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 HEEA060918Oil Cooler · cloggedOIL COOLER HAS HIGH OIL TEMPERATURE AND CORE IS CLOGGED.SDR HEEA060830Exhaust Stack · crackedEXHAUST ASSEMBLY CRACKED.SDR HEEA060661Carbon Seal · leakingSEAL LEAKING. REPLACED WITH SERVICEABLE SEAL.SDR 99ZZZX1683Trunnion · corrodedSPLINES BADLY CORRODED. TRUNNION SCRAPPED AT 1/2 LIFE.SDR 99ZZZX1224Blade · corrodedDISCOVERED DURING DAILY INSPECTION, CORROSION AND SEPARATION AT TIP.SDR 99ZZZX1349Actuator · failedLINEAR ACTUATOR FAILED AT FULL STROKE WITH HIGH ALTITUDE. TAIL ROTOR PITCH FIXED AT 100 PERCENT. ACTT: 1,228.2 HOURS.SDR HEEA060416Cover · wornFLOAT COVER WORN.SDR HEEA060409Indicator · sticksTOT INDICATOR NEEDLE STUCK AT ZERO ON START.SDR HEEA060388Actuator · failedACTUATOR INOPERATIVE. WILL NOT BEEP UP AND DOWN.SDR HEEA060359Case Assy · crackedCRACK INDICATION. REPLACED WITH SERVICEABLE CASE.SDR 99ZZZX2444Skin · crackedAD 99-02-01. HORIZONTAL STABILIZER OPENING, LEFT SIDE, HAS CRACK TO SEAM.SDR HEEA060215Fitting · crackedUPPER LEFT TAILBOOM FITTING CRACKED. REPLACED WITH SERVICEABLE FITTING.SDR HEEA060166Gps · malfunctionedGPS NOT FUNCTIONING CORRECTLY.SDR HEEA060150Transponder · erraticTRANSPONDER REPORTED INOPERATIVE. PERFORMED PRELIMINARY INSPECTION AND FOUND SENSITIVITY WEAK AND ERRATIC. UNABLE TO ADJUST.SDR 99ZZZX43Blade · corrodedDISCOVERED DURING DAILY INPSECTION, HEAVY CORROSION ALONG TRAILING EDGE (APPEARS TO BE INTERGRANNULAR CORROSION IN TRAILING EDGE EXTRUSION).SDR 99ZZZX229Mount · chafedREPLACED RESTRAINT AND MOUNT WITH NEW PARTS.SDR 99ZZZX228Restraint · chafedREPLACED RESTRAINT AND MOUNT WITH NEW PARTS.SDR 98ZZZX4811Mount · chafedREPLACED TUBE AND MOUNT WITH NEW PARTS SUPPLIED BY BELL HELICOPTER.SDR 98ZZZX4810Tube · chafedREPLACED TUBE AND MOUNT WITH NEW PARTS SUPPLIED BY BELL HELICOPTER.SDR 98ZZZX4807Tube · chafedREPLACED TUBE WITH NEW PARTS SUPPLIED BY BELL HELICOPTER.SDR CA981130024Channel · cracked(CAN) CRACK FOUND ON THE LEFT CHANNEL OF THE SPAR AT THE SUPPORT FOR ONE OF THE ATTACHMENTS FOR THE TAIL BEAM. PART TC: 2,747.SDR 98ZZZX4754Release Cable · malfunctionedCARGO HOOK MANUAL RELEASE CABLE TOO SHORT. APPLIES TO ALL BELL 206L SERIES HELICOPTERS UTILIZING ONBOARD SYSTEMS E-72 ELECTRONIC LOAD WEIGH SYSTEM. WITH THE LOAD CELL INSTALLED BETWEEN THE CARGO HOOK AND LOAD TROLLEY, FULL TRAVEL CANNOT BE OBTAINED WITH THE SDR 98ZZZX4358Seal · failedON PART 135 FLIGHT, PILOT NOTICED HIGH ENGINE OIL PRESURE AND FLICKERING TRANS OIL PRESS LOW LIGHT. AFTER REDUCING POWER, LIGHTS WENT OUT. PILOT CONTINUED FLIGHT FOR 10 MINUTES WHEN TRANS OIL PRESS LIGHT CAME ON STEADY. PILOT MADE PRECAUTIONARY LANDING AND SDR 98ZZZX4755Frame · damagedREMOVAL OF FRAME TO REPLACE WORKING RIVETS ON UPPER FITTING. LOWER LT AND RT ATTACHMENT CASTINGS CHAFING FRAME IN RADIUS.SDR 98ZZZX4081Skin · crackedSIX INCH CRACK WAS FOUND ON TAIL BOOM SKIN AT THE FORWARD LOWER CUT-OUT AREA FOR THE HORIZONTAL STABILIZER. SUBMITTER STATED BELL HELICOPTER HAS ISSUED AN OPERATION SAFETY NOTICE ON THIS PROBLEM.SDR 98ZZZX4744Battery · damaged90-DAY LIFE VEST INSPECTION FOUND MOISTURE GETS PLUGS AND CAUSES BATTERY CASE TO SWELL AND WIRE CONNECTION TO LIGHT TO PUSH OUT OF CASE.SDR HEEA0016120Support · bentRECEIVING INSPECTION REVEALED: BEND BEYOND SERVICEABLE LIMITS ON G.P. SUPPORT PRESSURE OIL STRUT. PART OVERHAULED W/O 16671.SDR CA980916069Trunnion · brinnelled(CAN) DURING TAIL