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 97ZZZX220Lever 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 96ZZZX5841Blade · wornDURING NORMAL AIRCRAFT USAGE NEW YORK HELICOPTER HAS NOTED THE LEADING EDGE OF THE MAIN ROTOR BLADE IS EXPERIENCING ABNORMAL WEAR IN THE FORM OF SCALING/SPLINTERING ON A MODERATE LEVEL. NEW YORK HELICOPTER IS AWAITING RECOMMENDATIONS FROM BELL HELICOPTER TEXTSDR 97ZZZX235Lever Assy · wornDAILY INSPECTION FOUND BEARINGS AND SPACERS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-01 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH NAS6605D64 BOLTS. NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. WORN PARTS TT 310.3 HOURS.SDR 97ZZZX233Lever Assy · wornDAILY INSPECTION FOUND BEARINGS AND SPACERS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206010-337-001 BEARINGS, 2 EACH NAS6605D64 BOLTS. NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. WORN PARTS TT 330.3 HOURS.SDR 97ZZZX232Lever Assy · wornDAILY INSPECTION FOUND BEARINGS AND SPACERS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH NAS6605D64 BOLTS. NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. WORN PARTS TT 293.1 HOURS.SDR 97ZZZX2672Seal · leakingREPLACED FREE WHEELING UNIT TAIL ROTOR OUTPUT DRIVE SEAL DUE TO LEAKING OIL.SDR HEEA968053Indicator · stuckNEEDLE STUCK ON ZERO AND WOULD NOT INDICATE. TIME SINCE REPAIR 138:20.SDR 96ZZZX5573Tail Boom · loose rivetsDURING 100-HOUR INSPECTION MECHANIC NOTED 9 EA RIVETS LOOSE BY THE TAIL ROTOR GEARBOX AT STATION 174.105.SDR 96ZZZX5513Lever 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. SUBMITTESDR CA960924022Blade · separation(CAN) SKIN SEPARATION FROM LEADING EDGE OF BOTH BLADES.SDR HEEA967800Stiffener · crackedSTIFFENER IS CRACKED. (CRACKED AT TOP IN BENT ARM 4 7/8 FROM TOP EDGE. REPLACED WITH SERVICEABLE STIFFENER.SDR HEEA967797Bulkhead Assy · crackedFORWARD BULKHEAD ASSY CRACKED AT 3 EACH ATTACHMENT SHIM LOCATIONS. FOUND CRACKS DURING COMPLIANCE OF T.B. 206L-94-169. ALSO FOUND SEVERAL LOOSE RIVETS ATTACHING TAIL ROTOR GEARBOX SUPPORT FITTING TO AFT END OF TAILBOOM ASSY AND SEVERAL LOOSE(WORKING) RIVETS SDR 97ZZZX234Blade · corrodedDURING DAILY INSPECTION FOUND BLADE SKIN CORROSION AND DELAMINATION AT BLADE TIP.SDR 96ZZZX5165Switch · failedPILOT REPORTED SEEING SMOKE APPEAR FROM THE AIR CONDITIONER VENTS AND BY GROUND PERSONNEL SEEING SMOKE APPEAR FROM TAILBOOM AND AIR CONDITIONER DUCT AREAS. INSPECTION OF THE AIR CONDITIONER SYSTEM REVEALED THE HIGH PRESSURE SWITCH FAILED CAUSING THE RECEIVER/SDR HEEA967676Clamp · failedDURING VISUAL CHECK OF START/GENERATOR FOUND HEAD OF "T" BOLT BROKEN OFF AND LAYING IN ENGINE PAN. CLAMP HAD REMAINED ON STARTER GEN BUT WAS UNCOUPLED. REPLACED WITH SERVICEABLE CLAMP.SDR 96ZZZX5512Link 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. SUBMITTESDR 96ZZZX5511Lever 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. SUBMITTESDR HEEA967636Indicator · stuckTOT NEEDLE STUCK ON ZERO, WON'T INDICATE.SDR 96ZZZX3967Hub · stiffPILOT NOTED