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 = '7602' 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 = '7602' 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 AUS20030131Rod End · separated(AUS) MIXTURE CONTROL SYSTEM ROD END FAULTY.SDR AUS20030011Cable · worn(AUS) ENGINE MIXTURE CONTROL INNER CABLE WORN.SDR 2002FA0001396Control Cable · brokenDURING 100 HOUR INSPECTION, FOUND THAT THE FOLLOWING CONTROL CABLES WHERE BROKEN ON THE ENGINE SIDE WHERE TWO PIECES OF SHROUD OF SWAGED TOGETHER.SDR 2002FA0001395Control Cable · brokenDURING 100 HOUR INSPECTION FOUND THAT THE FOLLOWING CONTROL CABLES WERE BROKEN ON THE ENGINE SIDE WHERE TWO PIECES OF SHROUD OF SWAGED TOGETHER.SDR CA021105010Shaft · loose(CAN) CARBURETOR RUNNING LEAN AT ALTITUDE, THROTTLE SHAFT LOOSE, ENGINE RUNS POORLY WITH THIS CARBURETOR. TIME SINCE FACTORY OVERHAUL IS 542.1 HOURS.SDR AUS20020914Cable · worn(AUS) MIXTURE CONTROL CABLE INNER WIRE WORN TO LESS THAN 50% OF NORMALTHICKNESS. CABLE DIAMETER WAS 62MM (0.024IN) INSTEAD OF THE NORMAL DIAMETER 1.6MM (0.062IN).SDR 2002FA0000822Swivel · failedTHIS ITEM IS INSTALLED ON A CESSNA T337G THAT HAS HAD TCM TSIO-520 ENGINES INSTALLED AS AN STC MODIFICATION. THE PART IS A BALL-TYPE SWIVEL THAT CONNECTS THE MIXTURE CABLE TO THE MIXTURE CONTROL ARM. THE BALL HAS PULLED OUT OF ITS SWAGED HOUSING. THIS IS THE TSDR H792002F00001Control Cable · failedTHIS AIRCRAFT, ENROUTE, ON TAKEOFF THE PILOT NOTICED A ROUGHNESS IN THE ENGINE OPERATION. THE PILOT ELECTED TO LAND AT AIRPORT TO HAVE MAINTENANCE TROUBLESHOOT ROUGHNESS. MAINTENANCE DISCOVERED THAT THE MIXTURE CONTROL CABLE HAD FAILED AT THE CRIMP SWIVEL JOSDR 2002FA0000005Arm · wornDURING ANNUAL INSPECTION FOUND MIXTURE ARM ROD END ATTACHING BOLT LOOSE. ATTEMPTED TO TIGHTEN BOLT BUT FOUND THERE WAS STILL PLAY. DISASSEMBLED ROD END ATTACHING BOLT AND A STEEL SERRATED BEARING INSERT FELL OUT OF THE BRONZE MIXTURE ARM. THIS WAS CAUSED BYSDR BSY2001F00023Cotter Pin · sheared(CLT)(MIR) RIGHT ENGINE SHUT DOWN IN FLIGHT. COTTER PIN SHEARED NUT BACKED OFF MIXTURE CABLE CAUSING MIXTURE TOO LEAN. REPLACED BOLT, NUT AND COTTER PIN. OPS CHECKED OK.SDR CA011108007Control Cable · separated(CAN) DURING ANNUAL INSPECTION THE ENGINES WERE BEING REMOVED FOR REPLACEMENT. DURING INSPECTION OF THE ENGINE CONTROLS, BOTH THE LT MIXTURE CONTROL CABLE P/N 600035-549 AND RIGHT HAND MIXTURE CONTROL CABLE P/N 600035-547 WERE FOUND TO BE SEPARATED AT THE SWAGSDR AUS20010979Shaft · separated(AUS) MIXTURE CONTROL VERNIER FAILED CAUSING CENTRE KNOB AND 177.8MM(7IN) OF SHAFT TO