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 HALA2009080800357Throttle · out of adjustETOPS SIGNIFICANT SYS - ENG THRUST LEVERS MISALIGNED IN NORM MODE. RT THRUST LEVER LAGS 1/2 KNOB W/EPR MATCHED LT ENG N1-EGT-F/F HIGH AND N2 IS LOW 2 PERCENT. INSPECTED LINKAGES AND BRGS T/S IAW FIM 73-21-00. NO PIMU FAULTS. ADJUSTED THROTTLE LEVERS IAW ASDR HALA2009072800335Throttle Cable · lack of lubeETOPS SIGNIFICANT SYS -THROTTLE FRICTION EXCESSIVE AND THROTTLE RANGE BINDS IN SPOTS. AUTO THROTTLES CAN NOT OVERCOME THIS AND MISS COMMANDED AIRSPEEDS BY AS MUCH AS 30 KNOTS. ACCOMPLISHED FIM 76-11-00 FIG 105A CLEANED/LUBED PEDESTAL THROTTLE HANDLE LINKAGE.SDR 2009FA0000642Throttle Cable · damagedLOSS OF ENG PWR OCCURRED DURING FLIGHT. NO ACCIDENT, NO INJURIES. IT WAS DETERMINED THE THROTTLE CABLE HAD DISCONNECTED FROM ROD END AT THE FUEL CONTROLLER. JAM NUT APPARENTLY LOOSENED AT THE ROD END. THROTTLE CABLE DOES NOT HAVE A KEYWAY TO PREVENT TURNINSDR DXTA2009072003732Bushing · wornLT ENGINE SHUTDOWN ON CONTROLS AND SPEED BRAKE TEST. FOUND BUSHING IN RT ENGINE BELLCRANK WORN. REPLACED BUSHING. C/W RIGGING CHECK OF LT FCU, FLOW DIVIDER AND AIRFRAME TO ENGINE CABLE. RE-RIGGED FCU TO FUEL FLOW DIVIDER. ADJUSTED GROUND IDLE. ENGINE RUNSDR CA090813008Switch · unserviceableAFTER SELECTING GEAR UP, LANDING GEAR INDICATOR CIRCUIT BREAKER WOULD TRIP. ACFT COMPLETED FLIGHT WITH NO INCIDENT, AS THE GEAR IS MANUALLY DRIVEN. UPON INVESTIGATING THE PROBLEM, THE THROTTLE SWITCH WAS DISCOVERED TO BE THE SOURCE OF THE PROBLEM. THE SWITCSDR HALA2009071700312Pulley · wornETOPS SIGNIFICANT SYS - NR1 ENG THRUST CONTROL CABLE TLB-1 4TH PULLEY AFT OF CLUTCH PACK QUADRANT HAS EXCESSIVE PLAY. REMOVED AND REPLACED NR 1 ENG THRUST CABLE TLB-1 4TH PULLEY AFT CLUTCH PACK. OPS CHECK SECURITY CHECK OK IAW AMM 20-10-07.SDR HALA2009071700311Pulley · wornETOPS SIGNIFICANT SYS - NR 1 ENG THRUST CONTROL CABLE TLA-1 3RD PULLEY AFT OF CLUTCH PACK QUADRANT HAS EXCESSIVE PLAY. REMOVED AND REPLACED NR 1 ENG THRUST CONTROL CABLE TLA-1 3RD PULLEY IAW AMM 20-10-07 SECURITY AND CONDITION AND OPS CHECK GOOD.SDR HALA2009071700310Pulley · wornETOPS SIGNIFICANT SYS - NR 2 ENG THRUST CONTROL CABLE TRA-1 2ND PULLEY AFT OF CLUTCH PACK QUADRANT HAS EXCESSIVE PLAY. REMOVED AND REPLACED NR 2 ENG THRUST CONTROL CABLE TRA-1, 2ND PULLEY AFT OF CLUTCH PACK IAW AMM 20-10-07. OPS CHECK AND SECURITY CHECK OK.SDR HALA2009071700304Throttle · unknownETOPS SIGNIFICANT SYSTEM - ON CLIMB, LT THROTTLE IS ADVANCED 4 INCHES FORWARD OF RT THROTTLE TO MATCH N1 AND N2 BETWEEN ENGINES. DURING CRUISE THE SEPARATION IS 1 INCH. C/W PIMU BITE PROCEDURE NR 1 & 2 ENGS. NO FAULTS NOTED C/W TLA RESOLVER ADJUSTMENT