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 AALA202001149010Warning System · activatedAIRCRAFT NOT GROUNDED: REJECTED TAKEOFF 50-60 KNOTS - BRAKE TEMP HIGHEST 275C - LGA RUNAWAY 13 DUE TO "THRUST LEVERS NOT SET" ANNUNICATION. VISUALLY INSPECTED ALL TIRES AND BRAKES, FOUND NO DAMAGE AS IAW MCM-05-96-10 BRAKE TEMPS NOT MEET EXCEEDANCE OPS CKS NORSDR ASAA2020011431850Resolver · wornNR 2 THRUST LEVER HAS EXCESSIVE PLAY. GROUNDED - YES. REPLACED NR 2 THRUST LEVER ANGLE RESOLVER ASSY REF AMM 76--11-05 PB 401. COMPLETED NR 2 THRUST LEVER ANGLE RESOLVER ADJUSTMENT REF AMM 76-11-05-820-801 THRU STEP 2.F. NR 2 ENG THRUST LEVER FREE PLAY ELIMINASDR ASAA2020011331843Knob · looseKNOB HANDLE ON NR 2 THROTTLE IS LOOSE AND WOBBLY. GROUNDED - YES. TIGHTENED KNOB.SDR CDNA2020010922001Throttle Cable · severedAS REPORTED BY PILOTS: "WE WERE MEDEVAC STATUS DEPARTING PHL BOUND FOR YIP WITH 3 PAX ON BOARD. NORMAL ENGINE START AND TAXI FROM ATLANTIC FBO RAMP TO APPROACH END OF RWY35. CLEARED FOR TAKEOFF RWY35. AS I MOVED THE POWER LEVERS FORWARD TO SET TAKEOFF POWER, JSDR AALA201912239010Throttle · stiffAIRCRAFT WAS GROUNDED: RIGHT THRUST LEVER. STUCK 1/2 WAY BETWEEN CLIMB DETENT AND 0 DURING LANDING. WAS ABLE TO GET BOTH THROTTLES TO 0 DURING ROLLOUT. PER TSM 76-11-00-810-820-A. ACCOMPLISHED RESISTANCE CHECK OF ARTIFICIAL FEEL UNIT IAW 76-11-00-820-041-A. SDR AALA2019121879015Throttle · bindingAIRCRAFT WAS GROUNDED: PILOT REPORTS LEFT THROTTLE VERY STIFF/BINDING WITH SCREECHING NOISE WHEN AUTO THROTTLES ON. MAINTENANCE REPORTS NUMBER 1 THROTTLE CONTROL LEVER FAILED FORCE CHECK. REMOVED AND REPLACED ENGINE THRUST MODULE IAW AMM 76-11-01. TEST AND OPSSDR AALA2019120659012Engine · slowAIRCRAFT WAS GROUNDED: PILOT REPORTS FROM SHORTLY AFTER T/O UNTIL 18,000 LEFT ENGINE COMMANDED THRUST WAS 2-3% BELOW N1 COMMANDED THRUST SECTOR. GAP SLOWLY DECREASED UNTIL ALL NORMAL AT 18,000 FT. MAINTENANCE PERFORMED ENGINE ACCELERATION CHECK IAW AMM 71-00-0SDR FQAR20191210015Throttle Cable · kinkedDURING A SCHEDULED INSPECTION, TECH HAD A HARD TIME PULLING THE THROTTLE BACK TO IDLE, INSPECTED CABLE AND FOUND IT TO BE KINKED NEAR THE CONSOLE END, CABLE WAS INSTALLED AT THE FACTORYSDR AALA201912029017Power Lever · bindingAIRCRAFT NOT GROUNDED: RIGHT TRHUST LEVER WOULD NOT MOVE MORE THAN AN INCH FOR TAKEOFF. INSPECTED RT THRUST LEVER FOR ANY JAM AND NONE FOUND. MOVED THRUST LEVER FWD AND BACK AND MOVEMENT IS SMOOTH IAW AMM 76-11-00-001 AND FIM76-11-00.SDR SWIA2019122747419Gearbox · failedLH ENGINE THROTTLE CONTROL GEARBOX ASSY FAILED FUNTIONAL TEST IAW TASK 76-10-00-830-801. REMOVED AND REPLACED THE LT THROTTLE CONTROL GEARBOX IAW AMM. RIGGING AND OPERATIONAL CHECKED GOOD.SDR SWIA2019110546707Throttle · out of adjustLH THROTTLE OUT OF LIMITS AND HAS