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 YH7R2015FA0000450Shunt · failedENGINE FLAMED OUT DURING FLIGHT. INSPECTION OF ACFT FOUND THAT THE FUEL SHUTOFF VALVE WAS CYCLING FROM THE OPEN POSITION TO THE CLOSED POSITION WHEN BATTERY POWER, POWER WAS APPLIED AND THE FUEL SHUT OFF VALVE SWITCH WAS PLACED IN THE OPEN POSITION. IT WAS DSDR CA151019006Support · cracked(CAN) THE PILOT COMPLAINED OF HAVING FELT A SEVERE VIBRATION ON PEDALS AND SHAKING OF INSTRUMENTS CONSOLE. MAINTENANCE PROCEED TO INSPECT THE ACFT AND FOUND THAT THE TAIL ROTOR GEAR BOX SUPPORT HAD BROKEN OFF ON ONE STUD. NORMAL LANDING WAS PERFORMED WITHOUSDR CA150706012Jam-Nut · loose(CAN) DURING ARRIVAL INSPECTION, ONE OF THE MR PITCH CHANGE LINKS WAS FOUND TO HAVE BOTH THE UPPER & LOWER JAM NUTS LOOSE. THE UPPER NUT HAD THE REQUIRED SAFETY BUT NO TORQUE ON EITHER END OF THE LINK.SDR EVCA20150608077Connector · burnedAPPROXIMATELY 5 MINUTES AFTER DEPARTING BASE, PILOT & CREW STATED THAT THEY SMELLED AN ELEC BURNING SMELL. THEY RETURNED TO BASE SAFELY. UPON INSPECTION, ELEC CONNECTOR AT AFT EVAPORATOR BLOWER ASSEMBLY TO BE BURNT. SITUATION WAS SIMILAR TO THAT DESCRIBED ISDR CA150318011Blade · damaged(CAN) THE PILOT NOTED AN INCREASE IN VIBRATION. POST LANDING INSPECTION REVEALED A NR OF MID-SPAN STATION ALONG THE T/E OF BLADE WERE VOIDED AND THE SKIN SEPARATED FROM T/E EXTRUSION. AFTER THE ACFT SAT STATIC OVERNIGHT THE MECHANIC NOTED ADDITIONAL VOIDING SDR CA150218007Turbine · exploded(CAN) THE ACFT WAS ENROUTE TO THE REPAIR STATION AND 10 MINUTES OUT THE PILOT ENCOUNTERED A HUGE EXPLOSION LIKE SOUND WITH A MASSIVE LT YAW OF THE ACFT. STABILIZED THE ACFT AND SUCCESSFULLY CONDUCTED AN AUTOROTATION AND EMERGENCY LANDING. THE TURBINE SECTIONSDR EVCA2014111700073Attach Fitting · crackedDURING ROUTINE MAINTENANCE THE INSPECTION REVEALED A CRACKED ON THE UPPER LT TAIL BOOM ATTACHMENT FITTING PN 206-032-409-001.SDR YTRA2014102129501Flex Hose · chafedPILOT REPORTED LOSS OF HYD POWER CAUSING HIM TO MAKE LAND IN THE FLYAWAY PORTION OF HIS INTENDED LANDING ZONE.SDR EVCA2014082500069Attach Fitting · crackedDURING ROUTINE INSPECTION FOUND TAIL BOOM ATTACHMENT FITTING PN 206-032-409-001 CRACKED.SDR PBVA2014092500000Warning Light · illuminatedAFTER 30 MINUTES IN CRUISE FLIGHT, TOT SUDDENLY WENT TO 840 CA, PRECAUTIONARY LANDING WAS MADE AND MAINTENANCE WAS CALLED. TOT SYSTEM WAS TESTED AND FOUND TO BE WORKING NORMAL. NO EXTERNAL DAMAGE WAS NOTED TO ENGINE. ENGINE WAS R & R AND SENT TO ENGINE SHSDR EVCA2014052900060Stiffener · crackedDURING A ROUTINE 300 HOUR INSPECTION THE MECHANIC