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 = '369D' 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 = '369D' 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 3M3A13040017Actuator · malfunctionedPILOT REPORTED CYCLIC JERKED LEFT WHILE IN FORWARD FLIGHT AND FELT AS IF TRIM WAS IN FULL LEFT POSITION. UPON INITIAL INSPECTION OF AIRCRAFT PERFORMED A FUNCTIONAL CHECK OF TRIM ACTUATORS. CONFIRMED TRIM MOTOR TO BE CORRECTLY CORRESPONDING TO INPUTS MADE TO CYSDR 2025FA0000153Strut · brokenLEFT HAND REAR LANDING GEAR STRUT ASSEMBLY BROKEN AT BRACE ASSEMBLY ATTACHMENT BOLT DURING LANDING. OTHER MINOR DAMAGE TO SURROUNDING AREA OCCURRED. TOTAL TIME ON PART IS UNKNOWN.SDR 2025FA0000101Bulkhead · damagedCRACKS AND BUCKLING FOUND IN BULKHEAD STA 155.75 AND ALONG TAIL BOOM FAIRING AND TURTLE DECK.SDR 2024FA0000309Fitting · wornFOUND CENTER BEAM LANDING GEAR FITTING RETAINER BORE WORN OUT OF LIMITSSDR 3M3A202401060001Unknown · unknownON JANUARY 1ST 2024, N514PA EXPERIENCED AN ENGINE CHIP LIGHT DURING A 135 TOUR FLIGHT. THE PILOT MADE A PRECAUTIONARY LANDING. ALL PASSENGERS WERE REMOVED WITH A SECOND HELICOPTER CARRYING MAINTENANCE PERSONNEL. LARGE CHUNKS OF ROLLER BEARING CAGE MATERIAL WERSDR 2020FA0000360Gear · shearedTAIL ROTOR TRANSMISSION P/N 369D25400 SERIAL NUMBER 1539 WAS RECEIVED FOR UNIT MAKING METAL. UPON INSPECTION AND DISASSEMBLY IT WAS NOTED THAT THE 369D25434 INPUT GEAR SERIAL NUMBER 5304-1950 WAS SHEARED AT THE LOCATION OF THE ROLL PIN INSTALLATION POINT ON TSDR X2RL2020061800001Bearing · seizedPILOT COMPLAINED OF STICKY T/R PEDAL MOVEMENT, FOUND T/R SWASHPLATE PIVOT BEARING SEIZED. REMOVED T/R SWASHPLATE AND SENT IT FOR REPAIR, INSTALLED SERVIVEABLE UNIT. WE HAVE 7 INCIDENTS IN THE LAST YEAR WITH THESE BEARINGS 369A7951-13 SEIZING, ALL UNDER 200 HOSDR X2RA2020061500001Bearing · seizedPILOT NOTICED THE COLLECTIVE MOTION WAS RATCHETY. INSPECTION FOUND THAT THE BEARINGS, SELF-ALIGNING, WERE SEIZED UP SOLID. REPLACEMENT OF THE LINK ASSY CURED THE ISSUE. THE LINK HAD BEEN INSTALLED NEW, 3 DAYS BEFORE WITH 11.4 HOURS TSN AT REMOVAL.SDR 2019FA0000298Coupling · brokenFAILURE OF THE AFT COUPLING. FRACTURE OF COUPLING. SEE ENGINEERED PRODUCTS 8130-3 WORK ORDER # MDI1167 DATED MARCH 20, 2018 FOR PART DETAIL.SDR K2DA2019052800001Bleed Valve · stuckPILOT PERFORMED ENGINE POWER ASSURANCE CHECK AT 80% TQ AND 2,000 FT AGL AND REPORTED A +1* ON THE POWER CHECK WHICH WAS A SIGNIFICANT DIFFERENCE IN THE POWER CHECK TAKEN THE DAY PRIOR (+30). UPON LANDING, MAINTENANCE PERSONNEL WERE CALLED AND IT WAS DISCOVEREDSDR CA190326009Compressor · fod(CAN) THE RENTAL ENGINE RAN HOT FROM THE FIRST DAY I FLEW IT. THE STARTS WHERE VERY SLOW BUT STILL IN PARAMETERS. THE TOT WAS APPROX. 