HIGH RESISTANCE WHEN MOVING. (C-CHECK) RO: 11/04/2019 PERFORMED ADJUSTMENT AND RIGGING CHECKS OF THROTTLES. OPS CHECKS GOOD.SDR ASAA2019092730856Lever · out of position#2 ENG VALVE CLOSED LIGHT REMAINS BRIGHT BLUE WITH ENGINE SHUT DOWN. GROUNDED - YES. FOUND START LEVER OUT OF DETENT. CYCLED LEVER LIGHT EXTINQUISHED. OPS CHECK OK ON ENGINE RUN REF TO B737-800 AMM 71-00-00. OK FOR SERVICE.SDR ASAA2019092230793Screw · looseNUMBER 2 THRUST LEVER VIBRATES AND RATTLES INTERMITTENTLY IN CRUISE FLIGHT. GROUNDED - YES. SECURED LOOSE SCREW ON NR 2 ENG THROTTLE LEVER NO HISTORY.SDR AALA201909179004Control Box · bindingAIRCRAFT WAS GROUNDED: PILOT REPORTS RT THROTTLE STUCK, VERY HARD TO MOVE ON APPROACH, ONE KNOB ABOVE IDLE. AUTO-THROTTLE WAS OFF. MAINTENANCE REMOVED AND REPLACED RT ENG LWR CONTROL BOX. COMPLIED WITH ALL TEST AND ADJUSTMENTS IAW AMM 76-11-10-404-015-ROO AND SDR QXEA2019090900348Control Quadrant · faultyON TAKEOFF AUTO THROTTLE OVRD APPEARED WITHOUT MANUAL INPUT, AT ACCELERATION HEIGHT MESSAGE DISAPPEARED ( AUTOTHROTTLE CHANNELS BOTH INOPERATIVE ). REMOVED FROM SERVICE. R & R THRUST CONTROL QUADRANT ASSEMBLY IAW AMM TASK 76-11-01-000/400-801-A. THRUST REVERSESDR AALA201908079011Throttle · malfunctionedAIRCRAFT NOT GROUNDED: PILOT REPORTS LOW SPEED REJECTED TAKEOFF DUE TO ECAM MESSAGE THROTTLE NOT SET REFERENCE. MAINTENANCE ACCOMPLISHED FUNCTIONAL TEST OF ECU BOTH THROTTLES. CHECKS OK IAW AMM 73-21-60. AFS TEST PASSED IAW AMM 22-96-00, IAW AMM 73-21-60.SDR AALA201907299024Unknown · malfunctionedAIRCRAFT WAS GROUNDED: PILOT REPORTS LEFT ENGINE THRUST LEVER LINKAGE BINDING. NOT AUTO THRUST. AUTO THRUST NORMAL. MAINTENANCE ACCOMPLISHED FIM TASK 76-11-00 FIG 105A. ACCOMPLISHED THRUST LEVER LOAD TEST IAW AMM 76-11-00-501. NO PROBLEMS FOUND AT THIS TIME. NSDR AWHA2019073100000Power Lever · out of rigDURING POST COMPRESSOR WASH ENGINE RUN MAINTENANCE FOUND PROP STARTING TO GO INTO BETA WHEN THE POWER LEVER WAS AT THE GATE. THE MECHANIC DETERMINED THE ENGINE CONTROLS WERE OUT OF RIG AND ADJUSTED REAR CLEVIS AND 11" ROD AS NEEDED AND SAFETIED. OPERATIONAL SDR AALA201907229024Throttle Control · faultyAIRCRAFT WAS GROUNDED: PILOT REPORTS AUTO-THROTTLE DISCONNECTED AND THROTTLE HAD APROX. 1 INCH SPLIT. CA MCDU INDICATES CLIMB 1 F/O MCDU INDICATES CLIMB 2. MAINTENANCE REMOVED & REPLACED TCQ ASSY IAW AMM TASK 76-11-00-000-801-A/400-801-A. OPS CHECK NORMAL.SDR ABXA20190717126Transducer · faultyDURING TAKEOFF, NEITHER ENGINE REACHED TAKEOFF N1 SPEED (109.7). THE RIGHT ENGINE N1 INDICATED 108.8 AND THE RIGHT EGT INDICATED 925 CELSIUS. THE LEFT ENGINE N1 INDICATED 107.9. THE CREW ABORTED THE TAKEOFF AT 125 KIAS. THE AIRPLANE WAS REMOVED FROM SERVICE (GSDR AALA201907129010Gearbox · stickingAIRCRAFT WAS GROUNDED: PILOT REPORTS DURING