FOUND STIFFENER CRACKED.SDR CA140516007Counter · cracked(CAN) THIS ACFT WAS OPERATING, LOCATED AT 3000 FT ABOVE SEA LEVEL. IT TOOK OFF FOR A MISSION WITH 2 CREW, 2 PASSENGERS AND 400 LBS OF FUEL, IAW CREW TESTIMONIALS, ONCE IN AIR, 1 MINUTE AFTER TAKING OFF THE PILOT FELT HEAVY VIBRATION ON PEDALS AND TRANSMITTED SDR CA140325006Bearing · misinstalled(CAN) THE FEATHERING BEARING WAS STAKED FAR TOO TIGHT. CAUSING RESTRICTION ON TAIL ROTOR CONTROL. THIS WAS NOTED ON A PRE FLIGHT POST MAINTENANCE INSPECTION. THE BLADE ARE THE VAN HORN BLADES INSTALLED UNDER STC SH10-22. ASSY REMOVED AND NEW ASSEMBLY INSTALLSDR YTRA20140313001Engine · making metalTHE PILOT MADE A PRECAUTIONARY LANDING DUE TO AN ENG CHIP LIGHT ILLUMINATION.SDR YTRA20140318001Bleed Air Sys · contaminatedPILOT REPORTED A SMOKE SMELL IN THE AFT PORTION OF THE FUSELAGE. ON INVESTIGATION THE MECHANIC FOUND THAT OIL HAD SEEPED INTO THE BLEED AIR CABIN HEATER SYS. WHEN THE HEAT FROM THE BLEED AIR HEATER WARMED THE OIL IN MADE A SMOKE SMELL.SDR EVCA2014022600057Web · crackedDURING A ROUTINE INSPECTION FOUND THE FOLLOWING CRACKED, WEB PN 206-033-110-187 & STIFFENER PN 206-033-110-239.SDR EVCA2014021900056Fitting · crackedDURING ROUTINE INSPECTION FOUND THE TAIL BOOM FITTING, PN 206-032-409-001, CRACKED.SDR EVCA2014071700063Mount · corrodedWHEN DISASSEMBLY OF ACFT AFTER IT WAS DECOMMISSION, MECHANIC FOUND ENG MOUNT SUPPORT LEG CORRODED THROUGH.SDR CA140127001Bolt · sheared(CAN) IN FLIGHT PILOT COULD FEEL VIBRATION IN THE AIRFRAME, DECIDED TO LAND. ENGINEER INSPECTED AIRFRAME INCLUDING REMOVAL OF DRIVESHAFT COVERS AND COWLS AS REQUIRED AND A DETAILED INSPECTION OF THE TAIL ROTOR AND DRIVE SYS ACCOMPLISHED. A TEST FLIGHT WAS ACSDR CA140109003Plug · leaking(CAN) ACFT HAD JUST DEPARTED FROM AN OFFSHORE PLATFORM WHEN THE T/R PEDALS LOCKED UP AT APPROXIMATELY MID-TRAVEL. PILOT CONTINUED ON AND MADE AN UNEVENTFUL EMERGENCY LANDING. AT THIS TIME, T/R FLAPPING BEARINGS ARE SUSPECT, BUT INITIAL INSPECTION HAS REVEALEDSDR 7ALA2013F00000Starter Gen · failedSTARTER GENERATOR FAILED IN FLIGHT. ACFT LOST POWER FOR BOOST PUMPS, LIGHTING AND RADIOS. ACFT LANDED AT NEAREST AVAILABLE AIRPORT. NO DAMAGE TO ACFT. BRUSH DETERIORATION SEEMS TO BE THE CAUSE.SDR YTRA2013073000002Duplex Bearing · spalledMAIN ROTOR TRANSMISSION DUPLEX BEARING, BEARING SET SPALLING.SDR CA130722009Blade · delaminated(CAN) AN AME NOTICED T/R BLADE HAD SOME PAINT MISSING. FURTHER INVESTIGATION THE AME FOUND NEAR THE TIP OF THE T/R BLADE A DELAMINATION HAD OCCURRED ON THE ONE SIDE OF THE T/R BLADE THROUGH A TAP TEST. HE INSPECTED THE