ROTOR BLADE REMOVAL, TRUNNION FELT RATCHETY AND HAD NO PRELOAD. TRUNNION RACE BRINNELLED BEYOND LIMITS.SDR CA980916068Bearing · loose(CAN) ON DAILY INSPECTION, TAIL ROTOR BLADE OUTBOARD BEARING LOOSE AUXILIARY IN THE BLADE. PART TC:SDR 98ZZZX3552Skin · crackedCRACK FOUND ACROSS TOP SKIN BETWEEN HORIZONTAL STABILIZER.SDR HEEA0015879Actuator · inoperativeACTUATOR INOPERATIVE. TRIES TO MOVE ONLY ONE WAY.SDR HEEA0015476Transceiver · malfunctionedVHF RADIO WILL NOT TURN OFF.SDR HEEA0015292Transceiver · failedON FIRST FLIGHT, VHF TRANSMITTED GARBLED.SDR 98ZZZX3094Hinge · wornDURING ROUTINE INSPECTION, FOUND T/R GEARBOX FAIRING HINGE WORN, FILLER DOOR MISSING. THE FILLER DOOR HAD CONTACTED ONE TAIL ROTOR BLADE. THIS BLADE WAS FOUND UNSERVICEABLE. TAIL ROTOR HUB BLADE ASSY WAS REPLACED. AIRCRAFT WAS VISUALLY INSPECTED AND RETURNSDR HEEA0015209Splice · mismanufacturedAFT FLANGE OF T-ANGLE SPLICE IS TRIMMED TOO SHORT TO PROVIDE PROPER EDGE DISTANCE FOR .1562 INCH RIVETS. THE AREA WHICH IS TRIMMED TOO SHORT IS ON THE SIDE OF PART, JUST INBOARD OF WHERE THE CURVE BEGINS TO MATCH THE SHELL CONTOUR.SDR HEEA0015208Intercostal · mismarkedINTERCOSTAL MISMARKED. PART SERVICEABLE. VENDOR MISPACKAGED P/N 206-033-410-021S WAS ORDERED, THE BHT PICK TICKET HAS -021S P/N ON IT; BUT A -025S INTERCOSTAL WAS SENT.SDR HEEA0015204Fitting · mismanufacturedFITTING MISMANUFACTURED. FORWARD CORNERS OF FITTING WHERE FITTING CONTACTS FORWARD TAILBOOM BULKHEAD FRAME. THE AFT END OF THE FITTING IS RADIUSED AND IS NOT REQUIRED TO BE.SDR 99ZZZX1225Blade · corrodedDISCOVERED DURING DAILY INSPECTION, SKIN CORRODED, SEPARATED AND TORN ON LOWER SIDE TIP.SDR HEEA0015048Transceiver · failedTRANSCEIVER WILL NOT POWER UP.SDR HEEA0014873Center Case · corrodedMAIN ROTOR GEARBOX HAS CORROSION IN BOLT HOLES.SDR HEEA0014754Input Line · wornGEARBOX INPUT LINE IS WORN.SDR HEEA0014730Encoder · malfunctionedENCODER ALTITUDE NOT RECEIVED BY ATC.SDR CA980421028Skin · damaged(CAN) THE MOUNTING FLANGE OF THE MAINTENANCE STEP HAS A CAVITY WHICH ALLOWS MOISTURE TO COLLECT AND FREEZE/EXPAND CAUSING A RUPTURE IN THE SKIN OF THE A/C AND DAMAGE TO THE HONEYCOMB BENEATH.SDR HEEA0013715Actuator · failedINOPERATIVE.SDR 98ZZZX1701Tube · chafedWHILE REMOVING RENTAL ENGINE AND TRANSFERRING HARD LINE P/N 23058110-A FROM RENTAL ENGINE TO ORIGINAL ENGINE, SEVERE CHAFING NOTED UNDER ADEL CLAMP. THIS IS SCAVENGE OIL LINE FROM BOTTOM OF COMPRESSOR TO THE N1 SIDE OF GEARBOX. ABRASIVE DUST AND AIRBORNE DIRSDR HEEA0013115Input Shaft · wornINPUT SHAFT SPLINES WORN BEYOND LIMITS. REPLACED WITH SERVICEABLE PART.SDR HEEA0013114Bearing · failedBEARING BREAKING DOWN ON ROLLER. REPLACED WITH SERVICEABLE PART.SDR HEEA0013113Bearing · groovedBEARING HAS GROOVES ON ROLLERS. REPLACED WITH SERVICEABLE PART.SDR CA980305001Tube · worn(CAN) VERTICAL TUNNEL AND FORWARD PILOT AND COPILOT SEAT AREAS OPENED, AND THEN WHILE MOVING COLLECTIVE, LEVER WAS FOUND CONTACTING BOTH OIL PRESSURE AND TORQUE PRESSURE LINES. TUBES WERE WORN AND PROTECTIVE PAINT WAS WORN OFF OF LEVER. TUBES ADJUSTED FOR CLSDR 98ZZZX1347Wire Rope · frayedDURING 100-HOUR INSPECTION, CARGO HOOK RELEASE CABLE WAS DISCOVERED SEVERELY FRAYED ON BOTH ENDS OF CABLE INSIDE CABLE HOUSING. THIS CABLE WAS PREVIOUSLY REPLACED 2 YEARS AGO AND 681 HOURS ACCRUED ON THIS INSTALLATION BEFORE FAILURE. WHEN PERFORMING EXTERNAL
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