SEPARATE FROM MIXTURE CONTROL.SDR AUS20010947Lever · failed(AUS) MIXTURE CONTROL VERNIER FAILED. CENTRE KNOB AND SHAFT SEPARATED FROM MIXTURE CONTROL.SDR AUS20010693Cable · failed(AUS) LH ENGINE MIXTURE CUTOFF CONTROL CABLE WORN AND BROKEN AT A POINT 190MM (7.48IN) FROM THE ENGINE END ATTACHMENT BEARING.SDR 20010525CW007Control Cable · brokenENGINE STARTED TO SPAR DOWN IN FLIGHT. PILOT ATTEMPTED TO ADJUST MIXTURE, AFTER TURNING ON THE BOOST PUMPS. PILOT STATED, THE MIXTURE CABLE WAS LOOSE IN HIS HAND. ENGINE SHUT DOWN AND AIRCRAFT WAS LANDED , GEAR UP IN A FIELD. UPON EXAMINATION, THE MIXTURE SDR 20010326AP001Control Unit · malfunctionedPILOT REPORTED THAT THE CONTROL WAS HARD TO MOVE. FOUND IN THE LOGS THAT THE INSTALLER HAD LUBED THE CONTROL. LUBRICATION WILL GUM UP THE DRY LUBE AND MAKE IT HARD TO MOVE.SDR 20010423CW010Control Cable · brokenRIGHT ENGINE SHUT DOWN IN FLIGHT, FOUND RIGHT MIXTURE CABLE BROKEN. REMOVED AND REPLACED CABLE. OPS CHECKS GOOD.SDR 20010319CW008Control Cable · separatedSTART UP, PILOT PUSHED MIXTURE FORWARD, COULD NOT START LEFT MOTOR OR GET FUEL FLOW. INVESTIGATION REVEALLED MIXTURE KNOB WOULD MOVE, ROD END AT MIXTURE CONTROL DID NOT. FOUND CABLE HOUSING SEPARATED FROM FACTORY CRIMP INSIDE FUSELAGE AT CONTROL COLUM AREA.SDR 20010222CW001Lever · brokenMIXTURE CONTROL BROKE ON GROUND RUN UP. BREAK APPEARS TO BE DEFECT IN MATERIAL.SDR AU010043Cable · misinstalled(AUS) ENGINE MIXTURE CONTROL INNER CABLE ONLY ENGAGED IN THE ENGINE CONTROL END BY APPROXIMATELY 1.5 TURNS.SDR 20010129CW015Control Cable · bindingMIR / DTW- RIGHT ENGINE LOST POWER ON TAKE OFF, ABORTED TAKEOFF. FOUND MIXTURE NOT GOING TO FULL RICH BECAUSE OF MIXTURE CABLE BINDING. REMOVED AND REPLACED MIXTURE CABLE . OPS CHECKED GOOD.SDR 20001026SH015Control Cable · bindingRIGHT HAND MIXTURE CABLE (HARD TO MOVE IN-FLIGHT). (X)SDR SIMA2721Lever · brokenDFW - FLT 3872 - LEFT CONDITION LEVER APPEARED TO BE SLIGHTLY BENT TO THE LEFT. THIS CAUSED THE INTERFERENCE WITH OPERATION OF GUST LOCK DURING LANDING ROLL-OUT. FIRST OFFICER REPORTED IT WAS DIFFICULT TO GRASP THE GUST LOCK WITH CONDITON LEVER AT MAX. FOUNSDR AU000938Control Cable · failed(AUS) MIXTURE CONTROL CABLE FAILED AT SWAGED END FITTING.SDR 20000925SH009Control Cable · brokenPILOT REPORTED THAT ON CLIMB, RIGHT ENGINE WOULD NOT LEAN OUT. PILOT THEN TURNED BACK TO AIRPORT AND AN UNEVENTFUL LANDING WAS MADE. PILOT THEN DISCOVERED RIGHT ENGINE WOULD NOT SHUT DOWN WHEN MIXTURE CONTROL WAS PULLED BACK TO IDLE CUT-OFF. UPON INSPECTIONSDR 20000404SH011Ball Joint · failedTHIS BALL