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 CA970311002Seal · leaking(CAN) NR 1 SEAL LEAKING. PART TC: 11,543.SDR CA970226068Pivot Support · cracked(CAN) PIVOT SUPPORT FOUND CRACKED FROM FRICTION SPLIT TO BASE OF SUPPORT. APPROXIMATELY 1" CRACK.SDR 97ZZZX1142Indicator · burnedDURING NORMAL FLIGHT, PILOT NOTICED A BURNING SMELL. SHORTLY THEREAFTER, COCKPIT BEGAN TO FILL WITH SMOKE. AN EMERGENCY LANDING WAS MADE WITHOUT INCIDENT. MECHANIC FOUND ART HORIZ INOP AND BURNED INTERNALLY. (HEAVY SMOKE ON INSTRUMENT GLASS.) INSTRUMENT RESDR CA970304001Cylinder Support · cracked(CAN) DURING 100 HOUR INSPECTION OF THE UPPER DECK FLIGHT CONTROLS, A CRACK WAS FOUND IN THE FORWARD R/H WEB ON THE TOP EDGE.SDR HEEA979104Mount · separationMOUNT SEPARATION BEYOND LIMITS.SDR HEEA979066Indicator · failedINDICATOR NEEDLE WILL NOT GO PAST 4%. REPLACED WITH SERVICEABLE GAUGE.SDR HEEA979063Transponder · inoperativeTRANSPONDER MODE C INOPERATIVE. PERFORMED PRELIMINARY INSPECTION. FOUND POWER OUT LOW, ADJUSTED V101. NO HELP. REPLACED V101 CAVITY TUBE P/N C2080A. REPAIRED. BENCH CHECK GOOD.SDR CA970227006Hydraulic Pump · sheared(CAN) HYDRAULIC PUMP DRIVE SHAFT SHEARED AT A POINT JUST BEFORE THE SPLINE AREA.SDR CA970311090Case · worn(CAN) ENGINE POWER CHECK DOWN. COMPRESSOR CASE WAS FOUND WORN AND PIECES FOUND MISSING FROM LINING AT 4TH AND 5TH STAGES.SDR CA970311089Pylon Support · loose(CAN) BEARING LOOSE, TEFLON COMING OFF BEARING.SDR CA970212005Line · split(CAN) SPLIT PITOT LINE CONNECTING PITOT TUBE TO THE PITOT DRAIN AND PITOT SYSTEM. SUSPECT WATER FROZE IN LINE AND CAUSED IT TO SPLIT.SDR CA970206015Bolt · cracked(CAN) WHILE BUILDING UP AN ENGINE AND INSTALLING A COMPRESSOR, THE BOLT USED TO RETAIN THE COMPRESSOR TO THE GEARBOX. IT WAS A NEW BOLT, BUT UPON CLOSE EXAMINATION USING A GLASS, A CRACK WAS FOUND WHERE THE LANDS CONVERGE.SDR 97ZZZX902Servo · bindingNOTED BINDING IN-FLIGHT CONTROLS. REPLACED RT SERVO. INTERNAL PROBLEMS DUE TO BEING CLOSE TO TBO.SDR 97ZZZX901Hose · leakFOUND HYDRAULIC LEAK CAUSED BY CHAFING AT ADEL CLAMP SECURING HOSE TO DECK. REPLACED LINE AND INSTALLED SERVICEABLE ADEL CLAMP, P/N MS21919WDG9.SDR HEEA978939Sensor · malfunctionSENSOR DOES NOT TRANSMIT FUEL QTY WHEN TANK IS FULL.SDR CA970311084Circuit Breaker · worn(CAN) FORWARD BOOST PUMP INTERMITTANT. NOT SWITCHING ON. CIRCUIT BREAKER WORN.SDR CA970311083Blower Assy · vibration(CAN) BLOWER ASSY DEVELOPED A VIBRATION SHORTLY AFTER INSTALLATION. BUTTERFLY VALVE WAS CRACKED AND SQUIRREL CAGE OF BLOWER WAS LOOSE DUE TO BEARING FAILURE.SDR 97ZZZX900Tail Boom · crackedAT 100 HOUR INSPECTION, CRACK WAS FOUND AT LEFT HAND REAR ATTACH POINT FOR TAIL ROTOR GEARBOX. CRACK WAS .25 INCH LONG AND EXTENDED THROUGH THE MOUNT HOLE. CRACK WAS ONLY VISIBLE FROM INSIDE THE TAIL BOOM.SDR CA970311081Sending Unit · failed(CAN) FUEL