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 CA050728009Lever · failedAIRCRAFT LANDED, WHILE FOLLOWING MARSHALLER'S HAND SIGNALS ONTO THE FBO RAMP, THE THROTTLE WAS ADVANCED TO COMPLETE TURN. WHEN THE THROTTLE WAS ADVANCED IT WAS UNRESPONSIVE ON TWO FULL MOVEMENTS. THE AIRCRAFT WAS SHUT DOWN WITH THE MIXTURE. A QUALIFIED AME SDR AU510001992Control Cable · brokenLT ENGINE POWER CONTROL CABLE BROKEN BETWEEN POWER LEVER AND CABLE JOINT.SDR 2005FA0001198Wedge · brokenCABLE BROKE AT THE S3 WEDGE WHERE THE BARREL END CONNECTS TO THE INTERNAL CABLE. THIS AREA IS NOT VISIBLE AS THERE IS AN INTERNAL SLEEVE THAT COVERS THE CABLE IN THIS AREA. ( CE07200516270) (K)SDR CA050718012Throttle Cable · brokenON START UP AT THE BASE, THE N1 WENT DIRECTLY TO MAXIMUM RPM. THE PILOT ATTEMPTED TO SHUT THE ENGINE WITH THE THROTTLE CONTROL AND DID NOT GET ANY EFFECT ON THE ENGINE. THE PILOT CALLED AN AME THAT COULD SHUT THE ENGINE BY ACTIVATING THE GAS PRODUCER LINKAGESDR 05FDEA01850Wire · brokenABORTED TAKEOFF DUE TO ENG NR 2 FAILED TO STABILIZE AT 40 PERCENT POWER, WITH NR 1 ENG THROTTLE SET NORMALLY TO PRODUCE 40 PERCENT N1 THE NR 2 THROTTLE WAS THREE KNOB WIDTHS AHEAD AND STILL ONLY PRODUCING 25 PERCENT N1. FOUND WIRE BROKEN INSIDE RING TERMINAL.SDR 2005FA0000941Throttle Cable · brokenDURING CROSS COUNTRY TO KINGMAN, DURING A TOUCH AND GO PROCEDURE THE STUDENT DECREASED THE THROTTLES BUT THE RIGHT ENGINE POWER DID NOT REDUCE. DECLARED AN EMERGENCY AND DURING THE LANDING FLARE THE MIXTURE WAS CUT OFF KILLING THE ENGINE. MAINTENANCE PERSONNSDR COMA0560346Gearbox · crackedWHEN PERFORMING EO 76-011 AD, THE RIGHT ENGINE THROTTLE GEARBOX HOUSING WAS FOUND CRACKED AT THE ATR ATTACH POINT. REMOVED AND INSTALLED A SERVICABLE GEARBOX.SDR RAIA00506001Switch · malfunctionedLT ENGINE IDLE STOP FAILED. MAINTENANCE REMOVED AND REPLACED NR 1 IDLE STOP SWITCH. OPS CHECKED GOOD.SDR C1HA200593004Power Lever · out of rigUPON APPLICATION OF T/O THRUST, NR 3 ENGINE POWER LEVER TO FORWARD STOP AND EPR ONLY 2.05 FULL T/O EPR = 2.13 T/O ABORTED IAW CHAMPION PROCEDURES. SOC, MX CONTROL NOTIFIED. ALL OTHER ENGINE PARAMETERS IN YELLOW BAND FOR NR 3, PERFORMED STATIC RIG CHECK IAW MSDR C1HA200593003Rod · out of adjustUPON APPLICATION OF FULL T/O THRUST NR 3 ENGINE POWER LEVER WENT TO FORWARD STOP AND EPR ONLY 2.00 (T/O EPR 2.09) T/O ABORTED IAW CHAMPION PROCEDURES. SOC, MX CONTROL NOTIFIED. ALL OTHER PARAMETERS IN YELLOW BAND FOR NR 3, NR 3 ENGINE INTAKE AND EXHAUST INSPSDR CA050510008Throttle Cable · misaligned(CAN) ON