THAT WITH INCREASED RPM, TAIL ROTOR PEDALS BECAME STIFF. THE T/R BLADE FEATHERING BEARINGS WERE NOT FOUND TO BE CRACKED. TAIL ROTOR HUB ASSY WAS REMOVED AND VISUALLY INSPECTED IAW BELL 206L-4 MM. NO OBVIOUS DEFECTS HAVE BEEN NOTED. A THOROUGH TSDR 96ZZZX4842Drive Shaft · wornDURING DISASSEMBLY FOR OVERHAUL, FOUND WORN DRIVESHAFT SPLINES (SMALL END) AND WORN INTERNAL GEAR SPLINE. (PARTS SCRAPPED). SUSPECT IMPROPER LUBRICATION.SDR CA960605006Door · cracked(CAN) DURING FLIGHT THE TWO REAR DOORS OPENED COMPLETELY. THE RIGHT REAR DOOR STARTED TO VIBRATE AND BROKE AT STATION 116 AT THE INTERIOR REINFORCEMENT.SDR 96ZZZX3413Bearing · failedTHE ENGINE CHIP DETECTOR LIGHT ILLUMINATED IN CRUISE FLIGHT OVER THE GULF OF MEXICO. THE PILOT LANDED THE HELICOPTER ON NEAREST OFFSHORE PLATFORM, APPROXIMATELY 7 MILES AWAY. MAINTENANCE INSPECTED THE CHIP DETECTOR PLUGS AND FOUND THE LOWER PLUG COVERED WITHSDR HEEA967162Link Assy · rubber separateLINK ASSY RUBBER SEPARATION AT LOWER BEARING.SDR 96ZZZX3162Transceiver · burned smellWHEN VHF CIRCUIT BREAKERS WERE PUSHED IN, THE FREQUENCY INDICATOR LIGHTS FLASHED ON/OFF. DURING HOVER TO THE MAINTENANCE PAD FROM THE BACK ROW, PILOT SMELLED FUMES. REMOVED VHF RADIO AND INSTALLED SERVICEABLE RADIO AND REMOVED BURNED SMELL. VISUALLY INSPECTSDR 96ZZZX3412Fitting · crackedDURING SERVICE CHECK, NOTED FORWARD CROSSTUBE FITTING WAS CRACKED. FITTING WAS FOUND CRACKED IN THE SAME AREA AS REPORTED ON MDR SUBMITTED ON 2-7-94. THE FITTING WAS MANUFACTURED IN OCTOBER, 1992, WHICH IS DIFFERENT FROM THE PREVIOUSLY REPORTED CRACKED FITTISDR CA970513007Saddle · cracked(CAN) SKID GEAR SHIFTED LATERALLY ALLOWING SADDLE TO WEAR ON LUG ON SKID CROSS TUBE.SDR 96ZZZX3019Fitting · chafedFORWARD CROSS TUBE STRAP ASSY WORN INTO RIGHT FORWARD CROSS TUBE FITTING. REPLACED FITTING PER PRODUCT SUPPORT WEAR LIMITS.SDR 96ZZZX2934Seal · leakingDURING FLIGHT, THE TRANSMISSION PRESSURE CAUTION LIGHT ILLUMINATED. THE PRESSURE GAUGE INDICATED 30 PSI. DURING FINAL APPROACH, PRESSURE DROPPED TO 20 PSI AND TO 10 PSI DURING HOVER. UPON LANDING, PRESSURE RETURNED TO 25 PSI. AIRCRAFT WAS INSPECTED AND THESDR 96ZZZX2447Fitting · crackedDURING SERVICE CHECK, NOTED MLG FITTING WAS CRACKED. FITTING WAS FOUND CRACKED IN THE SAME AREA AS REPORTED ON MDR SUBMITTED ON 2-7-94. THE FITTING WAS MANUFACTURED IN OCTOBER, 1992, WHICH IS DIFFERENT FROM THE PREVIOUSLY REPORTED CRACKED FITTINGS.SDR 96ZZZX2192Exhaust Stack · crackedDURING A DAILY INSPECTION AT THE LAST FLIGHT OF THE DAY, THE MECHANIC NOTED THE ENGINE EXHAUST STACK WAS CRACKED. THE CRACK ORIGINATED AT THE CENTER WELDED SEAM APPROXIMATELY 2 INCHES FROM THE FLANGE ON THE FORWARD SIDE OF THE STACK. THE CRACK CONTINUED DOWNSDR 96ZZZX2201Link Idler · wornDAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH PN 206-010-338-001 SPACERS, 4 EACH PN 206-010-337-001 BEARINGS, 2 EACH PN 206-010-338-003 BUSHINGS, 2 EACH PN NAS6605D64 BOLTS, AND 1 EACH PN 206-010-470-101SDR 96ZZZX2200Lever Assy · wornDAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH PN 206-010-338-001 SPACERS, 4 EACH PN 206-010-337-001 BEARINGS, 2 EACH PN 206-010-338-003 BUSHINGS, 2 EACH PN NAS6605D64 BOLTS, AND 1 EACH PN 206-010-470-101SDR 96ZZZX2203Link Idler · wornDAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH PN 206-010-338-001 SPACERS, 4 EACH PN 206-010-337-001 BEARINGS, 2 EACH PN 206-010-338-003 BUSHINGS, 2 EACH PN NAS6605D64 BOLTS, AND 1 EACH PN 206-010-470-101SDR 96ZZZX2202Lever Assy · wornDAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH PN 206-010-338-001 SPACERS, 4 EACH PN 206-010-337-001 BEARINGS, 2 EACH PN 206-010-338-003 BUSHINGS, 2 EACH PN NAS6605D64 BOLTS, AND 1 EACH PN 206-010-470-101SDR 96ZZZX1592Wire Rope · brokenDURING A FUEL STOP ON A NORMAL WALK-AROUND, PILOT NOTICED SOMETHING HANGING DOWN BELOW THE CARGO HOOK. FURTHER INVESTIGATION FOUND THE CARGO HOOK EMERGENCY RELEASE CABLE BROKE COMPLETELY THROUGH 2 INCHES FROM CONNECTION ON CARGO HOOK.SDR 96ZZZX1810Tank Assy · wornWHILE PERFORMING A 100-HOUR INSPECTION, THE MECHANIC NOTED THE BOLTS SECURING THE ENGINE OIL TANK TO THE SUPPORT WERE FOUND WEARING INTO THE TANK FLANGE, ON THE FORWARD END OF TANK. SUBMITTER BELIEVES BOLTS SECURING THE TANK TO SUPPORT HAD WORN INTO THE FLANGSDR 96ZZZX2340Bearing · groovedAT 3,000-HOUR OVERHAUL, BEARING ROLLER FOUND TO HAVE DEEP GROOVE ON ONE ROLLER, SCRAPPED BEARING.SDR 96ZZZX1813Bearing · pittedFOUND AT 3,000-HOUR OVERHAUL, MAST BEARING OUTER RACE THRUST AREA HAS PITTED AREA - SCRAPPED BEARING.SDR 96ZZZX2344Link 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, AND 1 EACH 206-010-470-101 BEARING. SUSPSDR 96ZZZX2343Lever 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, AND 1 EACH 206-010-470-101 BEARING. SUSPSDR CA960129026Seal · leaking(CAN)SEAL LEAKING TO THE POINT WHERE OIL HAS TO BE ADDED DAILY.SDR CA960129025Seal · leaking(CAN)SEAL LEAKING. OIL HAS TO BE ADDED AT THE RATE OF 1 QUART PER 30 HOURS OF OPERATION.SDR CA960129024Seal · leaking(CAN)SEAL LEAKING. OIL HAS TO BE ADDED DAILY.SDR CA960129023Seal · leaking(CAN)SEAL LEAKING. REQUIRES OIL TO BE ADDED TO GEARBOX DAILY.SDR CA960129022Seal · unseats(CAN)WHILE GREASING HEAD THE SEAL BECOME DISLODGED AND MOVE INBOARD, AND HAVE TO BE RESEATED.SDR 96ZZZX2342Link 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, AND 1 EACH 206-010-470-101 BEARING. SUSPSDR 96ZZZX2341Lever 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, AND 1 EACH 206-010-470-101 BEARING. SUSPSDR CA960111021Frame · cracked(CAN)CRACK FOUND ON TOP AFT RADIUS OF ANGLE P/N 206-032-308-005 ATTACHED TO STN 217.84 FRAME P/N 206-032-307-109.SDR 96ZZZX300Pitch Horn · loose studDURING DAILY INSPECTION, FOUND THE PITCH LINK STUD ON THE PITCH HORN WAS LOOSE. SUSPECT CAUSE IS THE STUD WAS NOT PERMANENTLY SECURED AT THE FACTORY. ALSO, THE PITCH HORN WAS NOT PROPERLY TORQUED AT THE FACTORY CAUSING THE PITCH HORN TO BECOME LOOSE ON THE TSDR 96ZZZX281Link Idler · wornDURING DAILY 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.
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