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 = '206L4' 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 = '206L4' 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 CA080611002Bearing Race · fractured(CAN) THE PUSH-PULL CONTROL ASSY CENTER RACE FRACTURED AS A RESULT OF FATIQUE. THE FRACTURE OCCURED NEAR WHERE THE ASSY WAS LOCATED IN AN INSTALLATION-INDUCED BEND RADIUS.SDR CA080122010Bearing · chafed(CAN) DURING A PHASE INSP, MECHANIC FOUND A CHAFED AREA ON TOP OF THE COLLECTIVE LEVER BEARING EAR P/N 206-010-447-109. FURTHER INSP REVEALED CHAFING AT BOTTOM OF BOTH SWASHPLATE ROTATING RING BEARING EARS. CHAFED AREAS APPROX 0.020-0.040 INCH DEPTH. MECHANICSDR CA071023004Nut · failed(CAN) WHILE INVESTIGATION MAST BEARING PLAY, UNABLE TO REMOVE NUT (BEARING TORQUE). MAST ASSEMBLY SENT TO MFG FOR INVESTIGATION. NEW MAST ASSEMBLY PROVIDED BY MFG. (TC NR 20071023004)SDR CA071023002Nut · loose(CAN) WHILE INVESTIGATING MAST BEARING PLAY. UNABLE TO REMOVE NUT (BEARING TORQUED). MAST ASSY SENT TO MFG FOR INVESTIGATION. NEW MAST ASSY PROVIDED BY MFG (TC NR 20071023002).SDR CA071001002Tube · leaking(CAN) HELICOPTER DEVELOPED FUEL LEAK SITTING IN HANGER. BONDING MATERIAL BETWEEN ALUMINUM FLANGE AND RUBBER TUBE IS ALMOST NON-EXISTENT. THE RUBBER ALSO SEEMS TO HAVE SWELLED. (TC NR 20071001002)SDR YTRR116570Governor · fluctuatesAIRCRAFT EXPERIENCED TORQUE FLUCTUATIONS OF 10 PERCENT TO 15 PERCENT DURING CRUISE FLIGHT.SDR HEER117209Fitting · crackedUPPER LT TAILBOOM ATTACH FITTING CRACKED. REPLACED FITTING.SDR CA070626001Hose · debonded(CAN) FUEL HOSE ASSY DEBONDED CAUSING FUEL LEAK FROM FWD TANKS. THE RUBBER BELLOW PART OF THE TUBE ASSEMBLY DEBONDED FROM THE ALUMINUM TUBING. THIS HOSE ASSEMBLY IS LOCATED ON THE LT SIDE FWD FUEL TANK. REFER TO HELICOPTER IPB FIGURE 28-3 ITEM NR 57. (TC NR 2SDR YTRR114335Attach Fitting · crackedON PREFLIGHT PILOT FOUND TAILBOOM MOVEMENT EXCESSIVE. ON INSPECTION FOUND TAILBOOM ATTACH FITTING CRACKED.SDR CA070216001Housing · damaged(CAN) BYPASS INDICATOR BORE MISSING ONE 0.062 INCH DIA OIL PASSAGE AT BOTTOM OF BORE BREAKING THROUGH THE SMALLEST RECESSED BORE DIAMETER OF .375 INCH. PICTURE OF PART WITH THE MISSING HOLE ATTACHED. (TC NR 20070216001)SDR CA070126006Tail Boom · damaged(CAN) UPON CHANGING FORMER P/N 206-020-113-093 ON VERTICAL FIN, DAMAGE/GOUGING DETECTED ON THE IB FIN SKIN WITHIN CLOSE PROXIMITY TO VERTICAL FIN MOUNTING HOLE. IT IS SUSPECTED THAT WHEN ORIGINALLY FITTING THE COWLS THAT THE FORMER WAS TRIMMED AND THAT AT THISSDR CA061208004Pump · lack of lube(CAN) GREASE FOUND WASHED OUT CAUSING PREMATURE WEAR OF DRIVE SPLINES LEADING TO HYDRAULIC SYSTEM FAILURE. 