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 COMA0210020Eec · defectiveFLIGHT 5023 DURING CLIMB OUT OF MCO THE #2 ENGINE POWER LEVER INPUT WAS IN EXCESS OF ONE INCH BEFORE IT TOOK EFFECT.REPLACED THE #2 EEC.SDR AUS20020557Cable · fouled(AUS) NR 4 ENGINE THROTTLE CABLE CAUGHT AROUND ELECTRICAL CONNECTOR LOCATED IN CABIN ROOF AREA AT SEAT ROW 2/3.SDR BSY2002F00009Throttle Cable · failedRIGHT THROTTLE CABLE BROKE ON FINAL APPROACH. SHUT ENGINE DOWN, FEATHERED PROP, LANDED. NO PROBLEM. REMOVED AND REPLACED RIGHT THROTTLE CABLE OPS. GOOD.SDR QXEA0200797Power Lever · defectiveMSO- ON TAKEOFF FLIGHT CREW REPORTED, NR 1 POWER LEVER UNABLE TO ADVANCE PAST FLIGHT IDLE. ABORTED TAKEOFF. FERRY FLIGHT TO PDX. REMOVED AND REPLACED POWER LEVER QUADRANT. OPERATIONAL CHECK GOOD, AIRCRAFT WAS RETURNED TO SERVICE.SDR CA020510023Control Cable · broken(CAN) INBOUND CREW REPORTED NR 1 ENGINE THRUST LEVER SEEMED TO HAVED SNAPPED. NO CONTROL OVER THRUST. ENGINE SHUT DOWN. MAINTENANCE FOUND NR 1 THRUST LEVER CABLE BROKEN AT PULLEY ON NR 1 ENGINE PYLON.SDR 2002FA0000641Control Cable · failedEND OF THROTTLE CABLE CAME APART A SURAGE.SDR MALA020257Controller · faultyDURING FLIGHT 2822, FLIGHT IDLE STOP OPEN LIGHT ILLUMINATED AFTER T/O. AIR RETURN TO DTW. MAINTENANCE RESET F1 STOP, OK CHECK NOT GOOD AT THIS TIME. WITH POWER LEVERS OFF, LT POWER LEVER GOES BELOW F1. MAINTENANCE REMOVED AND REPLACED CONTROL QUADRANT. ALSDR MALA020236Controller · stickingAFTER TAKEOFF ON FLIGHT 2801, F1 STOP OPEN LIGHT. QUADRANT F1 STOP MECHANISM STICKING. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED CONTROL QUADRANT.SDR CA020531003Brace · unsecure(CAN) A/C LEVELED OFF AT FL290. CREW ATTEMPTED TO THROTTLE BACK & NOTICED LT POWER LEVER JAMMED AT 95.1 PERCENT N1. QRH / INFLT SHUT-DOWN PERFORMED ON LT ENGINE & A/C DIVERTED. ALL ENGINE PARAMETERS INDICATED NORMAL AT ITS PRESENT POWER SETTING PRIOR TO SHUT-SDR CA020405028Throttle Cable · contaminated(CAN) ENGINE NR 2 THROTTLE JAMMED IN DESCENT , IN IDLE POSITION. MAINTENANCE FOUND THE THROTTLE CONTROL CABLE ASSEMBLY WATER SOAKED AND ALSO FOUND THE ELASTOMER SLEEVE RIPPED OPENED. BOTH PARTS WERE REPLACED ; THE THROTTLE CONTROL CABLE ASSY.REPLACED I.A.W. SDR AUS20020329Bracket · misinstalled(AUS) THROTTLE AND MIXTURE CABLE CLAMP BRACKET INSTALLED UPSIDE DOWN.SDR 2002FA0000749Control Cable · frayedDURING ROUTINE MAINTENANCE FOUND A FRAYED ENGINE CONTROL CABLE. THE FRAYED PORTION WAS LOCATED IN THE AFT FUSELAGE WHERE THE CABE GOES OVER A 90DEGREE TURN PULLEY. THIS IS THE FIRST OF THREE CABLE PROBLEMS THIS OPERATOR HAS FOUND IN THE LAST 90 DAYSSDR 2002F00367Throttle · inoperativeFLT 108, WHEN SETTING MAX TAKEOFF POWER LEFT THROTTLE LAGS BEHIND RIGHT THROTTLE. ABOVE 100 KTS IAS LEFT EPR DECREASED .03 WITH THROTTLE AT FORWARD STOP LIMIT. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED TSDR 2002FA0000348Throttle Cable · brokenDURING NORMAL MAINTENANCE INSPECTION THE NR 2 ENGINE THROTTLE CABLE (FS-512 R) WAS FOUND TO BE SEVERELY FRAYED WITH APPROXIMATELY 50 PER CENT OF THE STRANDS BROKEN. THE OTHER CABLES DID NOT HAVE ANY BROKEN STRANDS BUT DID HAVE SOME WIRES BROKEN.SDR AUS20020173Throttle · broken(AUS) LT ENGINE THROTTLE SLIDING END ASSEMBLY BROKEN.SDR CA020221008Bolt · worn(CAN) DURING DESCENT, THE FLIGHT CREW WERE UNABLE TO RETARD THE NR 1 THROTTLE LEVER. THE ENGINE WAS SHUTDOWN THROUGH THE GLARE SHIELD'S FIRE PUSH BUTTON. EMERGENCY LANDING WAS DECLARED. MAINTENANCE STAFF VERIFIED THE BOLT SECURING THE "THROTTLE CONTROL LEVER SDR CA020221007Gearbox · failed(CAN) RT REV ICON ON N1 GUAGE AND REV UNSAFE CAUTION MESSAGE APPEARED AFTER TAKEOFF. RT ENGINE THROTTLE GEARBOX ASSEMBLY REMOVED AND REPLACED. AIRCRAFT BACK IN SERVICE.SDR SWAA020321Throttle · obstructedAIR TURNBACK, IN FLT ENGINE SHUTDOWN, DURING CLIMBOUT DISCOVERED THE NR 2 ENGINE THROTTLE WOULD NOT RETARD BELOW 88 PERCENT N1, HAD TO SHUT ENGINE DOWN AND LAND SINGLE ENGINE. FOUND DEBRIS IN THE THROTTLE QUADRANT AT 6 O'CLOCK ENGINE POSITION. REMOVED DEBRISSDR AUS20020068Control Cable · broken(AUS) LT ENGINE POWER CONTROL CABLE BROKEN.SDR SWIA200210628Gearbox · faultyRT REV CAUTION ICON ON N1 GAUGE IN FLIGHT WITH REV UNSAFE CAUTION MESSAGE AFTER LIFTOFF. REMOVED AND REPLACED RT ENGINES THROTTLE GEAR BOX ASSEMBLY.SDR 2002F00212Control Cable · defectiveFLT 205, DURING TAKEOFF, DEPARTING SFO REJECTED THE TAKEOFF BECAUSE THE LEFT ENGINE WOULD NOT REACH TAKEOFF EPR WITH EEC AND ENGINE LIMITER ON. EEC LIMITER OFF NOT CHECKED. 1.72 EPR COMMANDED, 1.67 ACTUAL. AIRCRAFT RETURNED TO THE GATE AND MAINTENANCE REMOVSDR 2002F00985Control Cable · contaminatedPRECAUTIONARY SHUTDOWN OF LEFT ENGINE BECAUSE OF INABILITY TO REDUCE POWER FROM CRUISE. SUSPECT MOISTURE IN POWER CONTROL TELEFLEX CABLE ASSEMBLY FREEZING AT HIGH ALTITUDE. (M)SDR 0127Nut · looseAIRCRAFT WAS ON DESCENT INTO MSP, AFTER REDUCING POWER THE ENGINE KEPT SPOOLING DOWN AT THAT POINT THE PILOTS SHUT THE ENGINE DOWN. ACFT LANDED WITH NO FURTHER PROBLEMS. INVESTIGATION REVEALED THE HMU LEVER NUT HAD LOOSENED UP ENOUGH TO ALLOW THE LEVER TO SLSDR P5CA0200627Control Unit · out of rigNR 3 ENG WOULD NOT ACHIEVE T/O THRUST. 