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 = '208B' 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 = '208B' 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 FXTA20210505004Pressure Switch · failedLOW FUEL PRESSURE LIGHT CAME ON DURING START-UP. SENSOR ON ENGINE HAD FAILED.SDR FXTA2020030326001Pressure Switch · failedLOW FUEL PRESSURE CAS MESSAGE. SENSOR ON ENGINE FUEL/OIL HEAT EXCHANGER FAILED.SDR DEMA2020020720Caliper · tornPILOT BEGAN TO TAXI FOR TAKEOFF AND REALIZED HIS RIGHT BRAKE WAS UNRESPONSIVE. PILOT RETURNED TO GATE. UPON INSPECTION, FOUND BRAKE CALIPER PISTON PACKING TORN CAUSING LOSS OF BRAKE FLUID. BRAKE CALIPER WAS REMOVED, DISASSEMBLED, CLEANED, REASSEMBLED WITH NEW SDR 2020FA0000162Torque Tube · crackedDURING THE LAST PHASE INSPECTION A CRACK WAS DISCOVERED IN THE LEFT ELEVATOR TORQUE TUBE.SDR 2020FA0000079Structure · crackedWE HAVE EXPERIENCED MULTIPLE OCCURRENCES OF CRACKING IN THE CONTROL PEDESTAL STRUCTURE OF C208 AND C208B'S. THE PARTS FROM THE C208 IPC 53-22-00 FIG 1 ARE: PANEL ASSY-LH 2613247-7, PANEL ASSY - RH 2613247-1, AND SUPPORT ASSY 2613010-11. THE CRACKS OCCUR IN TSDR COEA2020011601946Jackscrew · lack of lubeFLIGHT 8799, ENROUTE GEG-EAT/AIR TURNBACK DISCREPANCY: DURING CLIMB OUT, THE FLAP MOTOR CIRCUIT BREAKER POPPED. THE AIRCRAFT WAS RETURNED TO GEG AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. CORRECTIVE ACTION: MAINTENANCE INSPECTED THE FLAP SYSTEM ANSDR DEMA20191231001Transponder · failedON FINAL APPROACH, NR 1 TRANSPONDER FAILED. WHILE PILOT WAS CHANGING TO NR 2 TRANSPONDER, THE NR 1 TRANSPONDER BEGAN TO SMOKE. PILOT PULLED CIRCUIT BREAKER FOR NR 1 TRANSPONDER. LANDED WITHOUT INCIDENT.SDR FXTA2020010924001Attach Bracket · damagedLH INBOARD AFT FLAP BELLCRANK UPPER ATTACH POINT HOLE ELONGATED.SDR 9PMA2020042700008Bracket · failedPIC REPORTS SLIGHT VIBRATION FELT ON LANDING IN COLLEGE STATION. ONCE AIRCRAFT WAS SHUT DOWN PILOT REPORTS EXHAUST DUCT BRACKET HAD CRACKED. NO FURTHER DAMAGE CAUSED TO AIRCRAFT OR CREW.SDR COEA2019112601797Indicator · erraticFLIGHT 8775 ROUTE: PHX-FLG DISCREPANCY: DURING TAKEOFF, THE TORQUE GAUGE BEGAN TO GIVE ERRATIC READINGS. PILOT ELECTED TO DECLARE AN EMERGENCY AND RETURN TO PHX. LANDED WITHOUT FURTHER INCIDENT. CORRECTIVE ACTION: MAINTENANCE REPLACED THE TORQUE INDICATOR. ALSDR M36R201911260018Turbine Blades · corrodedA STANDARD BORESCOPE INSPECTION OF THE COMPRESSOR TURBINE BLADES WAS CONDUCTED WITH NO DEFECTS NOTED IN ACCORDANCE WITH THE PRATT AND WHITNEY CANADA MAINTENANCE MANUAL. THE TECHNICIAN ELECTED TO DO AN ADDITIONAL INSPECTION OF THE BLADES THROUGH THE EXHAUST DUCSDR ENHA20191111618Wire · damagedPILOT LOG PAGE DISCREPANCY: "USE OF WINDSHIELD HEAT CAUSED ELECTRICAL