198.3 HRS SINCE PREVIOUS LUBRICATION. (TC NR 20061208004)SDR CA061208003Tach Generator · worn(CAN) GREASE FOUND WASHED OUT CAUSING PREMATURE WEAR OF DRIVE SPLINES LEADING TO HYDRAULIC SYSTEM FAILURE. 298.7 HRS SINCE PREVIOUS LUBRICATION. (TC NR 20061208003)SDR CA061109006Skin · cracked(CAN) CRACK FOUND IN SKIN UNDER FWD BEARING OIL COOLER SUPPORT RT STA 192.00 BUTT 4.0. REPAIR WAS MADE IAW BHT-206-SRM-4-2 (TC NR 20061109006)SDR CA061011012Gland Nut · cracked(CAN) DURING THE FIRST OVERHAUL OF THREE SERVO ACTUATORS 2 WERE FOUND TO HAVE CRACKS ON THE GLAND THAT RETAINS THE PISTON SEAL. BOTH SERVO ACTUATOR GLAND ASSEMBLIES WERE CRACKED IN THE SAME AREA. (TC NR 20061011012)SDR ALGR111218Panel · crackedROOF PANEL CRACKED 2 PLACES ON LT AFT TRANSMISSION MOUNT.SDR ALGR111208Panel · crackedROOF PANEL CRACKED APPROX. 1.6.SDR ALGR111207Panel · crackedROOF PANEL CRACKED APPROX 6.3.SDR ALGR110830Coupling · mismanufacturedON INSPECTION OF FLEX COUPLING, FOUND PART TO BE MISMANUFACTURED ON END FACE SPLINES. REPLACED PART W/SERVICEABLE PART.SDR YTRR109168Gearbox · crackedDURING ROUTINE 100-HOUR AIRFRAME INSPECTION, FOUND TAIL ROTOR GEARBOX CASTING CRACKED.SDR ALG2006F00037Relay · failedIN LEVEL FLIGHT, BATTERY RELAY ILLUMINATED. MAINTENANCE ACTION: REPLACED RELAY. (K)SDR YTRR108175Indicator · failedENGINE OIL TEMPERATURE INDICATOR FAILED IN-FLIGHT.SDR ALG2006F00007Volt Regulator · malfunctionedGENERATOR FAIL LIGHT ILLUMINATED ON TAKEOFF. ATTEMPTED RESET AND SMELLED ACRID BURNING SMELL. LANDED AIRCRAFT AT THE NEAREST SAFEST PLACE. REMOVED AND REPLACED VOLTAGE REGULATOR WITH SERVICEABLE UNIT. ALL IAW MM. (K)SDR CA051220003Skin · damagedDURING A SCHEDULED DESTRUCTIVE TEST, FOUND SOME STABILIZER SKINS DAMAGED WITH TOOL MARKS AT SOME INSERT HOLES.SDR ALG2005F00122Actuator · out of adjustON TAKEOFF, RPM ROSE TO 104 PERCENT, THE PILOT WAS UNABLE TO BEEP DOWN TO NORMAL RANGE, RETURNED TO DEPARTURE. THE MECHANIC FOUND THE LINEAR ACTUATOR RANGE WAS SET TOO HIGH, HE ADJUSTED THE BEEP RANGE TO WITHIN THE LIMITS AND THE AC WAS RETURNED TO SERVICE. SDR ALG2005F00102Starter Gen · failedSTARTER/ GENERATOR FAILED ENROUTE TO WC 586, RETURNED TO BASE. REMOVED AND REPLACED STARTER/GENERATOR. (K)SDR ALG2005F00101Starter Gen · failedSTARTER/GENERATOR FAILED ENROUTE TO WC 586. RETURNED TO BASE. REMOVED AND REPLACED STARTER/GENERATOR. (K)SDR ALG2005F00106Warning System · false indicationDURING START