1.58 MAX PWR WAS APPLIED, THRUST LEVER WAS MOVED TO FIREWALL THRUST W/ MAX EPR OF 1.38. OTHER PARAMETERS NORMAL WHEN ASSOCIATED W/ & EPR SETTING OF 1.38 ENG RUN TO MAX POWER FOR OPS CK INTO WIND (250/11). ENG SLOW TO RSDR SWAA013428Throttle · malfunctionedIN FLIGHT ENGINE SHUT DOWN, DECLARED EMERGENCY. AT FL 390, NR 1 ENG THROTTLE WOULD NOT RESPOND. CAME BACK TO 85.1 PERCENT N1, AFTER 30 MINUTES WENT TO 79 PERCENT N1. NO OTHER ABNORMAL INDICATION FOUND BEFORE SHUT DOWN. C/W NR 1 ENG INSP, C/W NR 1 EEC BITE SDR O3X2001F00000Control Cable · brokenAIRCRAFT PREPARED TO DEPART GATE, AS THE POWER LEVERS WERE PUSHED FORWARD. THE CREW NOTICED THAT THE LT ENGINE WAS NOT RESPONDING TO THE INPUT. DURING INSPECTION BY MAINTENANCE PERSONNEL. THE LT POWER LEVER CABLE WAS FOUND SHEARED. THE CABLE HAD SHEARED APSDR C8GA20010019Bolt · missingFLT 201 FROM MIA TO CCS. AFTER TAKEOFF NR 1 ENGINE STAYED AT FULL POWER AND WOULD NOT RESPOND TO THROTTLE MOVEMENT. ACCOMPLISHED NR 1 ENGINE SHUTDOWN AND AIR TURNBACK TO MIA AND LANDED WITHOUT ANY INCIDENT. INVESTIGATION FOUND THE LOWER THRUST CRANK BOLT WASDR COMA0110160Power LeverFLIGHT #5056. POWER LEVER SPLIT DURING T/O.POWER LEVER SPLIT WITHIN LIMITS. AIRCRAFT RETURNED TO SERVICE.SDR CA011219003Throttle Cable · failed(CAN) UPON REACHING CRUISE ALTITUDE, WHILE ATTEMPTING TO SET CRUISE POWER LEFT THROTTLE CABLE JAMMED AT 38 INCHES MANIFOLD PRESSURE. MTCE INSP REVEALED. LE THROTTLE CABLE SEIZED UPON ATTEMPTS TO FREE CABLE, CABLE BROKE APPROX. 1 INCH INSIDE CABLE FROM QUADRASDR ABXA010615Switch · wornDURING TAXI INTO GATE, THE NR 2 THRUST REVERSER DEPLOYED UNCOMMANDED, WOULD NOT STOW. DFDR DATA WAS REVIEWED AND THE DATA SHOWED THAT THE REVERSER DID NOT STOW AFTER LANDING. THE THROTTLE MICROSWITCH PACK WAS FOUND WORN WHICH PREVENTED THE THRUST REVERSER FRSDR CA011218002Throttle Cable · failed(CAN) DURIING A ROUTINE EMMA CHECK 46, THE LT ENGINE THROTTLE CABLE TURNBUCKLE END WAS FOUND FRACTURED AND WAS ONLY HELD TOGETHER BY LOCKWIRING. CABLE REPLACED.SDR SWIA200110377Control Cable · faultyRIGHT POWER LEVER WOULD NOT RETARD TO FLIGHT IDLE IN CRUISE FL22.0 OAT-15. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN CHECK. INSPECTED CABLE FROM POWER LEVER AND ENGINE QUADRANT. CYCLED POWER LEVER SEVERAL TIMES. INSPECTED CABLE FROM ENGINE QUADRANT TO HMU. CSDR PNSA011105Cable · frozenCOULD NOT SET TAKEOFF POWER FOR RT ENGINE. THAWED AIRFRAME POWER LEVER CABLE AND OP CHECK OK.SDR AUS20011284Pulley · worn(AUS) RT ENGINE THRUST CONTROL CABLE PULLEYS (2OFF) LOCATED AT STA 240.0 WERE FOUND TO BE WORN. FOUND DURING INSPECTION IAW AD/B767/118(EI 762-76-003).SDR BSY2001F00016Throttle Arm · failedRT ENGINE STAYED AT 2100 RPM ON APPROACH, SHUT ENGINE DOWN. INSTALLED NEW CONTROL LEVER ARM TO SHAFT THROTTLE ASSEMBLY OPS CHECKS GOOD.SDR CA011120007Cable · broken(CAN) THE CENTRE CABLE OF THE POWER LEVER CABLE BROKE APPROXIMATELY 4 INCHES