CLIMB OUT THRU FL 130 EICAS (L PRV) QRH COMPLETED - THRU FL 200 LT THROTTLE VERY HARD TO ADVANCE OR MOVE TO IDLE. A/T ARM OFF NO IMPROVEMENT. RETURN TO LHR. NO LT REVERSE ON LANDING. FOR T/S AND INFO ON PRV REFER TO L1425969. LT ENG PUSH PULL CABLE RSDR PNSA050502Disc · faultyON INTIAL CLIMB RT ENGINE ENCOUNTERED POWER SURGES. PILOT DECLARED EMERGENCY AND RETURNED TO ANC. DURING RETURN PILOT DISCOVERED RT SPEED LEVER HAD MOVED AFT FROM TAKEOFF POSITION. MAINTENANCE CHANGED FRICTION LOCK DISCS ON RT SPEED LEVER AND GROUND RUN ENGSDR CA050517007Arm · wornAFTER AN UNEVENTFUL FLT, CREW UNABLE TO GET THE RT ENGINE TO DROP BELOW 78 PERCENT NG AND IT HAD INSUFFICIENT REVERSE. MAINTENANCE INVESTIGATED AND FOUND THAT THE PIVOT ARM (50-944076-3) ON THE CAM CLUSTER HAD WORN ALLOWING IT TO SLIP ON THE CAM, CHANGING THESDR DJFA2005087Lever · splitCREW REPORTED THAT WHILE AT CRUISE FLIGHT 380, WITH ENGINE SYNCRONIZATION ON, BOTH ENGINES ROLLED BACK FROM N1 AT 98.0 TO 90.9, OAT WAS -63 DEGREES. THE ENGINE SYNCHRONIZATION WAS TURNED OFF AND ENGINE IGNITERS WERE TURNED ON. THE CREW WAS THEN ABLE TO INCRESDR CA050425009Push-Pull Cable · contaminated(CAN) WHILE IN CRUISE AT 340, AFTER 2.5 HRS IN FLIGHT, NR 2 ENGINE THROTTLE JAMMED. QRH APPLIED WING ANTI-ICE SELECTED. AFTER CRUISING AT 260, THROTTLE CONTROL RECOVERED AND NORMAL OPERATION UP TO FL 360 AND THE REMAINING OF THE FLIGHT. THROTTLE CONTROL VESDR MASA200500311Gearbox · wornCOMPLIED WITH THROTTLE GEARBOX INSPECTION OF NR 2 ENGINE AND FOUND WEAR TO BE ACCEPTABLE AND WITHIN LIMITS OF MESA EO CRJ-76-0004. REMOVED AND REPLACED.SDR MASA200500310Gearbox · wornCOMPLIED WITH THE THROTTLE GEARBOX INSPECTION OF THE NR 1 ENGINE AND FOUND WEAR TO BE ACCEPTABLE AND WITHIN LIMITS OF MESA EO CRJ-76-0004. REMOVED AND REPLACED.SDR CA050419009Pulley · binding(CAN) ACFT DEPARTED & RETURNED WITH PRECAUTIONARY ENGINE SHUTDOWN DUE TO JAMMED POWER LEVER. MX ABLE TO DUPLICATE SYMPTOMS. POWER LEVER CIRCUIT INSPECTED & IN RT SIDEWALL AT PULLEY ASSY, A SMALL SCREW NR 4 DIAMETER .375 INCH LONG FOUND IN IMMEDIATE VICINITY. SDR CA050418011Throttle Cable · damagedPILOTS REPORTED LT THRUST LEVER SPLIT (AFT) IN T/O DETENT. FOUND AFT THROTTLE CABLE EXTREMLY STIFF. THIS WAS SECOND OCCURENCE TO THE COMPANY IN A WEEK FIRST SUBMISSION ON SDR NUMBER 20050418010SDR CA050418010Throttle Cable · failedLEFT THROTTLE WOULD NOT STAY IN DETENT WAS REPORTED BY FLIGHT CREW. THROTTLE FORCE CHECK FAILED AND AFT CONTROL CABLE WAS DETERMINED FAULTY.SDR ALG2005F00022Throttle · misused1ST START, STARTED