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 AU000571Power Lever · out of adj(AUS) LH POWER LEVER OUT OF ADJUSTMENT AND LAGGING BEHIND THE RH POWERLEVER.SDR 20000802SH030Throttle Cable · inaccurateOWNER REQUESTED THROTTLE CABLE BE CHANGED DUE TO CABLE CREEPING. WHEN CABLE WAS COMPARED TO ORIGINAL CABLE, NEW CABLE WAS FOUND TO HAVE MANY DIFFERENCES: LENGTH WAS LONGER; FIREWALL SLEEVE IN DIFFERENT LOCATION; LARGER DIAMETER; ENGINE MOUNT ATTACHMENT COMPLSDR 00FDEA00459Control Cable · damagedDURING DESCENT, NR 2 THROTTLE STUCK AT 88 PERCENT N2. THROTTLE WILL MOVE BUT N2 REMAINS AT 88 PERCENT N2 AND THROTTLE RETURNS TO ORIG POS. REMOVED AND REPLACED NR 2 ENG PUSH PULL CABLE REF MM 76-11-01-2. RIGGED PER DC-10 MM 76-11-01-2 AND SECURED ALL ROD ENSDR P2EA00212Control Cable · looseMCI - FLT 589 - EMERGENCY DECLARED, NR 1 ENGINE SHUT DOWN 5 MINUTES BEFORE LANDING, AIRCRAFT RETURNED TO MCI, LANDING UNEVENTFUL. LOST THROTTLE CONTROL NR 1 ENGINE: EPR 2.09, N1 91 PERCENT, EGT 450, N2 91 PERCENT, AND FUEL FLOW NORMAL. FOUND LOOSE HARDWARE SDR RRXA002849Lever · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AT THE NECK DOWN AREA WITH HFEC ON THE NR 1 THROTTLE LEVER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-21.SDR RRXA002844Lever · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AT THE NECK DOWN AREA WITH HFEC ON THE NR 1 THROTTLE LEVER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-21.SDR CA001122020Throttle Cable · seized(CAN) A NEW THROTTLE CABLE RECEIVED FROM CESSNA WAS INSTALLED ON THE AIRCRAFT BUT SEIZED UP WHEN THE CABLE WAS FLEXED TO ALLOW HOOKUP TO THE THROTTLE CABLE. ANOTHER NEW CABLE FROM CESSNA WAS TRIED WITH THE SAME RESULT.A THROTTLE CABLE MADE BY MCFARLANE MCC2995SDR CA000824026Rod End · separated(CAN) PILOT REPORTED LACK OF THROTTLE RESPONSE. THE AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND THROTTLE ROD END SEPARATED FROM BALL AT THROTTLE ARM ON THE FUEL CONTROL. A NEW ROD ENDSDR 20000718SH004Ball Joint · detachedDURING STARTING SEQUENCE, PILOT ATTEMPTED TO SHUT DOWN THE ENGINE DUE TO SLOW START. ENG KEPT RUNNING, PILOT WENT TO EMERG SHUT OFF. UPON INSP, POWER LEVER ''END'' HAD COME OFF OF ''BALL JOINT'' WHICH IS ATTACHED TO FUEL CONTROL. THE SAFETY PIN THAT SAFTIESSDR AC2A0000064Control Cable · damagedAFTER LANDING ON SS169C, MOVED ENGINE THROTTLES TO GROUND IDLE WHILE LOADING AND UNLOADING PASSENGERS. WHEN THROTTLES MOVED BACK TO FLY, NR 2 THROTTLE MADE A NOTICEABLE CLICK AT THE FULL OPEN POSITION AND TRAVEL FURTHER FORWARD IN THE QUADRANT. PULLED THROTTSDR CA000621033Cable · bent(CAN) DURING APPROACH, UNABLE TO MOVE NR 3 ENGINE THRUST LEVER. INFLIGHT SHUTDOWN CARRIED OUT AS PER PROCEDURE. AFTER INSPECTION, MAINTENANCE FOUND TELEFLEX CABLE BENT WITH GROOVE SPLINE BROKEN. TELEFLEX CABLE AND FUEL FLOW REGULATOR LOWER BOX REPLACED AND AIRSDR HNAA0000047Engine · out of rigNR 1 ENGINE POWER LEVER WOULD NOT ADVANCE PAST 82 PERCENT