SECOND T/R BLADE AND FOUND A DELAMINATISDR EVCA20130722045Engine · power lossPILOT STATED AFTER TURNING FINAL TO BASE, THE ACFT EXPERIENCED A PARTIAL ENGINE LOSS OF POWER (SIMILAR TO ROLLING THE ENGINE TO FLIGHT IDLE). THE ACFT WAS APPROX 80 TO 100 FT ABOVE THE GROUND AT ABOUT 40 KTS. THE PILOT MADE AN EMERGENCY LANDING WHICH RESULTESDR YTRA52117/175/178Mast · mismanufacturedMAST POLE MFG INCORRECTLY. SCALLOP FOR DRIVE LINK THROUGH BOLT MACHINED IN WRONG LOCATION.SDR 2013FA0000424Bearing · failedA/C WAS ON A BRAVO TOUR, PILOT HEARD A BANG FOLLOWED BY A POWER LOSS AND ENTERED A AUTOROTATION TO THE RIVER EMERGANCY FLOATATION ACTIVATED AND A LANDING WAS MADE. FOUND NR 2 ENGINE COMPRESSOR BEARING FAILED.SDR CA130724008Circuit Breaker · tripped(CAN) DURING FLIGHT, THE PILOT SAW THAT THE NR 1 ENGINE OIL TEMP REACHED 119 DEGREES C FOR 2 MINUTES AND THAT THE CB1, CB17 POPPED OUT. IT`S ALWAYS HAPPENED WHEN THE HELICO IS IN STATIONNARY FLIGHT POSITION FOR A LONG PERIOD AND THE OUTSIDE TEMP IS HIGH, ABOSDR EOPA201306260001Fuel Filter · leakingFUEL FILTER ASSY, PN 1743640-01, LEAKING FROM PRESS TO TEST BUTTON.SDR ALGA201306187453Blade · destroyedNR 1 GRIP FINGER DOUBLER CORRODED AND SEPARATED APPROX 8".SDR EOPA130529265Fuel Filter · leakingAIRFRAME FUEL FILTER, SEEMED FUNCTIONAL, NO NOTICABLE DEFECT. UPON POST FLIGHT INSPECTION, ENGAGED BOOST PUMPS, FUEL LEAKED PAST THE BYPASS PRESS-TO-TEST BUTTON. REPLACED THE AIRFRAME FUEL FILTER ASSY WITH SERVICEABLE ASSY.SDR ALGA050820137398Strap · deterioratedFOUND STRAP MATERIAL DETERIORATED AND WIRES EXPOSED ON STRAP.SDR YTRA20130324100Tail Boom · damagedTAILBOOM WAS DAMAGED UNDER HIGH WIND CONDITIONS ON AN OFFSHORE PLATFORM.SDR YTRA2013073000001Mast · mismanufacturedMAST POLE MANUFACTURED INCORRECTLY. SCALLOP FOR DRIVE LINK THROUGH BOLT MACHINED IN WRONG LOCATION. MAST POLE HAS 44 RIN.SDR YTRA2013032613085Mast · mismanufacturedON INSPECTION NOTED THAT PC LINKS WERE NOT PROPERLY ALIGNED. IN THE COURSE OF THE INVESTIGATION NOTED THAT MAST POLE MASTER SPLINE AND DRIVE LINK COLLAR SET NOTCH WERE NOT AT THE CORRECT ANGULAR ORIENTATION. REMOVED MAST POLE AND CONTACT BHT.SDR CA130411004Drive Shaft · cracked(CAN) OPERATOR FOUND 2 SMALL CRACKS ON THE DRIVESHAFT FROM RIVET HOLE IN FLANGE ADAPTER DRIVESHAFT WAS REPLACED.SDR 2013FA0000087Circuit Breaker · unserviceableDURING FLIGHT THE PILOT NOTED SMOKE EMANATING FROM THE AFT CABIN AREA AND MADE AN EMERGENCY LANDING IN A FIELD LOCATION. AFTER TROUBLESHOOTING OF THE SYS, NOTED THE CIRCUIT BREAKER WAS IN THE OPEN POSITION AND THEREFORE DID NOT TRIP AS REQUIRED AFTER AFT