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 = '206L3' 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 = '206L3' 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 EVCA2026100126Blower Motor · unserviceableELECTRICAL SMELL WHEN AIR CONDITIONER IS TURNED ON. AFT BLOWER MOTOR WAS THE CAUSE. SYSTEM MEL'ED UNTIL A REPLACEMENT ARRIVES.SDR EVCA20250623001Pump · failedHYDRAULIC FAILURESDR EVCA202503250001Angle · crackedLH & RH FS 145 & STIFFENER CLIP CRACKEDSDR EVCA20250228001Stiffener · crackedUPPER BOX BEAM FWD STIFFENERS CRACKED. PN 206-033-110-229 & 206-033-110-197SDR EVCA20241204001Stiffener · crackedVERTICAL TUNNEL AFT RH STIFFENER CRACKED. VERTICAL TUNNEL SKIN CRACKED AT WL 65.0SDR EVCA202406240002Blade · crackedM/R BLADE INBOARD TRIM TABS CRACKEDSDR EVCA202406240001Blade · crackedM/R BLADE INBOARD TRIM TABS CRACKEDSDR EVCA202404220002Heater · odorBURNING SMELL FROM HEATER, COULD NOT DUPLICATE.SDR EVCA202402190024Unknown · odorSTRONG FUEL SMELL IN AIRCRAFT ON STARTUP. AMT PULLED HAT RACK AND FUEL VALVE COVER, PERFORMED VISUAL INSPECTION AND NO LEAKS DETECTED. PERFORMED GROUND RUN AND LEAK CHECK OF ENGINE - NO LEAKS DETECTED. SIGNED OFF AS NO DISCREPANCIES NOTED.SDR EVCA202308220002Stiffener · crackedR/H FS 145 STIFFENER CLIP CRACKED.SDR EVCA202308220001Frame · crackedL/H FS 145 FRAME CRACKED.SDR EVCA08222023Stiffener · crackedL/H FS 145 STIFFENER CLIP CRACKED.SDR EVCA03102023Blade · unserviceableMR BLADE TRIM TAB CTRACKEDSDR EVCA20230119001Stiffener · crackedLEFT HAND VERTICAL TUNNEL STIFFENER IS CRACKED ON UPPER ENDSDR EVCA01122023Fuel Control · leakingFUEL SMELL IN CABIN UPON TAKE OFF. FOUND FUEL SEEP AT FUEL CONTROL UNIT.SDR EVCA010320233Ring · cracked1/2 INCH CRACK AT UPPER LH INBOARD SIDE OF TAILBOOM RING.SDR EVCA2023010300001Hose · crackedHOSE CRACKED AT THE ATTACHMENT FITTING CAUSING A LOSS OF HYDRAULIC FLUID AND THE LOSS OF HYDRAULIC ASSISTED FLIGHT CONTROLS.SDR EVCA202212200001Unknown · odorFUEL SMELL IN CABIN UPON TAKE OFF. NO DISCREPANCIES NOTED DURING INSPECTION. COULD NOT DUPLICATE.SDR EVCA202211230022Stiffener · crackedSTIFFENER AT FORWARD EDGE OF BOX BEAM IS CRACKED ON RH SIDE (.2 INCH).SDR 2022FA0000299None · malfunctionedPILOT REPORTED THE FOLLOWING: "AT ROUGHLY 230 P.M., I WAS MAKING MY WAY BACK FROM A NORTH CANYON TOUR LANDING SOUTH TAKEOFF WEIGHT 3767 POUNDS. WINDS WERE ABOUT 9 KTS GUSTING 18 FROM THE DIRECTION OF A ABOUT 220 AND I RECEIVED VERY LITTLE TO NO TURBULENCE THOSDR EVCA102921Angle · crackedDOING A VISUAL INSPECTION FOUND THE RH 145 BULKHEAD UPPER ANGLE CRACKED AROUND FASTENERS.SDR EVCA102521(2)Bracket · crackedLH PASSENGER DOOR OPENER BRACKET IS CRACKED.SDR EVCA102521Ring · crackedUPPER LH ATTACHMENT FITTING ON TAILBOOM RING IS CRACKEDSDR EVCA08192021Bulkhead · crackedWHILE DOING THE 300 HOUR PERIODIC INSPECTIONS WE NOTICED WORKING RIVETS AT STA. 145. WE OPENED ON THE BULKHEAD PANELS AND USED A BORESCOPE AND FOUND A CRACK ON THE RH 145 BULKHEAD FLANGE ATTACHED TO THE ROOF.SDR EVCA06182021Blade · damagedMAIN ROTOR BLADE SPAN-WISE WEIGHT COVER SEPARATED FROM BLADE IN FLIGHT.SDR EVCA06022021Blade · damagedMAIN ROTOR BLADE SPAN-WISE WEIGHT COVER SEPARATED FROM BLADE IN FLIGHT.SDR EVCA051720212Panel · crackedPILOT'S CRUSH PANEL IS CRACKED AT THE CENTER NUTPLATE. WE WILL REPLACE THE CRUSH PANEL.SDR EVCA0517211Skin · debondedLEFT HAND ELEVATOR TRAILING EDGE IS DEBONDED THE ENTIRE LENGTH OF THE ELEVATOR. WE WILL REPLACE THE PART.SDR EVCA2020093003Disc Pack · corrodedDURING ROUTINE INSPECTION, NR 6 TAIL ROTOR DRIVE SHAFT DISC PACK HAS CORROSION BETWEEN DISCS.SDR EVCA202009183Combustion Liner · crackedDURING INSPECTION, CRACKS WERE VISUALLY FOUND ON THE ENGINE COMBUSTION LINER.SDR EVCA2020031611Attach Fitting · crackedUPPER L/H TAILBOOM ATTACH FITTING CRACKED. REMOVED DAMAGED FITTING PN 206-032-409-001P AND INSTALLED NEW FITTING PN 206-032-409-001P IAW BHT-206-SRM-1 6-3-1.SDR EVCA2020011700000Bulkhead · crackedDURING PERIODIC INSPECTION, FOUND LT BULKHEAD AT FS 145 UPPER FLANGE CRACKED AT RIVET ATTACHMENT.SDR IAVA2019101600001Skin · crackedCRACK ON UPPER TAIL BOOM SKIN AT STATION 172 FROM 3RD RIVET FORWARD OF CASTING ON SKIN SPLICE SEAM TO 4TH RIVET AT TAIL ROTOR GEARBOX CASTING ATTACHMENT RIVET LINE.SDR EVCA201910100003Blade · corrodedBOTH RED & WHITE MR BLADES HAVE CORROSION IN BLADE PIN RETENTION RECEPTACLES. REMOVED MR BLADE ASSY(S). PN: 206-015-001-115, SN(S) BH482876 & BH482878, AND REPLACED WITH SERVICEABLE MR BLADES PN: 20633000-101, SN(S): A074 & A075. SEE FAA FORM 337 DATED 10/8/2SDR W7OA20200204001Blade · damagedTHIS IS OUR SECOND SET OF VAN HORN AVIATION TAIL ROTOR BLADES PN 2062200-301 THAT WE HAVE ENCOUNTERED CRACKS/DEBONDING IN THE LOWER/UPPER LEADING EDGES AND SKIN OF THE BLADES. OUR FIRST SET HAD A TOTAL TIME OF 1821.3 HOURS WHEN THE CRACKS/DEBONDING (UPPER LEASDR EVCA2019050800001Connector · burnedCREW REPORTS ELECTRICAL BURNT SMELL IN REAR CABIN WHEN AIR CONDITIONING TURN ON. REPLACED 2 EACH WIRE CONNECTORS ON AIR CONDITIONER COMPRESSOR RELAY P/N RC10-250F IN ACCORDANCE WITH SERIES ELECTRICAL SYSTEM INSTALLATION DWG. NO. 206EC-856 AND BHT-ELEC-SPM CHAPSDR EVCA2019050200000Structure · crackedONE INCH CRACK FOUND ON UPPER TOP DECK. IT IS LOCATED AT STA 147, WL 72, AND BL 11.SDR 2019FA0000069Bulkhead · crackedDURING AN OAS INSPECTION A SMALL CRACK WAS FOUND ON THE TOP RIGHT HAND SIDE OF THE AFT FUSELAGE BULKHEAD P/N 206-032-308-003, NEXT TO THE TAILBOOM ATTACHMENT BOLT HOLE. AFTER FINDING THE CRACK ON THIS AIRCRAFT WE QUICKLY INSPECTED OUR A/C. IT