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 aircraft_model_key = '750' 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 aircraft_model_key = '750' 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 DXTA200601342Bleed Valve · sticksR HP DUCT O'PRESS CAS MESSAGE APPEARED DURING T/O ROLL. REPLACED RT ENGINE HIGH PRESSURE BLEED AIR VALVE WITH OVERHAULED IAW MM CH-36-11-00, PERFORMED ENGINE POWER RUN, OPS CHECKED GOOD.SDR DXTA200601339Seal · leakingLANDING GEAR WOULD NOT RETRACT. HEARD LOUD THUMP FROM NOSE AREA CLIMBING THRU 19000'. TROUBLESHOT, REPACKED NOSE GEAR STRUT ASSY IAW CE750 MM CHAP 32-20-02 AND C/W FUNCTION CK OF GEAR SYSTEM IAW CHAP 32-42-00 OF CE 750 MM. ALL OPS CHECKS GOOD, NOSE GEAR WASDR DXTA200601337Display · inoperativeON TAKEOFF ROLL , THE NR 1 DU BECAME DISTORTED AND THEN BLANKED OUT AND THEN CAME ON. TAKEOFF DISCONTINUED < 80 KTS. DEFERRED IAW NJA CE-750 MEL , C/W APPENDIX A 34-12 CAT C DUE 04-18-06. REMOVED NR 1 PFD DISPLAY UNIT DUE TO INTERNAL FAILURE INSTALLED SERVISDR DXTA200601328Acm · failedSTRONG ENVIRONMENTAL SMELL IN COCKPIT LEAVING FL380 TO FL360, DIVERTED TO LAS. REMOVED AND REPLACED THE FORWARD ENVIRONMENTAL CONTROL UNIT'S ACM C/W OPERATIONAL AND LEAK CHECK WITH NO DEFECTS NOTED AT THIS TIME. ALL MAINTENANCE PERFORMED IAW CESSNA CITATION SDR DXTA200601324Acm · failedAFTER PULLING THE POWER BACK FOR DESCENT, GOT A STRONG SMELL. COCKPIT ACM BECAME HARD TO CONTROL. FOUND COCKPIT ACM TO HAVE FAILED. REMOVED ACM AND INSTALLED OVERHAULED UNIT. OPERATIONAL AND LEAK CHECKS GOOD. WORK DONE IAW CHAPTER 21-51-00 OF THE CITATION SDR DXTA200601323Strut · malfunctionedAFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. LANDING GEAR HANDLE WOULD NOT MOVE FROM A/C DOWN POSITION. CHECKED AIRCRAFT, FOUND NOSE STRUT NOT FULLY EXTENDED, DISASSEMBLED NOSE STRUT. REMOVED AND REPLACED STRUT ORIFICE WITH NEW. RE-SEALED AND SERVICED STSDR DXTA200601320Electrical Sys · unknownUNABLE TO EXTEND GEAR NORMALLY DUE TO PREVIOUS ELECTRICAL PROBLEM (ABNORMAL CONDITION WITH THE CROSS TIE CLOSED RIGHT GEN ON APU OFF BATTERY NR 2 OFF EMERGENCY BUS WAS NOT POWERED NR 2 DC BUS SWITCH DID NOT INDICATE NORMAL OR EMERGENCY), EXTENDED GEAR MANUALLYSDR DXTA200601318Pcu · malfunctionedAIRCRAFT/AUTOPILOT STARTED OSCILLATING IN FLIGHT (FL430). THE TRIM CLACKER WOULD ACTIVATE REPEATEDLY TO COMPENSATE. TRIED TAKING A/P OFF AND FLYING MANUALLY AND TRIMMING, THEN REACTIVATED A/P. AFTER A MINUTE THE SAME AS ABOVE OCCURRED. PULLED C/B AND THEN SDR DXTA200601316Pump · inoperativeAT FL 