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 CA061025005Cartridge · intermittent(CAN) ABOVE 7000 FEET BOOST PUMP LIGHT WOULD COME ON. BELOW 7000 FEET WARNING LIGHT WOULS EXTINGUISH. BOOST PUMP CARTRIDGE P/N 1C27 REPLACED. (TC NR 20061025005)SDR CA060829001Fitting · corroded(CAN) DURING INSPECTION, A LEAK WAS DISCOVERED IN THE HYDRAULIC SYSTEM PRESSURE SIDE CROSS FITTING (AN 937-D6). DISASSEMBLY REVEALED CORROSION AT MATING SURFACE OF O-RING AND CROSS. PART REPLACED WITH NEW. O-RINGS AND RETAINING RING REPLACED. SYSTEM SERVICED SDR CA061121002Magnetic Seal · leaking(CAN) MAIN ROTOR GEARBOX MAGNETIC SEAL HAS EXCESSIVE LEAKAGE FROM MAIN INPUT SEAL. (TC NR 20061121002)SDR CA060818005Case · eroded(CAN) AIRCRAFT WAS IN FOR AN INSPECTION. THE COMPRESSOR CASE HALVES HAD 23 HOURS LT TO A 1750 INSPECTION. MFG REQUESTED THAT WE CARRY OUT THE INSPECTION. IT WAS FOUND THAT THE 2ND AND 3RD STAGE STATOR BLADES WERE SO UNDER CUT FROM EROSION (NEAR THE ROOT OF THESDR YTRR110586Bulkhead · crackedTAIL ROTOR GEARBOX CASTING PANEL & BULKHEAD ON TAILBOOM ASSEMBLY WAS FOUND CRACKED DURING ROUTINE INSPECTION. REPLACED PANEL & CASTING.SDR CA060725006Governor · inoperative(CAN) UNIT HAD ABOUT 25.0 HOURS THIS INSTALL. PILOT REPORTED THAT GOVERNOR WOULD BLEED OFF IN FLIGHT BY 4 TO 5 PERCENT THEN COME BACK TO NORMAL AFTER A FEW SECOND 10 TO 15 SECONDS. THEN IT WOULD BE FINE FOR SOME TIME. UPON REPORTING THIS THE AIRCRAFT WAS REMOSDR CA060801004Fitting · cracked(CAN) A CRACK WAS FOUND FROM THE AFT TOP RIVET HOLE. THE CRACK STARTS AT THE TOP OF THE FITTING AND TRAVELS DOWNWARD THROUGH THE RIVET HOLE AND APPROXIMATELY .2500 FURTHER. (TC NR 20060801004)SDR KBM2006F00233Hose · leakingFREE WHL RETURN HOSE ASSY (FREE WHL TO FIREWALL) LEAKING. REMOVED AND REPLACED. (K)SDR CA060622003Support · corroded(CAN) FIN ATTACH POINTS WERE BEING INSPECTED AS PER ASB 206-06-107, CF2006-12. A LARGE CORROSION PIT WAS FOUND ON THE BOTTOM BOLT HOLE. THE SUPPORT INSTALLATION IS TO BE REPLACED AS PER THE ASB WITH A ONE-PIECE CASTING. (TC# 20060622003)SDR KBM2006F00218Pressure Switch · inoperativeSWITCH INOPERATIVE, CAUTION LIGHT FOR FUEL PRESSURE, DID NOT ILLUMINATE WHEN AFT SWITCH IS IN OFF POSITION, REMOVED AND REPLACED. (K)SDR KBM2006F00217Sump · sticksFUEL SUMP, UNIT STICKS OPEN, REMOVED AND REPLACED. (K)SDR CA070227009Control Lever · stiff(CAN) LEVER CONTROL LEVER HARD TO MOVE ON A FUNCTIONAL CHECK. (TC NR 20070227009)SDR KBM2006F00206Bushing · wornBLEED VALVE, VANE BUSHING WORN, HIGH OPERATIONAL TOT, REMOVED AND REPLACED (K)SDR KBM2006F00216Scroll · crackedENGINE COMPRESSOR SCROLL FITTING FOR HEATER DEMISTER IS CRACKED. BLEED AIR SYSTEM, REMOVED AND REPLACED. (K)SDR CA060605005Skid · corroded(CAN) DURING A ROUTINE 300 HR INSP OF THE AC, IT WAS NOTED THAT A SMALL PIECE OF PAINT HAD FALLEN OFF OF THE LOWER AFT END OF THE TAIL SKID ASSY, AT THE LOWER WELD BEAD JOINT. UPON FURTHER INVESTIGATION, IT WAS NOTED THAT A SMALL HOLE (APPROX .1875) WAS PRESENSDR KBM2006F00215Coupling · unserviceableCOUPLING, UNIT INSERVICEABLE, REMOVED AND REPLACED. (K)SDR CA060605008Longeron · cracked(CAN) DURING A ROUTINE 300 HR INSP, A CRACK WAS FOUND ON THE LONGERON ABOVE THE LT REAR PASSENGER DOOR, AT THE FWD ATTACHMENT TO THE ROLLOVER BULKHEAD. THE CRACK ORIGINATED AT THE ATTACHING RIVETS. THE LONGERON WAS REPLACED WITH A NEW PIECE, AND THE AIRCRAFT WSDR CA060605006Web · cracked(CAN) DURING A ROUTINE 300 INSP ON THE AIRFRAME, A CRACK WAS NOTED ON UPPER AFT SECTION OF THE SEAT WEB ASSY. THIS AREA IS PRONE TO STRESS AND CRACKS WHEN THE SEAT PANEL (THAT IS ATTACHED TO IT) IS REMOVED, AND NO SUPPORT IS ADDED TO THE TOP OF THIS WEB ASSY. SDR CA060606009Control Cable · broken(CAN) CABLE BROKE APPROXIMATELY 9.5 FROM END. (TC NR 20060606009)SDR KBM2006F00214Pressure Switch · intermittentFUEL PRESSURE CAUTION LIGHT INTERMITTENT, REMOVED AND REPLACED. (K)SDR KBM2006F00163Coupling · defectiveCOUPLING, UNIT HAS SHARP EDGES ON SPLINE, REMOVED AND REPLACED. (K)SDR KBM2006F00152Indicator · faultyFUEL QUANTITY INDICATOR, LIGHTS WILL NOT ILLUMINATE, REMOVED AND REPLACED. (K)SDR KBM2006F00151Indicator · malfunctionedDUAL TACH, GAUGE LIGHT WILL NOT ILLUMINATE, REMOVED AND REPLACED. (K)SDR KBM2006F00150Indicator · stuckTACH INDICATOR, NO INDICATION, NEEDLE STUCK, REMOVED AND REPLACED. (K)SDR KBM2006F00149Regulator · inoperativeAC BATTERY LOW POWER, REMOVED AND REPLACED. REGULATOR MALFUNCTIONED, REMOVED AND REPLACED. (K)SDR KBM2006F00148Drive Shaft · overtempMDS TEMP INDICATES IN FWD COUPLING, SHOW OVERTEMP CONDITION. DISASSEMBLED, CLEAN AND INSPECTED FOR OVERTEMP. NO DEFECT FOUND THIS TIME. REASSEMBLED WITH 8 INNER GREAT BOLT (PN NGS 660110, PO 2314)(4 NGS M8324811-235),( 2 EA 206-040-272-001)(4 EA MS210043-4)SDR KBM2006F00125Indicator · leakingAIRSPEED INDICATOR LEAKS, 500 FT/ MIN. REMOVED AND REPLACED. (K)SDR JJWA108403Housing · corrodedENGINE OIL LEAK FROM OIL FILTER HOUSING CAP FOUND TO BE CAUSED BY SEVERE CORROSION AROUND CAP RETAINER STUD BASES, WITH MISSING METAL MIGRATED TO O-RING SEAL AREA. INSTALLED TSO: 0.0 PN 23035102 HOUSING ASSEMBLY. RUNUP LEAK CHECKS FOUND PROBLEM RESOLVED. SUGGSDR KBM2006F00124Chin Bubble · crackedCHIN WINDOW HAS SMALL CRACKS NEAR LOWER DRAIN HOLE, REMOVED AND REPLACED. (K)SDR KBM2006F00123Encoder · malfunctionedNO ATITUDE READING AT TRANSPONDER TO ATC. REMOVED AND REPLACED ENCODER. (K)SDR ALG2006F00029Vhf Comm · inoperativeDURING FLIGHT, VHF RADIO DISPLAY WENT BLACK AND WOULD NOT RECEIVE OR TRANSMIT. AC LANDED, MAINTENANCE REMOVED AND REPLACED VHF RADIO, FUNCTION CHECKED GOOD AND RETURNED TO SERVICE. (K)SDR CA060316007Manifold · malfunctionedDURING PILOT TRAINING AIRCRAFT COMPLETED A HYDRAULICS OFF LANDING. HYDRAULIC SWITCH WAS THEN TURNED BACK ON AND THE FORE AND AFT MOVEMENTS CAME BACK HOWEVER THE LATERAL MOVEMENTS DID NOT COME BACK TO NORMAL HYDRAULIC ON. AIRCRAFT WAS THEN SHUT DOWN AND HYDRASDR KBM2006F00112Window · crackedWINDOW, RT CHIN BUBBLE WINDOW IS CRACKED. REMOVED AND REPLACED. (K)SDR KBM2006F00111Window · crackedCO PILOT WINDOW CRACKED, REMOVED AND REPLACED. (K)SDR 2006FA0000716Extinguisher · explodedA NEW 1.25 LB EXTINGUISHER MODEL 344, SN W-968052 CLASSIFICATION 2-B; C WAS INSTALLED IN THE AIRCRAFT ON MARCH 6, 2006. IT WAS REMOVED OVERNIGHT AND REINSTALLED AT 8:50 AM ON MARCH 7, 2006. AS THE HELICOPTER WAS STARTING, THE END EXPLODED OUT OF THE EXTINGUISDR 2006FA0000492Coupling · failedHYDRAULIC PUMP TACH DRIVE COUPLING BRAZE WELDING FAILED, CAUSING COUPLING TO SEPARATE FROM DRIVE GEAR SHAFT. MFG SHOULD CHECK THE STRENGTH OF BRAZE AFTER WELDING. WHEN THIS COUPLING FAILS, LOSS OF ROTOR TACH OCCURS. (K)SDR 2006FA0000491Coupling · failedHYDRAULIC PUMP TACH DRIVE COUPLING BRAZED WELDING FAILED CAUSING COUPLING TO BECOME LOOSE. MFG SHOULD CHECK THE STRENGTH OF BRAZE AFTER WELDING. WHEN THIS COUPLING FAILS, LOST OF ROTOR TACH OCCURS. (K)SDR 2006FA0000490Coupling · separatedHYDRAULIC PUMP TACH DRIVE COUPLING BRAZED WELDING FAILED CAUSING COUPLING TO SEPARATE FROM DRIVE GEAR SHAFT. MFG SHOULD CHECK THE STRENGTH OF BRAZE AFTER WELDING. WHEN THIS COUPLING FAILS, LOSS OF ROTOR TACH OCCURS. (K)SDR KBM2006F00107Tach Generator · failedN2 READING WENT TO -0- IN A SHORT FINAL, REMOVED AND REPLACED TACH GENERATOR. (K)SDR KBM2006F00102Transponder · malfunctionedTRANSPONDER, UNIT INOPERATIVE. DOCS NOT INDICATE MODE C. REMOVED AND REPLACED. (K)SDR CA060222001Line · crackedON REINSTALLATION OF FUEL LINES IN FUEL VALVE COMPARTMENT TUBE ASSY WAS TORQUED AND FERRULE WAS FOUND TO BE CRACKED. TUBE ASSY WAS SUSPECTED TO BE CRACKED ON REMOVAL BUT NO LEAKS DETECTED. LINE REMOVED FROM SERVICE. RECOMMEND BETTER VISUAL INSPECTION OF ALUSDR CA060213002Air Duct · melted(CAN) DURING MAINTENANCE, AN AME NOTICED THAT HE COULD NOT MOVE THE HEATER AIR OUTLET. ON CLOSER INVESTIGATION, HE FOUND THE OUTLET MELTED. NO OTHER DAMAGE WAS NOTED. (TC NR 20060213002)SDR KBM2006F00085Bearing · wornTACH GENERATOR, BAD BEARINGS, REMOVED AND REPLACED. (K)SDR CA060131004Tee Fitting · crackedWHILE IN CRUISE FLIGHT, THE PILOT FELT FEEDBACK SHOCK IN THE CYCLIC CONTROL. THE PILOT ISOLATED HYDRAULICS AND MADE AN UNSCHEDULED LANDING. MAINTENANCE CREW PERFORMED AN INSPECTION OF THE HYDRAULIC FLIGHT CONTROL SYSTEM. A TEE FITTING THE LEFT HAND SERVO ACSDR KBM2006F00045Unknown · unknownENGINE OIL PRESSURE AND TORQUE GAUGE FLUCTUATED AND DROPPED TO ZERO, REMOVED AND REPLACED. (K)SDR KBM2006F00047Pump · low pressureBOOST PUMP LOW PRESSURE, REMOVED AND REPLACED. (K)SDR KBM2006F00046Valve · leakingVALVE ASSY, UNIT LEAKING, REMOVED AND REPLACED. (K)SDR ALG2006F00012Tachometer · inoperativeIN FLIGHT NR INDICATOR DROPPED TO 20 PERCENT. REMOVED ROTOR TACHOMETER AND REPLACED WITH SERVICEABLE UNIT. WORK ACCOMPLISHED IAW MM. (K)SDR KBM2006F00049Radio · malfunctionedVHF RADIO, WHEN MIC IS KEYED THE LIGHTS DIM, REMOVED AND REPLACED. (K)SDR KBM2006F00048Indicator · inoperativeBOWL INDICATOR ASSY, UNITS INDICATOR POPS AT RANDOM. REMOVED AND REPLACED. (K)
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