ALSO HAS THE SAMESDR EVCA201809052Attach Fitting · crackedTAILBOOM ATTACHMENT FITTING UPPER LEFT TAILBOOM SIDE CRACKED. AMT'S REMOVED AND REPLACED TAILBOOM FITTING.SDR EVCA20180618181Structure · crackedDURING INSPECTION, A CRACK WAS SUSPECTED IN EXTRUSION NEAR BS 73 OVER THE RT FWD LANDING GEAR FITTING. REMOVED AND REPLACED THE CRACKED EXTRUSION.SDR EVCA20180523211Mount Flange · crackedWHILE PERFORMING A SCHEDULED 100 HR INSPECTION, A CRACK WAS FOUND ON THE TAILBOOM MOUNTING RING PN: 206-032-400-027 APPROXIMATELY 3 INCHES IN LENGTH BELOW THE UPPER LEFT ATTACHMENT FITTING.SDR EVCA201803090001Structure · corrodedPILOT DISCOVERED A CRACK IN WING WALK COMPOUND LOCATED ON THE RT CABIN ROOF. INVESTIGATED AND FOUND CORROSION UNDER THE WING WALK COMPOUND.SDR EVCA201802061Attach Fitting · crackedDURING SCHEDULED INSPECTION AND COMPLIANCE WITH FAA AD 2013-25-10 MAINTENANCE TECHNICIAN FOUND A 1.125" CRACK IN UPPER LEFT HAND TAILBOOM ATTACH FITTING PN: 206-032-409-001. UPON REMOVAL OF THE TAILBOOM FROM THE AIRCRAFT TO FACILITATE REPAIR MAINTENANCE TECHNISDR EVCA201708260001Connector · burnedFLIGHT CREW REPORTED A BURNING ODOR EMANATING FROM THE AFT CABIN. DURING INSPECTION, IT WAS DISCOVERED THAT THE CONNECTOR TO THE TRANSPONDER CONTROL UNIT IN THE INSTRUMENT PANEL SHOWED SIGNS OF OVERHEATING AND MELTING. CONTACTS APPEAR TO HAVE SHORTED CAUSING TSDR EVCA201705301Tube · damagedWHILE PERFORMING INSPECTION OF THE AIRCRAFT, FOUND ONE CYCLIC TUBE TO HAVE THE FIXEDAND NON ADJUSTABLE CLEVIS ON THE TRANSMISSION BELLCRANK END OF THE CONTROL TUBE TO BE ROTATING WITHIN THE TUBE.SDR EVCA201611021Blower Motor · burnedDURING FINAL APPROACH TO SCHEDULED LANDING PILOT AND FLIGHT CREW REPORTED SMELLING A STRONG ELECTRICAL BURNING SMELL. UPON MAINTENANCE INSPECTION FOUND THE ARMATURE OF THE AFT AIR CONDITIONING EVAPORATOR BLOWER MOTOR TO SHOW EVIDENCE OF EXCESSIVE HEAT. THERESDR AC2R2016052301Structure · crackedCRACK ON LT SIDE OF ACFT AFT LOWER SHELL, AT BS 140-150. CRACK IS FROM WL 35-54, BL 26. CRACK IS ADJACENT TO TIEDOWN, STEP WHICH IS MOUNTED TO AIRFRAME. CRACK WAS CAUSED BY HIGH WINDS MOVING ACFT, WHILE THE ACFT WAS STILL TIED TO HELI-DECK.SDR EVCA20160215001Angle · crackedFOUND CRACKS AT BOX BEAM INTERFACE WITH FWD VERTICAL CONTROL TUNNEL ON RT SIDE. FOUND ANGLE, PN 206-033-110-229 & WEB PN 206-033-110-183, CRACKED. MAXIMUM CRACK LENGTH OF APPROX 2 INCHES.SDR EVCA201512281Blower Motor · inoperativeIN FLIGHT CREW REPORTED ELEC BURNING SMELL. ACFT RETURNED TO BASE. UPON INSPECTION FOUND FAIL AFT AIR CONDITIONER BLOWER MOTOR.SDR CA160119009Rotor · separated(CAN) ACFT WAS ON AN AERIAL APPLICATION MISSION WHEN IT WAS REQUIRED TO MAKE A FORCED LANDING. INITIAL REPORTS STATE THE TAIL ROTOR SEPARATED FROM THE ACFT.
Back to Bell 206L-3