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 = '7600' 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 = '7600' 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 2006FA0000575Solenoid · inoperativePROLONGED OPERATION IN MANUAL MODE CAN CAUSE SOLENOID OVERHEATING AND PISTON SEIZURE. FAILURE OF THE PISTON MOVEMENT MAY RESULT IN THE PILOT BEING UNABLE TO APPLY ADDITIONAL MANUAL THROTTLE BEYOND THE VOL (GATE). THIS CAN RESULT IN ROTOR RPM DECAY IN CERTAINSDR F06019Switch · out of rigAIRCRAFT RETURNED TO GATE DUE TO A SPOILER FAULT MESSAGE. MAINTENANCE RIGGED THROTTLE QUADRANT SWITCHES.SDR COMA0560841Cable · brokenFLIGHT 5208- EN ROUTE CIT-CVG, THE LEFT ENGINE WOULD NOT RESPOND TO THROTTLE INPUT, CREW DECLARED AN EMERGENCY AND PERFORMED INFLIGHT SHUT-DOWN OF THE LEFT ENGINE. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE LEFT ENGINE "S" CABLE.SDR CHQA200600004Resolver · failedDURING DESCENT, RECEIVED EICAS MESSAGE "ENG 2 REV DISAGREE" ALONG WITH AMBER "REV" OVER ENGINE 2 N1 INDICATOR. IN ADDITION TO AFOREMENTIONED EICAS MESSAGE AND INDICATION, EICAS MESSAGE "ENG 2 REV FAIL" APPEARED MULTIPLE TIMES. CREW ALSO NOTICED VIBRATION OR SDR P5CA0501413Engine · malfunctionedNR 3 ENG THRUST LEVER WOULD NOT ADVANCE TO TAKEOFF POWER ON T/O ROLL. LOW SPEED ABORT PERFORMED. A/C RETURNED TO BLOCKS. VISUAL INSPECTION OF THROTTLE & PEDESTAL MECHANISM PERFORMED PER MM 76-11-03. NO DISCREPANCIES FOUND AUTOTHROTTLE. FULL POWER ENGINE SDR S2YA05074ARelay · malfunctionedSHORTLY AFTER TAKEOFF, THE CREW REPORTEDA LT FADEC MAJOR CAS MESSAGE. MX REQUESTED THE PERFORMED AN AIR-TURN-BACK BECAUSE OF PRIOR HISTORY. MX REPLACED 2 RELAYS AND SCHEDULED A TEST FLIGHT. AFTER THE TEST FLIGHT HAD NO DISCREPANCIES THE AC WAS RETURNED TO SSDR 05FDEA03312Tube · looseDURING DESCENT THRU FL200, NOTICED NR 2 ENGINE WOULD NOT SPOOL UP FOR LEVEL OFF. N1 REMAINED AT LESS THAN 35 N1, N2 60 PERCENT. NR 2 THROTTLE HAD A VERY LIGHT TRAVEL FORCE AND FELT DISCONNECTED. ACCOMPLISHED RED TABS AND SHUT DOWN ENGINE DUE TO ENGINE BEISDR CA060104003Controller · failedGOVERNOR FAILED TO CONTROL ENGINE RPM. WHEN THROTTLE INCREASED TO 100% ROTOR SPEED. GOVERNOR CONTROL ASSEMBLY REPLACED WITH NEW. AIRCRAFT GROUND RUN AND TEST FLIGHT SATISFACTORY.SDR CA050929001Shaft · broken(CAN) DURING POST ENGINE CHANGE RIGGING NR 1 ENGINE SPRING STRUT ASSEMBLY WAS REMOVED DUE TO EXCESSIVE PLAY (SLOPPY AT LOOSE). AFTER DISASSEMBLY AND INSPECTION SHAFT P/N87620130 WAS BROKEN AT POINT RIVET P/N MS204170AD3. THE SIZE OF THE RIVET LEAVES MINIMAL MSDR QXEA200501227Ecu · inaccurateSEA FLIGHT 2026 - NR 1 ENGINE MANUAL CAUTION LIGHT ILLUMINATED, STAYED ILLUMINATED AFTER CHECKLIST PROCEDURE. MAINTENANCE RESET NR 1 ENGINE ECU PER DHC-8 200 AMM MCN 27631-01. RAN NR 1 AND NR 2 ENGINE AT VARIOUS POWER SETTINGS. NR 1 ECU STAYED ON. CYCLED NSDR CA050418008Nut · crackedUPON INSP NOTICED CRACKED JAN NUT ON LINEAR ACTUATOR.SDR