TAKEOFF, A/T FAILED TO FULLY ADVANCE THRUST OF LT ENGINE 1/2 KNOB WIDTH STAGGER. MAINTENANCE REMOVED AND REPLACED UPPER CONTROL GEARBOX IAW AMM 76-11-12. ALL RIGS AND OPS CHECKS GOOD.SDR AALA201907019040Master Switch · faultyAIRCRAFT WAS GROUNDED: PILOT REPORTS ON SHUTDOWN, ENG #1 KEPT RUNNING WITH ENG #1 MASTER SWITCH IN OFF SHUTDOWN ENG #1 WITH FIRE SWITCH REPEAT. MAINTENANCE REMOVED AND REPLACED ENG 1 MASTER SWITCH IAW ESPM 20-45-21.SDR YADA20190630001Power Lever · stuckPILOT REPORTED THAT WHILE ON TAXI OFF THE BLOCK THAT AFTER LIFTING THE LEFT HAND POWER LEVER INTO GROUND FINE, IT BECAME STUCK. THE LEFT POWER LEVER WOULD NOT MOVE AND NEITHER WOULD THE RIGHT POWER LEVER. AIRCRAFT RETURNED TO PARKING BLOCK AND ENGINE WERE SHUTSDR ASAA2019062829896Resolver · out of adjustTHROTTLES MISMATCHED BY HALF A KNOB WIDTH AT T/O AND CLIMB POWER (#1 AHEAD OF #2). MATCHED UP NORMALLY AT CRUISE POWER. GROUNDED - YES. REMOVED RT THRUST LEVER ANGLE RESOLVER IAW AMM 76-11-05-801-F00. INSTALLED RT TLAR AND AUTOTHROTTLE BRAKE ASSEMBLY PER AMM 7SDR DXTA2019062412525Throttle · obstructedRIGHT ENGINE POWER LEVER STUCK - ON LANDING ROLLOUT, ATC GAVE CLEARANCE TO MAKE NEXT LEFT TURN. THE RIGHT SEAT PILOT ADVANCED THE RIGHT THROTTLE TO ASSIST THE TURN. WHEN HE ATTEMPED TO RETARD THE THROTTLE IT STUCK ABOUT HALF WAY. PIC GRABBED THE RIGHT THROTSDR AALA201906209046Unknown · malfunctionedAIRCRAFT NOT GROUNDED: PILOT REJECTED TAKE OFF. FLEX SELECTED, NO 1 WENT TOGA NO 2 WENT FLEX. MAINTENANCE ACCOMPLISHED OPS TEST OF THROTTLE CONTROL UNIT IAW AMM 76-11-00-710-040, NO FAULTS FOUND. NO DEFECTS NOTED IN PFR, AIRMAN, OR CMS. NO RECENT HISTORY OF DISDR 2020FA0000198Lock Nut · looseTHROTTLE DISCONNECTED IN FLIGHT. THROTTLE FAILED TO WIDE OPEN THROTTLE CONDITION, PILOT USED MIXTURE TO CONTROL ENGINE POWER OUTPUT AND MADE SUCCESSFUL LANDING WITHOUT INCIDENT. MECHANIC FOUND THAT AN AN4-35A UNDRILLED BOLT WAS INSTALLED IN THE THROTTLE ARM.SDR ASAA2019061769698Lever · stickingENGINE 2 THRUST LEVER STICKS IN REVERSE WHEN COMING BACK TO IDLE THRUST GROUNDED - YES. PERFORMED PFR CHECK NO FAULTS NOTED OPERATIONAL CHECK IAW 78-31-00-710-042-A PERFORMED T/R TEST THRU CFDS IAW 78-00-00-810 NO FAULTS NOTED PERFORMED GENERAL VISUAL #2 ENGSDR AALA201906079001Rod End · lack of lubeAIRCRAFT WAS GROUNDED: PILOT REPORTS LEFT THROTTLE LAGS OR STICKS AT LOWER EPR THAN RIGHT THROTTLE WITH AUTO THROTTLE ON. MAINTENANCE LUBRICATED L/H THROTTLE ROD ENDS IAW AMM 12-21-05 AND ACCOMPLISHED L/H THROTTLE FORE AND AFT FORCE TEST IAW AMM 76-11-00-501, SDR 2WAA2019061103Nut · backed outAT TOP OF CLIMB LH ENGINE STUCK IN CLIMB SETTING NO THROTTLE RESPONSE BE IT FULL OR IDLE. COMPLETED QRH IDLE 12.2.5 AND 12.2.10 ENGINE. NORMAL SHUTDOWN. LANDING WEIGHT 122.2. DURING T/S DISCOVERED LH