SENDING UNIT SENDING ERRONEOUS READINGS. DROPPING FROM 15-20 GALS TO ZERO.SDR CA970311080Cooler · corrosion(CAN) PRIOR TO INSTALLATION, THE INSPECTION REVEALED CORROSION AT BOTH THE INLET AND OUTLET PORTS, AS WELL AS A SUBSTANTIAL AMOUNT ON THE BYPASS VALVE.SDR CA970219003Tube Assembly · corroded(CAN) ALUMINUM MAIN FUEL SYSTEM SUPPLY TUBE HAS A STEEL SLEEVE BETWEEN THE "B" NUT AND THE TUBE (FLARE), THIS SLEEVE WAS FOUND BADLY CORRODED. THE TUBE FLARE AND ADJOINING FITTING WERE ALSO CORRODED ALMOST TO THE POINT OF FAILING.SDR CA970311076Filter · wrong part(CAN) FACET OIL FILTER FOUND INSTALLED IN ENGINE OIL SCAVENGE FILTER LOCATION DURING 200 HOUR CHECK.SDR CA970311074Seal · leaking(CAN) T/R ASSY INPUT SEAL FOUND LEAKING EXCESSIVELY.SDR CA970421056Gear · worn(CAN) REAR ADAPTER SPLINES WORN WELL BEYOND LIMITS.SDR AU970150Starter Gen · faulty(AUS) STARTER/GENERATOR HAD EXCESSIVE ARMATURE BALANCE BAND GRINDING TO ACHIEVE BALANCE - PERSONNEL/MAINTENANCE ERROR - UNAPPROVED REPAIRSDR CA970211003Linear Actuator · cracked(CAN) ACTUATOR EXTEND LIMIT SWITCH HOUSING WAS FOUND CRACKED. A RIGGING CHECK WAS CARRIED OUT, NO LIMITS EXCEEDED.SDR 97ZZZX786Seal · under spec3 HOURS AFTER SEAL INSTALLATION, PILOT NOTICED OIL LEAK IN STARTER/GEN AREA DURING PREFLIGHT INSP. DURING GROUND RUN, ENG OIL WAS FOUND TO BE LEAKING AT A RATE OF 12 DROPS PER MINUTE. STARTER/GEN WAS REMOVED AND P/N A6854424 WAS FOUND HALF OUT OF SEAL BORE. SDR CA970528021Bypass Valve · stuck(CAN) UNABLE TO ADJUST START CYCLE COMPRESSOR STALLING AND FAST EXCELLERATION OF N1 RPM NOTED AT 20 PER N1 FUEL PRESSURE WAS NOTED AS HIGH AS +30 PSI. POSSIBLE BYPASS VALVE STUCK OPEN. REPLACED.SDR CA970528020Fuel Control · loose(CAN) GROUND IDLE RPM DROPPED TO 57 PERCENT N1 IDLE SPEED. ADJUSTMENT SCREW FOUND TO BE EASY TO ROTATE BY HAND. NO BUILT IN FRICTION FELT. REASON FOR LAST REMOVAL. REPLACED.SDR 97ZZZX208Gps · malfunctionGPS CONTINUALLY DUMPS ALL INFORMATION WITHOUT WARNING AND DISPLAYS A FAILURE CODE. NR 08. REPLACED WITH SERVICEABLE UNIT.SDR 97ZZZX201Pump · seal leakHYDRAULIC PUMP LEAKING STATICALLY AT INPUT SEAL. TBO TIME IS 3600 HRS ON THIS COMPONENT. REPLACED WITH SERVICEABLE UNIT.SDR HEEA968685Linear Actuator · faultyINSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND ACTUATOR RETRACTED VERY SLOW AND INTERMITTENTLY. FOUND VENDOR REPAIRED MOTOR WAS DEFECTIVE.SDR 97ZZZX206Hose · leakingENGINE DRIVEN FUEL PUMP INLET LINE LEAKING AT FLARE FITTING DUE TO A CRACK. REPLACED WITH SERVICEABLE LINE.SDR 97ZZZX405Support · corrodedDURING REPAIR IN LANDING LIGHT BAY AREA, MECHANIC NOTED BELLCRANK SUPPORT P/N 206-030-111-3 EXCESSIVELY CORRODED. REPLACED BELLCRANK AND SUPPORT P/N 206-030-111-003.SDR GJQR9600100Blade · debondedBLADE REPLACED DUE TO DEBOND DETECTED DURING POST FLIGHT. BLADE MAKES CLICKING SOUND AND