICATION. A POWER ON PRECAUTIONARY LANDING WAS MADE. THE ENGINE WAS REMOVED AND REPLACD WITH A LOANER ENGINE. THE DISCREPANT ENGINE AS AN ASSEMBLY WAS SENT SDR CA050130002Bearing · seized(CAN) UPON INSPECTION OF THE LONG TAIL ROTOR PITCH CHANGE TUBE THE WALKING BEAM WAS OBSERVED TO BE A LITTLE RATCHETY TO ROTATE EVEN THOUGH IT ONLY ROTATES ABOUT 30 DEGREES OF TRAVEL. UPON THIS INSPECTION THE PART WAS REMOVED AND FURTHER INSPECTED. THE BEARINSDR CA050125001Indicator · malfunctioned(CAN) AFTER THE AIRCRAFT WAS COLD SOAKED FOR OVER AN HOUR, THE GUAGE RESPONSE WAS VERY SLOW WHILE THE ENGINE OIL TEMP WAS ALLOWED TO STABILIZE AT 60 DEG.SDR CA050107004Housing · leaking(CAN) DURING A TEST FLIGHT FOLLOWING AN OPS NR4 INSPECTION, THE TRANSMISSION OIL PRESSURE LIGHT ILLUMINATED AND THE OIL PRESSURE DROPPED SLIGHTLY BELOW THE RED LINE. AN IMMEDIATE DECENT WAS CONDUCTED AND UPON LANDING A MAJOR OIL LEAK WAS DISCOVERED. THE SOURCSDR ALG2005F00008Chip Detector · malfunctionedDURING TAKEOFF, AFTER MAINTENANCE INSPECTED TAIL ROTOR CHIP FROM FIRST OCCURRENCE OF FLICKERING LIGHT. DURING TAKEOFF, DURING LT TURN TAIL ROTOR CHIP LIGHT FLICKERED ON AND OFF FOR APPROXIMATELY 15 SECONDS THEN REMAINED OFF. AIRCRAFT RETURNED, MAINTENANCE RESDR CA050104010Bleed Valve · failed(CAN) BLEED VALVE WAS INSTALLED AFTER OVERHAUL TO REPLACE A TIME EXPIRED UNIT. SUBSEQUENT POWER CHECK REVEALED HIGH TOT. BLEED VALVE WAS WAS RETURNED TO VENDOR TO CORRECT FAULT. PART WAS INSTALLED AND FAILED A SECOND TIME. PART WAS REPLACED WITH ANOTHER UNSDR CA041221005Bearing · rough(CAN) DURING BLOWER ASSEMBLY DISSASSEMBLY FOR CLEANING TAIL ROTOR DRIVESHAFT BEARING WAS FOUND TO FEEL ROUGH WHEN ROTATED.SDR CA041221006Disc · corroded(CAN) ON INSPECTION 4 DISC ASSY WHERE FOUND TO BE CORRODED AND HAD TO BE REPLACED.SDR CA041129017Combustion Liner · cracked(CAN) THE PILOTS WERE DOING TRAINING, THEY NOTICED AN INCREASE IN TOT. DID A POWER CHECK AND FOUND THAT THE ENGINE WAS BELOW SPEC. AIRCRAFT RETURNED TO BASE AND IT WAS DISCOVERED THAT THE THERE WAS A 1 INCH CRACK THAT FOLLOWED A WELD IN THE E ARM PIT AREA. NSDR CA041209008Line · cracked(CAN) WHILE ON A SLING OPERATION, PILOT NOTICED A FLUID LEAKING FROM THE BELLY IN THE CARGO MIRROR. THE AIRCRAFT WAS LANDED IMMEDIATELY AND IT WAS DISCOVERED THAT FUEL WAS LEAKING FROM A FUEL LINE FITTING. THE ENGINE WAS SHUT DOWN AND THE LINE WAS CHECKED FOR SDR YTRR099306Fuel Control · failedFUEL CONTROL PURCHASED NEW. ENGINE DEACCELERATED TO 88 PERCENT AND WAS NOT ABLE TO RECOVER.SDR KBM2004F00244Skid · corrodedREMOVED LANDING GEAR ASSY DUE TO RT SKID FAILURE, JUST AFT OF AFT CROSS TUBE MOUTH, FOUND HEAVY CORROSION IN AREA OF FAILURE. APPEARED TO BE RELATED FILL LENGTH SKID SHOES. REPLACED SKID GEAR WITH AAI STC NR SH139250, THIS GEAR WAS REMOVED SERVICEABLE FROM ASDR CA041029006Tach Generator · unserviceableOUT OF THE FOUR