MALA050255Control Unit · malfunctionedCLIMBING THROUGH 12800 AIRCRAFT YAWED TO THE RIGHT. RIGHT ENGINE SHOWED ZERO TORQUE, ZERO NP AND APPROXIMATELY 900 ITT. WHEN POWER WAS REDUCED RIGHT ENGINE OVERTEMP LIGHT ILLUMINATED BUT ITT REDUCED BELOW 900. OTHER ENGINE PARAMETERS APPEARED NORMAL. IGNITSDR CA050126006Spring Strut · broken(CAN) NR 1 ENGINE SHUTDOWN ON GROUND RUN DUE TO BROKEN CONTROL SPRING STRUT. UNABLE TO CONTROL THE ENGINE, SHUTDOWN BY THE TEE HANDLE. MFG IS INVESTIGATING THE EVENT.SDR 2005FA0000683Switch · bindingSWITCH DOES NOT FULLY EXTEND, CAUSING ENGINE TO REMAIN AT IDLE AFTER TWIST GRIP IS PLACE BACK INTO THE (VOL) POSITION DURING IN-FLIGHT EMERGENCY PROCEDURE TRAINING. REMOVED FROM SERVICE, REPLACED WITH NEW. (K)SDR TSAA0471076Line · obstructedFLT 840, NR 2 ENGINE PUTTING OUT LESS POWER THAN THE NR 1 ENGINE AT 1.89 EPR. SUSPECT NR 2 PT2 PROBE. REMOVED DEBRIS FROM THE PT2 SENSE TUBE BETWEEN THE ENGINE AND TRANSDUCER. ENGINE RUN-UP AND EPR CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE.SDR MALA040626Relay · malfunctionedAFTER DEPARTURE FROM MSP GEAR RETRACTED UP, FLIGHT IDLE STOP OPEN LIGHT REMAINED ON. AIR RETURN TO MSP. MAINTENANCE REPLACED TIME DELAY RELAY P/N M83726-28-2001P AS NEEDED. PERFORMED OPERATIONAL TEST OF F1 STOP MECH IAW AMM 76-10-60. OPS CHECK GOOD.SDR ALG2004F00056Amplifier · inoperativeIN CRUISE FLIGHT, BOTH ENGINES STARTED SURGING, EMERGENCY CHECK LIST COMPLIED WITH AND RUN ON LANDING. MAINTENANCE COMPLIED WITH VISUAL INSP OF BOTH ENGINES AND N1 AND N2 CONTROL SYSTEMS, COMPLIED WITH GROUND RUN CHECK AND AFTER ABOUT FIVE MINUTES EXPERIENCEDSDR HNAA0400087Switch · inoperativeNR 2 ENG TQ SURGE AFTER T/O. REMOVED AND REPLACED SWITCH 6141-S4, OPS CHECK GOOD. REMOVED AND REPLACED SWITCH 6141-S4 OPS CHECK GOOD.SDR QXEA200400460Tscu · malfunctionedOTH - FLIGHT 2121, NR 1 ENGINE AUTOFEATHERED AFTER TAKEOFF, OVERTORQUE AT 138 PERCENT NOTED. PEAK OVERTORQUE NOT NOTED. DURATION OF OVERTORQUE NOT NOTED. REPLACED TSCU, ENGINE HARNESS AND NR 1 PROPELLER ASSEMBLY. HARNESS S/N AA8411 HAD 13087.8 HOURS AND 18SDR CA040706001Rod · strippedSVA PILOT VALUE FEEDBACK CABLE ROD THREADS EXCESSIVELY WORN CAUSING ENGINE TO SURGE.SDR HEEA095228Actuator · malfunctionedDURING CRUISE FLIGHT NR 2 ENGINE BEEPED TO MINIMUM BY ITSELF. BEEPED ENGINE BACK UP BUT ENGINE AUTO BEEPED TO MINIMUM. COMPLIED WITH EMERGENCY CHECK LIST AND LANDED AT NEW ORLEANS.SDR 252TR0019Throttle · malfunctionedON TAKE OFF ROLL, LEFT THROTTLE WAS 2 KNOBS AHEAD OF RIGHT ENGINE THROTTLE. ABORTED TAKE OFF. MAINTENANCE FOUND RIGHT ENGINE PT2 LINE CLOGGED AT NOSE DOME. OBSTRUCTION WAS APPROX. 