JOINT IS THE CONNECTION BETWEEN THE MIXTURE CABLE AND THE THROTTLE ASSY. WHEN THIS JOINT FAILS THERE IS NO MIXTURE CONTROL. SUBMITTER STATED THIS IS SECOND NEW BALL JOINT SEEN FAIL WITH VERY FEW HRS ON THE PART. SUBMITTER SUSPECTED NEW PART USED TSDR 99ZZZX4212Control Cable · failedAIRCRAFT GRADUALLY LOST POWER AND CRASHED. INVESTIGATION FOUND THE THREADED END OF THE MIXTURE CABLE WAS FOUND SEPARATED FROM THE ROD END IN THE ENGINE COMPARTMENT. THE TIPS OF THE ELEVEN THREADS ON THE END OF THE CABLE WERE WORN SO THAT IT COULD BE INSERTEDSDR CA991027028Cable · damaged(CAN) DURING INSPECTION, NR 1 ENGINE LOWER CONDITION LEVER CABLE WAS BLENDED TO LIMITS AT THE STEEL PULLEY FORWARD OF THE FIREWALL. CABLE REPLACED.SDR MALA976565Condition Lever · out of adjustCREW NOTED PROP RPM ON LT PROPELLER WELL BELOW TAKEOFF SETTING SHORTLY AFTER V1 ROTATION. RETURNED TO DTW AND ACCOMPLISHED QRH FOR PROP MALFUNCTION. MAINTENANCE INSPECTED LT CONDITION LEVER RIGGING, FOUND OUT OF RIG, RE-RIGED THE LT CONDITION LEVER IAW 76-10SDR VNAA9908010Control Cable · bentFLIGHT CREW REPORTED LEFT ENGINE CONDITION LEVER DIFFICULT TO OPERATE. MAINTENANCE INSPECTED AND APPROVED THE AIRCRAFT FERRY FLIGHT TO CAK. THE LEFT HAND CONDITION LEVER CONTROL CABLE WAS REPLACED IN ACCORDANCE WITH MAINTENANCE MANUAL 76-11-31. FUNCTION CHESDR 99ZZZX2643Rod End · failedROD END CONNECTS THROTTLE CABLE TO ARM AT SERVO. BALL SEPARATED FROM SOCKET. ENGINE WENT TO FULL POWER AND HAD TO BE FEATHERED TO LAND.SDR AU990678Rod End · wrong part(AUS) LEFT ENGINE MIXTURE CONTROL TO FCU CONTROL ROD ROD END AND ATTACHING HARDWARE SUSPECT UNAPPROVED PARTS.SDR 99ZZZX2408Control Cable · brokenRIGHT ENGINE SHUT DOWN IN-FLIGHT. LANDED IN ZZV, FOUND MIXTURE CABLE BROKEN. SAFTIED MIXTURE FULL RICH, FERRIED TO CMH. REMOVED AND REPLACED CABLE.SDR 99ZZZX2197Control Cable · failedINSTALLED 3-19-99 AT 2,216.2 HOBBS. END BROKE OFF 5-14-99 AT 2,299.4. MIXTURE CONTROL CABLE FAILED ON RIGHT ENGINE. 83.2 HOURS/2 MONTHS.SDR 99ZZZX2086Control Cable · looseWHILE INSPECTING MIXTURE CONTROL DURING ANNUAL INSPECTION, LOOSENESS WAS NOTED IN MIXTURE CONTROL CABLE. UPON FURTHER INSPECTION, DETERMINED THE SWAGED PORTION OF CONTROL CABLE WAS SLIPPING. THE SWAGED PORTION CAME OFF WITHOUT TOO MUCH PRESSURE.SDR 99ZZZX1962Shroud · failedMIXTURE CONTROL COOLING SHROUD ASM MOUNTING TABS FAILED CAUSING SHROUD TO CUT INTO FUEL PRESSURE HOSE ASM (P/N 63521854540.00). THE DEFECT WAS FOUND DURING THE AIRCRAFT'S 100-HOUR INSPECTION. THE ENGINE WAS ONLY IN SERVICE 67 HOURS AT THE TIME OF INSPECTIONSDR AU990338Bolt · loose(AUS) MIXTURE CONTROL SYSTEM BOLT LOOSE.SDR 20001205SH003Control Cable · brokenAIRCRAFT LOST POWER AND COLLIDED WITH GROUND OBSTRUCTIONS FOLLOWING A FORCED LANDING OFF-FIELD. SUBSEQUENT INVESTIGATION REVEALED A BROKEN MIXTURE CABLE. AD-85-03-01 IS A ONE-TIME AD WHICH APPLIES TO THIS AIRCRAFT. THE AD INCORPORATED SE69-16. THE AIRCRAFTSDR 99ZZZX4013Control Cable · failedMIXTURE CABLE BROKE IN-FLIGHT CAUSING FORCED OFF-FIELD LANDING AND SUBSEQUENT INJURIES TO PILOT AND PASSENGER, AND DESTRUCTION OF THE AIRCRAFT. MIXTURE CABLE HAD BEEN REPLACED LESS THAN ONE YEAR PRIOR AND 99 FLIGHT HOURS HAD BEEN ACCUMULATED. THE CABLE SHOWESDR 99ZZZX2051Support · wornPILOT REPORTED MIXTURE SETTING CONSISTANCY WAS ERRATIC. INVESTIGATION INTO THE CONTROL MOUNT IN THE ENGINE COMPARTMENT REVEALED THE U-CHANNEL THAT SUPPORTS THE MIXTURE CONTROL HAD WORN TO AN EXTENT THAT THE CABLE HOUSING WAS SLIDING IN THE MOUNT. THE OUTER CSDR CA990401014Cable · damaged(CAN) LEFT CONDITION LEVER CONTROL CABLE FOUND DAMAGED.SDR 99ZZZX115Clamp · looseENGINE HAS HIGH BURN RATE DURING CRUISE. FOUND MIXTURE CONTROL CABLE HOUSING VERY LOOSE. INSTALLED TWO NEW CLAMPS.SDR AU981580Spring · missing(AUS) MIXTURE CONTROL LINKAGE ANTI-RATTLE SPRING MISSING. MIXTURE LEVER FITTED WITHOUT WAVE WASHERS. NO WAVE WASHERS FITTED BETWEEN THE THROTTLE BODY AND COLLAR. MANUFACTURING DEFECT. INCORRECT ASSEMBLY.SDR AU981626Cable · loose(AUS) ENGINE CONTROL CABLE FOUND WITH LOW TENSION. FURTHER INVESTIGATION FOUND THE CABLE TURN-BUCKLE TO BE LOCKWIRED AND BOTTOMED OUT - TENSION COULD NOT BE ADJUSTED.SDR 98ZZZX3458Control Cable · brokenPILOT REPORTED HAVING NO CONTROL OF MIXTURE. INSPECTION FOUND MIX IN FULL RICH POSITION ON FUEL SERVO AND CONTROL CABLE BROKEN. BREAK WAS DETERMINED TO BE INSIDE CABLE HOUSING AT CONSOLE END. NO RECORD OF CABLE REPLACEMENT FOUND. AIRCRAFT HAS 10,600 HOURS.SDR 98ZZZX3132Rod End · failedTHROTTLE CONTROL ROD END BEARING (HPIM TYPE) CARRIER FAILED LATERALLY. YOKE SEPARATION FROM YOKE CARRIER COULD RESULT IN LOSS OF THROTTLE CONTROL.SDR 98ZZZX2653Clamp · slippedMXITURE CONTROL CABLE HOUSING SLIPPED DUE TO INCORRECT MOUNTING CLAMP CAUSING INTERMITTENT LEAN RUNNING. INSTALLED PROPER CLAMP AND RIGGED SYSTEM TO PROVIDE CUSHION PER MM.SDR AU980306Support · cracked(AUS) ENGINE MIXTURE CONTROL CABLE CLAMP SUPPORT CRACKED.SDR AU980345Cable · failed(AUS) MIXTURE CONTROL CABLE FAILED AT ENGINE END FITTING.SDR CA980331021Cable · stiff(CAN) BOTH PROP AND MIXTURE CONTROL CABLES VERY STIFF. AREA BEHIND TURBO BADLY CORRODED. CABLES REPLACED.
Back to JASC 7602