580 DEGREES AT GROUND IDLE AND 580-600 AT FLIGHT IDLE WITH 18-20 PSI TQ. THE SECOND STARTS WERE OK, THEY WOULD BE ON THE HOTTESDR CA190507012Stator · broken(CAN) UPON ROUTINE INSPECTION OF COMPRESSOR CASE HALFS (WHILE ENGINE WAS REMOVED FROM AIRFRAME) IT WAS FOUND THAT ONE OF THE 6TH STAGE STATOR BLADES HAD BROKEN OFF ONE OF THE CASE HALFS AND BEEN INJESTED INTO THE COMPRESSOR CENTRIFUGAL COMPRESSOR SECTION, AND SDR 2019FA0000028Uniball · defectiveHELICOPTER LEFT A WARM HANGER ON A COLD MORNING , FLEW OUT TO JOBSITE, SAT FOR ABOUT 30 MINS IN 11 DEGREES F WEATHER, AND COLLECTIVE WOULD NOT GO UP FROM BOTTOM OF TRAVEL STOP. HEAT WAS APPLIED TO THE UNI-BALL PART OF SWASHPLATE AND COLLECTIVE WOULD OPERATE ASSDR MKHR2018091300000Bolt · shearedDURING CRUISE FLIGHT THE PILOT EXPERIENCED AN EXCESSIVE TAIL ROTOR VIBRATION. THE PILOT THEN EXECUTED A PRECAUTIONARY LANDING. WHEN CREW ARRIVED TO INVESTIGATE THE VIBRATION THE INITIAL DISCOVERED WAS THAT THE OUTBOARD TAIL ROTOR FORK BOLT WAS SHEARED.SDR 2018FA0000463Exhaust Pipe · crackedEXHAUST PIPE CRACKED ON THE AFT LOWER MOUNT FLANGE ALLOWING AFT MOUNT SADDLE TO SLIDE OUT OF POSITION. CRACK OCCURRED 79.4 FLT HRS FROM NEW.SDR X2RA2018F00000Fuel Control · failedPILOT EXPERIENCED DELAYED HOT AND ERRATIC STARTS. FOUND PLAY IN THE POINTER ROD, THIS WOULD AFFECT THE START SCHEDULING. THE SLOP IS WHERE THE POINTER ROD ENGAGES THE THROTTLE ARM. AT TIMES THE THROTTLE SEEMED AS IF IT WERE HITTING A STOP. FIRST START OK, SDR K2DA20160707146Bearing · spalledAIRCRAFT PERFORMED A PRECAUTIONARY LANDING FOR AN ENGINE CHIP LIGHT WHILE CONDUCTING AN AIR TOUR. THERE WERE NO SECONDARY INDICATIONS AND THE AIRCRAFT LANDED SAFELY. AFTER CLEARING THE CHIP LIGHT IAW THE MANUAL, THE AIRCRAFT WAS FLOWN BACK TO BASE. IT WAS DSDR K2D2016F00002Bearing · damagedTHE COMPRESSOR WAS REMOVED FROM THE ENGINE GEARBOX AND IT WAS DISCOVERED THAT THE COMPRESSOR SPUR ADAPTER GEARSHAFT JOURNAL HAD A WORN AREA WHERE METAL WAS REMOVED. AFTER INSPECTION OF THE GEARBOX, IT WAS DETERMINED THAT THE 2.5 BEARING HAD FAILED AND WAS THESDR CA160215013Support · broken(CAN) DURING INSPECTION OF FRONT PEDAL SUPPORT IT WAS NOTED THAT BOTH UPPER TANGS OF THE LEFT PEDAL SUPPORT WERE BROKEN OFF. THERE MAY BE SOME INDICATIONS THAT A TANG CRACKED AND THEN SNAPPED ALSO BREAKING THE OTHER UPPER TANG. THE LOWER TANGS OF THE PEDAL SUPSDR CA160120019Abrasion Strip · missing(CAN) MAIN ROTOR BLADE ABRASION STRIP SEPARATED FROM BLADE