3 INCHES INSIDE OF OPEN END OF PT2 LINE. CLEARED PT2 LINE AND ACCOMPLISHED ESDR MALA040379Condition Lever · damagedRT CONDITION LEVER WILL NOT CONTROL PROP INTO MIN MAX RANGE. PILOT REPORTED DIFFICULTY IN THE MIN/MAX RANGE. MAINTENANCE REMOVED AND REPLACED RT CONDITION AIRFRAME CABLE PN 82180 PERFORMED MASTER RIG TEST RAN ALL CHECKS GOOD.SDR 03FDEA02179Linkage · missingINFLIGHT TOTAL LOSS OF NR 1 ENGINE THROTTLE CONTROL. ENGINE NR 1 ACCELERATED TO 90 PERCENT N1 & N2, SUSPECT ZERO SPEED PROTECTION HAS ENGAGED. ENGINE SHUTDOWN IAW CHECKLIST. FOUND NR 1 ENG THROTTLE CONTROL LINKAGE AFT ROD-END BEARING MISSING. CAPT CONFIRMEDSDR P5CA0300985Sense Line · looseSTART FAILURE NR 3 ENGINE - RETURN TO BLOCKS. INSPECTED NR 3 ENGINE, FOUND CDP SENSE LINE AT EEC LOOSE. CLEANED AND PROPERLY SECURED CDP LINE. ENGINE RUN ACCOMPLISHED WITH ALL PARAMETERS NORMAL.SDR QXEA200301409Switch · out of adjustON FLIGHT 2172 DURING APPROACH WHEN BRINGING CONDITION LEVERS TO 1050, POWER LEVERS FLIGHT IDLE NR 1 ENGINE SURGED FOR ABOUT 2 SECONDS. WHEN POWER LEVERS WERE ADVANCED AHEAD OF FLIGHT IDLE SURGE STOPPED. UPON INSPECTION FOUND NR 1 POWER LEVER BETA BACKUP SWISDR QXEA200301356Condition Lever · malfunctionedON FLIGHT 2301 UNCOMMANDED NP OF 1020 WHEN 850 SELECTED. ALL OTHER ENGINE FUNCTIONS NORMALLY. RESET CONDITION LEVERS TO 1020 AND RESET AT 850 WITH NO FURTHER OCCURRENCE. NO POWER PLANT MESSAGE ON NR 2 ENGINE. REMOVED AND REPLACED FUEL CONTROL WIRE HARNESS.SDR C2010312003MTLine · chafedDURING DAILY INSPECTION THE P/C AIR SENSE LINE WAS FOUND TO BE DAMAGED BEYOND LIMITS. THE DAMAGE WAS CAUSED BY THE THREADED PORTION OF A SCREW RUBBING AGAINST THE LINE. THE SCREW ATTACHES TWO CLAMPS TOGETHER AS REQUIRED BY CEB 1198. THE CLAMPS (P/N 6749387-03 SDR P5CA0300955Push-Pull Cable · failedNR 4 ENGINE THROTTLE BINDED NR 4 ENG FUEL CONDITION MOTOR POPPED C/B. REPLACED ENGINE PUSH PULL CABLE IAW MM 76-11-07 OPS CK OK. REPAIRED WIRE IAW STANDARD PRACTICES 20-00-00. OPS CK OK IAW AMM 76-11-00SDR MALA030424Relay · damagedDURING FLIGHT NR 3168, AFTER TAKEOFF WHEN THE GEAR WAS RETRACTED THE FLT STOP LIGHT ILLUMINATED AND KNOB POPPED UP. AIR RETURN TO DTW. MAINTENANCE PERFORMED TROUBLESHOOTING OF FLIGHT IDLE STOP SYSTEM, IAW MM 76, FOUND RELAY 20GA OUTER SHELL DAMAGED, REPLACSDR CA030915012Comparator · damaged(CAN) PILOT REPORTED DROOP IN RPM AT TAKEOFF. FLEW TO BASE WITH NO PROBLEM. CHANGED OUT GOVERNOR. COULD NOT RIG CONTROLS AS PER MAINTENANCE MANUAL. INVESTIGATION RESULTED IN FINDING INOPERATIVE DROOP COMPENSATOR DUE TO SHEARED RIVET. RIVET REPLACED, CONTROLS RSDR 189201Warning Light · illuminatedON 08/25/03, APPROX. 1143(UTC), FLT 4500, AIRCRAFT ABORTED TAKEOFF WHEN THE FLIGHT IDLE STOP OPEN LIGHT ILLUMINATED AFTER GEAR RETRACTION. AIRCRAFT RETURNED TO FIELD.SDR VNAA0307009Heater · out of positionWHILE CREW WAS DOING CHECKLIST AND CHECKING FLIGHT CONTROLS. AILERONS FELT LIKE THEY WERE HANGING UP. MAINTENANCE INSPECTED AND FOUND ENGINE CONDITION LEVER CABLE HEATER RUBBING ON AILERON CABLE. MAINTENANCE REPOSITIONED HEATER AND FOUND NO DAMAGE TO THE CASDR HEEA088421Motor · splitTORQUE SPLIT, DEAD SPOT BEEPING FROM 60 TO 90 PERCENT. TO BE SENT TO VENDOR FOR REPAIR.SDR 175051Warning