PER MSDR 2009FA0000654Throttle Cable · frozenDURING FLIGHT TRAINING, RT THROTTLE CABLE FROZE JUST BELOW MID TRAVEL. PROP WAS FEATHERED AND ENG WAS SHUTDOWN FOR UNEVENTFUL LANDING. MX FOUND CABLE BOUND ON THE ENG END IN THE RIGID SHEATH AREA. A HALF MOON SHAPED SLIVER OF METAL WAS FOUND BETWEEN THE SHESDR DXTA2009070803724Lever · frozenLT THRUST LEVER STUCK WHILE IN CRUISE. IT WAS NO LONGER STUCK ONCE WE DESENDED BELOW 2000 FT. FOUND MOISTURE IN THRUST LEVER CABLE ON LT ENGINE. REMOVED MOISTURE FROM CABLE, CLEANED AND LUBED CABLE. OPS CHECK GOOD. WORK PERFORMED IAW MM 76-10-00-201.SDR DXTA2009063003710Throttle Cable · frayedWHEN ATTEMPTING TO ADJUST POWER AFTER TURNING ANTI-ICE ON AT FL450, THE RT PWR LEVER WAS STUCK AND WOULD NOT MOVE FWD OR BACKWARD. ON DESCENT AND UPON REACHING +7 DEGREES CELSIUS THE LEVER WOULD MOVE AGAIN. REMOVED AND REPLACED STIFF LT & RT FORWARD FUSELAGE SDR CA090702008Control Cable · broken(CAN) AFTER A NORMAL ENGINE START THE CREW COMPLETED THE NECESSARY CHECKS AND STARTED TO TAXI. DURING THE TAXI IT WAS NOTICED THAT THE RT PWR LEVER FELT LOOSE. THE CREW BEGAN TO MOVE IT AND IT WAS APPARENT THE EITHER THE CABLE WAS BROKEN OR THE LINKAGE HAD CSDR A6WA200940361Throttle Cable · obstructedDURING MODIFICATION OF THE ENGINE SUPPORT BEAM REWORK ON RT AND LT UPPER AND LOWER PYLON TO FUSELAGE FITTING TO ELIMINATE HOW EDGE DISTANCE AND FOULING CONDITION WITH THE TROTTLE CABLE. REWORK ON RT LAND LT UPPER AND LOWER PYLON TO FUSELAGE FITTING C/O MODSUMSDR DXTA2009062503699Throttle Cable · out of adjustDURING SPEED BRAKE TEST, RT ENGINE SHUTDOWN. NORMAL FORCE USED DURING TEST. (REPEAT WRITE UP). REMOVED RT LWR COWLING ADJUSTED THROTTLE CABLE FRICTION BLOCKS. CHECKED FRICTION IN COCKPIT-FRICTION IS GOOD ON RT THROTTLE LEVER- RAN ACFT AND CHECKED FOR ENGINE SDR A6WA200940347Throttle Cable · fouledREWORK RT AND LT UPPER AND LOWER PYLON TO FUSELAGE FITTINGS IN ORDER TO ELIMINATE LOW EDGE DISTANCE AND FOULING CONDITION WITH THE THROTTLE CABLE. RT AND LT UPPER AND LOWER PYLON TO FUSELAGE FITTINGS TRIMMED IAW SB A601R-53-059, REV F PART C AND MODUSM TC 601SDR HALA2009061600243Throttle · malfunctionedETOPS SIGNIFICANT SYSTEM, ENG THRUST LEVER MISALIGNED 1 KNOB DURING TAKEOFF CLIMB, CRUISE WITH EEC'S OFF ALIGNMENT NOT CHECKED WITH EEC'S ON. ALL PARAMETERS NORMAL. PERFORMED FIM 76-11-00 NR 1 THROTTLE 5 LBS FWD PUSH 4 LBS PULL BACK. NR 2 THROTTLE 5.5 LBS PSDR IPXA09556199Throttle · out of adjustRIGHT ENGINE WOULD NOT GO TO REQUESTED TAKEOFF THRUST. RETURNED TO BFM. ADJUSTED NR 2 ENGINE THROTTLE IAW MM 76-11-03 AND COMPLIED WITH TAKEOFF POWER TEST 13 IAW MM 71-00-00-3. OPS CHECK GOOD, 1.73 EPR OBTAINED.SDR RAIA2009052600002Lever · out of adjustFLT 8020 - IAD - ABORTED TAKEOFF DUE TO WHEN THRUST SET, IT STARTED RANDOMLY SWITCHING BETWEEN T/O 1 AND ALT T/O 1. MAINTENANCE SWAPPED FADEC 1B AND 2B AND PERFORMED AN ADJUSTMENT AND TEST OF THE THRUST LEVER IAW AMM PROCEDURES FOLLOWED BY AN AIRCRAFT ENGINE SDR DXTA2009051403649Throttle · out of rigDURING SPEED BRAKE TEST WITH ENGINES RUNNING, RT THROTTLE WAS MOVED FWD AND THEN BACK TO IDLE. AT THE IDLE STOP, RT ENGINE SHUTDOWN. INSPECTED NR 2 ENGINE S/N PCE-JC0408 THROTTLE RIGGING. FOUND THROTTLE RIGGING TO BE OUT OF MM LIMITS. RE-RIGGED THE NR 2 ENGINSDR DXTA2009051303648Spring · brokenENGINE SHUTS OFF WHEN BROUGHT BACK TO IDLE, ON GROUND. REMOVED & REPLACED THROTTLE SPRING RAN FOR OP'S AND SLAM CHECKS. SYSTEM OP'S CHECKS SATISFACTORY AT THIS TIME. ALL WORK DONE IAW MM 76-10-00SDR 2009FA0000397Throttle Cable · frozenDURING TRAINING FLIGHT, LT THROTTLE FROZE. CREW SHUTDOWN ENGINE WITH MIXTURE AND LANDED UNEVENTFULLY. RESEARCH OF FLEET RECORDS SHOW THIS IS BECOMING COMMON ( 1 PRIOR INFLIGHT AND ONE DURING GROUND MX OPERATIONS IN THE PAST 2 MONTHS) TROUBLESHOOTING FINDS THE SDR FDEA200905061557Throttle Cable · bindingPDX - MEM ON INITIAL DESCENT CLEARANCE, THE NR 2 THROTTLE WOULD NOT RETARD, N1 WAS APPROX 80 PERCENT ON N2. THROTTLE REMAINED FROZEN DURING ARRIVAL AND ENGINE WAS SHUTDOWN PER QRH ON DOWNWIND AT 4000 FT NR 2 THROTTLE DID FREE UP ON SHORT FINAL AND NO FURTHERSDR FDEA200905051541Throttle · bindingON DESCENT NR 2 THROTTLE WAS BINDING AND WOULD NOT RETARD TO IDLE POSITION UNTIL TOUCHDOWN. REMOVED AND REPLACED NR 2 ENGINE THROTTLE PUSH PULL CABLE.SDR C2XA09RI083Relay · inoperativeFLIGHT 2236 - EWR - DURING APPROACH INTO EWR THE CREW REPORTED THAT THE "FADEC GOES INTO ETO WHEN THE LANDING GEAR IS LOWERED". THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT WHERE MAINTENANCE FOUND THE CONDITION TO BE A NORMAL OPERATION OF THE SYSTEM PER THE ROSDR FDEA200904211369Push-Pull Cable · stuckAT FL 360 IN CRUISE NR 1 AND NR 3 THROTTLES RAPIDLY CAME TO IDLE WHILE NR 2 STAYED AT ITS CRUISE SETTING (95.4). DISCONNECTED AUTO THROTTLES AND TRIED TO MARRY THROTTLES. NR 2 WAS FROZEN AND REMAINED FROZEN THROUGHOUT FLIGHT. IN DESCENT HAD TO SHUTDOWN ENGSDR HALA2009040700135Lever · out of adjustETOPS SIGNIFICANT SYSTEM, SPLIT THROTTLES, LEFT FWD BY 3/4 HANDLE. PERFORMED FIM 73-21-00 BLOCK ONE NO SIGNIFICANT FAULTS PER PROCEDURE. ACCOMPLISHED THRUST LEVER ANGLE (TLA) RESOLVERS ADJUSTMENT PER AMM 73-21-11-825-002-N00, OK FOR SERVICE.SDR DXTA2009040603578Throttle · stuckNR 1 ENGINE THROTTLE LEVER STUCK AT CRUISE POWER SETTING. ALTITUDE FL360/-49DEG C SAT. DESCENDED AND REGAINED FULL CONTROL AT FL260/ -27DEG C