ENG, BEGAN HYD CHK, COMPLETED HYDR CHECK, ENG FLAMED OUT. WENT THROUGH ENG SHUTDOWN PROCEDURES, NOTICED THROTTLE WAS NOT QUITE PASSED IDLE DETENT. DUE TO THIS FACT, ATTEMPTED A SECOND START, PRIOR TO ENG IDLE, ENG FLAMED OUT. MAINT DETERMSDR 2005FA0000410Throttle · misinstalledREF: (ATC0515) NR 1 ENGINE THROTTLE TELEFLEX CABLE OUTER SLEEVE RETAINING NUT FOUND TO HAVE COME ADRIFT, ALLOWING THE OUTER PORTION OF TELEFLEX CABLE TO MOVE. THE RETAINING NUT, ALTHOUGH DRILLED FOR WIRE LOCKING, THERE IS NO EVIDENCE OF WIRE LOCKING BEING CARSDR UPS05843967Throttle · stuckNR 2 THROTTLE STUCK IN IDLE DURING VISUAL APPROACH. NR 2 AND NR 3 REVERSERS USED IN FLIGHT PRIOR TO APPROACH. DURING T/S RAN ENG NR 2 & CYCLED T/R 3 TIMES AFTER CYCLING T/R THROTTLE CLD ONLY ADVANCE 2-3 BEFORE JAMB WITH ENG SHUTDOWN THROTTLE WLD MOVE FULL TRSDR 2005FA0000197Throttle Cable · damagedAFTER TAKEOFF, THROTTLE WOULD NOT COME BACK. THROTTLE HAD TO BE FORCEABLY PULLED BACK OUT OF TAKEOFF SETTING. CABLE WAS FOUND BAD. (GL11200507568) (K)SDR AU510001960Nut · separated(AUS) NR 2 ENGINE POWER CONTROL LEVER CONTROL CRANK RETAINING NUT LOCATED ON THE MAIN ACCESSORY GEARBOX CROSS SHAFT ADRIFT. THE CRANK MOVED OFF THE CROSS SHAFT AND POWER LEVER CONTROL WAS LOST. THE RESULT OF THE UNCONTROLLED POWER LEVER ALLOWED AN UNCOMMANDED SDR AU510001847Control Cable · brokenRT ENGINE POWER LEVER CABLE BROKEN AT END FITTING WHERE IT ATTACHES TO THE HYDROMECHANICAL UNIT (HMU).SDR P5CA0501320Clamp · looseON PREFLIGHT, NR 4 THROTTLE WOULDN’T ADVANCE FORWARD. T/S FOUND SHIELD SUPPORT BRACKET CLAMPS LOOSE AT PUSH PULL CABLE. SECURED PUSH PULL SHIELD SUPPORT BRACKET CLAMPS PER MM 76-11-05. OPS CHECK OK.SDR AU510001681Rod End · separatedCARBURETOR THROTTLE ARM DISCONNECTED FROM RODEND DUE TO USE OF INCORRECT HARDWARE. LIMITED INFORMATION PROVIDED. PERSONNEL/MAINTENANCE ERROR.SDR DXTA200500567Power Cable · out of rigON LANDING THE POWER LEVERS WERE BROUGHT TO IDLE AND LEFT ENGINE FAILED (AT IDLE). ADJUSTED FLOW DIVIDER TO FUEL CONTROL INTERCONNECT ROD FOR PROPER IDLE DETENT. RIGGED AFT POWER CONTROL CABLE TO PROVIDE SLIP FIT OF ROD END AT BOLT. GROUND RAN AND NUMEROUS SDR CA050117009Power Lever · frozen(CAN) DURING CRUISE FLIGHT, NOTICED BY CREW THAT THE NR1 ENGINE POWER LEVER WAS FROZEN IN POSITION. THE ENGINE WAS SHUTDOWN AND AN UNEVENTFUL LANDING WAS COMPLETED. WITH WARMER TEMPERATURES, POWER LEVER WAS ABLE TO MOVE FREELY THROUGH ITS FULL RANGE OF TRAVELSDR DXTA200500539Control Lever · malfunctionedLEFT ENGINES SHUTS DOWN WHEN THROTTLE