400 THE HYDRAULIC VOLUME LOW -A- CAME ON. THE HYDRAULIC -A- QUANTITY GAUGE WAS SHOWING 12 PERCENT AND NORMAL PRESSURE. UPON LANDING THE QUANTITY WAS DOWN TO 10 PERCENT. REMOVED AND REPLACED LEFT ENGINE DRIVEN HYDRAULIC PUMP, LEAK AND OPERATIONALLY CHESDR DXTA200601315Connector · malfunctionedCONSTANT CHIME AND BRIEF MASTER WARNING RECEIVED DURING TAKEOFF ROLL. FOUND LT FLAP RESOLVER CONNECTOR JL041 WITH MOISTURE. CLEANED AND DRIED PLUG JL041 PERFORMED NO TAKEOFF WARNINGS, OPS CHECK WITH NO DEFECTS NOTED. WORK DONE IAW 750 M/M CH27-50-01 REV 12.SDR DJFA2006222Acm · malfunctionedTHE CREW REPORTED THAT WHILE TAXIING THE AIRCRAFT IN KFLL NOTICED SMOKE IN THE FLIGHT DECK AND CABIN. THE AIRCRAFT WAS SHUT DOWN AND AN EMERGENCY EVACUATION PROCEDURE WAS PERFORMED. MAINTENANCE ISSUED MEL 21-01-01 FOR THE ENVIRONMENTAL CONTROL UNIT AND THE ASDR DXTA200601310Seal · failedDURING GEAR RETRACTION UNLOCK LIGHT FLICKERED AS NOSE GEAR THUMPED IN WHEEL WELL 4 TIMES. PERFORMED FUNCTIONAL CHECK ON SYSTEM AND COULD NOT REPRODUCE GEAR THUMP. RE-PACKED UPPER AND LOWER NOSE STRUT. REF O/A 1.9 REPLACED NOSE LEFT AND RIGHT GEAR UPLOCK SWISDR DXTA200601329Uplock Switch · out of adjustDURING CLIMB OUT PHASE OF FLIGHT, NOSE GEAR APPEARS TO BE MAKING "BUMPING NOISE". ADJUSTED RT MLG UPLOCK SWITCH, WAS .05 OUT OF SPEC. WORK DONE REF CE 750 MM CH 32-30-00. ALSO, FOUND UPLOCK AREA DIRTY AND GUMMED UP. CLEANED AND LUBED UPLOCK COMPONENTS. SESDR DXTA200601309Uplock Hook · stickingSEVERAL NOSE GEAR BUMPS FELT IN FLIGHT. FOUND MLG UPLOCK HOOKS STICKING. CLEANED AND LUBED UPLOCK HOOKS IAW CE750 MM CHAPTER 32-30-05. OPS CHECK GOOD. ACCOMPLISHED CITATION X GEAR BUMP TROUBLESHOOTING CHECK LIST. ALL WORK ACCOMPLISHED IAW CESSNA MM CHPT 3SDR DXTA200601305Acm · odorFL 410 IN CRUISE, EXPERIENCED A BURNING SMELL IN THE COCKPIT. PASSENGERS ALSO CONFIRMED THE SMELL IN CABIN. LANDED ASAP AND DID NOT HAVE TIME TO TROUBLESHOOT ENVIRONMENT CHECKLIST. SMELL WENT AWAY AFTER ENGINE SHUT DOWN. REMOVED AND REPLACED COCKPIT ACM. SDR DXTA200601301Strut · out of rigONCE LANDING GEAR WAS RETRACTED, RED UNLOCK LIGHT REMAINED ILLUMINATED. FOUND NOSE EXTENSION OUT OF LIMITS AND NOSE UPLOCK CABLE RIGGING TOO TIGHT. ADJUSTED NOSE GEAR RELEASE CABLE IAW 750 M/M 32-30-00. REPLACED NOSE STRUT IAW 750 COMPONENT M/M 32-20-02. OSDR DXTA200601299Position Switch · looseAFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. LANDING GEAR HANDLE WAS STUCK IN THE DOWN POSITION. FOUND NOSE GEAR TORQUE LINK SQUAT CAM LOOSE. SECURED AND ADJUSTED CAM. CHECKED NOSE