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 98ZZZX790Gauge · stuckACCUMULATOR PRESSURE GAUGE IS PART OF STC SA-4378-WP AVIADESIGN INC., HYDRAULIC LANDING GEAR RETRACTION SYSTEM. GAUGE SHOWED NEEDLE STUCK AT 250 PSI WITH ZERO PRESSURE ON SYSTEM DURING AIRCRAFT INSPECTION. SUBMITTER RECOMMENDED A BETTER QUALITY GAUGE BE USEDSDR 98ZZZX13Tube Assy · leakOXYGEN SYSTEM LEAK. INSPECTION FOUND B-NUT CRACKED AT AFT BULKHEAD ATTACHMENT (3 PLACES). FURTHER INSPECTION REVEALED B-NUT AT T-FITTING ATTACHMENT CRACKED IN 2 PLACES.SDR 98ZZZX182Breaker · failedDUPLICATED A REPORTED FAILURE AND ISOLATED CIRCUIT BREAKERS ON NR 1 BUSS TO SHOW THAT THEY WERE FAULTY. INSTALLED 2 EACH NEW 50 AMP BREAKERS. FUNCTION CHECKED SATISFACTORY ON GROUND AND THEN PERFORMED MAINTENANCE FLIGHT CHECK. SUBMITTER STATED THE BREAKERS SDR 97ZZZX4307Lead · defectiveNEW PROPELLER DE-ICE HEAT LEADS WERE PURCHASED FROM DISTRIBUTER. THESE LEADS WERE IN THE ORIGINAL MANUFACTURER PACKAGING. WHEN THE PACKAGE WAS OPENED AND LEADS INSPECTED, FOUND OF THE 5 PACKAGED LEADS, 2 LEADS HAD LOOSE TERMINAL ENDS THAT WERE EASILY PULLED SDR 97ZZZX4200Hose · splitOXYGEN HOSE IN LEFT HEADLINER AFT OF COCKPIT 'D' WINDOW WAS FOUND SPLIT WHEN SYSTEM WAS ACTIVATED. HOSE IS A SHORT FLEXIBLE HOSE THAT IS VERY TWISTED WHEN INSTALLED. RECOMMEND A REPLACEMENT OF SHORTER OXYGEN HOSE FOR THIS AREA.SDR 97ZZZX3554Support · crackedLOOSE AFT RIVETS IN CABIN DOOR HINGE LED TO FURTHER INVESTIGATION. FOUND HINGE SUPPORT INSIDE DOOR ASSY CRACKED TO A LENGTH OF 4 INCHES THROUGH 4 EACH RIVET HOLES. SUGGEST HINGE AFT RIVETS MAY HAVE BEEN IN A LOOSE CONDITION FOR AN EXCESSIVE LENGTH OF TIME.SDR 97ZZZX3195Bellcrank · misdrilledFIRST PHASE INSPECTION FOUND SLACK IN HORIZONTAL CONTROL. LOCATED PLACE OF LOOSE CONNECTION FORWARD ELEVATOR BELLCRANK TO PUSH/PULL TUBE WAS MISDRILLED TO .3125 INCH; SUPPOSED TO BE .25 INCH.SDR 97ZZZX2869Tire · defectiveTWO INCH KNOT RAISED ON EDGE OF TIRE TREAD ADJACENT TO SIDEWALL. NO OTHER APPARENT TIRE DAMAGE. .2187 TREAD DEPTH. TIRE TIME IN SERVICE, 348.4 HOURS. TOTAL LANDINGS, 404.SDR 97ZZZX2806Fire Warn · activatedON 6-2-97 AT 1003.9 HOBBS TIME, THE RIGHT ENGINE FIRE WARNING LIGHT ILLUMINATED ON CLIMB-OUT. THE ENGINE WAS MONITORED WITH NO SECONDARY INDICATIONS OF A FIRE. THE FIRE WARNING LIGHT EXTINGUISHED AFTER ONE MINUTE AND DID NOT ILLUMINATE AGAIN.SDR 97ZZZX2085Hinge · crackedNOSE GEAR DOOR HINGE CRACKED AT RIVET HOLE ON INBOARD SIDE. SUSPECT CAUSE IS THAT THE HINGE IS .75 INCH THICK WITH AN OVERSIZE -4 CHERRY MAX RIVET HOLDING IT TOGETHER. ALL THE RIVET HOLES ON THE HINGE DECREASE THE AMOUNT OF METAL LEFT ON THE HINGE AT THE RIVSDR CA970505001Transducer · failed(CAN) DURING CRUISE FLIGHT THE PILOT NOTICED THE #1 ENGINE OIL PRESSURE READING ZERO, NO CAUTION LIGHT ILLUMINATION AND ALL OTHER PARAMETERS READING NORMAL. AIRCRAFT RETURNED TO BASE. POST FLIGHT INVESTIGATION FOUND THE OIL PRESSURE TRANSDUCER TO BE FAULTY. THSDR 97ZZZX1887Shaft · shearedCREW REPORTED RIGHT ICE DEFLECTION DOOR IS INOPERATIVE. FOUND RIGHT ICE DOOR SHAFT ASSY SHEARED AT BOLT HOLE FOR ACTUATOR ATTACHMENT ARM. NO BINDING NOTED ON DOOR ASSY. REMOVED AND REPLACED SHAFT ASSY WITH A NEW UNIT. GROUND OPS CHECKED OK. REFERENCE BEECSDR 97ZZZX1745Pump · shaft failedENGINE WENT TO IDLE CUT OFF IN-FLIGHT. (FLAME OUT.) MAIN ENGINE PUMP SEIZED. ENGINE SHAFT BECAME WORN AND ROUNDED OFF SPLINES.SDR CA970401009Windshield · failed(CAN) AIRCRAFT HAD CLIMBED TO FL 230 WITH THE WINDSHIELD HEAT ON. SHORTLY AFTER THE HEAT WAS TURNED OFF A LOUD BANG WAS HEARD AND THE LT WINDSHIELD SHATTERED INTO A RIVER OF LATTICE-LIKE CRACKS ON THE INNER LAMINATIONS. WINDSHIELD HAD BEEN INSTALLED 18 MONTSDR CA970528029Windshield · cracked(CAN) WHILE CLIMBING THROUGH 15,000 FEET THE RIGHT HAND WINDSHIELD WAS SEEN TO CRACK AND DELAMINATE OVER A 2 X 3 SQUARE INCH AREA. THE FAILURE OCCURRED IN THE LOWER LEFT HAND CORNER OF THE WINDSHIELD, ADJACENT TO THE WINDSHIELD HEAT INPUT TERMINAL.SDR JZBR14404Windshield · shatteredLEFT (PILOT) WINDSHIELD SHATTERED DURING CLIMB-OUT AFTER TAKEOFF. REMOVED AND REPLACED WINDSHIELD IAW MM 56-10-00 AND KIT 101-5043-1. ALL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.SDR 97ZZZM717Windshield · brokenIN CRUISE FLIGHT, TURNED WINDSHIELD HEAT ON, AFTER SEVERE MINUTES PILOTS SIDE WINDSHIELD PLY SHATTERED. CONSULTED EMERGENCY PROCEDURES CHECKLIST AND CONDUCTED EMERGENCY PROCEDURES. DECLARED EMERGENCY WITH ATC, AND REQUESTED VECTORS TO NEAREST AIRPORT (TEB). SDR 97ZZZX1754Cargo Door · mismodifiedAFT CARGO DOOR MOD/INSTALLATION PERFORMED ON ACFT IS UNAIRWORTHY. E.M.S. MODIFICATIONS WERE BEING DONE WHEN PROBLEMS IN THE DOOR AND ADDED STRUCTURE WAS NOTICED. AN UNBUCKED RIVET, DRILLED HOLES NOT FILLED WITH RIVETS, AND OVER BUCKED RIVETS