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 = '1900D' 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 = '1900D' 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 GLBA96012Fire Loop · failedRDU - CREWS MADE SEVERAL REPORTS OF RIGHT FIRE T-HANDLE ILLUMINATING IN-FLIGHT. MAINTENANCE CURED PROBLEM BY REPLACING BOTH RIGHT FIRE LOOPS. REFERENCE: OPERATOR CONTROL NR 96ZZZX1760. (X)SDR 96ZZZX1760Fire Loop · failedRDU - CREWS MADE SEVERAL REPORTS OF RIGHT FIRE T-HANDLE ILLUMINATING IN-FLIGHT. MAINTENANCE CURED PROBLEM BY REPLACING BOTH RIGHT FIRE LOOPS. REFERENCE: OPERATOR CONTROL GLBA96012.SDR GLBA96031Uplock Switch · lack of lubeFSD - CRWE REPORTED AUTOFEATHER CB POPPED ON FINAL WHEN GEAR WAS SELECTED DOWN. MAINTENANCE LUBRICATED RIGHT GEAR UPLOCK SWITCH. SYSTEM OPS CHECK GOOD. (M)SDR 96ZZZX2612Propeller Blade · splitDURING ROUTINE MAINTENANCE, THE LEFT PROPELLER WAS FOUND DELAMINATED ON ONE BLADE. MAINTENANCE REMOVED AND REPLACED PROPELLER.SDR GLBA96030Flap Pos Trans · failedFSD - CREW REPORTED THE FLAPS WOULD NOT RETRACT FOLLOWING TAKEOFF. CREW MADE AN AIR TURN BACK FOLLOWED BY AN UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED FLAP POSITION INDICATOR TRANSMITTER. SYSTEM OPS CHECK GOOD. (M)SDR 96ZZZX1753Blade · splitDURING ROUTINE MAINTENANCE, PROPELLER BLADE, SN 1655, WAS FOUND TO HAVE A 4 INCH SPLIT ON TRAILING EDGE. REPAIRED IAW HARTZELL MM AND FORM 8110-3 FROM HARTZELL.SDR GLBA96006Actuator · failedLEFT MAIN LANDING GEAR FAILED TO EXTEND AND CB POPPED. CIRCUIT BREAKER WAS RESET AND GEAR EXTENDED. AIRCRAFT WAS FERRIED TO MX STATION. LEFT MLG ACTUATOR WAS CHANGED AND GEAR SWINGS COMPLETED. RII ITEM COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE. (M)SDR C2XA96CL016Airspeed Ind · inoperativePIT - FLT 3333 - CREW REPORTED AFTER TAKEOFF, THE FIRST OFFICER'S AIRSPEED INDICATOR WAS INOPERATIVE. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE FIRST OFFICER'S AIRSPEED INDICATOR. OPERATIONAL CHECKS WERE GOOD IAW B1900D MM 34-11-00. AIRCRASDR 96ZZZX1653Rivets · looseDURING SCHEDULED INSPECTIONS, LOOSE FASTENERS ON BOTH SIDES OF VERTICAL STABILIZER FORWARD SPAR WERE NOTED. ALTHOUGH A SIMILAR PROBLEM WAS ADDRESSED IN SB 2044 ON EARLIER MODEL 1900S, ADDITIONAL EVALUATION AND STUDIES ARE RECOMMENDED AS OTHER PREVIOUS IDENTIFSDR 96ZZZX1148Buss Module · pin defectBOTH TRANSPONDERS AND BOTH ENCODERS WERE INTERMITTENTLY REPORTING INCORRECT