THROTTLE PUSH PULL CABLE ROD HAD COME LOOSE FROM FCU. POWER SDR CA190528017Washer · missing(CAN) QTY 2 COTTER PINS MS24665-132 AND QTY 2 WASHERS AN960PD316L WERE NOT INSTALLED AS SHOWN IN MANUFACTURING DRAWINGS. VIKING IS CONTINUING TO INVESTIGATE (TC# 20190528017)SDR O9IA2019052100001Switch · out of rigON APPROACH INTO ANC, THE RT ENG ENGAGED AUTOFEATHER MODE UNCOMMANDED. POWER WAS APPLIED AND AUTO FEATHER WAS NO LONGER ENGAGED. AIRCRAFT LANDED WITHOUT INCIDENT. UPON ARRIVAL AT THE HANGAR, MAINTENANCE INSPECTED THE SYSTEM AND NOTED THAT THE RIGGING ON THESDR CA190516024Nut · loose(CAN) DISCLOSURE LETTER RECEIVED LT-S6-18-0012 VERS3. ON MARCH 15 2018 A THROTTLE QUADRANT HAS BEEN RETURNED, DUE TO ONE LEVER FOUND WITH ADDITIONAL HANDLING LOAD WITHIN CRUISE RANGE DURING A FLIGHT ACCEPTANCE EVENT. CL-350 THROTTLE QUADRANT ASSEMBLY SOLENOID SDR CA190619001Cable · separated(CAN) THROTTLE REPORTED LOOSE. INSPECTED AND FOUND THROTTLE CABLE SEPARATED WHERE SLEEVE CRIMPS ON THE FLEXIBLE SHAFT. (TC# 20190619001)SDR CA190529022Control Cable · broken(CAN) C-XXXX HAD A REJECTED TAKE OFF DUE TO THE R/H ENGINE HAVING NO RESPONSE WITH POWER LEVER MOVEMENT. REPLACED BROKEN R/H POWER CABLE PEDESTAL SEGMENT AND BALL JOINT ASSEMBLY GROUND RUN FUNCTION TESTED SERVICEABLE. THE PHASE INSPECTION MANUALS HAVE BEEN RESDR VNAA2019050811101Gearbox · failedMX DIVERSION DUE TO RH THRUST REVERSER UNLOCK MSG. EMERGENCY DECLARED AND TRUCKS ROLLED. PLANE LANDED SAFELY AND MX DEFERRED RH THRUST REVERSER. SUPPLEMENTAL INFORMATION. MX REPLACED THE RH THROTTLE GEARBOX AND THROTTLE LOCKOUT SWITCH. OPS CHECK GOOD.SDR 2019FA0000145Push-Pull Cable · defectiveAFTER ENGINE INSTALLATION THROTTLE SPRING BACK WAS EXCESSIVE WITH LOSS OF THROTTLE CONTROL. THROTTLE WOULD GLADLY GO TO IDLE AND STAY THERE EVEN WHEN FULLY ADVANCED. FACTORY AIRFRAME ATTACHMENT IS ON THE FLEXIBLE CABLE 2.5 INCHES AWAY FROM SOLID ATTACHMENT SECSDR CA190423010Link · separated(CAN) DURING RUN UP IT WAS NOTED THAT THE IDLE WAS HIGH (AROUND 70% BELTS ENGAGED)..UPON INSPECTION IT WAS FOUND THAT THE BEARING HAD COME OUT OF THE B564-2 LINK AT THE SERVO END. (TC# 20190423010)SDR CA190422003Switch · failed(CAN) NR 1 ENGINE ECU MANUAL CAUTION ILLUMINATED AT 50FT AGL, TORQUE SPLIT IN CRUISE NOT WITHIN MEL CRITERIA, SOC ELECTED TO RETURN AC TO DEPARTURE AIRPORT. MAINTENANCE REPLACED 6121-S11 MICRO-SWITCH, C/O TEST IAW AMM 76-10-16. BETA BACKUP SWITCH 1&2 BACK TOSDR CA190403020Pushrod · worn(CAN) DURING INSPECTION IT WAS DISCOVERED THAT THERE WAS WEAR ON THE RH POWER LEVER PEDESTAL PUSH ROD. IT WAS DETERMINED TO ORIGINATE FROM INTERFERENCE WITH THE LH PROPELLER CONTROL. AFTER CONSULTATION WITH BEECHCRAFT IT WAS FOUND THAT THE DIAGRAM SHOWING INSTSDR DALA201904012066Resolver · failedCREW PERFORMED A