TORQUE. AIRCRAFT RETURNED TO THE FIELD. RIGGED AND TRIMMED NR 1 ENGINE.SDR CA000614005Nut · loose(CAN) INVESTIGATION REVEALED THE P/N 016A-43298 LT-RT THREADED ADJUSTMENT ROD ON THE POWER LEVER ATTACHMENT TO THE ENGINE, HAD COME LOOSE AND HAD MOVED, CAUSING A POWER LEVER MISMATCH. IT IS ASSUMED THAT THE LOCKNUTS WERE NOT SUFFICIENTLY TORQUED FOLLOWING ASDR 20001018AP002Lever · groovedWHILE INVESTIGATION A PILOT REPORT OF AN ENGINE THAT WAS SLOW TO SHUT DOWN, THE MECHANIC DISCOVERED THE RIGHT FUEL CONDITION LEVER HAD A GROOVE WORN IN IT. THE GROOVE WAS CAUSED BY NORMAL CONTACT WITH THE PEDESTAL, AS THE LEVER IS MOVED FOR AND AFT. THE DAMASDR CA000614010Throttle Control · defective(CAN) AT SCHEDULED MAINTENANCE FUNCTION, THE THROTTLE CONTROL WAS FOUND TO BE DEFECTIVE. THE OUTER CASING (SHROUD) HAD SEPARATED AT A SWAGED FITTING NEAR THE ENGINE END.SDR EIA2000021Nut · missingHKG - AT CRUISE, NR 1 ENGINE ROLLED BACK. NO THROTTLE RESPONSE. ATTEMPTED AIRSTART WITH NO RESULTS. DURING INSPECTION, FOUND NR 1 ENGINE STRUT AREA THROTTLE CONTROL BOX SECURING NUT MISSING, AND CONTROL BOX DISENGAGED FROM CONTROL SHAFT. BOTH BEVEL AND WASSDR COMA0010106Lever · malfunctionedLEFT ENGINE POWER LEVER ADVANCED CAUSING OVER TORQUE AND OVER TEMP. DOWN LOADED DFDR AND FOUND TORQUE AND TEMP EXCEEDENCE TO BE WITHIN M/M LIMITATIONS.SDR CA000505005Cable · failed(CAN) NR 1 ENGINE LOWER POWER CABLE BLENDED TO 50 PERCENT AT THE ENGINE FIREWALL METAL PULLEY. NEW CABLE INSTALLED.SDR 2000UALA00208Switch · failedON GEAR RETRACTION WARNING HORN CAME ON. RETURNED TO DEN. *S/D* REPLACED NR 1 THROTTLE SWITCH. OPERATIONAL CHECK OK.SDR AU000327Screw · loose(AUS) THROTTLE OVERRIDE KNOB OPERATING CABLE SEPARATED DUE TO A LOOSE GRUB SCREW.SDR CA000511043Cable · separated(CAN) DURING TAKEOFF, THE LEFT ENGINE REMAINED AT MAXIMUM RPM WHEN CLIMB POWER WAS SELECTED FOR BOTH ENGINES. MAINTENANCE FOUND THE LEFT THROTTLE CABLE BROKEN WITHIN THE PEDESTAL AREA AT THE POINT WHERE THE CABLE ENTERS THE HOUSING. CABLE REPLACED.SDR COMA0010054Solenoid · malfunctionedFLIGHT IDLE SOLENOID CIRCUIT BREAKER TRIPPED. REPLACED THE LEFT HAND SOLENOID.SDR 00FDEA00252Throttle · failedNR 2 ENGINE THROTTLE WOULD NOT RETARD. *S/D* PERFORMED THRUST LEVER FRICTION BRAKE ADJUSTMENT IAW MM 76-11-1. AC OK FOR SERVICE.SDR 20000510SH018Control Cable · brokenPILOT DISCREPANCY REPORT THAT POWER LEVER HAS NO AUTHORITY OVER LEFT ENGINE. MAINTENANCE FOUND POWER LEVER CONTROL CABLE BROKEN IN WING ROOT AREA. CABLE SHOWS EVIDENCE OF BEING KINKED. BREAK IS IN THIS AREA. CABLE REPLACED WITH CONTROL CABLE C8102414. ENGISDR MALA000251Throttle Cable · stuckNR 1 THRUST LEVER FROZE A 90% N1 UNABLE TO CONTROL ENGINE. DESCENDED INTO WARMER AIR REGAINED CONTROL OF ENGINE. MX REMOVED SADDLE PANEL ON NR 1 NACELLE AND DRIED OUT CABLES AND PANEL, REINSTALLED PANEL AND SEALED FROM MOISTURE.SDR 20000515SH019Switch · brokenTHE LOW POWER GEAR UP WARNING SWITCH ON THE THROTTLE