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 = 'B200' 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 = 'B200' 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 96ZZZX837Power Supply · failedCABIN FLUORESCENT LIGHTS WERE TURNED ON FOR AN OPERATIONAL CHECK DURING A POST-FLIGHT INSPECTION. THE LIGHTS CAME ON, BLINKED SEVERAL TIMES, AND THE CIRCUIT BREAKER TRIPPED. SMOKE WAS NOTED AT THE REAR OF THE CABIN. POWER WAS IMMEDIATELY REMOVED FROM THE ACSDR 96ZZZX1379Shroud Ring · lug missingBINDING, WHEN PROPELLER WAS ROTATED, FOUND DURING MORNING PRE-FLIGHT. THE POWER SECTION WAS REMOVED AND SENT TO DALLGO AIRMOTIVE. D.A. FOUND A MISSING LOCATING LUG FROM THE PT SHROUD RING THAT WAS BINDING UP THE ROTATION OF THE POWER SECTION.SDR 96ZZZX5065Sensor · malfunctionedART-2100, SN 1018 SOFTWARE S/W DASH 01/01, MOD 1. STABILIZATION TOO SENSITIVE. PAINTS HEAVY LEFT/RIGHT. AUTOTILT DROPS ANTENNA. BENDIX/KING RECOMMENDED SOFTWARE CHANGE. INSTALLED ART-2100. NEW SOFTWARE LEVEL S/W DASH 01/02, MOD 1. NO ATTEMPT WAS MADE TSDR 96ZZZX5011Art Sensor · malfunctionANTENNA STABILIATION TOO SENSITIVE. RADAR PAINTS HEAVY LEFT AND RIGHT. AUTOTILT DROPS ANTENNA.SDR 96ZZZX572Gauge · stuckTHIS GAUGE IS PART OF STC-SA4378-WP, HYDRAULIC LANDING GEAR RETRACTION SYSTEM. GAUGE FOUND STUCK AT 500 P.S.I. DURING AIRCRAFT INSPECTION. SUBMITTER RECOMMENDS A BETTER QUALITY GAUGE BE USED IN SYSTEM.SDR 96ZZZX28Bearing · spalledDURING PRE-FLIGHT WHILE TURNING RIGHT PROPELLER, HEARD AN UNUSUAL NOISE COMING FROM POWER SECTION. INSPECTED CHIP DETECTOR AND MAIN OIL SCREEN AND FOUND SMALL QUANTITIES OF METAL. REMOVED POWER SECTION FOR REPAIR. FOUND NR 4 BEARING RACE STARTING TO SPALL. SDR CA951219107Windshield · cracked(CAN)INNER PANE OF THE WINDSHIELD SHATTERED AT 29,000 FEET AT MAX. PRESSURE DIFFERENTIAL. EMERGENCY DESCENT TO 16,000 FEET WAS INITIATED AND PRESSURE REDUCED.SDR 96ZZZX5066Sensor · defectiveFACTORY SERVICED RADAR STILL NOT WORKING. PAINTS FALSE TARGETS. PAINTS HEAVY ON RIGHT SIDE. AUTOTILT DROPS ANTENNA. AUTOTILT WAS DISABLED BY BENDIX/KING FIELD SERVICE ENGINEER. ALSO, AWAITING NEW SOFTWARE LEVEL.SDR 96ZZZX5014Art Sensor · malfunctionNEW RADAR UPGRADE. ANTENNA STABILIZATION TOO SENSITIVE. RADAR PAINTS HEAVY LEFT/RIGHT. AUTOTILT DROPS ANTENNA. BENDIX/KING OFFERED NEW SOFTWARE LEVEL.SDR 95ZZZX6334Valve · screws failedIN-FLIGHT LOSS OF HYDRAULIC FLUID. LANDING GEAR EXTENDED DUE TO LOSS OF FLUID. AIRCRAFT DIVERTED FOR LANDING. INSPECTION REVEALED SOLENOID VALVE LOCATED ON HYDRAULIC POWER PACK