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 jasc_code = '7603' 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 jasc_code = '7603' 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 95ZZZX2691Bracket · brokenTHE BRACKET ON WHICH THROTTLE CONTROL AND MIXTURE CONTROL CABLES ARE ATTACHED WAS FOUND BROKEN.SDR 95ZZZX3220Lever Assy · bentFOUND LEVER ASSY WORN THIN TO POINT OF BENDING. WORN THIN BY RUBBING ON PEDESTAL AND BENDING.SDR 9507493204Throttle Contl · malfunctionedDURING CLIMBOUT FROM MSP, RECEIVED ENG 2 THR LEVER FAULT MESSAGE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND RETURNED TO MSP WHERE AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REPLACED THE NR 2 ENGINE THROTTLE CONTROL UNIT. OPERATIONAL CHECK OK.SDR COM11878Power Lever · wornCREW REPORTED, THAT POWER LEVERS WERE NOT EVEN AT FLIGHT IDLE STOP. THE RT POWER LEVER FLIGHT IDLE STOP PIN AND ROLLER WERE FOUND TO BE WORN OVER 50 PERCENT. THE RT POWER LEVER ASSY WAS REPLACED.SDR VTZA95147Flt Idle Baulk · failureFLT NR 8014 - IAD-MGW - DURING CLIMB-OUT THE GEAR WOULD NOT RETRACT WHEN HANDLE SELECTED UP. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE FLIGHT IDLE BAULK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W)SDR 95ZZZX2880Control Cable · failedOUTER HOUSING FAILED ALLOWING THROTTLE TO CLOSE, BUT NOT OPEN. AIRCRAFT MADE A SUCCESSFUL FORCED LANDING. NO DAMAGE OR INJURIES.SDR CAL950265Control Cable · bindingCLE - FLT 0639 - NR 2 ENGINE THROTTLE JAMMED AFTER LEVEL OFF WHILE ACCELERATING TO CRUISE SPEED. THE PILOT BEGAN A DESCENT AND THE THROTTLE STARTED TO UNJAM. THE THROTTLE WAS COMPLETELY FREE AT 14,000 FEET. THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT LANDED WSDR 9505466625Control Cable · disconnectedDURING TAKEOFF ROLL, THE NR 4 ENGINE WOULD NOT RESPOND TO POWER LEVER MOVEMENT AND THE TAKEOFF WAS ABORTED. THE CONTROL CABLE IN THE PYLON WAS FOUND TO HAVE DISCONNECTED AT THE PYLON DRUM. THE CABLE BOX IN THE PYLON WAS REPLACED AND THE SYSTEM OPERATION CHECSDR 95ZZZX2703Throttle Assy · cable frozeAFTER TAKEOFF ON SECOND POWER REDUCTION, THROTTLE FROZE. PRIOR TO FLIGHT, ENGINE COMPARTMENT HAD BEEN CLEANED WITH PERMATEX BIODEGRADABLE AEROSOL SPRAY. IT TURNED OUT TO HAVE A WATER BASE THAT LEFT DROPLETS ON THE CABLE END THAT FROZE AT ALTITUDE. IT THAWNESDR COM31054Power Lever · out of adjustWHEN RT POWER LEVER IS ADVANCED ABOVE FLIGHT IDLE, ENGINE OVERSPEEDS. ADJUSTED POWER LEVER CONTROLS AIRFRAME RIGGING TO M/N SPECS. SYSTEM OPERATES NORMAL.SDR 95ZZZX1796Control Cable · separatedTHROTTLE CABLE SEPARATED WHILE ACFT ON RAMP AT TIME OF START-UP.SDR SCNA95046Control Cable · bindingAIRCRAFT WAS CRUISING AT FLIGHT LEVEL 370 WHEN DESCENDING POWER ON NR 2 ENGINE WOULD NOT RETARD BELOW 93 PERCEHT N1, 89 PERCENT N2, FF 5200. NR 2 WOULD NOT ADVANCE OR RETARD. CONTINUED TO TRY TO MOVE THROTTLE UNTIL FL 180. SECURED NR 2 ENGINE AT FL 180, COMSDR 9503245507Circuit Breaker · trippedDURING TAKEOFF AS TAKEOFF POWER WAS APPLIED, THE NR 1 THRUST LEVER WAS UNABLE TO REACH FULL TAKEOFF. THE TAKEOFF WAS ABORTED. THE LEFT REVERSER INTERLOCK CIRCUIT BREAKER WAS RESET AND THE SYSTEM CHECKED OK.SDR 95ZZZX1665Drum · cable brokenFLT 201 - DURING TAKEOFF ROLL AT APPROX TAKEOFF KNOTS, NR 1 ENGINE HAD SUDDEN LOSS OF POWER WITH ALL PARAMETERS GOING TO ZERO (EGT, EPR, F/F) CREW REJECTED TAKEOFF AND REVERSED THRUST WAS USED. AT THIS TIME, NR 2 ENGINE HAD COMPRESSOR STALL. INSPECTED NR 1 ESDR 9503221149Power Cables · malfunctionedDURING LANDING THE NR 2 ENGINE POWER LEVER COULD NOT BE RETARDED AND THE ENGINE WAS SHUT DOWN DURING ROLLOUT. THE THROTTLE BOOT WAS CLEANED, DRIED WITH ALCOHOL, AND THE OPERATION CHECKED OK. LATER AT MSP, THE LONG AND SHORT ENGINE PUSH/PULL CABLES WERE REPLASDR AALA950319Control Box · defectiveRDU - FLT 0879 - EN ROUTE ORD/RDU DURING CRUISE, LT ENGINE POWER