WHILE IN FLIGHT. VIBRATION CAUSED BY IMBALANCED ROTOR DISK REQUIRED RETURN TO BASE. ACFT WAS SHUTDOWN. NO FURTHER DAMAGE TO ACFT NOTED. REMAINING 4 ROTOR BLADES HAVE SAME HRS FLOWN AND HAVE BEEN RESDR CA160118014Snap Ring · damaged(CAN) ENGINE CHIP LIGHT ILLUMINATED DURING FLIGHT. UPON ENGINE DISASSEMBLY DISCOVERED THE SNAP RING THAT HOLDS THE SPUR ADAPTER GEARSHAFT TO THE BACK OF THE COMPRESSOR TO BE MANGLED. SNAP RING GROOVE HAD SINCE WORN FLAT.SDR K2D2016F00000Blade · delaminatedON SUNDAY 12 13 15, A TAIL ROTOR BLADE, PN 500P3100-105, SN C922, 491.6 TSR, WAS FOUND IN A DELAMINATED STATE, DURING A PREFLIGHT INSPECTION. THE LE HAD DELAMINATED FROM THE BLADE ABOUT 2" IN LENGTH. PROBABLE CAUSE OF THE DELAMINATION IS IMPROPER CURE TIME FSDR K2DA2015121501Blade · delaminatedDURING PREFLIGHT INSPECTION, FOUND TAIL ROTOR BLADE, PN 500P3100-105, SN C922 LE DELAMINATED FOR APPROX 2 INCHES ON BOTH SIDES OF THE BLADE.SDR CA150917008Blade · debonded(CAN) DURING SCHEDULED INSPECTION THE L/E EROSION STRIP WAS FOUND DEBONDED DURING CLEANING PRIOR TO INSPECTION, AS IT CRINKLED WITH FINGER PRESSURE.SDR CA150812006Chip Detector · failed(CAN) DURING SCHEDULED INSPECTION CHIP DETECTOR PLUG, P/N 23088398, WAS FOUND TO HAVE NO MAGNETIC PROPERTIES. THERE ARE NO INSTRUCTIONS FOR CONTINUED AIRWORTHINESS REQUIRING CHECK OF THE MAGNETIC PROPERTIES OF THE PLUG.SDR CA150812005Bracket · cracked(CAN) STROBE BRACKET CRACKING AT JUST AFT OF MOUNTING POINT. IF IT DEPARTED THE AIRCRAFT THE STOBE ASSY WOULD GO INTO THE TAIL ROTOR.SDR MKHA20150507001Tail Rotor · brokenDURING A FLIGHT THE PILOT EXPERIENCED EXCESSIVE VIBRATION. THE PILOT MADE A PRECAUTIONARY LANDING & NOTIFIED MX. MX DISCOVERED THE PITCH HORN ON THE OTBD TAIL ROTOR BLADE WAS BROKEN OFF.SDR CA150331007Blade · damaged(CAN) DURING REGULAR 100HR INSPECTION, TAP TEST OF THE MAIN ROTOR BLADE DISCOVERED A VOID. THE BLADE HAS BEEN SENT FOR REPAIR.SDR CA141127008Valve · failed(CAN) DUE TO THE DURATION OF THE FLIGHT, PILOT FELT HE WAS GETTING AN ERRONEOUS FUEL QTY READING AND DECIDED TO LAND AND REFUEL. UPON REMOVING THE FUEL CAP, HE IMMEDIATELY OBSERVED THAT THE INTERNAL FUEL CELL HAD COLLAPSED AS IT WAS MOSTLY BLOCKING THE FUEL FSDR CA141022010Blade · debonded(CAN) DURING INSPECTION CRACKS WERE NOTED IN THE SEALANT COVERING THE ROOT FITTING TO DOUBLE ADHESIVE. SEALANT WAS REMOVED TO EXPOSE THE ADHESIVE BOND LINE. ROOT FITTING ATTACH BOLTS WERE LOOSENED TO RELIEVE THE FITTING. A DISBOND IN THE ROOT FITTING TO DOUSDR CA140903012Bearing · rough(CAN) AFTER LANDING AND DURING ENGINE WIND DOWN, A LOUD SQUEAL WAS HEARD COMING