MOUNTING PAD EARS, ONE EAR WAS FOUND COMPLETELY BROKEN OFF.SDR ALG2004F00067Latch · crackedDURING FLIGHT, LT REAR PASSENGER DOOR POPPED OPEN IN FLIGHT AC LANDED ON SS154 THE DOOR WAS SHUT AND SECURED. AFTER TAKE OFF THE DOOR POPPED OPEN AGAIN AIRCRAFT LANDED. THE MECHANIC FOUND A 3 INCH CRACK ABOVE THE LOWER LATCH. THE DOOR WAS REMOVED AND REPLACSDR CA041027001Drag Pin · wornAFT CAST SURFACE OF DRAG PIN ASSY THAT IS PART OF M/R GEARBOX CONTACTED YOKE OF ISOLATION MOUNT. CONTACT DUE TO EXCESSIVE CASTING MATERIAL AFT OF BEARING BORE. COMPONENT SHOP RECEIVED AN ISOLATION MOUNT FOR REPAIR THAT HAD FRETTING/CONTACT MARKS ON YOKE. MARKSDR CA041029005Bearing · spalledTHE AIRCRAFT WAS ON A FLIGHT WHEN A TRANSMISSION CHIP LIGHT OCCURRED, APPROPRIATE ACTION WAS TAKEN. THERE WAS FERROUS METAL FOUND ON THE TRANSMISSION OIL MONITOR AND TRANSMISSION CHIP DETECTORS. THE TRANSMISSION AND MAST WERE REMOVED FOR INVESTIGATION. THE MSDR 2004FA0000850Turbine Wheel · failedDURING GROUND RUN, AFTER SCHEDULED TURBINE REPLACEMENT, LEAK CHECKS HAD BEEN COMPLETED AT IDLE POWER. WHILE ADDING POWER, AT ABOUT 85 PERCENT N2 THE NR3 TURBINE WHEEL EXPERIENCED AN UNCONTAINED FAILURE DESTROYING THE ENGINE AS WELL AS DAMAGING THE COWLING, ROSDR 2004FA0000849Turbine Wheel · failedDURING GROUND RUN, AFTER SCHEDULED TURBINE REPLACEMENT, LEAK CHECKS HAD BEEN COMPLETED AT IDLE POWER. WHILE ADDING POWER, AT ABOUT 85 PERCENT N2 THE NR 3 TURBINE WHEEL EXPERIENCED AN UNCONTAINED FAILUE DESTROYING THE ENGINE AS WELL AS DAMAGING THE COWLING, ROSDR JJWA0059046Blade · failedTAIL ROTOR BLADE, SENT TR BLADES INSPECTION, BLADE FAILED SKIN THICKNESS TEST WAS .0064 ON UPPER SURFACE, NOT REPAIRABLE. WARRANTY CLAIM.SDR IIFR004FAngle · crackedLT LOWER CAP ANGLE PN 206-031-200-037 CRACKED 5.250 IN. MEASURED FROM THE FORWARD TIP OF THE CAP ANGLE ON THE HORIZONTAL SECTION AND OF THE CAP ANGLE ON THE HORIZONTAL SECTION AND 5.625 IN. FROM THE FORWARD TIP OF THE CAP ANGLE ON THE VERTICAL SECTION GOING SDR CA041007002Tail Rotor · misrigged(CAN) TAIL ROTOR FLAPPING ANGLE FOUND SET TO 18 DEGREES INSTEAD OF THE CORRECT ANGLE OF 12 DEGREES ALLOWING POSSIBLE COTACT WITH TAILBOOMSDR KBM2004F00232Drag Pin · crackedSPIKE MOUNT CRACKED JUST FORWARD OF DOG LEG RADIUS. CAUSE UNKNOWN, SENT FOR EVALUATION. INSTALLED SERVICEABLE SPIKE MOUNT.SDR CA041109006Drag Pin · unserviceable(CAN) DURING INSPECTION THE DRAG LINK BEARING WAS FOUND SMOKING. THIS A NEW STYLE IN WHICH BEARING AND NOT WHOLE ASSEMBLY IS REPLACED. NEW BEARING INSTALLEDNOTE: THIS STYLE OF BEARING WAS INTRODUCED THROUGHT B206-00-173 TO ELIMINATE THE PROBLEM WITH THE STAKINSDR CA050216010Hanger Assy · rotated(CAN) PILOT REPORTED A HIGH FREQUENCY VIBRATION. UPON INVESTIGATION, THE BEARING IN THE FORWARD HANGER ASSEMBLY OF THE OIL COOLER BLOWER WAS FOUND TO BE ROTATING. BLOWER ASSEMBLY REPLACED.SDR CA041109007Check