QUADRANT WAS FOUND BROKEN INTERNALLY. WHEN THE THROTTLES WERE ADVANCED THE SWITCH WOULD OPEN AND SHORT TO GROUND CAUSING THE LANDING GEAR CONTROL CIRCUIT BREAKER TO OPEN. WHEN THE THROTTLES WERE PULLED BASDR DLL10000643Control Cable · brokenFROM ABOUT 13000 FT TO GROUND, NR 2 ENGINE WAS NOT RESPONSIVE TO THROTTLE MOVEMENT. ENGINE SHUT DOWN AT TOUCH DOWN WITH FUEL SWITCH. FOUND TELEFLEX CABLE END BROKEN AT FFR END. REPLACED CABLE, NOW CKS OK.SDR AU000223Bearing · seized(AUS) RT ENGINE POWER CONTROL ROD END BEARING SEIZED AT THE UPPER CONCENTRIC SHAFT ASSEMBLY.SDR MALA000246Control Cable · failedDURING CRUISE 1, 3, & 4 THRUST LEVERS RETARDED, NR 2 STUCK AND WE TURNED IT OFF. A/T NR 2 STILL STUCK AT 95.91 N1 AFTER ABOUT 20 MINUTES IT BECAME UNSTUCK. MX REPLACED NR 2 TELEFLEX CABLE PN188949. ALL CHECKS GOOD. NO MOISTURE NOTED REINSTALLED PANELS AS REQSDR 20000511SH004Control Cable · roughFUEL CONTROL CABLE ROUGH AND DIFFICULT TO MOVE. (X)SDR CA000323007Cable · frayed(CAN) NR 3 THROTTLE REPORTED TO BE JAMMED BETWEEN UNIT 4 AND 4. CABLE CASING ASSY INNER TEFLON SHEATHING FOUND FRAYED. LOWER THROTTLE BOX, CABLE ASSY, AND CABLE CASING REPLACED.SDR CA000322010Throttle Cable · damaged(CAN) PILOT REPORTED THROTTLE STUCK HALF WAYS WHICH RESULTED IN A HARD LANDING. CABLE DISASSEMBLED AND FOUND SEVEN BROKEN STRANDS ABOUT .75 INCH FROM SWAGGED END WITH ABOUT 1.50 INCH MISSING (ON THE COCKPIT SIDE OF THE CONTROL).SDR 00FDEA00096Throttle · frozenPRIOR TO DESCENT, NR 2 THROTTLE FROZE IN POS. PERFORMED IN FLT ENGINE SHUTDOWN CKLIST & APPRO RED TABS. REMOVED AND REPLACED NR 2 ENG THROTTLE PUSH-PULL CABLE WITH MM 76-11-01-2. RAN NR 2 ENG IAW DC10 JRH.SDR AALA20000309Throttle · jammedMIA - FLT 1300 - DURING TAKEOFF ROLL, LEFT THROTTLE JAMMED AT TAKEOFF POWER. SHUTDOWN ENGINE AND RETURNED AND LANDED MIA WITHOUT INCIDENT. (M)SDR CA000224015Shaft · binding(CAN) START LEVER STIFF AND SPONGY. FOUND ENGINE CROSS SHAFT BINDING. INNER AND OUTER CROSS SHAFT REPLACED.SDR GLBA2001036Engine · out of rigUNSCHEDULED LANDING - RIGHT ENGINE POWER LEVER LIMITED ON TORQUE. RIGGED RIGHT ENGINE, OPS CHECKED GOOD.SDR 00FDEA00075Switch · failedALL 4 GEAR IND STAY RED ON BOTH PNLS. RAN RED TAB PROC WITH NO RESULTS. REMOVED AND REPLACED NR 3 SUBPEDESTAL THROTTLE SWITCH ASSY PER DC10 MM 76-11-04-2. OPS CHECK GOOD.SDR CA000224020Cable · damaged(CAN) DURING APPROACH ENGINE POWER INCREASED. PILOT COULD NOT CNTL ENGINE WITH THROTTLE CNTL AND CARRIED OUT A MISSED APPROACH. ON A SUBSEQUENT APPROACH AND LANDING, PILOT USED MIXTURE CNTL TO SHUT DOWN ENGINE PRIOR TO TOUCHDOWN. A/C HAD TO BE TOWED FROM RUSDR SIMA0291Control Cable · inoperativeDFW - FLT 3748 - NR 2 ENGINE FAILED INFLIGHT. WHEN NUMBER 2 LEVER WAS ADVANCED DID NOT HAVE A PLUS TORQUE OR ITT INCREASE. TORQUE REMAINED AT 20 PERCENT ITT AT 500 DEGREES. REMOVED AND REPLACED RIGHT ENGINE POWER CABLE FROM NACELLE IAW SAAB MM 76-10-46. PESDR CA000128059Brace · loose(CAN) ON