SPARKS TO COME FROM L/H CIRCUIT BREAKER PANEL"SDR AXSA201910030001Fire Detector · shortedENGING FIRE WARNING AND ANNUCIATOR ACTIVATED AFTER TAKE OFF, STAYED ON DURING LANDING AND TAXI. NO VISIBLE SIGNS OF FIRE NOTED.SDR ENHA201910030001Pad · detachedDURING DEPARTURE, TURNED LEFT ONTO TAXIWAY THEN TURNED LEFT ONTO RUNWAY AND DEPARTED. ON LANDING, EXITED RUNWAY WITH A RIGHT TURN ONTO TAXIWAY. AFTER EXITING THE RUNWAY, NOTICED THE LEFT BRAKE WAS NOT WORKING. TAXIED TOWARD THE TERMINAL, BUT WITH THE WSDR ENHA2019092600005Skin · crackedFROM FAA FORM 337: REPAIRED SMALL CRACK APPROXIMATELY 1" LENGTH ON RIGHT WING UPPER SKIN JUST FORWARD OF TRAILING EDGE AT RIGHT WING STATION 53. STOP DRILLED CRACK AND INSTALLED SMALL REPAIR PATCH IAW MODEL STRUCTURAL REPAIR MANUAL 51-78-00-8.SDR ENHA2019092600004Skin · damagedFROM FAA FORM 337: REPAIRED SMALL HOLE APPROXIMATELY 1/8" DIAMETER ON RIGHT WING UPPER SKIN JUST FORWARD OF TRAILING EDGE AT RIGHT WING STATION 46. INSTALLED SMALL CIRCULAR PATCH IAW MODEL STRUCTURAL REPAIR MANUAL 51-78-00-8.SDR EHNA2019092600003Skin · crackedFROM FAA FORM 337: FOUND RT UPPER FUSELAGE SKIN (P/N 2611001-2) CRACKED AT FS 186.45, RBL 25.40, AND WL 141.00. REPLACED SKIN P/N 2611001-2 WITH NEW PART IAW FIELD REPAIR #FR-208B0319-7011.SDR ENHA2019092600002Skin · dentedFROM FAA FORM 337: LEFT OUTBOARD HORIZONTAL STABILIZER LEADING EDGE DENTED. REPLACED OUTBOARD LEADING EDGE SKIN P/N 2632000-3, LEADING EDGE RIB P/N 2632021-7 AND P/N 2632021-8 WITH NEW PARTS USING ORIGINAL RIVET SIZE AND SPACING IAW SRM 55-30-00.SDR ENHA2019092600001Bulkhead · crackedFROM FAA FOR 337: REPAIRED SMALL CRACK IN FUSELAGE BULKHEAD @ FS 400. STOP DRILLED CRACK AND INSTALLED DOUBLER IAW MODEL SERIES STRUCTURAL REPAIR MANUAL 53-20-00.SDR MTNA20190906001Brake Assy · contaminatedON TAXI OUT THE RIGHT RUDDER PEDAL WENT TO THE FLOOR WITH NO BRAKING ACTION. MAINTENANCE BLED THE RT BRAKE SYSTEM IN ACCORDANCE WITH C208 MAINTENANCE MANUAL CH 32-40-00. NO FURTHER DEFECTS NOTED.SDR ENHA2019090600000O-Ring · wornFROM PILOT IRREGULARITY REPORT: "1115M HAD A LEFT BRAKE FAILURE AFTER LANDING RWY 19R. AS I WAS TAXING DOWN C I WAS USING A COMBINATION OF THE RIGHT BRAKE AND PROP REVERSE TO SLOW DOWN. EVERY TIME I CAME OUT OF PROP REVERSE THE PLANE VEERED MORE TO THE RIGHT SDR EPUA201908263001Potentiometer · failedDURING FLIGHT PILOT NOTICED SMOKE IN THE COCKPIT COMING FROM THE MAP LIGHT DIMMING RHEOSTAT. MAINTENANCE INSPECTED AIRCRAFT AND DEFERRED THE MAP LIGHT ACCORDING TO COMPANY PROCEDURES. POTENTIOMETER PART NUMBER S2619-1 WAS NOTED AS DEFECTIVE COMPONENT.SDR EPUA201908198001Wire · damagedDURING FLIGHT PILOT INDICATED THAT THE FUEL FLOW GAUGE READ ZERO DURING CLIMB AND CRUISE. MAINTENANCE INSPECTED AIRCRAFT