Valve · unserviceable(CAN) UPON TROUBLESHOOTING FOR STARTING SNAG, FOUND THAT FUEL WASN'T BEING DELIVERED TO THE FUEL NOZZLE. REPLACED CHECK VALVE. THE REMOVED VALVE WAS FOUND TO HAVE A CRACKING PRESSURE OF APPROXIMATELY 15 PSI.SDR KBM2004F00222Fcu · inaccurateFUEL SENDER NOT TRANSMITTING CORRECT QUANTITY. INSTALLED NEW UNIT.SDR ALG2004F00063Drain · openAFTER TAKE OFF, WAS NOTIFIED BY RADIO OF LEAKING FUEL IN FLIGHT, LANDED, EVACUATED PASSENGERS AND PERFORMED EMERGENCY SHUTDOWN, NOTIFIED MAINTENANCE. MAINTENANCE FOUND EXTERNAL FUEL FILTER DRAIN OPEN, CLOSED DRAIN, COMPLIED WITH GROUND RUN LEAK CHECK, NO DEFESDR CA040917005Mount · misaligned(CAN) LOWER MOUNTING BASE WAS FOUND TO BE INSTALLED 90 DEGREES FROM CORRECT ALIGNMENT TO ALLOW ENGAGEMENT OF LOCK PIN.SDR YTRR097021Fuel Control · malfunctionedENGINE WOULD NOT ACCELERATE ABOVE IDLE. REPLACEMENT OF THE FUEL CONTROL UNIT ALEVIATED THE PROBLEM. THE FUEL CONTROL WAS OVERHAULED.SDR CA041223005Pitch Link · cracked(CAN) DURING A SCHEDULED 100-HOUR INSPECTION TWO (2) VERTICAL CRACKS WERE FOUND ON A MAIN ROTOR PITCH LINK. THE CRACKS (APPROX. .180)SDR CA040901002Drive Assy · damaged(CAN) TWICE WITHIN A 20 HOUR PERIOD,THE YELLOW TEMP INDICATERS CHANGED COLOUR, AND GREASE WAS LEAKING FROM THE FWD. END OF THE DRIVE SHAFT. THE SHAFT WAS REPLACED AND NO FURTHER PROBLEMS HAVE BEEN REPORTED.THE SPHERICAL COUPLING WAS REPLACED ON THE PROBLEM SHASDR ALG2004F00048Relay · overheatedIN FLIGHT CREW AND PASSENGERS SMELLED SMOKE, LANDED AT FIRST AVAILABLE PLATFORM (WC 620) AND AFTER LANDING AIRCRAFT EXPERIENCED TOTAL ELECTRICAL FAILURE. REMOVED AND REPLACED AIRCRAFT BATTERY AND BATTERY RELAY, SET GENERATOR VOLTAGE AND INSPECTED WIRES IN AIRSDR YTRR096994Fuel Control · malfunctionedFUEL CONTROL WAS OVERHAULED. INSTALLED AND AFTER 164.1 TSO THE START ACCELERATE COULD NOT BE ADJUSTED AND THE ENGINE WOULD HANG AT 60 PERCENT N1 AND COULD NOT BE INCREASED FURTHER.SDR YTRR096993Governor · malfunctionedTHE GOVERNOR WAS INSTALLED AND AFTER 65.8 HOURS N2 WAS NOT ADJUSTABLE ABOVE 97 PERCENT. THE GOVERNOR WAS REPLACED AND THE PROBLEM DISAPPEARED.SDR KBM2004F00196Resistor · intermittentFUEL QUANTITY READING INTERMITTENTLY 35-40 GALLON. REPLACED R1 AND R2 RESISTOR WITH A NEW UNIT AND OPS CHECKED GOOD.SDR CA040819002Restraint · delaminated(CAN) DURING DAILY INSPECTION IT WAS NOTED THE FLAP RESTRAINT HAD BECOME DELAMINATED AT BEARING HOUSING.SDR CA040817007Pump · malfunctioned(CAN) ON STARTUP OF THE ENGINE THERE WAS A HOWLING NOISE COMING FROM THE ENGINE. THE NOISE WOULD ONLY BE ON STARTUP AND WOULD GO AWAY ONCE THE ENGINE WAS RUNNING. IT WAS DETERMINED THAT THE NOISE WAS COMING FROM THE FUEL PUMP AND WAS REPLACED.SDR 2004F00356Bleed Valve · failedWHILE HOVERING FOR TAKEOFF A LOUD BANG CAME FOR THE ENGINE COMPARTMENT FOLLOWED BY A TORQUE FLUCTUATION AND A RIGHT YAW. CHECKED ALL THE SYSTEMS