SAT. REMOVED LT ENG LWR COWLINGS. VERIFIED AFT CABLE ROUTING, NO DEFECTS NOTED. LUBERCIATED AFT CONTROL CABLE WITH SDR GUUA93832032909ASwitch · out of adjustLANDING GEAR WARNING HORN IS ACTIVATED AT 79.5 TO 80 PERCENT, N1 WITH LT POWER LEVER AND 75 PERCENT, N1 WITH RT PWR LEVER. ADJUSTED LANDING GEAR POWER LEVER SWITCHES. TEST FLIGHT SATISFACTORY.SDR MASA2009032600108Spring Strut · brokenASH 2907 GJT. NR 1 PROP RPM ROSE TO 1020 RPM AND ENGINE WOULD NOT SHUT DOWN. MASSIVE POWER LEVER SPLIT ON APPROACH. DURING SHUTDOWN, NR 1 PROP WOULD NOT FEATHER WHEN CONDITION LEVER MOVED TO START/FEATHER POSITION AND ENGINE WOULD NOT SHUT DOWN OR FEATHER ISDR DXTA2009032703569Throttle Cable · frozenLT THROTTLE FROZE AT FL 350. UNFROZE AT FL 240. REPLACED LT ENG AFT THROTTLE CONTROL CABLE WITH NEW. OPS CHECKED GOOD IAW MM 76-10-00 AND MM 71-20-00-201 FOR LOOSENING REAR ENG MOUNT.SDR CA090401003Throttle Cable · broken(CAN) IN FLIGHT PILOT REPORTED LOSS OF THROTTLE CONTROL. THROTTLE WENT TO FULL AS DESIGNED. ACFT FLOWN BACK AND ENGINE SHUTDOWN, LANDED SAFELY. INSP REVEALED THROTTLE INNER CABLE BROKEN WHERE CABLE GOES THRU FIREWALL. NEW CABLE INSTALLED.SDR CA090320003Control Cable · broken(CAN) PILOT LANDED AFTER DROPPING PASSENGERS ON SKI RUN. THROTTLE TWIST GRIP DID NOT RESPOND WHEN ROLLED TO IDLE SETTING PRIOR TO ENGINE SHUTDOWN. ACFT WAS FLOWN BACK TO BASE AND ENGINE SHUTDOWN AT HMU INPUT LEVER MANUALLY BY AME. THROTTLE CABLE FOUND BROKEN USDR ASOA200900295Lever · jammedLEFT THRUST LEVER JAMMED AT FULL THRUST. ADJUSTING FRICTION LOCK HAD NO EFFECT. SECURED ENGINE IN FLIGHT IAW JAMMED THRUST LEVER QRH PROCEDURE. EMERGENCY DECLARED.SDR FDEA200903140918Push-Pull Cable · frozenAT TOP OF DESCENT THE NR 2 THROTTLED JAMMED FOLLOWED THE QRH AND AT AROUND 10K' THE THROTTLE WAS RECOVERED. EXPECT FREEZING OF THE PUSH-PULL ABLE AS PER QRH. THE AIRPLANE WAS SOAKED DURING THE TURN OUT OF KSHV BEGAN REMOVING THE PUSH-PULL CABLE IN REF TO AMSDR CA090319013Cable · sheared(CAN) THE PILOT WAS CLEARED TO LAND, ATTEMPTED TO THROTTLE DOWN BUT THROTTLE WAS UNRESPONSIVE. EVASIVE ACTION WAS TAKEN, MIXTURE WAS LEANED TO DECREASE ENGINE SPEED (RPM), AND THE ACFT SAFELY LANDED UNDER THESE CONDITIONS. AN APPRENTICE ENGINEER, UNDERTOOK THSDR UALA2009031200758Actuator · faultyLT ENG THROTTLE WILL NOT ADVANCE FULLY FWD. FOUND L REV INTERLOCK ACTUATOR PREVENTING FULL TRAVEL. REPLACED L ENG REV INTERLOCK ACT, CHECKS OK.SDR CA090407004Nut · separatedKNOB JAM NUT BECAME SEPARATED FROM ACTUATING KNOB.SDR FDEA200903040835Push-Pull Cable · damagedAT TOP OF DESCENT NR 2 ENG WOULD NOT RETARD BELOW 74 PERCENT N1. NR 2 THROTTLE WAS AT LEAST TWO KNOB WIDTHS ABOVE NR 1 AND NR 3 THROTTLES. SHUTDOWN NR 2 ENG ON APPROACH. UNEVENTFUL APPROACH AND LANDING. FINISHED REMOVING OLD PUSH-PULL CABLE AND INSTALLED NESDR CA090304005Support Bracket · cracked(CAN) THE FLIGHT CREW SNAGGED THE JOURNEY LOG WITH A DEFECT OF "AUTOFEATHER U/S". MX REPLACED THE HIGH PRESSURE AUTOFEATHER SWITCH. THE FLIGHT CREW REPORTED NO FURTHER PROBLEMS. 