BROUGHT BACK TO FLIGHT IDLE. SUSPECT QUADRANT SWITCH. RAN ACFT, FOUND IDLE TO LOW. PERFORMED POWER CONTROLS ADJUSTMENT, SET IDLE, FLIGHT IDLE ADJUSTMENTS. CHECKED TAKEOFF POWER AND CUTOFF. OPS CHECK GOOD ALL IAW CE560SDR AU510002160Cable · failedLH ENGINE THROTTLE CABLE FAILED IN AREA UNDER SHEATH.SDR DJFA2005049Cable Assy · bindingCREW REPORTED THAT WHILE AT CRUISE FL390 FOR APPROXIMATELY 15 MINUTES, THEY WERE UNABLE TO ADJUST THE LEFT POWER LEVER AS IT WOULD NOT MOVE. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS DIVERTED TO KELP. WHILE DESCENDING THROUGH FL220 THE LEFT POWER LEVER HAD SDR PNSA041203Power Lever · separatedDURING INTIAL TAKEOFF ROLL LEFT POWER LEVER REVERSE TRIGGER CAME LOOSE AND FELL IN QUANDRANT. FLIGHT CREW ABORTED TAKEOFF AND RETURNED TO GATE.SDR AMTA200401475Lever · stuckUPON LEAVING CRUISE AT FL 410 LT ENGINE THROTTLE LEVER STUCK AT 1.5 EPR AND 85 PERCENT N1 IT UNSTUCK AT FL 240 AND WAS THEN NORMAL. PERFORMED FIM 76-11-00, FIG 103, STEPS 1, 1A, 2, 11, 22. SYSTEM OK. ALL OPS NORMAL. (GL11200508816) (K)SDR CALA0500034Throttle Cable · jammedTHE NR 1 THROTTLE JAMMED AND DID NOT RETARD (STUCK AT 83 PERCENT N1) ON INITIAL LEVEL OFF. THE NR 1 ENGINE WAS SHUTDOWN FOLLOWING QRH. THROTTLES SPLIT. TRIED TURNING OFF AUTOTHROTTLE TO NO AVAIL. THE NR 1 THRUST CONTROL PUSH-PULL CABLE WAS REMOVED AND REPLSDR RAIA00411009Switch · dirtyPIT- SPEED BRAKE DISAGREE MESSAGE. MAINTENANCE CLEANED THRUST LEVER SWITCHES, PERFORMED HIGH SPEED TAXI AND FUNCTIONAL TEST OF SPOILER/SPEED BRAKE SYSTEM.SDR 51011082004Throttle Cable · frozenDURING DESCENT INTO FAIRBANKS AK, PILOT REPORTED "A STUCK LT POWER LEVER" PILOT PERFORMED A PRECAUTIONARY ENGINE SHUT DOWN PER THE CHECKLIST AND CONTINUED HIS DESCENT. APPROX 8 MILES FROM THE AIRPORT THE PILOT "BUMPED" THE POWER LEVER AND FOUND IT TO BE "FREE"SDR CALA0500033Throttle Cable · stiffTHE THROTTLES WOULD NOT REDUCE TO CLIMB POWER IN VNAV CAPTAIN SIDE THROTTLES WERE VERY STIFF. TROUBLESHOOTING FOUND BOTH NR 1 & NR 2 ENGINE THRUST CONTROL PUSH-PULL CABLES AT FAULT. THE NR 1 & NR 2 ENGINE THRUST CONTROL PUSH-PULL CABLES WERE REMOVED AND REPLSDR 2005FA0001397Throttle Cable · failedTHROTTLE CABLE BROKEN INSIDE OF CABLE HOUSING 26 INCHES FROM CABLE END. NOTED THAT CABLE ASSEMBLY MAKES TIGHT RADIUS BEND BEHIND INSTRUMENT PANEL, JUST AFT OF FIREWALL. (K)SDR 2004FA0000842Bracket · crackedA STUDENT NOTICED ON PRE-FLIGHT A CRACK ON THE THROTTLE BELLCRANK SUPPORT BRACKET, (PN 269A8460-1)MOUNTED TO THE CARBURETOR. THE CRACK WAS LOCATED JUST BELOW THE