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 CA980406033Tunnel · cracked(CAN) AFT CROSSTUBE TUNNELS P/N 206-031-301-121 AND P/N 206-031-302-269 CRACKED IN NUMEROUS LOCATIONS.SDR CA980406032Longeron · cracked(CAN) ON INSPECTION, RIGHT LONGERON CRACKED.SDR CA980311004Sensor · cracked(CAN) DURING 1200 HOUR INSPECTION AN OIL MONITOR WAS FOUND CRACKED 360 DEG. OF RADIUS BETWEEN BOLT HEAD AND SHAFT.SDR CA980406036Mount · scored(CAN) ISOLATION MOUNT FOUND WITH DEEP SCORES AXIALLY AND RADIALLY.SDR CA980311010Jackshaft · cracked(CAN) CRACK DETECTED VISUALLY DURING INSPECTION. CRITICAL PART. ATTACHES PILOTS COLLECTIVE STICK TO AIRFRAME.SDR AU980262Main Rotor Sys · stoppage(AUS) MAIN ROTOR, TAIL ROTOR AND DRIVE SHAFT COMPONENTS - SUSPECT FOLLOWING DYNAMIC ROLLOVER ON 2/13/98.SDR CA980225005Bearing · split(CAN) INNER RACE SPLIT ON MAIN ROTOR TRUNNION BEARING.SDR CA980406031Pump · leaking(CAN) ENGINE DRIVEN FUEL PUMP DRAIN SEAL LEAKING BEYOND LIMIT. PUMP ALSO MAKING LOUD SQUEALS DURING START-UP.SDR CA970421052Exciter · stripped(CAN) STRIPPED THREADS ON CONNECTIONS, POSSIBLY CORROSION. REPLACED.SDR CA970421051Lead · stripped(CAN) STRIPPED THREADS ON LEAD CONNECTOR, CORROSION MAY BE CAUSE. REPLACED.SDR CA970421050Stud · loose(CAN) LOOSE STUD ON ENGINE ACCESSORY DRIVE GEARBOX. REPLACED.SDR CA970421049Nozzle · cracked(CAN) FUEL NOZZLE CRACKED BEYOND LIMITS. REPLACED.SDR CA980220001Blade · corroded(CAN) MAIN ROTOR BLADES REMOVED FROM HUB FOR MAINTENANCE. BLADE BORES WERE FOUND CORRODED BEYOND LIMITS. THIS 4TH TIME AFTER BORE BUSHING CHANGES THE CORROSION HAS REAPPEARED.SDR 98ZZZX815Gauge · failedN1 WILL NOT GO PAST 13 PERCENT ON START AND SMALL NEEDLE DOES NOT CORRELATE WITH OUTSIDE SCALE NEEDLE.SDR CA980317076Switch · failed(CAN) ''G'' SWITCH FAILED CAUSING SPONTANEOUS ACTIVATION OF UNIT.SDR CA980317080Connector · burned(CAN) CARGO HOOK RELEASE CABLE BURNT THROUGH DUE TO ARCING FROM DEFECTIVE PIN IN CARGO HOOK ELECTRICAL RELEASE CONNECTOR PLUG. WIRE WAS GROUNDING OUT THROUGH CARGO HOOK.SDR CA980317075Fcu · failed(CAN) ENGINE HAD HUNG START AT 25% NG. MAX LIGHT OFF TEMP AFTER FCU ADJUSTMENT OF ONE FULL TURN. FCU HAS 0.0 HOURS SINCE OVERHAUL.SDR CA980317085Fcu · out of adj(CAN) FCU RECEIVED WITH PAPERWORK TO INDICATE THE MAXIMIUM FLOW WAS SET TO 235 PPH AS PER INSTRUCTIONS. THE MAXIMUM FUEL FLOW SCREW WAS APPROX 1/16 DOWN FROM MAX MARK. CLOSER TO MAX MARK THEN MIN.SDR CA980317079Fcu · failed(CAN) ENGINE FLAMED OUT DURING START AT 55% NG AND AT 35-40% NG ON SUBSEQUENT ATTEMPT. FUEL CONTROL UNIT REPLACED.SDR CA970421038Ring Grooves · worn(CAN) FRONT SEAL RING GROOVES WORN BEYOND LIMITS.SDR AU980202Bearing · failed(AUS) TRANSMISSION FREE WHEEL ASSEMBLY FORWARD BEARING PNO206-040-205-005 AND SHAFT BEARING SURFACE PNO 206-040-222-005 FAILED.SDR 98ZZZX1426Exhaust Stack · crackedDURING A POST-FLIGHT INSPECTION, FOUND LT EXHAUST STACK CRACKED ALONG ENTIRE LENGTH OF TOP WELD SEAM. REMOVED AND REPLACED WITH SERVICEABLE ASSY.SDR 98ZZZX323Governor · failedGOVERNOR SLOW TO RESPOND TO POWER CHANGES (HIGH AND LOW SIDE).SDR 98ZZZX295Actuator · inoperativeINTERNAL MOTOR SHUT-OFF INOPERABLE.SDR 98ZZZX294Indicator · failedNO INDICATION ON N1 TACHOMETER GAUGE.SDR 98ZZZX293Cartridge · failedFUEL PUMP DOES NOT PUMP FUEL DUE TO FAILED CARTRIDGE.SDR CA980430001Blade · cracked(CAN) PILOT REPORTED MR VIBRATION. ENGINEER FOUND ONE CHORDWISE CRACK FROM THE BLADE SPAR TO THE TRAILING EDGE AT APPROX 90.5 INCHES FROM THE TIP.SDR CA971231009Line · leaking(CAN) FUEL NOTED DRIPPING FROM