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 96ZZZX111Link Idler · wornDAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS6604D64 BOLTS, 1 EACH 206-010-470-101 BEARING. NORMAL USDR 96ZZZX110Lever Assy · wornDAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS6604D64 BOLTS, 1 EACH 206-010-470-101 BEARING. NORMAL USDR 95ZZZX6864Link Idler · wornDAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS6605D64 BOLTS, 1 EACH 206-010-470-101 BEARING. NORMAL USDR 95ZZZX6863Lever Assy · wornDAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS6605D64 BOLTS, 1 EACH 206-010-470-101 BEARING. NORMAL USDR 95ZZZX6854Link Idler · wornDAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS6605D64 BOLTS, 1 EACH 206-010-470-101 BEARING. NORMAL USDR 95ZZZX6853Lever Assy · wornDAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS6605D64 BOLTS, 1 EACH 206-010-470-101 BEARING. NORMAL USDR HEEA955971Tub · mis mfgSUPPORT ANGLES FOR L/H AND R/H CREW SEAT BACK LOWER PANELS WERE INSTALLED 3/16" TOO FAR FORWARD. SUPPORT ANGLES FOR AFT CENTER DOOR POST WERE INSTALLED 3/16" TOO FAR FORWARD. SUPPORT ANGLE FOR LOWER AFT CENTER BROOM CLOSET VERTICAL ANGLES WERE ALSO INSTALLEDSDR HEEA955970Crosstube · corrodedCROSSTUBE IS CORRODED. (CORROSION AT MOUNT PAD .011 BEYOND LIMITS.)SDR CA951116023Spring · broken(CAN)DURING INSPECTION OF THE T/R DRIVE SHAFT BEARING HANGERS IN ACCORDANCE WITH ASB 206-95-86RA, 2 SPRINGS WERE FOUND BROKEN.SDR CA951122011Cyclic Tube · cracked(CAN)TWO CRACKS FOUND IN UPPER ATTACHMENT SLOT STARTING FROM INSIDE AND PROGRESSING OUTWARD. CRACKS WERE STILL WITHIN THE BEVELLED SLOT OF THE UPPER MOUNTING BOLT AREA.SDR 96ZZZX267Regulator · failedPRECAUTIONARY LANDING DUE TO TOTAL ELECTRICAL FAILURE. PILOT WRITE UP: LOST ALL ELECTRICAL POWER, INSTRUMENT WENT TO ZERO, NO LOADMETER INDICATION. MAINTENANCE EVALUATION REVEALED VOLTAGE REGULATOR FAILED.SDR 95ZZZX6903Engine Leg · defectiveWHEN INSTALLING LEGS TO AIR FRAME, FOUND UPPER END OF LEG AT WELD CONTACTS OTHER LEG.SDR 95ZZZX6343Reservoir · water contamPRECAUTIONARY LANDING DUE TO HYDRAULIC FLUID LOST DURING START. MAINTENANCE EVALUATION REVEALED THAT WATER GETS IN RESERVOIR AND CAUSES FLUID TO FORM, SIPHONING FLUID OVERBOARD THROUGH VENT LINE.SDR HEEA955927Bearing · failedENGINE REMOVED DUE TO #1 BEARING FAILURE. UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING: #1 BEARING SEPARATOR BROKEN INTO MANY PIECES, INNER AND