HAD LOOSE CAP. OF THE SIX SCREWS, ONE WAS BROKEN, TWO MISSING, AND THREE LOOSE.SDR 95ZZZX6467Probe · defectiveFUEL TRANSMITTER PROBE HAS LOW RESISTANCE BETWEEN SIGNAL AND RETURN. PART INSTALLED AND CHECKED SATISFACTORY 9-21-95. PILOT REPORTED PROBLEM 10-12-95, WHEN TAKING AIRCRAFT FOR TEST FLIGHT, AIRCRAFT HAD NO FUEL ADDED TO AUXILIARY TANKS. PART WAS REPLACED BEFOSDR 96ZZZX5062Sensor · failedNEW RADAR UPGRADE FROM RDR2000 TO RDR2100. FACTORY NEW ART-2100, SN P1003, FAILED. ANTENNNA STABILIZATION FAULT. AUTOTILT DROPS ANTENNA.SDR 95ZZZX6010Selector Valve · defectiveTHIS UNIT IS PART OF STC SA4378WP, HYDRAULIC LANDING GEAR RETRACTION SYSTEM. LANDING GEAR SELECTOR VALVE BYPASSING FLUID INTERNALLY.SDR 95ZZZX5256Engine · failedENGINE FAILED DURING LEVEL CRUISE FLIGHT AT 13,000 FEET MSL. NO WARNING OR INDICATION OF A PROBLEM PRIOR TO SUDDEN POWER LOSS. SECURED ENGINE AND LANDED. CAUSE OF FAILURE IS UNKNOWN AT THIS TIME. ENGINE IS TO BE RETURNED TO MANUFACTURER FOR INSPECTION AND SDR 95ZZZX5857Gauge · failedTHIS GAUGE IS PART OF STC-5A4378WP AVIADESIGN, INC., HYDRAULIC LANDING GEAR RETRACTION SYSTEM. GAUGE FOUND PEGGED ON HIGH SIDE. FOUND ANOTHER GAUGE WITH SAME SYMPTOM, IT HAD INTERNAL FAILURE. SUBMITTER RECOMMENDS A BETTER QUALITY GAUGE BE USED IN SYSTEM.SDR 95ZZZX3629Rib · crackedDURING PRE-BUY INSPECTION, FOUND BOTH LEADING EDGE RIBS IN WING ROOT BY NACELLE CRACKED. ALSO, FOUND THE SCREWS INSIDE THE PANEL THAT SECURE THIS AREA WERE LOOSE. THE END RESULT CAN LEAD TO A CRACKED LEADING EDGE IF NOT FOUND. SUBMITTER SUGGESTS A FLEET INSSDR 95ZZZX3628Rib · crackedDURING PRE-BUY INSPECTION, FOUND BOTH LEADING EDGE RIBS IN WING ROOT BY NACELLE CRACKED. ALSO, FOUND THE SCREWS INSIDE THE PANEL THAT SECURE THIS AREA WERE LOOSE. THE END RESULT CAN LEAD TO A CRACKED LEADING EDGE IF NOT FOUND. SUBMITTER SUGGESTS A FLEET INSSDR 95ZZZX4029Flow Control · malfunctionPILOTS REPORTED THE LT BLEED AIR FLOW CONTROL UNIT WAS NOT FLOWING AT ALTITUDE. WITH THE RT FLOW CONTROL UNIT SELECTED OFF, THE CABIN ALTITUDE CLIMBED AT ABOUT 2,500 FPM. PERFORMED THE FLOW CONTROL UNIT TEST IN THE BEECHCRAFT 200 MM 21-10-00, PAGES 207 THROUSDR 95ZZZX4028Pneumostat · faultyPILOTS REPORTED THE LT BLEED AIR FLOW CONTROL UNIT WAS NOT FLOWING AT ALTITUDE. WITH THE RT FLOW CONTROL UNIT SELECTED OFF, THE CABIN ALTITUDE CLIMBED AT ABOUT 2,500 FPM. PERFORMED THE FLOW CONTROL UNIT TEST IN THE BEECHCRAFT 200 MM 21-10-00, PAGES 207 THROUSDR 95ZZZX4025Gyro · defectiveWHILE ON A PART 91 TRIP TO ROD FROM OWB, THE COPILOT'S