APPROACH NR 2 ENGINE WOULD NOT RETARD BELOW 93 PERCENT. CREW SHUT DWN ENGINE AND DECLARED AN EMERGENCY. MAINTENANCE FOUND THE HOLD OPEN STRUT ON THE UPPER CORE COWL DOOR HAD FALLEN ONTO THE THROTTLE MECHANISM AND JAMMED THE THROTTLE CONTROLS.SDR 2000ZZZX361Control Cable · bentNOSE GEAR FAILED TO EXTEND. FOUND THE ALTERNATE AIR CABLE (PIPER P/N 554051) NOT ROUTED CORRECTLY IN ENGINE COMPARTMENT AND TY WRAP BROKEN WHICH ALLOWED ALTERNATE AIR CABLE TO BECOME ENTANGLED TO THE NOSE GEAR LOWER DRAG LINK (PIPER P/N 38040-02) AND BOLT (PISDR 2000ZZZX255Throttle Cable · brokenCMH - LEFT THROTTLE STUCK AT FULL THROTTLE. REMOVED AND REPLACED BROKEN THROTTLE CABLE. OPS GOOD.SDR CA991229043Lever · slipped(CAN) CAMBOX INPUT LEVER SLIPPING ON SHAFT, DUE TO INTERFERENCE FROM IMPROPERLY RIGGED FUEL SHUTOFF LINKAGE. OPERATOR REQUESTS TORQUE VALUE FOR IMPUT LEVERFROM MANUFACTURER, NOTE SHAFT IS SERRATED STANDARD MAINTENANCE PRACTICES CAN BE IMPLOYED.SDR 99FDEA00505Throttle · failed99-288 - ON T/O FROM LFPG, MISC DISPLAY IND NO AUTOLAND AND AUTOPILOT 1 AND 2 WOULD NOT ENGAGE. GOT AILERON DISAGREE ALERT. PERF FCC NR 1 AND 2 RTS PER MM 22-00-00-5, (TASK 22-00-00-701-801). ALL RTS PASSED DUE TO PREVIOUS HISTORY. CAT 2 PRECAUTIONARY AND SDR DLM88992791Throttle · bindingAFTER T/O, LEVELING AT 6,000 FEET, LEFT THROTTLE WOULD NOT MOVE BACK. STUCK AT F/F APPROX 6000 PPH. MOVING LEFT THROTTLE TOOK EXCESSIVE FORCE. COULD SEE LEFT FUEL CONTROL LEVER MOVING AS ATTEMPT WAS MADE TO MOVE LEFT THROTTLE. RETURNED CVG UNEVENTFULL LANSDR CA991230040Cable · stuck(CAN) AFTER COMPLETING THE DECENT CHECKS, THE CREW ATTEMPTED TO REDUCE POWER ON BOTH ENGINES. THE POWER LEVER FOR THE RT ENGINE WOULD NOT MOVE. ALL ATTEMPTS TO MOVE THE POWER LEVER WERE UNSUCESSFUL SO THECREW ELECTED TO SHUT THE RT ENGINE DOWN. ON THE GROUND,SDR CA991229010Rod End · loose(CAN) DURING SCHEDULED INSPECTION, THE NR 2 ENGINE CONDITION CONTROL ROD FROM THE TERMINAL QUADRANT TO THE HYDROMECHANICAL FUEL CONTROL UNIT WAS FOUND TO HAVE A LOOSE ROD END AND WAS MISSING A RETAINING RIVIT. THE ROD WAS REPLACED.SDR VNAA9912006Power Lever · failedDURING THE TAKEOFF ROLL, THE CREW ADVANCED THE POWER LEVERS BUT THEY FAILED TO FULLY RELEASE. THE CREW ABORTED TAKEOFF AND PROCEEDED TO CHECK THE SYSTEM. AFTER GROUND CHECKS WERE COMPLETED THE AIRCRAFT WAS CLEARED TO ATTEMPT ANOTHER TAKEOFF. THE AIRCRAFT TOSDR 99ZZZX4554Control Cable · seizedUPON REACHING CRUISING ALTITUDE FROM PLB, THE THROTTLES ON THE RIGHT SIDE WOULD NOT ADVANCE OR RETARD IN-FLIGHT. THE CAPTAIN SHUT DOWN THE NR 2 ENGINE AND LANDED UNEVENTFULLY IN PLB.SDR MALA976644Power Lever · jammedDURING DESCENT OUT OF 28,000 AS THE POWER LEVERS RETARDED, THE NR 1 POWER LEVER STOPPED AT 78 PERCENT. CREW DISENGAGED THE AUTO THROTTLES AND THE NR 1 POWER LEVER WAS JAMMED, WOULD NOT RETARD. IT WOULD HOWEVER MOVE FORWARD. AS WE DESCENDED INTO WARMER TEMP
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