LEVER FROZE AND UNABLE TO REDUCE POWER FOR DESCENT/LANDING. ACCOMPLISHED LT ENGINE SHUT DOWN AND AIRCRAFT LANDED RDU WITHOUT INCIDENT. REPLACED LT ENGINE THROTTLE LOWER CONTROL BOX AND LOWER CSDR 9503211149Pwr Lever Cable · lack of lubeDURING LANDING (AMS), THE NR 2 ENGINE POWER LEVER COULD NOT BE RETARDED AND THE ENGINE WAS SHUT DOWN DURING ROLLOUT. THE POWER LEVER CABLE WAS CLEANED, LUBRICATED, AND OPERATION CHECKED OK.SDR COM11789Control Cable · brokenGO AROUND BUTTON ON LEFT POWER LEVER IS INOPERATIVE. REPAIRED BROKEN WIRE IN POWER LEVER QUADRANT.SDR 95ZZZX1417Control Cable · looseSWAGED SLEEVE AT ENGINE END OF THROTTLE CABLE WAS FOUND LOOSE AND SLIDING ON CABLE FREELY. FOUND DURING ANNUAL INSPECTION. THIS PROBLEM CONTINUES TO EXIST ON MANY AIRCRAFT ON ALL ENGINE CONTROL CABLES.SDR COM11778Control Cable · bindingRT POWER LEVER IS BINDING. REPLACED TELEFLEX CABLE ASSY.SDR VTZA95080Speed Lever · out of adjustDURING TAKEOFF, FLT NR 6319, IAD TO CLE, ABORTED THE TAKEOFF DUE TO THE LEFT ENGINE ONLY MAKING 89 PERCENT TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENT.S MAINTENANCE RERIGGED NR 1 ENGINE SPEED LEVER. GROUND RUNS GOOD. AIRCRAFT WAS RELEASED ANSDR CAL950105Linkage · bindingEWR - FLT 0063 - TAKEOFF WAS ABORTED AT 110 KNOTS WHEN THE NR 2 ENGINE THROTTLE WOULD NOT MOVE PAST THE 25 DEGREE ANGLE POSITION. MAINTENANCE FOUND THE NR 2 ENGINE THROTTLE BINDING. THE POWER LEVER LINKAGE WAS MISALIGNED AT THE QUADRANT CONNECTION AND AN ADDSDR COM31030Cable Assy · bindingPOWER LEVERS ARE DIFFICULT TO MOVE. REPLACED DEFECTIVE SECTIONS OF LT AND RT POWER CONTROL CABLES. LT P/N: C82180-3; RT P/N: C82224-7; RT P/N: C82146-3.SDR 95ZZZX957Return Spring · brokenAIRCRAFT PREPARING FOR TRIP, ENGINES RUNNING ON RAMP. WHEN POWER LEVERS WERE ADVANCED AND BROUGHT BACK TO IDLE, NR 1 ENGINE UNEXPECTEDLY SHUT DOWN. FOUND POWER LEVER LOCKING TAB RETURN SPRING BROKEN ALLOWING POWER LEVER TO GO TO CUT OFF WHEN IDLE POSTION WASSDR 95ZZZX1650Control Cable · brokenDESCENT RATE CONTROL (DRC) DEFECTIVE DUE TO VERNIER CONTROL GETS TWISTED WHEN THE CONTROL FOR WING SPOILERS IS TURNED. THIS CAUSES CABLE TO VERNIER CONTROL TO TWIST AND BREAK. PRECISE FLIGHT INC., STC SA1456NM.SDR 95ZZZX651Control Cable · defectiveAT ANNUAL INSPECTION, THROTTLE WAS FOUND TO HAVE .50 INCH OF TRAVEL AFTER CARBURETOR WAS AGAINST THE IDLE SPEED SCREW. MOVEMENT WAS STILL FREE AND SMOOTH. SUSPECT THE INNER CORE OF THE FLEXIBLE CABLE WAS BROKEN AND THE OUTER SPINAL WIRES WERE STILL CONNECTED.SDR COM31012Power Lever · defectiveTHE POWER LEVERS CAN BE RETARDED BELOW THE FLIGHT IDLE GATE WITHOUT USING THE RELEASE TRIGGERS. REPLACED THE POWER LEVER QUADRANT ASSY.SDR HEEA954175Control Cable · defectiveCABLE RATCHETY. RECEIVED ON AIRCRAFT N5748M ON 12-26-94.SDR 95ZZZX645Control Cable · brokenTHROTTLE AND MIXTURE CONTROL CABLES ARE BREAKING AT THE THREADED END WHERE THE CABLE ATTACHES TO THREADED PORTION OF CABLE. THIS HAS OCCURRED 11 TIMES ON THIS AIRCRAFT SINCE MAY, 1994. SUBMITTER STATED THAT BEECH AIRCRAFT HAS BEEN NOTIFIED OF PROBLEM, WITH NSDR AALA950038Control Cable · defectiveLAX-BOS - FLT 94 - DURING CRUISE, NR 2 ENGINE THROTTLE LEVER FROZE. ACFT PROCEEDED TO BOS. NR 2 ENGINE SHUTDOWN DURING APPROACH TO BOS AND ACFT LANDED WITHOUT INCIDENT. REPLACED NR 2 ENGINE THROTTLE CABLE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. SDR 95ZZZX398Control Cable · brokenPOWER CABLE BROKE. PILOT HAD NO CONTROL OVER ENGINE. USED EMERGENCY THROTTLE. REPLACED POWER CABLE WITH CESSSNA SERVICE KIT SK208-94.SDR VTZA95001Power Cable · failureDAY-IAD - FLT 6942 - DURING CRUISE, THE RT ENGINE TELEFLEX CABLE FROZE IN FLIGHT. UNABLE TO MOVE POWER LEVER. ACFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RT POWER CABLE. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W)
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