ALL IN GREEN AND THEN HOVERED TO PARKING. MAINTENANCE INSPECTED COMPRESSOR FOR FOD AND LEAKS, NO DEFECTED NOTED. SDR YTRR096996Governor · failedGOVERNOR WAS OVERHAULED AND AFTER 98.3 HRS TSO, THE ENGINE EXPERIENCE AN OVERSPEED THAT WAS CAUSED BY A HIGH SIDE FAILURE.SDR CA041110003Blade · cracked(CAN) DURING DI, THE TIP BLOCK WAS FOUND CRACKED ADJACENT TO IMPACT MARK.SDR CA050616008Seal · worn(CAN) FORWARD PTO SEAL REMOVED DUE TO OIL TRANSFER FROM ENGINE TO TRANSMISSION. UPON SEAL REMOVAL IT WAS FOUND THE IB SEAL LIP HAD BEEN FOLDED UNDER THE SEAL AT 2 LOCATIONS, APPROXIMATELY 1 INCH EACH. THE TENSION SPRING FROM THE SEAL HAD STAYED ON THE SEAL, ASDR CA040811009Clamp · missing(CAN) ON DECENT PILOT FELT A TAP ON THE TAIL ROTOR PEDALS, AND LOOKED INTO HIS SLINGING MIRROR AND DETERMINED THAT THE LT BEAR PAW WAS MISSING. AFTER LANDING HE NOTICED DAMAGE TO TAIL ROTOR BLADES, AND VERTICLE FIN. ON INSPECTION, IT WAS FOUND THAT A CLAMP TSDR CA040812005Strap · cracked(CAN) FOUND STRAP CRACKED AT 100 HOUR INSPECTION. PART REPLACED.SDR CA040812007Skin · cracked(CAN) DURING 100 HOUR INSPECTION, CRACK IN PAINT FORWARD OF NR3 HANGAR SUPPORT BRACKET. BRACKET REMOVED, PAINT REMOVED AND AREA FLUORESCENT PENETRANT INSPECTED. CRACK APPROXIMATELY 1.5 INCH.SDR CA040719001Battery · overheatedTHE 'BATTERY TEMP' WARNING LIGHT ILLUMINATED ON ROUTE. THE BATTERY WAS TURNED OFF FOR THE REMAINDER OF THE FLIGHT. UPON LANDING AND SHUTTING DOWN , THE PILOT NOTICED THAT THE BATTERY FELT VERY HOT TO THE TOUCH. WHILE TALKING TO THE MAINTENANCE DEPT ON THE PSDR CA041214002Blade · cracked(CAN) THE BLADE HAS A CHORDWISE CRACK AT BLADE STATION 12.64. THE CRACK IS 2.65 IN. (67.3MM) LONG ON THE DATA PLATE SIDE OF THE BLADE AND 0.4 IN. (10MM) LONG ON THE OTHER SIDE.SDR QR92004F00000Adapter · shearedENGINE REMOVED FROM SERVICE FOR ENGINE CHIP LIGHT ILLUMINATION, FOLLOWED BY ENGINE FAILURE DURING PINNACLE LANDING. TEAR DOWN ANALYSIS REVEALED COUPLING ADAPTER SHEARED AT PILOT DIAMETER CAUSING FAILURE. (SO09200408990)SDR CA040708012Drain Valve · leaking(CAN) DURING MAINTENANCE GROUND RUN IAW MM-1-5/27, THE ENGINE FLAMED OUT WHEN THE BOOST PUMPS WERE SHUT OFF. THIS FAILURE WAS REPEATABLE. TROUBLE SHOOTING REVEALED AIR ENTERING THE FUEL SYSTEM THROUGH THE AIRFRAME FUEL FILTER ASSEMBLY DRAIN VALVE. THE AIRFRAMESDR 2004FA0000643Gps · failedON A PILOT TRAINING FLIGHT, SMOKE WAS OBSERVED COMING OUT OF GPS FACE-PLATE AND THE DISPLAY WENT BLANK. CB WAS PULLED AND AIRCRAFT RETURNED TO BASE. AFTER SHUTDOWN, POWER WAS APPLIED TO GPS, OPERATION APPEARED NORMAL, BUT SELF DIAGNOSIS DISPLAYED A (DATA BASSDR CA040621008Powerpack · failedIT APPEARS THAT THE HYDROPACK HAD AN INTERNAL GEAR FAILURE. THE AIRCRAFT HAD NR INDICATIONS BUT NO HYDRAULIC PRESSURE. HYDROPACK WAS CHANGED AND AIRCRAFT RETURNED TO SERVICE.
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