RTO DUE TO NO RIGHT ENGINE THROTTLE RESPONSE FROM IDLE. FOUND RH ENGINE INBOARD SLEEVE MIDDLE LOCKING ACTUATOR BROKEN AND BAD RESOLVER INPUT TO EEC. REPLACED MIDDLE LOCKING ACTUATOR IAW AMM 78-31. PERFORMED, TESTED AND ENGINE RUN WITH CONFIRMSDR 3RAA201903288049Pushrod · abnormalRIGHT ENGINE FCU PUSHROD (FCU CONTROL ROD) ADJUSTMENT TURNBUCKLE JAMNUTS LOOSENED AND THE TURNBUCKLE BACKED OUT LENGTHENING THE PUSHROD OVERALL LENGTH CAUSING LOW ENGINE POWER. BOTH JAMNUTS WERE FOUND SAFETIED ONLY TO THE TURNBUCKLE INSTEAD OF TO THE TURNBUCKSDR 2019FA0000089Actuator Cable · unsecureDURING ANNUAL INSPECTION HEIM JOINT USED TO CONNECT THROTTLE CABLE TO THROTTLE BODY WAS FOUND TO BE PARTIALLY UNSCREWED FROM THROTTLE CABLE. THE WITNESS HOLE ALLOWED A WIRE TO PASS THROUGH, INDICATING INSUFFICIENT ATTACHMENT.SDR ASAA2019031828720Relay · faultyWHILE ACCOMPLISHING T/C 78273000 NR 1 ENG MAINT FAULT 76-31361 (THE START LEVER SIGNALS DISAGREE) - LONG TERM. GROUNDED - YES. REPLACED RELAY R565 PER FIM 76-11 TASK 801. REPAIR CONFIRMATION GOOD. ACCOMPLISHED ENG RUN AND BITE CHECK PER AMM TASK 71-00-00-700-8SDR YADA20190317001Rod End · separationPILOT REPORT: UPON DEPARTURE, THE LEFT ENGINE SURGED TO MAX TRANSIENT POWER WHERE WE SHUT DOWN THE ENGINE. IT WAS STARTING TO SHAKE AND DEEMED UNSAFE. TORQUE READING INDICATED 5000 LBS AND 840 ITT FOR ABOUT 13 SECONDS UNTIL MANUALLY SHUT DOWN NR 1 ENGINE. RIGSDR QXEA2019030700103Control Quadrant · defectiveDURING TAKE OFF AS SOON AS PWR LEVERS WERE BROUGHT ABOVE FLIGHT IDLE NR 2 PEC AND MASTER CAUTION LIGHT ILLUMINATED PWRPLANT MESSAGE SHOWED ON ED. ABORTED TAKE OFF. REMOVED FROM SERVICE. INTERROGATED CDS, FOUND FAULT CODES 200A/B, CLEARED CODES AND PERFORMED PLSDR 2019FA0000052Throttle Cable · brokenAFTER A 50 HOURS INSPECTION, THE INSPECTOR DURING ENGINE RUN-UP ON THE GROUND WITH FULL POWER ACHIEVED. REPORTED NOT TO BE ABLE TO REDUCE RPM TO IDLE. DEFECT WAS TRACED TO BROKEN THROTTLE CABLE INNER CABLE. NEW CABLE FITTED.SDR SWIA2019030545591Gearbox · failedRIGHT ENGINE THRUST LEVER JAMMED ON APPROACH. DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. (FLT#3111) FO: 03/04/2019 CLOSED REMOVED AND REPLACED RT ENGINE THROTTLE GEARBOX IAW AMM. OPS CHECK GOOD AT THIS TIME. THROTTLE MOVEMENT SMOOTH AT THIS TIME.SDR ASAA2019022228334Unknown · malfunctionedDURING CLIMB FROM FL360 TO FL380 A THROTTLE SPLIT DEVELOPED UP TO APPROX ONE KNOB WIDTH WITH THE NR 2 THROTTLE HIGHER THAN NR 1. AT CLIMB POWER BOTH ENGINES WERE PRODUCING FULL THRUST AND EQUAL ON ALL PARAMETERS. EXCEPT FOR THROTTLE SPLIT. AT POWER REDUCTION BSDR SWAA2019022630055Control Lever · crackedNR 1 ENGINE THRUST LEVER HAD A .25" CRACK AT THE NECK OF KNOB ATTACH POINT. REPAIRED LEVER PER EA.
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