TOT PEAKED AT 770 FOR ONE SECOND. MAINTENANCE WAS NOTIFIED. PERFORMED INSPECTION OF TOT INSTRUMENT IAW MM AND FOUND INSTRUMENT SERVICEABLE. PERFORMED HOT END INSPECTION IAW MM AND FOUND NO DEFECTS. REINSTALLED SAME AS REMOVED AND RELEASED AIRCSDR ALG2005F00108Engine · noisyLOUD HOWLING NOISE AT FLIGHT IDLE FROM THE ENGINE TRANSMISSION AREA. REPLACED ENGINE ASSEMBLY. (K)SDR ALG2005F00117Starter Gen · noisyPILOT HEARD LOUD NOISE FROM THE ENGINE COMPARTMENT. REMOVED STARTER GEN AND INSTALLED A SERVICEABLE TSO GENERATOR. RAN AC FOR 30 MINUTES AT GROUND IDLE AND 100 PERCENT RPM FOR 10 MINUTES WITH NO NOISE OCCURRING. REMOVED AND INSPECTED ENGINE CHIP PLUGS, CHECSDR ALG2005F00089Engine · making metalIN FLIGHT, ENGINE CHIP LIGHT ILLUMINATED. AFTER LANDING, NOTIFIED MAINTENANCE. THE ENGINE CHIP PLUG WAS FOUND TO HAVE METAL FLAKES. REMOVED AND REPLACED ENGINE WITH SERVICEABLE UNIT, IAW MM. (K)SDR ALG2005F00079Caliper · looseDURING DAILY INSPECTION THE MECHANIC FOUND ROTOR BRAKE BOLTS LOOSE AND A PAD WAS MISSING, REMOVED AND REPLACED BOTH CALIPERS WITH SERVICEABLE SET AND THE AC WAS RETURNED TO SERVICE. (K)SDR ALG2005F00083Blade · damagedDURING THE DAILY MAINTENANCE INSPECTION, IT WAS DETERMINED THE TAIL ROTOR BLADE TIP WAS DAMAGED BY STRIKING AN UNDETERMINED OBJECT. COMPLIED WITH THE CONDITIONAL INSPECTION, 5-28 SUDDEN STOPPAGE/ACCELERATION-TAIL ROTOR. (K)SDR CA050916004Filter · improper part(CAN) A PHYSICAL DIFFERENCE WAS NOTICED ON FILTERS 50-075-1. A SCREEN HOLE PATTERN WAS FOUND TO BE OUT OF SPECIFICATION. ATTACHED PICTURE SHOWING DIFFERENCES BETWEEN ACCEPTABLE AND NON-CONFORMING PARTS.SDR ALG2005F00066Bolt · defectiveDURING MAINTENANCE SERVICE CHECK, THE LT ROTOR BRAKE CALIPER WAS FOUND TO BE DEFECTIVE. THE FOLLOWING ITEMS WERE REMOVED AND REPLACED WITH SERVICEABLE COMPONENTS: ROTOR BRAKE DISK, BOLTS AND 2 ROTOR BRAKE CALIPERS. IAW MM. (K)SDR ALGA105863Bearing · failedTRANSMISSION ASSY MAKING METAL, DISASSEMBLED AND FOUND DUPLEX BEARING BREAKING DOWN. REMOVED AND REPLACED DUPLEX BEARING.SDR ALG2005F00063Transmission · failedTRANSMISSION CHIP LIGHT ILLUMINATED IN HOVER. MAINTENANCE REMOVED TRANSMISSION, MAST, AND OIL COOLER. A SERVICEABLE TRANSMISSION, MAST AND OIL COOLER WERE INSTALLED. FLUSHED TRANSMISSION OIL SYSTEM. IAW MM. GROUND AND LEAK CHECK, OK. (K)SDR CA060322005Spline · wornTHE ENGINE LOST POWER BECAUSE THE ENGINE DRIVEN FUEL PUMP FAILED. THE CAUSE OF THE PUMP FAILURE WAS DISENGAGEMENT OF THE DRIVE SHAFT SPLINES FROM THE DRIVER GEAR SPLINES DUE TO EXCESSIVE WEAR.SDR