EVAPSDR CA121214006Skin · cracked(CAN) THE ACFT HAS A 4.5" CRACK ON THE LT SIDE OF THE ROOF SHELL ASSY JUST IN FRONT OF THE FWD ENGINE FIREWALL. THIS WAS DISCOVERED FOLLOWING TROUBLESHOOTING ACTIONS, RELEVANT TO THE INVESTIGATION OF A NOISE BEING EXPERIENCED DURING LT PEDAL INPUTS DURING HOVSDR 2012FA0000814Skin · cracked1" CRACK ON LT SIDE OF TRANSMISSION UPPER CABIN ROOF SHELL STARTING AT A ROW OF RIVETS, SECOND INBD RIVET FS 146.3, LBL APPROX 8.65. REPAIRED IAW REPAIR NR 12RL-113.SDR 2012FA0000815Skin · cracked.7500" CRACK ON LT SIDE OF TRANSMISSION UPPER CABIN ROOF SHELL STARTING AT A ROW OF RIVETS, SECOND INBD RIVET FS 146.5 LBL APPROX 8.65. REPAIRED IAW MFG FIELD REPAIR NR 12RL-119.SDR CA121122005Stiffener · cracked(CAN) OPERATOR REPORTED A CRACKED STIFFENER. THE STIFFENER WAS REPLACED 775 HOURS AGO WHEN HELICOPTER HAD 1842 HRS.SDR CA121122004Stiffener · cracked(CAN) OPERATOR FOUND STIFFENER CRACKED.SDR ALGA2012110729129Unknown · unknownON INITIAL ROLL UP OF THROTTLE, THE RPM WAS NOTED AS WELL ABOVE 101 PERCENT AND WAS "BEEPED" DOWN TO 100 PERCENT. FIVE MINUTES INTO THE FLIGHT THE RPM WAS NOTED TO BE WELL BELOW LOWER REDLINE APPROX 98 PERCENT. ATTEMPTED TO BEEP THE RPM UP BUT WAS UNSUCCESSSDR ALGA2012101801Transceiver · smokeRADIO LOST DISPLAY, THEN STARTED SMOKING ON START UP. R & R VHF TRANSCEIVER.SDR EVCA201210120037Pump · failedHYDRAULIC PUMP FAILURE IN CRUISE FLIGHT.SDR CA121011008Blade · cracked(CAN) A M/R BLADE WAS FOUND CRACKED BY THE MECHANIC WHILE HE WAS CLEANING THE BLADE IN PREPARATION FOR A STATIC BALANCE CHECK AFTER A HUB CHANGE. THE CRACK IS APPROXIMATELY 3.6" LONG.SDR ALGA201210126702Drive Shaft · crackedSHAFT AFT RIVETED FLANGE IS CRACKED.SDR ALGA2012092105Rotor · wornHARD TO TURN N2 ROTOR. DISASSEMBLY IAW MANUAL, COMPLIED WITH PRELIMINARY FOUND GRAPHITE ON 9-12/13-18 SUMP COVER BORE LIFTTING CAUSE HEAVY RUBBING TO SEAL KNIVES CAUSE N2 ROTOR HARD TO TURN. REPLACED SUMP COVER ASSY.SDR ALGA2012091901Bearing · wornFOUND TAILROTOR HUB & BLADE ASSY ONE BEARING WORN.SDR QMLA2012082312140Frame · crackedA CRACK WAS FOUND IN FRAME, PN 206-032-308-103 AT STA 205.76. THE CRACK WAS BEHIND THE UPPER LT TAIL BOOM ATTACH FITTING. ONCE THE TAIL BOOM WAS REMOVED THE ENTIRE CRACK COULD BE SEEN.SDR CA120803004Lever · defective(CAN) DURING REPLACEMENT OF FUEL CONTROL LEVER, NEW LEVER FOUND TO HAVE MFG DEFECT. MATERIAL LEFT BEHIND ON INNER DIAMETER OF SERRATIONS DURING MFG PROCESS. MATERIAL DOES NOT ALLOW LEVER TO FULLY SEAT AGAINST SERRATED WASHER. ALL LEVERS PULLED FROM INVENTORY
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