OUTER RACE SPALLED, BEARING BALLS SCORED AND FLATTENED. SECONDARY DAMAGE - MUTE RUB ON 1STSTAGE WHEELSDR 95ZZZX7055Pitch Link · crackedFOUND CRACK ON OUTBOARD PITCH CHANGE LINK NEXT TO BEARING. SUBMITTER STATED PART WAS NEW FROM BELL, PROBLEM MAY BE FROM OVERSTAKING OF BEARING AT ASSEMBLY.SDR 95ZZZX6325Engine · making metalPILOT REPORTED ENGINE CHIP LIGHT. PRECAUTIONARY LANDING COMPLETED OK. EVALUATION OF ENGINE REVEALED EXCESSIVE METAL IN SCREEN AND CHIP PLUG.SDR HEEA955902Yoke · corrodedFOUND GREASE WATERY & BLACK COLORED. O/B BEARING JOURNAL BREAKING DOWN, EXCESSIVE CORROSION IN RETAINER BORES, AND SURFACE CORROSION ON YOKE BETWEEN JOURNALS. SCRAPPED YOKE LOCALLY.SDR 95ZZZX6587Strobe Lens · defectiveUPON INSPECTION, FOUND P/N A402A-R REFLECTIVE LENS INSIDE AT STROBE LENS HAD CHAFED THROUGH ALLOWING REFLECTIVE LENS TO DROP DOWN ONTO THE STROBE FLASH TUBE ASSY AT 978.8 HOURS. INSTALLED NEW STROBE LENS ASSY P/N A402A-R.SDR 95ZZZX6586Restraint · excess wearREMOVED RESTRAINT ASSY DUE TO EXCESS WEAR ON BOLT ASSY AFTER 978.8 HOURS OF USE. INSTALLED NEW RESTRAINT ASSY, P/N 222-320-823-125 INTO AIRCRAFT.SDR HEEA955879Yoke · bearing failedM/R YOKE OB BEARING JOURNAL ON BOTH SIDES BREAKING DOWN. REPLACED WITH SERVICEABLE M/R YOKE.SDR HEEA955864Blade · corrodedEXCESSIVE AMOUNT OF EXFOLIATION ON UPPER LEADING EDGE NEAR THE TIP WITH PIECES MISSING.SDR 95ZZZX7040Servo · defectiveSERVO DEFECTIVE. CATCHING WHEN LEVER IS LIFTED. REPLACED WITH NEW SERVO.SDR 95ZZZX6188Reservoir · fluid lossPRECAUTIONARY LANDING WAS MADE DUE TO LOSE OF HYDRAULIC FLUID. MAINTENANCE INSPECTION REVEALED THAT WATER HAD GOTTEN INTO THE RESERVOIR WHICH IN TURN CAUSED FOAM AND SIPHONING OF FLUID THAT DRAINED THE TANK THROUGH THE OVERFLOW LINE.SDR HEEA955843Shell Assy · separationFOUND LOWER SHELL ASSY (TUB) SEPARATED BOTH INSIDE AND OUT. THE OUTSIDE OF TUB WAS SEPARATED ALONG LAP SEAM FROM AFT END TO 44 1/2" FWD OF AFT EDGE. THE SEPARATION WAS 3" WIDE ALONG ENTIRE LENGHT; ONE SECTION 12" LONG THE WIDTH INCREASED TO 6". THE INSIDE OFSDR HEEA955841Freewheel · seal leakFREEWHEEL FORWARD SEAL LEAKING. REPLACED WITH SERVICEABLE FREEWHEELING UNIT.SDR HEEA955817Support · mis mfgPILOT HOLES DO NOT LINE UP WITH EXISTING ORIGINAL HOLES ON AIRFRAME CROSSTUBE TUNNEL AND FORWARD BAGGAGE COMPARTMENT PANEL.SDR HEEA955814Shell Assy · mis mfgDOUBLER ANGLES ON AFT SIDE OF L/H AND R/H AFT KICK PANELS ARE MISLOCATED AS MARKED ON SUPPORT