AND REPAIRED BROKEN INSULATION ON FUEL TRANSDUCER WIRING. GROUND OPERATIONAL CHECK WAS SATISFACTORY.SDR EPUA201908196001Transducer · failedDURING FLIGHT PILOT REPORTS THAT THE FUEL FLOW GAUGE IS FLUCTUATING BETWEEN 100 AND 450 PPH. MAINTENANCE REPLACED FUEL FLOW TRANSDUCER, OPS CHECK GOOD.SDR 2020FA0000036Pump · failedFUEL BOOST PUMP FAILED ON ENGINE RUN UP. UPON INSPECTION, FOUND FUEL BOOST PUMP IMPELLERS NO LONGER INTACT. ATTENTION TO THE ISSUE WAS INITIATED BY A LOW FUEL PRESSURE WARNING. A LOUD GRINDING NOISE COULD BE HEARD WHENEVER THE FUEL BOOST SWITCH WAS MOVED TO SDR EPUA20190801001Switch · malfunctionedENGINE FIRE ANNUNCIATOR LIGHT AND SIREN INTERMITTENT. MAINTENANCE INSPECTED AIRCRAFT AND REPLACED DEFECTIVE PRESS TO TEST SWITCH. NO OTHER DEFECTS NOTED.SDR EPUA20190728001Fire Loop · faultyAIRCRAFT ENGINE FIRE WARNING ANNUNCIATOR ILLUMINATED. A/C ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE IS CURRENTLY WORKING AIRCRAFT AND IS IN THE PROCESS OF REPLACING THE ENGINE FIRE LOOP.SDR AWHA2019073100000Power Lever · out of rigDURING POST COMPRESSOR WASH ENGINE RUN MAINTENANCE FOUND PROP STARTING TO GO INTO BETA WHEN THE POWER LEVER WAS AT THE GATE. THE MECHANIC DETERMINED THE ENGINE CONTROLS WERE OUT OF RIG AND ADJUSTED REAR CLEVIS AND 11" ROD AS NEEDED AND SAFETIED. OPERATIONAL SDR EPUA20190716001Fuel Control · leakingPILOT REPORTS " UPON DEPARTING A STRONG ODOR OF POLISH OR FUEL BEGAN FILLING THE CABIN. AT FIRST WE BELIEVED IT WAS FUEL ON GLOVES OR A RAG. AS WE FLEW THE SMELL BE GREW IN STRENGTH AND THE PASSENGERS NOTED IT AS WELL. WE RETURNED TO BASE. MAINTENANCE INSPSDR CA190712005Bracket · damaged(CAN) DURING INSPECTION OF C-XXXX IT WAS DISCOVERED THAT THE PROPELLER TKS NOZZLE WAS NOT SPRAYING INTO THE TKS FEEDER RING BUT INSTEAD WAS SPRAYING ONTO THE BACK OF THE PROPELLER BACK PLATE. FURTHER INVESTIGATION FOUND THAT THE SUPPLY NOZZLE BRACKET WAS INCORSDR 2019FA0000203Autopilot Sys · malfunctionedAIRCRAFT HAD A SLIGHT PORPOISE MOVEMENT WITH AUTO PILOT ON AND ALT HOLD SELECTED. ADVISED THAT HE FELT THE PORPOISING COULD BE DUE TO THE CARGO LOAD (THERE WAS A 300 KG ENGINE AND SOME OTHER ITEMS LOADED ONBOARD). THE PILOTS OPERATING THE AIRCRAFT IN GOROKASDR MUIA201906253001Control Unit · failedFLIGHT CREW REPORTED STANDBY ALTERNATOR SYSTEM HAD FAILED. REPLACED STANDBY ALTERNATOR CONTROL UNIT AND SYSTEM FUNCTIONS NORMALLY. AIRCRAFT RETURNED TO SERVICE IN ACCORDANCE WITH THE CARRIER GENERAL OPERATIONS MANUAL .SDR MTNA20190621001Control Unit · intermittentENGINE FIRE ALARM INTERMITTENTLY SOUNDED FALSE WARNING DURING FLIGHT. PERFORMED TROUBLESHOOTING OF THE SYSTEM, AND DETERMINED THAT THE FIRE DETECT CONTROL UNIT AND WARNING HORN WERE INTERMITTENT. REPLACED THE FIRE