THE ENGINE COMPARTMENT OVERBOARD DRAIN. FUEL LINE BETWEEN FUEL CONTROL AND GOVERNOR LEAKING.SDR CA971231008Tube · cracked(CAN) AIR LINE FROM COMPRESSOR SCROLL TO GOVERNOR CRACKED AT FLARE AT SCROLL END. THIS CAUSED ENGINE TO GO TO IDLE.SDR CA980406022Switch · contaminated(CAN) AIRFRAME FUEL CAUTION LIGHT TEST SWITCH FAILED DUE TO FUEL LEAKAGE/CONTAMINATION IN THE ELECTRICAL PORTION OF THE SWITCH.SDR CA980406021Directional Gyro · overheated(CAN) COIL ON FORWARD END OVERHEATED AND FAILED CAUSING SMOKE AND FUMES IN COCKPIT.SDR 97ZZZX5131Drain Valve · crackedDURING 100-HOUR INSPECTION, BURNER DRAIN VALVE WAS FOUND CRACKED UNDER O-RING BOSS AREA.SDR 97ZZZX5157Indicator · failedATTITUDE GYRO INDICATOR WILL NOT HOLD ATTITUDE.SDR CA971216042Blower · vibrating(CAN) CASEY BLOWER MOTOR HAD EXCESSIVE VIBRATION AFTER OVERHAUL.SDR CA971216001Line · broken(CAN) RIGID LINE BETWEEN BLEED VALVE AND COMPRESSOR SCROLL FITTING ALMOST BROKEN OFF.SDR CA971216041Window · separated(CAN) LEFT CHIN BUBBLE WINDOW DEPARTED AIRCRAFT SHORTLY AFTER TAKEOFF. NO DAMAGE CAUSED.SDR CA971113054Plug · worn(CAN) N1 TACH GENERATOR INDICATION INTERMITTENT. CANNON PLUG PIN WORN AND PUSHED IN.SDR CA970311071Tach Generator · failed(CAN) ENGINE OUT LIGHTS AND HORN ACTIVATED DURING FLIGHT. N1 TACHOMETER INDICTING SYSTEM NOT WORKING. TACH LATER REMOVED AND FOUND TO HAVE NO PULSE ON ROTATION.SDR CA971113053Governor · failed(CAN) ROTOR RPM DROOPS TO 98 PERCENT WITH NO RECOVERY BY GOVERNOR. UNABLE TO ADJUST TO MAINTAIN PROPER RPM. TWO PREVIOUS REMOVALS FOR SAME REASON. PART TC: 2.SDR CA971219008Blade · cracked(CAN) COMPRESSOR BLADE FOUND CRACKED AT BASE AND BLADE LEADING AGAINST NEXT BLADE. ONLY .0312 INCH HOLDING BLADE. PART TC: 13,693.SDR CA971113055Fuel Contrl Unit · failure(CAN) INSTALLED UNIT STARTS COOL AND SLOW. SUBSEQUENT START AFTER ADJUSTMENT LIGHT-OFF OCCURRED IMMEDIATELY, THROTTLE WAS IN CUTOFF POSITION. START ABORTED WITH FUEL VALVE BEING SELECTED OFF. FUEL FLOW WAS NOTED AT ALL TIMES, EVEN AT CUTOFF POSITION. FUEL SDR 97ZZZX4656Gearbox · leakedREMOVED GEARBOX DUE TO TORQUEMETER PISTON PLUG LEAKING OIL AT A RATE OF ONE DRIP EVERY 4 SECONDS.SDR 97ZZZX4810Bleed Valve · stickingVALVE APPARENTLY IS STICKING IN THE CLOSED POSITION AND DOES NOT OPEN UP WHEN POWER DEMAND IS DECREASED. THIS CREATES A MOMENTARY COMPRESSOR STALL RESULTING IN GUNSHOT TYPE SOUNDS COMING FROM THE EXHAUST ON THE TURBINE.SDR 97ZZZX4709Vane · failedPRECAUTIONARY LANDING DUE TO COMPRESSOR STALL. FOUND CASE EROSION AND LOSS OF VANE.SDR CA971113052Support Assembly · corroded(CAN) SEVERE CORROSION FOUND ON AFT LOWER SIDE OF TAIL ROTOR FORWARD CONTROL ROD BELLCRANK SUPPORT.SDR CA971113051Fuel Contrl Unit · failure(CAN) EXTREMELY HOT STARTS, HANGS AT 50-55 PERCENT N1. TRIM ADJUSTMENT LIMITS REACHED WITH NO EFFECT. FUEL CONTROL UNIT REPLACED.SDR CA971113049Fuel Contrl Unit · failure(CAN) SLOW COOL, INTERMITTENT HUNG STARTS, IDLE INCONSISTENT, TRIM ADJUSTMENT LIMITS REACHED WITH NO EFFECT. FUEL CONTROL UNIT REPLACED.SDR CA971113043Fuel Contrl Unit · failure(CAN) SLOW STAGNATED STARTS. THROTTLE ADVANCE NECESSARY TO ACHIEVE GROUND IDLE. FUEL CONTROL UNIT REPLACED.SDR CA971113042Fitting · misinstalled(CAN) SCAVENGE OIL FITTING LEAKED SINCE OVERHAUL INSTALLATION. OIL FITTING INSTALLED BACKWARDS. FITTING INSTALLED PROPERLY AND NEW SEALS INSTALLED.SDR CA971015055Plate · melted(CAN) STARTER GENERATOR FRICTION PLATE MELTED INTERNALLY ON ONE SIDE, RUNNING OUTBETWEEN DAMPER PLATES.
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