ALG2005F00041Engine · oil consumptionDURING HOT REFUELING AT BASE, THE PILOT WAS INFORMED THAT SMOKE COMING FROM THE EXHAUST STACK, HE SHUT THE AIRCRAFT DOWN. POST INSPECTION REVEALED THAT ENGINE OIL LEVEL WAS LOW (TWO LEVEL MARKS). THE MECHANIC REMOVED AND REPLACED THE ENGINE ASSY AND THE AIRCSDR ALG2005F00042Igniter · inoperativeDURING START, THE ENGINE FLAMED OUT. SECOND ATTEMPT WAS UNSUCCESSFUL. UPON INSPECTION, THE MECHANIC REMOVED AND REPLACED THE IGNITER PLUG AND THE AC WAS RETURNED TO SERVICE. (K)SDR CA050720005Blade · delaminatedAFTER DISCUSSION WITH A FSR FROM BHTC, LEARNED THAT THE TAIL ROTOR ON THIS AIRCRAFT HAD BEEN DAMAGED IN 2004. THE TECHNICAL LOG OF THE AIRCRAFT DID NOT DEMONSTRATE THAT THE PROPER INSPECTION WAS CARRIED OUT AS PER MM CHAP 5-28. BHTC CONFIRMED THAT THE PREVIOSDR ALGA104359Sleeve · wornBEARING AXIAL PLAY BEYOND MAX. INSTALLED NEW BEARINGS AND SLEEVES BY O/H SHOPSDR ALGA104358Bearing · wornBEARING AXIAL PLAY BEYOND MAX. INSTALLED NEW BEARINGS AND SLEEVES BY O/H SHOP.SDR ALGA104360Bearing · wornBEARING AXIAL PLAY BEYOND MAX. INSTALLED NEW BEARINGS AND SLEEVES BY O/H SHOP.SDR ALGA104357Sleeve · wornBEARING AXIAL PLAY BEYOND MAX. INSTALLED NEW BEARINGS AND SLEEVES BY O/H SHOP.SDR 2005F00049Engine · malfunctionedDURING TAKEOFF, WITH POWER ABOVE 80 PERCENT TORQUE AIRCRAFT BEGINS VIBRATIONS INCREASING TO SEVERE WITH OSCILLATION BETWEEN 20-30 PERCENT ON TORQUE GAUGE. MAINTENANCE REMOVED AND REPLACED ENGINE ASSY WITH SERVICABLE SERIAL NUMBER CAE-890158. WORK DONE IAW BESDR CA050125002Indicator · inoperative(CAN) AFTER THE AIRCRAFT WAS COLD SOAKED FOR OVER AN HOUR, THE GAGE RESPONSE WAS VERY SLOW WHILE THE ENGINE OIL TEMP WAS ALLOWED TO STABALIZE AT 60 DEG.SDR 2005FA0000377Fuel Cell · damagedDURING A SCHEDUALED 12 MONTH FUEL SYSTEM INSPECTION IAW MM, THE DEFECT WAS NOTED ON A CUSTOMERS AIRCRAFT. THE BOTTOM INSIDE OF THE AFT FUEL CELL WAS BLISTERED WITH .2500 INCH BLISTER IN DIAMETER, SPACED FROM .5000 INCH TO .2500 INCH APART. THE BLISTERS CONTISDR ALG2005F00002Filter · dirtyWHILE LIFTING UP TO A HOVER TO DEPART, N2 RPM BLED OFF TO BELOW 90 PERCENT AND WOULD RECOVER, THROTTLE WAS FULL OPEN AND MAX BEEP WOULD NOT INCREASE THE RPM. MAINTENANCE REMOVED THE P/C, CLEANED AND DID A SYSTEM AIR LEAK CHECK. REINSTALLED SAME P/C FILTER ANSDR ALGA098856Meter · spalledMETAL ON BOTH PLUGS, FOUND TORQUE METER AFT BEARING BREAKING DOWN, HEAVY SPALLING OUTER EDGES OF ROLLERS AND INNER RACE. REPLACED BEARING AND REPAIRED GEAR BOX.
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