ANGLES. SUPPORT ANGLES FOR FWD KICK PANELS DO NOT FIT CONTOUR OF TUB PROPERLY. PANEL IS TOO WIDE AT CENTER AND AFT ENDS TO FIT AIRFRAME.SDR CA951027006Spring · broken(CAN)DURING COMPLIANCE WITH BELL ASB 206-95-86 THE AME REMOVED SPRING FOR DIMENSIONAL INSPECTION FOUND SPRING BROKEN ON STUD WITH HARDWARE STILL IN PLACE. SPRING LOCATION WAS THE FIFTH HANGER FROM FRONT, O VER HORIZONTAL STABILIZERS.SDR 95ZZZX6324Relay · failedON SHORT FINAL, MAIN GENERATOR WENT OFF-LINE. PILOT IN AFT SEAT COULD SMELL BURNING ELECTRICAL WIRING. GROUND TEST REVEALED REVERSE CURRENT RELAY WAS DEFECTIVE.SDR 95ZZZX6244Seal · leakingINSTALLED NEW SEAL AND WEAR SLEEVE FOR REPAIR LEAK AT INPUT SEAL. NEW SEAL IS LEAKING AGAIN AFTER VERY SHORT TIME IN SERVICE. A COMMON PROBLEM, BUT NOT SO SOON. INSPECTION INTERVAL FOR GEARBOX IS 3,000 HOURS. CHANGING SEAL 10 TIMES NOT DESIRABLE. SEAL IS SDR 95ZZZX6243Seal · leakingINSTALLED NEW SEAL AFTER INSPECTION OF UNIT. STARTED LEAKING OIL AFTER VERY LITTLE TIME IN SERVICE. SUBMITTER STATED BELL SEEMS TO HAVE CHANGED MANUFACTURERS. SEAL IS GARLOCK TYPE, BUT BLACK INSTEAD OF USUAL ORANGE COLOR. APPEARS TO BE OF DIFFERENT MATERIASDR 95ZZZX6210Seal · leakingINSTALLED NEW SEAL AFTER OVERHAUL OF UNIT. STARTED LEAKING OIL AFTER VERY SHORT TIME IN SERVICE. NOT REALLY A COMMON PROBLEM. SUBMITTER STATED BELL SEEMS TO HAVE CHANGED MANUFACTURERS. SEAL IS BLACK INSTEAD OF USUAL ORANGE COLOR AND IS GARLOCK TYPE. SOMETSDR 95ZZZX6209Seal · leakingINSTALLED NEW SEAL AND REVERSED WEAR SLEEVE TO FRESH RUNNING SURFACE TO REPAIR LEAK AT INPUT SEAL. NEW SEAL IS LEAKING AGAIN AFTER VERY SHORT TIME IN SERVICE. A COMMON PROBLEM, BUT NOT AFTER SO LITTLE TIME. INSPECTION INTERVAL FOR GEARBOX IS 3,000 HRS. CHASDR TEIL959Seal · deteriorationAFTER ONLY 30 HOURS OF OPERATION WITH NEW STYLE SEAL, SEAL BEGAN TO DETERIORATE AROUND OUTPUT SHAFT SEALING SURFACE INTO OIL CAUSING OIL COLOR TO CHANGE TO BLACK. ACCUMULATION OF RUBBER SEAL MATERIAL ON CHIP PLUG DETECTOR FACE CAUSED CHIP PLUG DETECTOR TO BECOSDR 95ZZZX6189Support Fitting · shearedTAIL SKID CONTACTED GROUND IN SLOW REARWARD DRIFT. VERTICAL FIN CAME OFF. SUPPORT FITTING ON TAIL BOOM SHEARED ALLOWING VERTICAL FIN TO COME OFF.SDR HEEA955762Relay · defectiveGENERATOR MOTORS AFTER ENGINE SHUT DOWN. REPLACED WITH SERVICEABLE RELAY.SDR HEEA955752Indicator · defectiveWHEN POWER IS REMOVED AT 800 DEGREES, NEEDLE DOES NOT RETURN TO ZERO.SDR 95ZZZX5537Altimeter · hang-upPILOT REPORTED ALTIMETER HANG-UP AT 5,000 FEET. TESTED IN SHOP, UNIT STOPPED AT 12,000 FEET ON DESCENT. IT WOULD START AT 10,500 FEET. UPON DISASSEMBLY, INSPECTED INSHAKE ON ALL PIVOTS. THERE WAS NO INSHAKE AT ALL. THIS UNIT WAS MFG IN 1979 AND WAS NEVER SDR 95ZZZX5914Sleeve Assy · wornINSPECTED SWASHPLATE ASSY AT 878.2 HOURS, AND FOUND EXCESSIVE MOVEMENT IN SLEEVE ASSY. REMOVED SLEEVE ASSY DUE TO EXCESSIVE WEAR ON SLEEVE. ID BEARING GLOVES ASSY TSN 298.7 HRS. INSTALLED NEW SLEEVE, P/N 206-010-454-108, S/N RE-6092, ONTO SWASHPLATE ASSY.SDR 95ZZZX5913Switch · inopFORWARD FUEL BOOST PUMP PRESSURE SWITCH INOPERABLE AT 878.8 HOURS. REMOVED SWITCH, P/N 7G547, S/N 31002, AND INSTALLED NEW SWITCH, P/N 7G547, S/N 32230.SDR 95ZZZX5711Hose · rupturedAIRCRAFT HAD HYDRAULIC FAILURE. HOSE FROM HYDRAULIC PUMP TO FILTER RUPTURED.SDR 95ZZZX5543Cyclic Stick · brokeDURING THE POST-FLIGHT INSPECTION, THE PILOT EXERCISED THE CYCLIC CONTROL WITH THE HYDRAULIC POWER OFF. DURING THIS PROCEDURE, THE CYCLIC STICK BROKE COMPLETELY OFF WHERE IT CONNECTS TO THE CYCLIC PIVOT LEVER. CYCLIC STICK BROKE IN THE SAME MANNER AS DESCRIBSDR HEEA955612Drive Shaft · overtempBOTH FORWARD YELLOW TEMP. INDICATORS TURNED BLACK. REPLACED WITH SERVICEABLE DRIVE SHAFT.SDR 95ZZZX5716Engine · flame-outHELICOPTER EXPERIENCED 3 ENGINE FLAME-OUTS WITHIN APPROXIMATELY 5 MINUTES. THE AUTO RE-IGNITION STARTED THE ENGINE IN-FLIGHT EACH TIME. NORMAL LANDING WAS ACCOMPLISHED. A COMPLETE INSPECTION OF THE FUEL SYSTEMS, CONTROL SYSTEMS, FUEL FILTERS, AIR FILTERS, FSDR 95ZZZX6092Support · crackedDURING NDT INSPECTION FOR OVERHAUL, FOUND CRACK ON EARS OF SUPPORT FOR FLAP RESTRAINT.SDR CA950828013Switch · corrosion(CAN)ELECTRICAL TERMINAL STUD CORRODED, BROKE OFF WHEN NUTS WERE TIGHTENED.SDR HEEA955597Bearing · crackedBLADE BEARING CRACKED. ALSO DISCARDED 4 EACH SLEEVES P/N 206-010-733-003. BEARINGS SCRAPPED LOCALLY.SDR 95ZZZX4073Governor · malfunctionFROM CRUISE, A LOW POWER DESCENT INITIATED. WHEN POWER APPLIED, ENGINE RPM DECREASED. PILOT ENTERED AUTOROTATION, POWER REAPPLIED AND ENGINE FLAME-OUT OCCURRED. ENGINE RE-STARTED AND 95 PERCENT N2, BUT WHEN POWER APPLIED FOR LANDING, ENGINE FLAME-OUT. AUTOSDR HEEA955581Bracket · crackedRECEIVED NEW HANGER BEARING BRACKET WITH CRACKED, AFT VERTICAL FLANGE IN CENTER OF BRACKET.SDR HEEA955560Freewheel · making metalFREEWHEEL MAKING METAL. REPLACED FREEWHEELING UNIT.
Back to Bell 206B