ALTITUDE ABOVE 14,700 FEET DUE TO PIN 1 OF BM-72 BEING INTERMITTENTLY OPEN ON BUSS MODULE. BOTH GRAY CODE INFORMATION IS PARALLELED AT BUSS MODULES WHICH, IF ANY ONE PIN WOULD OPEN, ISDR CA960212019Light Bulb · burnt out(CAN)PILOT COULD NOT GET A NOSE GEAR DOWN INDICATION ON SELECTION. COMPLETED A TOWER FLYBY WHERE GEAR DOWN WAS CONFIRMED. INVESTIGATION CONFIRMED THAT THE BULBS WERE BURNT OUT.SDR 96ZZZX1732Rivets · looseDURING SCHEDULED INSPECTIONS, LOOSE FASTENERS ON BOTH SIDES OF VERTICAL STABILIZER FORWARD SPAR WERE NOTED. ALTHOUGH A SIMILAR PROBLEM WAS ADDRESSED IN SB 2044 ON EARLIER MODEL 1900S, ADDITIONAL EVALUATION AND STUDIES ARE RECOMMENDED AS OTHER PREVIOUS IDENTIFSDR S2YA950030Switch · loose wireTHE CABIN DOOR WARNING ANNUNCIATOR ILLUMINATED IN FLIGHT, THE LIGHT EXTINGUISHED WHEN THE CABIN DIFFERENTIAL PRESSURE DROPPED TO 1.0 PSI. THE CREW DIVERTED TO SBN FROM THE INTENDED DESTINATION OF MKE, FLIGHT NR 1053.1. THE AIRCRAFT WAS THEN FERRIED FROM SBN SDR 96ZZZX1657Rivets · looseDURING SCHEDULED INSPECTIONS, LOOSE FASTENERS ON BOTH SIDES OF VERTICAL STABILIZER FORWARD SPAR WERE NOTED. ALTHOUGH A SIMILAR PROBLEM WAS ADDRESSED IN SB 2004 ON EARLIER MODEL 1900S, ADDITIONAL EVALUATION AND STUDIES ARE RECOMMENDED AT OTHER PREVIOUS IDENTIFSDR 96ZZZX1656Rivets · looseDURING SCHEDULED INSPECTIONS, LOOSE FASTENERS ON BOTH SIDES OF VERTICAL STABILIZER FORWARD SPAR WERE NOTED. ALTHOUGH A SIMILAR PROBLEM WAS ADDRESSED IN SB 2044 ON EARLIER MODEL 1900S, ADDITIONAL EVALUATION AND STUDIES ARE RECOMMENDED AS OTHER PREVIOUS IDENTIFSDR GLBA96016Tire · failedFSD - CREW REPORTED NR 3 TIRE BLEW ON LANDING DUE TO FROZEN BRAKE. MAINTENANCE REMOVED AND REPLACED TIRE AND WHEEL ASSY AND THAWED BRAKE. (M)SDR S2YA960002Ventral Fin · damagedMAINTENANCE FOUND THE AFT BOTTOM SIDES OF BOTH VENTRAL FINS DAMAGED FROM OVERROTATION RUNWAY CONTACT DURING AN INSPECTION. DO NOT KNOW AT WHAT POINT THIS TOOK PLACE, TAKEOFF OR LANDING. RECEIVED BEECH ENGINEERING APPROVAL FOR THE REPAIR, COMPLETED IT, AND FISDR CA960131007Governor · faulty(CAN)ON TAKEOFF ROLL THE #2 PROPELLER WENT INTO UNCOMMANDED AUTOFEATHER AT 90 KIAS.TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO BLOCKS. GROUND INSPECTION REVEALED A FAULTY PROPELLER GOVERNOR WHICH WAS RE PLACED. CHECKED SERVICEABLE, AND THE AIRCRAFT RETURNED TSDR 96ZZZX890Sun Gear · defectiveALTHOUGH ALL INDICATIONS POINT TO AN ELECTRICAL DISCHARGE, THE