GEAR SQUAT SWITCH ADJUSTMENT, FOUND NORMAL. LANDING GEAR EXTENSION AND RSDR DXTA200601290Warning Light · illuminatedIN CRUISE, LEFT ENGINE ITT QUICKLY ROSE TO 860 AND SHARPLY DROPPED TO APPROX 820-830 SEVERAL TIMES. APPROX 10-15 BOUNCES IN A 10-15 SEC TIME. FL410, RAT -18, .90M. INSPECTED ALL THERMOCOUPLE CONNECTORS PER A23007C MM 77-21-10. APPLIED STABILANT 22 CONTACT ESDR DXTA200601283Controller · failedFLAPS FAIL CAS WHEN FLAPS SELECTED TO 5 DEGREES. TRIED TO RESET, MESSAGE RE-APPEARED. SLATS ARE EXTENDED AND FLAPS STOPPED AT 2-3 DEGREES, ABOUT 1 INCH DOWN. FOUND FAULTS NR 1-FEEDBACK & 7-CONTROLLER FAULTS. REPLACED FLAP CONTROLLER, LT POSITION SENSOR & LSDR DXTA200601282Windshield · brokenWINDSHIELD IN FRONT OF CO-PILOT SHATTERED IN FLIGHT AT FLIGHT LEVEL 350 SPEED .90 MACH. REMOVED CO-PILOTS SHATTER WINDSHIELD. PREPARED AIRCRAFT FOR NEW WINDSHIELD. INSTALLED NEW SEAL R881500, & INSTALLED NEW WINDSHIELD. PERFORMED AN ELECTRIC HEATED WINDSHISDR DXTA200601281Float Valve · unknownRT WING OVERFILL EICAS MESSAGE ILLUMINATED, FOLLOEWED BY A VENTING OF ALMOST 200 LBS OF FUEL FROM THE RIGHT WING. FUEL LOSS AMOUNT CONFIRMED BY FMS. - GAINED ACCESS TO THE RT OTBD WING VENT FLOOD VALVE ASSY FOUND VALVE TO OPERATE FREELY WITH NO BINDING. FOUNSDR DXTA200601280Seal · leakingLANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION AFTER TAKEOFF. INSPECTED NOSE LANDING GEAR AND FOUND GEAR EXTENSION BEYOND ALLOWABLE LIMITS. REMOVED LOWER PISTON ASSY AND REPACKED IAW 750 CMM CHP 32-20-02. REINSTALLED LOWER PISTON. C/W GEAR SYSTEM OSDR DXTA200601279Handle · inoperativeLANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION AFTER TAKEOFF.SDR DXTA200601277Flap System · warning lightFLAP FAIL LITE GOING FROM 5 TO 15. RESET ONCE AND TRIED AGAIN. FLAP FAIL LITE AGAIN. LANDED WITH FLAPS 5. - PLACED FLAP BREAKOUT BOX ON AIRCRAFT AND RAN FLAPS AND MONITERED VOLTAGES FROM FLAP RESOLVERS VERIFIED PROPER OUTPUT AND ASSEMETRY VOLTAGES WERE CORRSDR CWQR2006002Oxygen Bottle · unserviceableRECEIVED OXYGEN CYLINDER AND REGULATOR FROM CESSNA WITH A CYLINDER BEYOND ITS SERVICE LIFE. BOTTLE HAS 15 YEAR SERVICE LIFE PER CE750 M/M CHAP 5. BOTTLE MFD DATE 9/87. RED TAGGED BOTTLE AND RETURNED TO CESSNA PARTS.SDR DXTA200601274Pcu · failedWHILE AT FL 400 IN CRUISE " FLT CONTROL FAULT " CAS MSG ILLUMINATED WITH VIOLENT RT ROLL/YAW OF A/C. DISENGAGED A/P, CHG,D FC COMPUTER AND NOTED LIGHT ON RIGHT REAR FLT CONTROL SHUT OFF SWITCH, RT ELEV SHUT OFF. LIGHTED SWITCH WITH NON-COMMANDED ROLLS OCCURED SDR DXTA200601275Tube · out of adjustIN CRUISE FLIGHT, LEFT WING FUEL 3100 LBS., CENTER O LBS., RIGHT WING FUEL 3100 LBS., RECEIVED LEFT WING TANK O'FILL CAS MESSAGE. VISUAL CHECK SHOWED FUEL VENTING FROM LEFT WING. TURNED OFF LEFT CENTER WING TRANSFER AND YAWED AIRCRAFT. FUEL VENTING DID NOT SDR DXTA200601263Strut · malfunctionedAFTER TAKEOFF DURING GEAR RETRACTION, THE GEAR HANDLE WAS DIFFICULT TO MOVE OUT OF THE DOWN DETENT BUT EVENTUALLY DID MOVE TO THE UP POSTION. MAINS RETRACTED NOSE DID NOT. STILL HAD GREEN NOSE LIGHT AND RED UNSAFE LIGHT. HANDLE WAS MOVED TO GEAR DOWN AND 3 SDR DXTA200601264Valve · dirtyAFTER INITIAL CLIMB, LEVELING OFF AT FL130 (11800 LBS FUEL REMAINING), "WINGTANK O 'FULL R" AMBER CAS MESSAGE CAME ON AND FUEL STARTING POURING OUT OF RIGHT WING. IT EVENTUALLY STOPPED AFTER 8 MIN. LOST 400 LBS OF FUEL. FOUND RIVET AND DEBRIS LODGED IN RT FSDR DXTA200601260Landing Gear · malfunctionedGEAR WILL NOT RETRACT, HANDLE WOULD NOT MOVE. COMPLETED GEAR SWING, NO DEFECTS NOTED, CHECKED NOSE WHEEL CENTERING CHECK GOOD. COMPLETED LANDING GEAR TROUBLESHOOTING TREE FOR GEAR HANDLE FAULT, NO FAULTS FOUND IAW CE-750 M/M CHPT 32-30-00. CONNECTED DMC MONSDR DXTA200601259Odor · detectedA STRONG "SULPHUR" BURN SMELL WAS NOTED AT ALTITUDE 410 FL.. NO SMOKE NOTED BUT SMELL WAS PRESENT UNTIL AFTER LANDING. DURING THIS TIME, NOTICED THAT CABIN PACK TEMPERATURE COULD NOT BE CONTROLLED IN AUTO OR MANUAL. TEMPERATURE STAYED AT MAX HEAT. CABIN PASDR DXTA200601255Acm · odorAFTER INITIATING DESCENT HEARD A LOUD POP AROUND THE GALLEY AND BRIEFLY SMELLED AN ACRID SMELL. PAX SAW A BRIEF PUFF OF WHITE SMOKE AROUND THE GALLEY FLOOR. NO OTHER ABNORMALTIES IN FLIGHT. AFTER LANDING THERE WAS A SMELL OF BURNING RUBBER IN THE CABIN. RESDR DXTA200601254Controller · malfunctionedAFTER TAKEOFF, ONCE THE FLAP RETRACTION SEQUENCE HAD COMPLETED, THE AMBER MESSAGE "FLAPS FAIL" ILLUMINATED. ABNORMAL CHECKLIST PROCEDURES WERE COMPLIED WITH (FLAP RESET BUTTON), MESSAGE DID NOT CLEAR. FOUND FLAP CONTROLLER HAVE FAULTS. RESET FLAP CONTROLLERSDR DXTA200601251Squat Switch · failedAFTER TAKEOFF, THE LANDING GEAR HANDLE WAS STUCK IN THE DOWN POSITION AFTER CYCLING IT, IT WAS RETRACTED, BUT THE RED GEAR UNSAFE LIGHT WAS ON. AFTER FURTHER CYCLING, THE GEAR WAS FINALLY DEPLOYED WITH NORMAL INDICATIONS (3 GREEN NO RED). REMOVED AND REPLACESDR DXTA200601250Switch · failedRIGHT WING OVER FILL EICAS MESSAGE FOLLOWED BY FUEL VENTING OUT RIGHT WING. REMOVED AND REPLACED RIGHT WING OVER FULL SWITCH, OPS CHECK GOOD. NO LEAKS NOTED IAW 750 MM 