IN ADDED FORMER SDR 97ZZZX1487Bearing · failedFAILURE OF THE NR 2 MAIN GEAR OUTER WHEEL BEARING WAS FOUND DURING A GEAR LUBRICATION FOLLOWING A GEAR WASH. PREVIOUS TAXIING AND TOWING OF ACFT APPEARED NORMAL. BEARING CAGE ASSY APPEARS TO HAVE FAILED, AND RACE WAS SCORED AS A RESULT OF CAGE DISINTEGRATIONSDR 97ZZZX1486Wheel · bearing failedNR 3 MAIN OUTER WHEEL BEARING FAILED. WHEEL DEPARTED AIRCRAFT ON TAKEOFF. WHEEL SLID OVER AXLE NUT AND COTTER PIN. BEARING CONE SEIZED ON AXLE. AXLE WAS GALLED. BRAKE LINE FITTING SNAPPED OFF.SDR 97ZZZX1259Valve · stuck openCREW REPORTED IN-FLIGHT, FUEL STREAMING FROM RIGHT WING TIP. FOUND BOTH RIGHT WING FUEL VENT AIR INLET CHECK VALVES STUCK OPEN. REPLACED CHECK VALVES. NOTE: FUEL TANKS WERE FULL.SDR 97ZZZX1258Valve · stuck openCREW REPORTED IN-FLIGHT, FUEL STREAMING FROM RIGHT WING TIP. FOUND BOTH RIGHT WING FUEL VENT AIR INLET CHECK VALVES STUCK OPEN. REPLACED CHECK VALVES. NOTE: FUEL TANKS WERE FULL.SDR 97ZZZX1037Selector · intermittentLANDING GEAR DID NOT EXTEND WHEN GEAR HANDLE WAS SELECTED DOWN. FOUND GEAR SELECTOR ASSEMBLY INTERMITTENT. INSTALLED NEW GEAR SELECTOR ASSEMBLY; GEAR SYSTEM OPERATIONAL CHECK OK.SDR 97ZZZX850Gauge · stuckTHIS GAUGE IS PART OF STC SA 4378-WP AVIA DESIGN, INC., HYDRAULIC LANDING GEAR RETRACTION SYSTEM. GAUGE FOUND STUCK AT 1,150 PSI DURING AIRCRAFT INSPECTION. SUBMITTER RECOMMENDS A BETTER QUALITY GAUGE BE USED IN SYSTEM.SDR 97ZZZX1889Idler Gear · failedPILOT REPORTED AIR COND INOP. MAINT SUSPECTED 'QUILL SHAFT' HAD SHEARED. REMOVED AND FOUND SHAFT IN SERVICEABLE CONDITION. REMOVAL OF ACCESSORY CASE FOUND IDLER GEAR HAD FAILED RESULTING IN LOSS OF DRIVE FOR AIR/COND COMP. NO REASON FOR FAILURE HAS BEEN DESDR 97ZZZX864Fuel Filter · froze upPRECAUTIONARY SHUT DOWN FOR FLUCTUATING TORQUE AND WP. UPON INSPECTION, DETERMINED THE RIGHT FUEL SEDIMENT BOWL (FIREWALL FILTER) CONTAINED A SUFFICIENT AMOUNT OF ICE CRYSTALS TO RESTRICT FUEL FLOW. DISASSEMBLED, CLEANED, AND REINSTALLED FILTER ELEMENTS/ASSESDR 97ZZZX266Pump · defectiveINVESTIGATION FOR DEFECTIVE STANDBY FUEL PUMP FOUND OVERSIZE VANES IN PUMP STICKING. PUMP OK WHEN NEW, BUT VANES SWELL UP WHEN IN JET FUEL. SUGGEST TO ORDER NEW PUMPS FROM BATCH S/N 8AMXXX, AND 9AMXXX.SDR 97ZZZX265Pump · defectiveINVESTIGATION FOR DEFECTIVE STANDBY FUEL PUMP FOUND OVERSIZE VANES IN PUMP STICKING. PUMP OK WHEN NEW, BUT VANES SWELL