FROM THE POWER LEVER. CONTROL CONNECTION THE A/C WAS ON CLIMB OUT AT 16,000 FT. A/C WAS LEVELED FOR CRUISE WHEN POWER WAS SET THERE WAS NO RESPONSE TO RIGHT ENGINE WHEN POWER LEVER MOSDR PNSA011103Cable · frozenAT LEVEL OFF FROM CLIMB UNABLE TO REDUCE RT ENGINE SPEED. MAINTENANCE FOUND SPEED LEVER CABLE FROZEN. PURGED AND LUBRICATED AIRFRAME SIDE OF CABLE.SDR GTIA011090Throttle · lack of lubeLAX - DURING APPROACH AND DESCENT, THE RIGHT THROTTLE WOULD NOT ADVANCE FROM ITS IDLE STOP, ONCE THE RIGHT THROTTLE WAS MOVED FORWARD OFF TAIL STOP IT WOULD ADVANCE AND MATCH THE LEFT. CLEANED AND LUBED THROTTLES. PLACARD REMOVED. (M)SDR SABA011057Relay · failedFLIGHT 5212 GREENVILLE, NC TO CHARLOTTE; AIRCRAFT ABORTED TAKEOFF DUE TO NUMBER TWO ENGINE WAS SLOW TO ACCELERATE. ENGINE CONTROL UNIT SEEMED TO BE WORKING AS IT SHOULD. PILOT ALSO REPORTED A TWO KNOB SPLIT ON THE POWER LEVERS WITH NUMBER TWO LAGGING BEHIND.SDR AUS20011132Control Cable · seized(AUS) NR 1 ENGINE THRUST LEVER PUSH/PULL CABLE SEIZED.SDR LS1R076730Throttle Cable · brokenTHROTTLE CABLE IS BROKEN.SDR CA011101013Connector · failed(CAN) FOUND CONNECTOR P28EZ AT THROTTLE GEAR BOX SHORTED TO GROUND. REPLACED CONNECTOR AND OPS CHECKED SERVICEABLE. AIRCRAFT RETURNED TO SERVICE.SDR EISA20010127Throttle Cable · disconnectedEN ROUTE NR 3 ENGINE WENT TO MAX POWER. RETARDING THROTTLE HAD NO EFFECT. SHUT DOWN ENGINE. AFTER 20 MINUTES, MOVED START LEVER TO IDLE FOR 3 MINUTES TO PURGE FUEL CONTROL. FOUND NR 3 THROTTLE LINKAGE DISCONNECTED. INSTALLED BOLT AND COTTER KEY, INSPECTEDSDR AUS20011085Shaft · broken(AUS) THROTTLE LAYSHAFT CABLE CONNECTION FITTING BROKEN.SDR HEEA076462Throttle · stiffTHROTTLE STIFF. REPLACED WITH SERVICEABLE FUEL CONTROL.SDR HEEA076461Throttle · stiffTHROTTLE STIFF. REPLACED WITH SERVICEABLE FUEL CONTROL.SDR 2001FA0000398Throttle Cable · chafedPILOT COMPLAINED, RIGHT THROTTLE VERY STIFF, THROTTLE HAD BEEN REPLACED FOUR MONTHS EARLIER FOR SAME REASON. UPON REMOVAL IT WAS DISCOVERED THAT THE CABLE, WHICH WAS COVERED WITH FIRE SLEEVE, HAD BEEN CHAFFING ON THE LOWER PART OF THE TURBOCHARGER COMPRESSOR SDR AUS20011016Cable · distorted(AUS) NR 3 ENGINE THRUST CABLE KINKED IN THE AREA OF THE STRUT TO WING INTERFACE.SDR CA011011006Throttle Cable · frayed(CAN) DURING A DAILY INSPECTION, MAINTENANCE NOTED SCRATCHES ON THE SUPERCHARGER DUCT IN THE RT WHEEL WELL. DETAILED INSPECTION REVEALED WHEN THROTTLE WAS PLACED IN CRUISE POSITION, THE RT THROTTLE CABLE P/N 8302989 WAS SEVERELY FRAYED. THE FRAY WAS ONLY VISIBSDR BSY2001F00011Throttle Cable · broken(TFB) M.I.R. RIGHT ENGINE THROTTLE STUCK AT FULL THROTTLE. REMOVED AND REPLACED BROKEN THROTTLE CABLE.
Back to JASC 7603