DELAMINATION PRESENT AT BLADE ROOT DOUBLER AREA. (X)SDR 97ZZZX207Washer · crackedDURING A WEEKLY INSPECTION THE M/R BLADE BOLT LOWER WASHER WAS FOUND CRACKED. REMOVED WASHER. INSTALLED SERVICEABLE WASHER. ACFT TT 8079.6.SDR HAIGJQR0100Blade · debondedBLADE REPLACED DUE TO DEBOND DETECTED DURING POST FLIGHT. BLADE MAKES CLICKING SOUND AND DELAMINATION PRESENT AT BLADE ROOT DOUBLER AREA. REPLACED WITH CSF STOCK.SDR 97ZZZX101Panel · shortedWHILE IN-FLIGHT, THE PILOT NOTICED SMOKE AT THE CABIN OVERHEAD. AFTER MAKING PRECAUTIONARY LANDING, IT WAS NOTED THAT THE INSTRUMENT CIRCUIT BREAKER HAD POPPED. INVESTIGATION BY MAINT. REVEALED THAT THE LIGHTED PANEL HAD INTERNALLY SHORTED. THE PANEL WAS RESDR CA970311073Support · cracked(CAN) SUPPORT WAS CRACKED IN FORWARD UPPER RIGHT HAND RADIUS. NO CRACKS ALLOWED IN THIS AREA. THIS DAMAGE WAS VISIBLE ONLY WITH FUEL CELL REMOVED. AIRCRAFT TT: 15,819 HOURS.SDR CA970311072Channel · misrepaired(CAN) UNAPPROVED REPAIR INCORPORATED. NO REPAIRS ALLOWED IN THIS AREA PER STRUCTURES REPAIR MANUAL.SDR 97ZZZX943Blade · separationDISCOVERED DURING DAILY INSPECTION FOUND CORROSION AND SEPARATION BENEATH LOWER GRIP DOUBLES AND BETWEEN LOWER SKIN AND SPAR. CORROSION ON TRAILING EDGE UPPER AND LOWER SURFACES.SDR CA970311064Bulkhead · cracked(CAN) BULKHEAD FOUND CRACKED BEYOND REPAIRABLE LIMITS.SDR CA970311063Stiffener · cracked(CAN) THE STIFFENER THAT IS LOCATED BENEATH THE DOUBLER FOR EXTERNAL SCAVENGE OIL FILTER KIT WAS FOUND CRACKED. ONE OF THE NUTS HOLDING THE OIL FILTER WAS LOCATED TOO CLOSE TO THE RADIUS OF THE STIFFENER WHICH WAS THE CAUSE OF THE CRACKSDR CA970311066Support · cracked(CAN) SUPPORT WAS CRACKED IN FORWARD UPPER RIGHT HAND RADIUS. NO CRACKS ALLOWED IN THIS AREA. DAMAGE ONLY VISIBLE WITH FUEL CELL REMOVED. AIRCRAFT TT: 14,949 HOURS.SDR CA970311065Support · corroded(CAN) SUPPORT CORRODED BEYOND REPAIRABLE LIMITS.SDR CA970311062Longeron · misrepaired(CAN) AN UNAPPROVED REPAIR WAS INCORPORATED ON THE ENGINE LONGERON. THE STRUCTURAL REPAIR MANUAL DOES NOT ALLOW REPAIR OF THIS ASSY.SDR CA970311061Stiffener · chafed(CAN) STIFFENER HAD EXCESSIVE CHAFING DAMAGE CAUSED BY ENGINE OIL TANK DRAIN LINE.SDR CA961203020Cap · worn(CAN) DURING A SWASHPLATE INSPECTION, GREASE WAS FOUND AROUND THE TOP SEAL. COVER REMOVED AND SEAL AND CAP REPLACED.SDR CA970327011Bolt · misinstalled(CAN) SERVO SENT FOR REPAIR. PER AD CF96-11R2 AND BELL SB 206-67A-01, A BOLT WAS FOUND SUSPECT. UNIT REPAIRED, BOLT REPLACED.SDR 97ZZZX346Bolt Nut · mismanufacturedPURCHASE NEW MAIN ROTOR BLADE NUT FROM BELL SERVICE CENTER. DURING INSTALLATION, IT BECAME EVIDENT THAT THREADED BORE OF NUT WAS NOT PERPENDICULAR TO BEARING FACE OF NUT. TORQUING NUT TO REQUIRED 215 FOOT/POUND WOULD PUT EXTREME STRESS LOADS ON NUT AND HOLLO
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