POSSIBILITY OF A SUN GEAR FAILURE IS NOT BEING RULED OUT. THE NR 6 BEARING AND THE SUN GEAR WILL BE SHIPPED FOR FURTEHR INVESTIGATION.SDR 96ZZZX1654Rivets · looseDURING SCHEDULED INSPECTIONS LOOSE FASTENERS ON BOTH SIDES OF VERTICAL STABILIZER FORWARD SPAR WERE NOTED. ALTHOUGH A SIMILAR PROBLEM WAS ADDRESSED IN SB 2044 ON EARLIER MODEL 1900S, ADDITIONAL EVALUATION AND STUDIES ARE RECOMMENDED AS OTHER PREVIOUS IDENTIFISDR CA960122013Switch · out of adjust(CAN)ON APPROACH THE CREW SELECTED GEAR DOWN AND RECEIVED ONLY TWO DOWN AND LOCKED POSITION LIGHTS. THE GEAR WAS CYCLED AND EMERGENCY EXTENSION INITIATED. THE GEAR FINALLY FELL INTO PLACE AND A SUCCESSFUL LANDING CARRIED OUT. INVESTIGATION REVEALED THE MICROSSDR 96ZZZX3097Blade · splitDURING ROUTINE MAINTENANCE, THE TRAILING EDGE OF BLADE, SN 1733, WAS FOUND TO HAVE A 3 INCH SPLIT. REPAIRED IAW HARTZELL MM AND FAA FORM 8110-3 FROM HARTZELL. (X)SDR 96ZZZX1651Rivets · looseDURING SCHEDULED INSPECTIONS, LOOSE FASTENERS ON BOTH SIDES OF VERTICAL STABILIZER FORWARD SPAR WERE NOTED. ALTHOUGH A SIMILAR PROBLEM WAS ADDRESSED IN SB 2044 ON EARLIER MODEL 1900S, ADDITIONAL EVALUATION AND STUDIES ARE RECOMMENDED AS OTHER PREVIOUS IDENTIFSDR 96ZZZM381Ice Vane · crackedDURING ROUTINE MAINTENANCE, THE RIGHT FIXED ICE VALVE WAS FOUND TO TO HAVE SEVERAL CRACKS.SDR CA951228005Switch · frozen(CAN)JUST AFTER TAKEOFF THE CREW SELECTED FLAPS UP WITH NO CORRESPONDING MOVEMENT. AIRCRAFT RETURNED TO BASE AND INVESTIGATION FOUND THE MICRO SWITCHES FROZEN, PROBABLY FROM THE PREVIOUS NIGHTS WASHING OF THE AIRCRAFT. SWITCHES CLEANED, DRIED AND SYSTEM CHECKSDR 96ZZZM1304Bearings · wornDURING ROUTINE MAINTENANCE, BOTH AILERONS WERE DISCOVERED AS HAVING EXCESSIVE FREE PLAY. UPON INSPECTION OF COMPONENTS, ALL THREE ATTACHMENT BEARINGS AND MOUNTING HARDWARE WERE FOUND WORN AND LOOSE. BEARINGS AND HARDWARE REPLACED WITH NEW. (M)SDR 96ZZZX839Pt Disk · blade failureTHE POWER SECTION WAS HARD TO ROTATE WHEN BROUGHT INTO TEAR-DOWN INVESTIGATION AREA. PRE-INSPECTION REVEALED THE NR 2 STAGE 4 PT BLADES HAD FRACTURED AT THE ROOT, 6 ARE FRACTURED FROM .200 INCH TO .500 INCH IN FROM THE ROOT, THE REMAINING BLADES ARE FRACTUREDSDR 96ZZZX128Windshield · crackedCAPTAIN'S WINDSHIELD CRACKED ALONG THE OUTBOARD EDGE OF WINDSHIELD APPROXIMATELY 14 INCHES LONG. REMOVED AND REPLACED WINDSHIELD. AIRCRAFT HAD 74 FLIGHT HOURS AND 119 CYCLES SINCE NEW FROM BEECHCRAFT.SDR