THROTTLE CONTROL BELLCRANK ATTACH LUG AND WAS NOTICEABLE UPON APPLYING LATERAL PRESSURE TO A LINKASDR 2004FA0000841Bracket · crackedA STUDENT NOTICED ON PRE-FLIGHT, A CRACK ON THE THROTTLE BELLCRANK SUPPORT BRACKET, (PN 269A8460-1) MOUNTED TO THE CARBURETOR. THE CRACK WAS LOCATED JUST BELOW THE THROTTLE CONTROL BELLCRANK ATTACH LUG AND WAS NOTICEABLE UPON APPLYING LATERAL PRESSURE TO A LINSDR CA041006008Throttle Cable · broken(CAN) PILOT MAKING AN APPROACH TO SCHEDULED LANDING WHEN ENGINE POWER WENT TO IDLE WITH NO RESPONSE TO ACTIONS OF THROTTLE CONTROL. PILOT ELECTED TO LAND IN FIELD SHORT OF RUNWAY AND EXPERIENCED NO DIFFICULTY. AIRCRAFT EQUIPPED WITH TUNDRA TIRES. MAINTENANCESDR 4023Throttle Arm · brokenAIRCRAFT WAS ON APPROACH AND ENGINE WOULD NOT RESPOND TO POWER LEVER ADJUSTMENTS. ENGINE WAS SHUT DOWN AND LANDING WAS MADE. VISUAL INSPECTION REVEALED THROTTLE ARM BROKEN AT THROTTLE BODY. REPLACED WITH NEW.SDR 04FDEA02674Throttle · obstructedRTO DUE TO LOW POWER NR 2, ENG NR 2 THROTTLE WOULD NOT ADVANCE PAST REF. POINT 30 AND N1 ADVANCED TO 93 PERCENT VS 108 PERCENT REQUIRED. RTO OCCURRED AT 90 KTS. ENT BY: 273927 RPT BY: 096714 SHGN 11SEP04 02:40 GDL U IN WORK, ENT BY: 273927 RPT BY: 27392SDR P5CA0401191Actuator · malfunctionedAFTER PUSHBACK, ON ENGINE START NR 1 ENGINE FUEL CONDITION ACTUATOR CIRCUIT BREAKER OPENED. REMOVED AND REPLACED NR 1 FUEL CONDITION ACTUATOR, ALL OPS NORMAL.SDR 2004F00338Control Cable · brokenTHROTTLE CABLE BROKEN 12 INCHES FROM END OF CABLE. BROKEN AT AFT END OF FORWARD CABLE WHERE FORWARD CABLE ATTACHES TO AFT CABLE. (SO13200405891)SDR CA040831018Control Cable · kinked(CAN) FOLLOWING ONE FLIGHT, LT THROTTLE WAS VERY STICKY ON GROUND, NO PROBLEM IN FLIGHT. MAINTENANCE FOUND THE REAR CARGO CEILING PANEL OBSTRUCTING THE LT ENGINE PUSH/PULL CABLE QUADRANT. THE CEILING PANEL WAS KINKED BY LUGGAGE. STILL UNDER INVESTIGATION FOSDR ERAA097087Throttle · contaminatedWATER CONTAMINATED, EMERGENCY THROTTLE LOCKED UP. DUE L/O IN 96 HOURS. ECU SHAFT AND THROTTLE VALVE STIFF 6O ROTATE, FUEL PUMP DRIVE SHAFT VERY STIFF. INTERNAL CORROSION TO FUEL SYSTEM DUE 6O WATER CONTAMINATION. INHIBIT AND PRESERVE ENGINE FUEL SYSTEM IAWSDR MALA040520Control Cable · looseON DESCENT NR 2 POWER LEVER FROZE IN POSITION N1 94 PERCENT HARD TO SHUT ENGINE DOWN ON APPROACH THE POWER LEVER CAME LOOSE AND WAS POS TO FUEL OFF ENGINE WINDMILLED APPROX 15 MIN AT 7/5 PERCENT N2. MAINTENANCE REPLACED NR 2 ENGINE CONTROL CABLE (P/N 251561),
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