HEADING FLAG ON THE HSI WOULD NOT RETRACT. AFTER SEVERAL ATTEMPTS TO AUTOSLAVE AND FREE-SLAVE THE DIRECTIONAL GYRO, TRIP WAS ABORTED AND RETURNED TO HOME BASE. WERE ABLE TO DUPLICATE PROBLEM IN THE HANGASDR 95ZZZX3306Control Cable · chafedDURING PRE-FLIGHT INSPECTION, FND RUB MARK ON PROTECTIVE COVERING ON RT IDLE CNTRL CABLE. RUB AREA LOCATION IN RT WW, FWD OTBD SIDE, APPROX 2 INCHES INBD FROM ADEL CLAMP & ABOUT 1 INCH IN LENGTH. NOTICED SPACERS FOR BOTH WW ADEL CLAMPS WERE .75 INCH LONG & PSDR 95ZZZX3094Bearing · failedPILOT REPORTED AIR CONDITIONING WAS NOT WORKING. INSPECTION FOUND FORWARD SUPPORT BEARING HAD FAILED. THIS FAILURE CAUSED THE DRIVE QUILL TO SHEAR. THIS IS THE THIRD BEARING FAILURE OF THIS NATURE. BOTH BEARINGS WERE REPLACED AT 1111 HRS. SUBMITTER SUSPECSDR 95ZZZX3086Bearing · failedAT INSPECTION, AIR COND. DRIVE QUILL SHAFT WAS FOUND SHEARED. DISASSEMBLY FOUND THE AFT SUPPORT BEARING FAILED, IT APPEARS THE BEARING SEIZED AND SPUN ON THE DRIVE PULLEY DESTROYING THE PULLEY AND SHEARING THE DRIVE QUILL. THIS IS THE SECOND FAILURE OF THIS SDR 95ZZZX3110Indicator · stuckADI STUCK IN PITCH AND RED FLAG 'ATT'. THIS IS SAME PROBLEM AS BEFORE.SDR 95ZZZX2828Purge Tank · failedACFT DESCENDING THROUGH 10,000 FEET WHEN A JET FUEL ODOR COMING THROUGH AIR VENT. SMELL DISSIPATED. THERE WAS NO SMOKE IN THE ACFT. ALL ENG INSTRUMENTS INDICATING NORMAL. UPON LANDING, PILOT OPENED BOTH ENG COWLINGS LOOKING FOR OBVIOUS FUEL LEAK. FOUND ENSDR 95ZZZX2841Box Assy · detachedBOX FOUND CRACKED AT NUTPLATES AND DANGLING BY THE WIRES. THIS IS A HOT BUS AND COULD RESULT IN SEVERE DAMAGE TO THE AIRCRAFT IF IT SHOULD COME IN CONTACT WITH THE WING STRUCTURE. SUBMITTER SUGGESTS SHOULD BE MADE STIFFER AND A BETTER MATERIAL.SDR 95ZZZX1985Altimeter · malfunctionUNIT 40 FEET OFF AT ZERO, 100 FEET OFF AT 20,000 FEET. ENCODING OUTPUT OUT OF SPECS.SDR 95ZZZX1792Tire · bulgedTHE TIRE HAS 16 BULGES AROUND THE OUTSIDE EDGES ON THE OUTSIDE TREAD.SDR 95ZZZX1731Harness · misriggedUPON RE-FURBUSHING INTERIOR, THE SEAT BELT SHOULDER HARNESS WAS FOUND TO BE MADE WRONG. WHEN SEAT BELT WAS RELEASED, OCCUPANT WAS STILL TRAPPED IN THE SEAT BY HARNESS THE WAY IT WAS MADE.SDR 95ZZZX682Antenna · defectiveBOTH COMMS AND NAVS QUIT IN STATIC PRECIPITATION. THE COMM WOULD BECOME UNREADABLE AND BOTH NAV'S WOULD FLAG AND LOSS OF L/R DEVIATION. TESTED AIRCRAFT WITH DAYTON GRANGIER HIGH-VOLTAGE TESTER AND FOUND LORAN ANTENNA SOURCE OF NOISE. REMOVED AND REPLACED WT
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