S2YA950028Rudder Boost Sys · inoperativeTHE CREW OF FLIGHT NR 1902 AT MKE, ABORTED TAKEOFF ROLL AFTER THEY FELT RESISTANCE AT THEIR RUDDER PEDALS. THE PROBLEM WAS THOUGHT TO BE THE RUDDER BOOST SYSTEM. THEY RETURNED TO THE GATE AND MAINTENANCE MEL'D THE SYSTEM. (M)SDR S2YA950026Flap Motor · shortedTHE FLIGHT CREW NOTICED AN UNKNOWN SOURCE OF SMOKE IN THE CABIN (ACRID SMELL) AND NOTICED THE FLAPS WOULD NOT SELECT 17 OR 35 DEGREES FROM THE FULL UP POSITION. OUTSIDE MAINTENANCE WAS CALLED AND THE MECHANIC C/W THE MAINTENANCE ACTION FOR FLAPS INOP BY PULLISDR CA951108016Transmitter · intermittent(CAN) FUEL FLOW STARTS TO WORK INTERMITTENTLY AND THEN FAILS. FUEL FLOW (FF) TRANSMITTER INSTALLED ON OTHER ENGINE AND SNAG FOLLOWED TRANSMITTER. THIS IS THE FOURTH FF TRANSMITTER REPLACED ON A NEW AIRCRAFT. SUSPECT POOR QUALITY OF UNIT.SDR S2YA950025Trim · lack of lubeAFTER THE FLIGHT CREW ASCENDED TO FLIGHT LEVEL 230, THEY NOTICED THE ELECTRIC ELEVATOR TRIM APPARENTLY FROZE AND WOULD NOT MOVE MANUALLY. THE CREW DECIDED TO TURN BACK TO MKE AND CALL MAINTENANCE. A MECHANIC INSPECTED THE ELEVATOR TRIM SYSTEM, REMOVED VISIBLSDR 95ZZZX6364Windshield · failedUPON CLIMB-OUT, PILOTS WINDSHIELD SHORTED, BURNING OFF THE CONNECTION AT THE BOTTOM RT ELECTRICAL CONNECTION. (X)SDR 95ZZZX6297Windshield · shorted outUPON CLIMB-OUT, PILOTS WINDSHIELD SHORTED, BURNING OFF THE CONNECTION AT THE BOTTOM RT ELECTRICAL CONNECTION.SDR S2YA950024Air Distr · odorAS FLT 1093 - MKE-LSE - PROGRESSING IN THE AREA NORTH OF MSN, THE CREW NOTICED THE SMELL OF SMOKE IN THE CABIN, THOUGHT TO BE ENVIRONMENTAL. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO MSN. A MECHANIC WAS FLOWN THERE, HE GROUND RAN THE AIRCRAFT WITH ALL ESDR 95ZZZX6367Elt Tray · crackedDURING SCHEDULED INSPECTION OF AFT FUSELAGE, THE ELT MOUNTING TRAY WAS FOUND CRACKED AROUND 2 MOUNT HOLES. ADDITIONALLY, A 3 INCH CRACK ON AFT END OF TRAY WAS NOTED. COMPLETE ELT ASSEMBLY WAS REPLACED WTIH NEW UNIT.SDR 95ZZZX6314Bearing · failedNR 6 BEARING IN THE POWER SECTION FAILED. THE INVESTIGATION IS LOOKING AT ELECTRICAL DISCHARGE AS THE SUSPECTED CAUSE OF THE M.I.O. NR 6 BEARING HAS BEEN SENT TO PW & C FOR INVESTIGATION.SDR 95ZZZX6366Elt Case · crackedDURING MAINTENANCE IN AFT FUSELAGE, THE ELT WAS DISCOVERED AS HAVING CASE CRACKS, ADDITIONALLY, ELT MOUNTING TRAY HAD CRACKS EXTENDING FROM ALL FOUR MOUNTING SCREW HOLES. UNIT WAS REMOVED AND REPLACED