UP WHEN IN JET FUEL. SUGGEST TO ORDER NEW PUMPS FROM BATCH S/N 8AMXXX, AND 9AMXXX.SDR 97ZZZX1397Inverter · defectiveAUTOPILOT DISCONNECTED, FOUND DEFECTIVE INVERTER.SDR 96ZZZX6072Door Seal · failedBRISTLE MATERIAL ON SIDE OF INLET COWLING THAT SEALS ICE DEFLECTOR DOOR CAME LOOSE FROM ITS RETAINER STRIP SENDING NYLON HAIRS TOWARD ENGINE INLET SCREEN. A LARGE VOLUME OF THE HAIRS WERE INJESTED BY THE ENGINE AND ENGINE WAS SPLIT AT THE 'C' FLANGE FOR INSPESDR 96ZZZX5324Bearing · failedDURING MAINTENANCE AND LUBRICATION OF MAIN LANDING GEAR ACTUATORS AND INSPECTION, BEARING FELL APART ON REMOVAL. RACE, OUTER PORTION OF BEARING WAS BROKEN IN HALF. BEARING SCORED. PLATE, PN 115-811046-1, AND PLATE HAD TO BE REPLACED.SDR CA961016007Exhaust Stack · cracked(CAN) EXHAUST STACK FOUND CRACKED ALONG THE OUTBOARD WELD SEAM, APPROXIMATELY 5, 1/4" LONG. THIS STACK HAD BEEN REPLACED IN MAY 1995.SDR 96ZZZX5013Art Sensor · malfunctionSTABILIZATION TOO SENSITIVE. AUTOTILT DROPS ANTENNA. STAB OFF AND INFLIGHT 6.SDR 96ZZZX5076Flame Detector · malfunctionedLEFT ENGINE FIRE LIGHT CAME ON, SIGNAL VOLTAGE TOO HIGH. BEECH HAS NEW STYLE FLAME DETECTOR FOR BETTER RELIABILITY.SDR 96ZZZX5012Art Sensor · malfunctionTEN MONTHS AFTER CHANGING ART 2100'S, BENDIX/KING STILL HAS NOT COME OUT WITH A GOOD FIX. BASIC PROBLEM IS THE SOFTWARE WHICH CANNOT KEEP UP WITH 'GYRO PRECESSION'. FAULT LABEL: 'ANT FLT'.SDR 96ZZZX5766Inverter · inoperativeINVERTER INOP. NO AC OUTPUT.SDR 96ZZZX4386Indicator · gasket failedBEZEL GASKET ROLLED FROM SEAT ALLOWING PRESSURIZATION TO ENTER AIRSPEED INDICATOR. THIS CUASED LARGE ERROR IN AIRSPEED, ALTIMETER, AND V.S.I. DURING FLIGHT. UNIT HAD BEEN REPAIRED PRIOR TO FLIGHT. RECOMMEND A POST-ASSEMBLY INSPECTION TO DESIGN PRESSURE LIMISDR 96ZZZX4715Indicator · failedLANDING GEAR ACCUMULATOR PRESSURE GAUGE WAS PEGGED OUT ON THE HIGH SIDE. THE ABOVE PRESSURE GAUGE IS PART OF THE 'AVIADESIGN HYDRUALIC LANDING GEAR' MODIFICATION FOR BEECH 200 SERIES AIRCRAFT. STC SA4378WP.SDR 97ZZZX6226Limit Switch · out of adjustFLAPS WERE OBSERVED NOT TO BE OPERATING ON THE VOR RWY 15 @ ASE. FLAP HANDLE WAS PLACED IN THE UP POSITION ON THE LANDING ROLL OUT. SMOKE BEGAN TO ENTER CABIN. PROBLEM WAS DUE TO FLAP LIMIT SWITCH OUT OF ADJUSTMENT CAUSED FLAPS TO BIND IN THE UP POSITION, WSDR 96ZZZX3835Detector · malfunctionCREW REPORTED INTERMITTENT FIRE WARNING ON LEFT