DETECT CONTROL BOX AND WARNING HORN.SDR AWHA201906184001Master Cylinder · failedUPON TAXI TO RWY 20 FOR DEPARTURE FROM KPWT AT IDLE RPM (A TWY NE BOUND) LOSS OF BRAKING/STEERING CONTROL, RESULTED IN ACFT VEERING OFF PAVED SURFACE AND INTO THE GRASS ADJACENT TO TWY. ACFT WAS IMMEDIATELY SHUTDOWN AND SECURED. NO CONTACT WITH ANY OBJECT AND SDR EPUA2019062013001Fire Warning · false activationENGINE FIRE INTERMITTENTLY CAME ON IN FLIGHT. VISUALLY INSPECTED FIRE DETECTION SYSTEM. GROUND CHECKS AND RUN UP COULD NOT DUPLICATE. FIRE WARNING TEST OK.SDR COEA2019061431778Tape · burnedFLIGHT 7669 ENROUTE, LIGHT SMOKE COMING OUT OF #2 COMM. #2 COMM SWITCH WAS TURNED OFF & CONTINUED FLIGHT. CORRECTIVE ACTION: MAINTENANCE PERFORMED DETAILED VISUAL INSPECTION OF G430 AVIONICS RACK INCLUDING TRANSPONDERS, DME & ALL ASSOCIATED WIRING. FOUND SINGSDR MUIA20190518001Static System · contaminatedCREW REPORTED PIC AND SIC AIRSPEED INDICATORS AND PIC AND SIC VERTICAL SPEED INDICATORS GAVE ERRONEOUS READING IN HEAVY PRECIPITATION AND TURBULENCE. MAINTENANCE DRAINED WATER FROM BOTH STATIC SYSTEMS AND VERIFIED LT AND RT PITOT/STATIC MAST HEATERS ARE OPERATSDR 2019FA0000274Flap Track · wornFLAP TRACKS WORNSDR 2019FA0000273Flap Track · wornFLAP TRACKS WORNSDR 2019FA0000272Torque Tube · corrodedRUDDER TORQUE TUBE REQUIRES REPLACEMENTSDR 2019FA0000271Structure · dentedDENTED ELEVATORSDR 2019FA0000270Support Bracket · chafedFLAP LEADING EDGE CHAFING AND SUPPORT BRACKET WEARSDR 2019FA0000269Skin · chafedCHAFE DAMAGE ON LOWER COWLINGSDR 2019FA0000268Door Frame · corrodedLOWER CARGO DOOR THRESHOLD AIRFRAME SKIN CORRODEDSDR FXTA20190418001Support Bracket · damagedUPPER LH OUTBOARD FLAP BELLCRANK ATTACH BRACKET IS ELONGATED WHERE FLAP BELLCRANK ATTACHES IN WING.SDR CA190410014Bearing · broken(CAN) WHILE ON APPROACH, THE PILOT SELECTED 10 DEGREE FLAPS FOR LANDING. THE FLAPS THEN PROCEEDED TO FULLY EXTEND, WITH THE CIRCUIT BREAKER TRIPPING AT FULL EXTENSION. WHILE FULLY EXTENDED, FLAP INDICATOR SHOWED 5 DEGREES. DUE TO THE UNEXPECTED NOSE DOWN ATTITSDR CA190514016Bolt · broken(CAN) TIRE BLEW ON LANDING. BRAKE UNIT PN 030-18200 ANCHOR BOLTS (PN 069-01900) WERE FOUND BROKEN.SDR ENHA2019F00156Canister · fullFUEL SMELL IN COCKPIT. EPA CAN FULL.SDR FXTA20210505005Pressure Switch · failedLOW FUEL PRESSURE LIGHT CAME ON DURING START-UP. SENSOR ON ENGINE HAD FAILED.SDR MUIA201902154001Structure · contaminatedCREW PERFORMED AIR RETURN TO DEPARTURE AND REPORTED THAT THEY HAD SMOKE AND FUMES IN THE COCKPIT. MX FOUND DEICING FLUID/GLYCOL IN AREA BETWEEN LH WINDSHIELD AND INSTRUMENT PANEL GLARESHIELD. THIS AREA CONTAINS AN AIR LINE WHICH ROUTES BLEED AIR FOR THE PNEUMA
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