WITH NEW.SDR S2YA950027Cam · brokeDURING A POST-FLIGHT INSPECTION, FLIGHT CREW NOTICED THE OUTBOARD GEAR DOOR ACTUATING CAM HAD THE UPPER TANG BROKEN OFF. MAINTENANCE REPLACED THE CAM ASSY AND OPERATIONAL CHECKED GOOD. THE TANG THAT BROKE HAD SIGNS OF A PREVIOUS BREAK. (X)SDR 95ZZZX6365Elt Tray · crackedDURING SCHEDULED INSPECTION, THE ELT MOUNTING TRAY WAS DISCOVERED AS HAVING CRACKED EXTENDING FROM MOUNTING TRAY MOUNT SCREW HOLES. TRAY REPLACED WITH NEW.SDR 96ZZZX114Gas Shock · bentWHEN CLOSING THE CARGO DOOR, THE GAS SHOCK BENT. REMOVED AND REPLACED GAS SHOCK.SDR 95ZZZM587Clevis · seizedDURING NOSE LANDING GEAR MAINTENANCE, THE EXTEND RETRACT ACTUATOR YOKE CLEVIS WAS DISCOVERED SEIZED IN PISTON END. THIS CONDITION PRECLUDED ACTUATOR RIGGING AND RESULTED IN A ACTUATOR CHANGE. S/S RECOMMEND CLEVIS BE INSTALLED WITH ANTI-SEIZE COMPOUND DURING SDR 95ZZZM585Wheel · crackedDURING DETAILED INSPECTION, NOSE WHEEL WAS DISCOVERED CRACKED AROUND VALVE STEM HOLE. REMOVED AND REPLACED COMPLETE WHEEL ASSEMBLE P/N 114-8001-3.SDR 95ZZZX6315Sun Gear · failedPOWER SECTION FAILURE WAS CAUSED BY THE SUN GEAR FAILURE. THE SUN GEAR, CARRIER, CARRIER GEARS, PT SHAFT, AND THE RING GEAR WERE SENT TO PW & C FOR INVESTIGATION.SDR 96ZZZX115Gas Shock · bentWHEN CLOSING CARGO DOOR, THE GAS SHOCK BENT. REMOVED AND REPLACED SHOCK.SDR 95ZZZM586Wheel · crackedDURING ROUTINE INSPECTION, NOSE WHEEL WAS DISCOVERED CRACK AROUND VALVE STEM HOLE. REMOVED AND REPLACED COMPLETE WHEEL ASSEMBLY P/N 114-8001-3.SDR 95ZZZX6785Limiter · blownCLE - PLANE DEPARTED. UPON TRYING TO RETRACT GEAR, RECEIVED NO INTRANSIT LIGHTS INDICATION OF MOTOR OPERATION. PILOTS THEN TURNED BACK AND LANDED AT CLE. FLT 2403 DEPARTING CLE, REMOVED AND REPLACED BLOWN CURRENT LIMITER.SDR 95ZZZM548Elt Tray · brokenDURING SCHEDULED MAINTENANCE, THE ELT WAS DISCOVERED UNSECURED. MOUNTING TRAY FOUND BROKEN IN HALF. ELT WAS HANGING FROM REMOTE SWITCH WIRING AND ANTENNA CABLE. RUDDER CONTROL CABLE PULLEY AT FS 570- 107 CHIPPED, CAUSED BY A PIECE OF MOUNTING TRAY JAMMED INSDR 95ZZZX6458Blade · debondedFOUND LEADING EDGE OF COMPOSITE BLADE DEBONDED UNDER DEICE BOOT.SDR 95ZZZX6103Acm · seizedACM WILL NOT BLOW COOL AIR. FOUND ACM TURBINE SEIZED. REMOVED AND REPLACED ACM WITH OVERHAULED SERVICEABLE ACM. OPERATIONAL CHECK GOOD. ORIGINAL ACM HAD FULL OIL AND PROPERLY SERVICED. S/N OFF, 940911.
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