System · activatedFLIGHT 4558 FROM FWA TO PIT, SHORTLY AFTER TAKEOFF AIRCREW NOTICED THAT THE FLIGHT IDLE STOP OPEN LIGHT WAS ILLUMINATED. AIRCRAFT RETURNED TO FWA.SDR HEEA088629Support · wornCARDAN JOINT WORN CAUSING EXCESSSIVE WEAR ON INSIDE OF BASE SUPPORT. SCRAPPED.SDR HEEA088422Motor · malfunctionedSTICKS ON LOW SIDE GOING UP. TO BE SENT TO VENDOR FOR REPAIR.SDR GLBA2003097Actuator · malfunctionedRIGHT ENG WILL NOT MAKE T/O POWER. REMOVED AND REPLACED RT ENG ACTUATOR.SDR HEEA087135Actuator · erraticACTUATOR OPERATES ERRATICALLY AND HESITATES DURING MID TRAVEL. TO BE SENT TO VENDOR FOR REPAIR.SDR MALA030286Relay · malfunctionedDURING FLIGHT 2938, F1 STOP OPEN LIGHT ILLUMINATED AFTER GEAR RETRACTION MCX NOTIFIED UPON LANDING F1 STOP LIGHT ILLUMINATED NORMALLY AND F1 STOP FUNCTION APPEARS TO OPERATE NORMALLY. TRIGGER REQUIRED TO PULL POWER LEVERS BELOW F1. AIR RETURN TO MEM DUE TO FSDR 188721Warning Light · illuminatedFLIGHT 4506 FROM PIT TO CRW. SHORTLY AFTER TAKEOFF AFTER THE LANDING GEAR RETRACKED, AIRCRAFT RECEIVED THE FLIGHT IDLE STOP OPEN LIGHT. AIRCREW CYCLED THE GEAR AND THE FLIGHT IDLE STOP OPEN LIGHT STAYED ILLUMINATED. AIRCRAFT RETURNED SAFELY TO PIT.SDR HEEA086677Bearing · wornENGINE CONTROLS HAVE WORN BEARING. SCRAPPED.SDR BAQA087752Meter · inoperativeSLAVING METER INOPERATIVE. REPLACED WITH SERVICEABLE UNIT.SDR COMA0360189Switch · failedFLIGHT 5884 RT ENGINE ROLL BACK DURING T/O AND LATER DURING CLIMB. DEFERRED SPEED CONTROL PER MEL.SDR P5CA0300771Throttle · stuck# 4 ENG. SHUT DOWN ON DESCENT INTO PIK - THROTTLE STUCK AT 2.0 ON THROTTLE QUANDRANT ENG PARAMETERS NORMALS 75% M ONE MORE THIS HAPPENED ON DESCENT OIL PRESSURE AT LAST FEW MIN. OF FLT THROTTLE OK AFTER LANDING. ENG SHUT DOWN CHECKLIST COMPLIED WITH A/C CURRENSDR MWEA030036Line · disconnectedON LEFT THROTTLE, SPLIT INCREASED WITH ALTITUDE TO ABOUT 1 1/2 KNOBS. -- RECONNECTED PRESSURE TOTAL 2 LINE.SDR PCAA0301016Switch Actuator · bentPIT-FLIGHT#3729. CREW REPORTED THEY HAD NO FLIGHT IDLE STOP ON POWER LEVER QUADRANT (BOTH). MAINTENANCE INSPECTED AREA AND FOUND THE MICRO SWITCH ARM FOR THE BETA WARNING HORN SYSTEM WAS BENT CAUSING BINDING. SWITCH ARM WAS STRAIGNTENED, AND SYSTEM FUNCTIONALLSDR HEEA082403Shaft · wornTORQUE SHAFT BUSHING HOLES WORN. IN SHOP REPAIR.SDR BMAC020024SConnector · contaminatedPILOT REPORTED BRIEF ENGINE POWER LOSS ON RT ENGINE FROM 60 PERCENT TO 10 PERCENT TORQUE NOTED, (TWO TIMES) SHUT SRL AND TTL OFF. FLT UNEVENTFUL, WITHOUT INCIDENT FOR LAST 15 MINUTES AND SRL AND TTL STAYED OFF. PILOT ELECTED TO AIR RETURN TO CBE. MAINTENANCSDR MALA020629Ctot PanelDURING DESCENT AND APPROACH OF FLIGHT #3154 INTO MSP, LEFT ENGINE WOULD SURGEWHEN THE POWER LEVER WAS MOVED IN THE RANGE OF 50% TO 35% TORQUE. OK ABOVE OR BELOW THIS RANGE-CTOT WAS SELECTED OFF. ALSO THE POWER LEVER IS ON THE 64 DEGREE MARK WHEN THIS HAPPEN
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