FROM THE AFT OF THE HELICOPTER. IT WAS DETERMINED THAT THE NOISE WAS EMANATING FROM THE TAIL ROTOR PITCH CONTROL BEARINGS. THE TAIL ROTOR PITCH CONTROL LINKS WERE DISCONNECTED ANSDR CA140604010Tube · melted(CAN) DISCOVERED DURING ROUTINE PITOT STATIC TEST THAT SOME WELL INTENTIONED PERSON HAD PROTECTED THE STATIC LINE, ENGINE OIL PRESSURE LINES TOGETHER IN SPI-RAP WHICH MADE THE COLLECTION OF PIECES TOO LARGE FOR THE SPACE PROVIDED. THIS PREVENTED THE HEATER DUSDR CA140423011Bolt · unserviceable(CAN) T/R GEARBOX OIL WAS DARK AND EVIDENCE OF BLACK PASTE AND METAL ON CHIP PLUG. IT WAS DECIDED TO R & R T/R GEARBOX AND IN THE PROCESS OF DOING SO IT WAS DISCOVERED THAT THE COUPLING BOLT ATTACHING THE T/R DRIVESHAFT COUPLING TO THE T/R GEARBOX INPUT GEAR SSDR CA140217004O-Ring · missing(CAN) THE OVER RUNNING CLUTCH WAS PURCHASED AS AN EXCHANGE UNIT. THIS UNIT WAS INSTALLED AT TTAF 16552.9 HRS. THE INSPECTION CRITERIA IS A VISUAL OIL CHECK EACH 100 HRS, 300 HR HOOK TIME INSPECTION AND A 1800 HR OVERHAUL PERIOD. THIS UNIT AT INSTALL WAS TSO OFSDR CA140108003Arm · seized(CAN) DURING AN UNSCHEDULED BELL CRANK CHANGE, IT WAS DISCOVERED THAT THE GOVERNOR ARM WAS SEIZED. A RENTAL GOVERNOR WAS INSTALLED WHILE THIS UNIT GOES FOR REPAIR. INSPECTION OF THE CONTROL LINKAGE INDICATES THAT THE SPRING ROD PROTECTION SYSTEM HAD BEEN IN USSDR CA140108002Damper · collapsed(CAN) WHILE ATTEMPTING THE FIRST START OF THE DAY THE ACFT SUDDENLY SHIFTED TAIL LOW AND TO THE RIGHT. IT WAS DETERMINED THAT THE RT REAR LANDING GEAR DAMPER HAD COLLAPSED TO THE FULLY RETRACTED POSITION AND OIL WAS LEAKING FROM THE PISTON CAP AREA. THE DAMPSDR CA131119005Nut · failed(CAN) DURING SCHEDULED INSPECTION, A NUT WAS FOUND CRACKED. ON REMOVAL, THE NUT CAME APART IN TWO PIECES.SDR CA130930009Swashplate · damaged(CAN) DURING REMOVAL OF RENTAL TAIL ROTOR GEARBOX, IT WAS DISCOVERED THAT 1 OF THE DRIVE SPLINES FOR THE TAIL ROTOR SWASHPLATE WAS MISSING. THE RENTAL GEARBOX HAD BEEN INSTALLED FOR 40 HOURS AND WHEN IT WAS INSTALLED THE TAIL ROTOR SWASHPLATE HAD NO SIGNS OF SDR 2013FA0000650Bearing · failedPILOT HEARD UNUSUAL NOISE DURING START, JUST BEFORE IGNITION, 10-12 PERCENT OF N1. DESCRIBED NOISE AS A "RUMBLING-GEAR TEETH OUT OF MESH" SOUND FROM ENGINE ACCESSORIES GEARBOX. MAGNETIC METAL DETECTORS WERE FUNCTIONING BUT THE CAUTIONARY LIGHT IN THE COCKPISDR CA130925004Gearbox · making metal(CAN) TAIL ROTOR GEARBOX CHIP LIGHT ILLUMINATED, THE PILOT RETURNED TO STAGING. MAINTENANCE INSPECTED THE CHIP PLUG AND DISCOVERED A SMALL NR OF CHIPS, CLEANED, REINSTALLED AND FLYING RESUMED. CHIP LIGHT