ENGINE. FOUND LOWER FIREWALL FIRE DETECTOR BAD. THIS DETECTOR HAS BEEN SUPERCEDED BY A NEW STYLE.SDR 96ZZZX5063Sensor · malfunctionedART-2100, SN 1044, SAME OLD STAB PROBLEMS. ALSO, PAINTS SQUIGGLES BEYOND 40 MILE RANGE IN 'HEAVY THUNDERSTORMS'. BENDIX/KING RECOMMENDED STC MOD. EXCHANGED ART-2100 WITH NEW SOFTWARE LEVEL 01/03 AND MOD 2 FOR STC COMPENSATION. INSTALLED ART-2100, SN 1026.SDR 96ZZZX5010Art Sensor · defectiveANTENNA STABLIZATION WORKS ONLY IN LEVEL FLIGHT AUTOTILT STILL DROPS ANTENNA. S/W-01/12 SOFTWARE LEVEL DID NOT FIX PROBLEMS OF THE ORIGINAL RADAR UNIT. INSTALLED REPLACEMENT ART 2100, SN 1036, WITH THIRD BENDIX/KING SOFTWARE UPGRADE S/W-01/03 AND MOD STATUS SDR 96ZZZX4671Tire · defectiveTIRE DEVEOPED BUMP. SUPSECT CORD SEPARATION.SDR 96ZZZX5061Sensor · malfunctionedART-2100, SN 1016, SAME OLD PROBLEMS. STABILIZATION TOO SENSITIVE. PAINT HEAVY IN ROLL LEFT OR RIGHT. AUTOTILT DROPS ANTENNA. BENDIX/KING RECOMMENDED FACTORY EXCHANGE ART-2100, SN 1016. INSTALLED ART-2100, SN 1044.SDR 96ZZZX5064Sensor · malfunctionedART-2100, SN 1018, SAME PROBLEMS AFTER PREVIOUS SOFTWARE CHANGE. STABLIZATION TOO SENSISTIVE. PAINTS HEAVY LEFT OR RIGHT. AUTOTILT DROPS ANTENNA. INSTALLED ART-2100, SN 1016, SN DASH 01/02 MOD DASH 1.SDR CA960513005Blade · fractured(CAN)ENGINE SHUTDOWN FOLLOWING AN INCREASE IN ITT. AS THE POWER LEVER WAS BEING RETARDED, DRBRIS WAS SEEN TO BE COMING FROM THE EXHAUST. INITIAL REPORT INDICATE THIS TO BE A COMPRESSOR TURBINE BLADE FRACTU RE.SDR 96ZZZX1963Bearing · failedAIR CONDITIONING DRIVE PULLEY SUPPORT BEARING ON FORWARD END FAILED AND CAUSED THE QUILL SHAFT TO SHEAR. SUBMITTER STATED THIS IS THE FOURTH SUCH FAILURE IN 1,390 HOURS OF AIRCRAFT OPERATION. BEECHCRAFT RECOMMENDS THE QUILL SHAFT BE LUBED AT 600 HOURS AND THSDR 96ZZZX1333Switch · failedLT ENGINE FUEL PRESSURE SWITCH FAILED IN OPEN POSITION. TT: 2,131.8 HRS.SDR 96ZZZX1329Switch · failedRT ENGINE FUEL PRESSURE SWITCH FAILED IN OPEN POSITION. TT: 2,193.9 HRS. SUBMITTER STATED THIS IS THE 2ND SWITCH TO FAIL IN FLEET.SDR 96ZZZX966Solenoid · failedAIRCRAFT YAWS TO LEFT IN-FLIGHT AND VEERS LEFT ON GROUND. FOUND LEFT RUDDER BOOST CONTROL SOLENOID FAILED IN OPEN POSITION ALLOWING BLEED AIR TO THE BOOST ACTUATOR. REGARDLESS OF RUDDER BOOST SWITCH ON OR OFF, RIGHT RUDDER BOOST SOLENOID PREVIOUSLY HAD SAME
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