6 DAYS LATER A DIFFERENT FLIGHT CREW COMPLAINED OF AUTOFEATHER PROBLEMS ON FINAL SDR GLBA20090228AEngine · out of rigPOWER LEVERS SEEM OUT OF ADJUSTMENT. THERE IS A LARGE SPLIT BETWEEN LEVERS IN FLIGHT, THE LANDING GEAR WARNING HORN GOES ON AT ABOUT 2100 LBS OF TORQUE, AND THE ENGINES IDLE AT ABOUT 74% N1 WITH THE POWER LEVERS AT IDLE. MAINTENENANCE RIGGED THE NR 1 & 2 ENGSDR CA090225008Throttle Cable · broken(CAN) DURING ENGINE START, THE ENGINE RPM INCREASED TO ABOVE 2000RPM AND PILOT WAS UNABLE TO DECREASE RPM. MX FOUND THE THROTTLE CABLE HAD BROKEN INTERNALLY. INVESTIGATION FOUND THE CABLE HAD BROKEN AT THE APPROXIMATE LOCATION OF WHERE THE CABLE HSG EXITS THESDR DXTA2009021703513Throttle Cable · out of adjustADJUSTED RT AFT THROTTLE CABLE IAW MM PERFORMED ENG RUN, OPS CK GOOD.SDR DXTA2009021703512Throttle Cable · out of adjustADJUSTED LT AFT THROTTLE CABLE IAW MM PERFORMED ENG RUN. OPS CK GOOD.SDR ULXR2009021080902Throttle Control · wornTHIS TUBE WAS WORN AROUND THE CIRCUMFERENCE AT THE POINT WHERE IT PASSES THROUGH THE FIREWALL BOOT. DISCOVERED DURING A 300 HOUR INSPECTION AND REPLACED.SDR CA090206004Throttle Cable · frozen(CAN) PREMIER 1A ACFT, NR 2 THROTTLE CABLE FROZEN (MOISTURE) IN FLIGHT. THROTTLE CABLES BOTH FORE AND AFT SHEATHING BLOWN THROUGH WITH PRESSURIZED DRY NITROGEN AND FOUND SIGNIFICANT MOISTURE PRESENT. ACFT CABLES TO BE REPLACED PRIOR TO NEXT FLIGHT IAW MM.SDR CA090203002Power Cable · seizedTHE POWER CABLE WAS REPLACED 200 HRS PRIOR DUE TO VERY STIFF OPERATION AND 200 HRS LATER DURING A SCHEDULED INSPECTION. THE SAME CABLE WAS FOUND VERY STIFF AND HAD EXCESSIVE END PLAY. SUSPECT SUB-QUALITY AIRCRAFT PART.SDR DL76G090002Throttle · stuckLEFT ENGINE THROTLE WILL NOT ADVANCE. REPLACED LOWER CABLE FROM PYLON TO HMU PER AMM. INSPECTED ALL OTHER AREAS. NO TROUBLE FOUND. PULL TEST NOW AT 3 POUNDS. BEFORE WAS 6 POUNDS.SDR C2XA08IA257Resolver · intermittentFLIGHT 2070 - IAH-BRO - ON APPROACH INTO BRO THE CREW REPORTED THAT THE "E2 TLA FAIL" MESSAGE ILLUMINATED AND THE NR 2 ENGINE REMAINED AT SET THROTTLE UNTIL THE FADEC CIRCUIT BREAKER WAS RESET PER THE COCKPIT QRH. THE AIRCRAFT DIVERTED TO HRL AND LANDED WITHOSDR AC2A2008120579692Throttle Cable · brokenENGINE WOULD NOT RESPOND TO THROTTLE INPUTS. SUSPECT A BROKEN THROTTLE CABLE.
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