RETURNED THE NEXT DAY AND THE TAIL ROTOR GEARBOX WAS CHASDR 2013FA0000329Bracket · brokenCOLLECTIVE BUNGIE BRACKET BROKE IN FLIGHT. PILOT MADE A RUN ON LANDING WITH MINIMAL COLLECTIVE CONTROL.SDR CA130405009Swashplate · cracked(CAN) T/R SWASHPLATE REMOVED FROM ACFT FOR ROUTINE MAINTENANCE. DURING INSPECTION, NUMEROUS ROTATING SWASHPLATE DRIVE SPLINES WERE FOUND TO BE CRACKED AND SOME WERE BROKEN AWAY.SDR X33A2012121100001Fairing · missingTHE PILOT FELT TWO THUMPS AND A LOW FREQUENCY BUZZ FOR ONE SECOND. RETURNED TO BASE MECHANIC PERFORMED A VISUAL INSPECTION, REVEALING THAT THE MAIN RROTER FAIRING WAS MISSING AND THE SUPPORT STAR WAS DAMAGED. FURTHER INSPECTION IAW CHAPTER 62 TABLE 602, REVSDR CA121011011Sprag Clutch · damaged(CAN) DURING THE 100 HOUR INSPECTION, THE ENGINEER NOTICED THAT THE OIL IN THE CLUTCH WAS VERY DARK. HE REMOVED THE ASSY AND DISASSEMBLED THE CLUTCH. THE SPRAG ELEMENTS WERE BROKEN DOWN FROM THE TOP.SDR CA121004005Tube · broken(CAN) DURING FLIGHT THE PILOT FELT A RELEASE OF PRESSURE IN THE CYCLIC CONTROL AS HE WAS APPLYING PRESSURE AND TRIMMING THE CYCLIC AFT. AFTERWARDS HE WAS UNABLE TO ACTIVATE THE LONGITUDINAL TRIM ACTUATOR. HE FLEW BACK TO BASE AND UPON EXAMINATION OF THE TRIMSDR CA120716014Strap · torn(CAN) THE VELCRO STRAP SECURING THE ELT TO THE BASE SHOWS UV DETERIORATION. STRAP WAS VERY WEAK, WITH RIPPING ACCOMPLISHED VERY EASY. THESE ELT`S ARE MOUNTED IN FULL VIEW OF THE SUN THROUGH THE BUBBLE. STRAP REPLACED WITH SERVICEABLE.SDR 2012FA0000296Fcu · inoperativeWHILE IN FLIGHT, ACFT RPM`S AND N2 CLIMBED QUICKLY. RAISED COLLECTIVE AND ROLLED THROTTLE DOWN UNTIL THE RPM`S STABILIZED. ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. TROUBLESHOT SYS, FOUND THE FUEL CONTROL WAS NOT FUNCTIONING PROPERLY. A REPLASDR CA120424005Strut · broken(CAN) AFTER HELICOPTER WAS LOADED AND STARTED THE GEAR SPREAD AND A BANG WAS HEARD, UPON VISUAL INSPECTION, THE RT AFT STRUT WAS FOUND TO BE BROKEN WHERE THE DRAG BRACE ATTACHES TO THE LANDING GEAR STRUT. STRUT WAS REPLACED WITH NEW AND RETURNED TO SERVICE.SDR CA120215011Bearing · worn(CAN) PILOT REPORTED SUDDEN HIGH FREQUENCY VIBRATION DURING FLIGHT. ABORTED FLIGHT, LANDED. INSPECTION REVEALED OIL COOLER BLOWER BEARING WITH EXCESS WEAR. BLOWER ASSY REPLACED. NO VIBRATION NOTED ON RETURN TO SERVICE.SDR CA120123006Swashplate · worn(CAN) DURING A REGULAR INSPECTION THE TAIL ROTOR SWASHPLATE BEARING WAS TURNED BY HAND AND FOUND TO BE ROUGH. THE TAIL ROTOR SWASHPLATE WAS REMOVED FROM SERVICE AND A SERVICEABLE UNIT WAS INSTALLED.
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