28-20-07.SDR DXTA200601248Windshield · crackedTHE EXTERIOR LAYER OF RT FORWARD WINDSHIELD SCATTERED AT 41,000 FT. THIS EVENT WAS PRECEDED BY APPROXIMATELY ONE MINUTE OF A WSHLD HEAT INOP. REMOVED AND INSTALLED COPILOT WINDSHIELD IRT CE 750 MM 56-11-00. INSTALLED COPILOT'S SEAL AND SAFETIED. PERFORMED SDR DXTA200601268Flap System · failedWHEN THE FLAPS WERE SELECTED TO 5 DEG AT THE START OF THE APPROACH, FAILED (NEITHER FLAPS OR SLATS WOULD EXTEND). CHECKLIST PROCEDUES WERE FOLLOWED BUT THEY WOULD NOT RESET. INSPECTED WIRING TO FLAP J-BOX AND FLAP CONTROL BOX. NO DEFECTS FOUND. PERFORMED SDR DXTA200601267Flap System · failedAT 19,000 MSL AND 220 IAS SELECTED FLAPS TO 5 DEG. FLAPS FAIL CAS MESSAGE APPEARED WITH AMBER FLAP POSTION INDICATOR UNABLE TO RESET FLAPS AND LANDED WITH SLATS EXTENDED FLAPS 0 DEG. TROUBLESHOT FLAPS, FOUND NO FAULT CODES ON CONTROLLER. FLAPS ELECTRICLAL RSDR DXTA200601244Windshield · crackedDURING CLIMB THRU FL200, ARCING & SPARKING IN CAPT'S FWD WSHIELD, LWR LT CORNER. TURNING OFF LT WSHIELD HEAT SWITCH STOPPED ARCING BUT OUTER WINDSHIELD CRACKED ABOUT 10 SECONDS LATER. REMOVED SUNVISOR. REMOVED LT SIDE WINDOW TRIM PNL. REMOVE CTR POST TRIM SDR DXTA200601246Yoke · bindingCONTROL YOKE BINDS WITH A RACHET FEEL IN FLIGHT, IT IS MORE NOTICABLE ON LEFT YOKE. WITH AUTO PILOT ENGAGED A BUMPING CAN BE FELT ON LEFT CONTROL YOKE, NOT ON RIGHT. REMOVED COCKPIT FLOORBOARDS, DETERMINED THERE WAS A SPACER BINDING ON THE LEFT AILERON SECTOSDR DXTA200601253Metering Valve · failedDURING STATIC TAKEOFF, A/C MOVED FORWARD ON RUNWAY AND IT FELT LIKE ANTI-SKID WAS CYCLING FROM A DEAD STOP. ABORTED THE T/O LESS THAN 5 KTS. INSPECTED AIRCRAFT AND FOUND THE LT GEAR I/B AND O/B TIRES FLAT SPOTTED, REPLACED BOTH MAIN WHEELS, ALSO REMOVED AND SDR DXTA200601241Flap System · malfunctionedFLAPS FAILED IN UP POSITION DEPARTING KBUF, WOULD NOT RESET, DIVERTED TO CMH. VISUALLY INSPECTED FLAPS AND FLAPWELL COMPONENTS. LUBRICATED ACTUATOR BALLSCREWS PER CE-750 M/M 12-20-05. RESET BITE CODES ON FLAP CONTROLLER. CHECKED RESOLVER CONVERTER VOLTAGE SDR DXTA200601238Apu · malfunctionedUPON DESCENT INTO BCT, ATTEMPTED TO START THE APU TWICE. WHILE ATTEMPTING A SECOND START, SMELLED AN ELECTRICAL ODOR COMING FROM THE OVERHEAD GASPER. ABANDONED ALL FURTHER ATTEMPTS TO START APU. PERFORMED OPERATIONAL CHECKS OF THE APU AND INSPECTED APU, NO SDR DXTA200601239Acm · making metalIN CRUISE GOT STRONG BURNING SMELL FOR 2 TO 3 MIN FOLLOWED BY A LOSS OF CONTROL OF THE COCKPIT PAC TEMP. TEMP WENT HOT AND COULD NOT BE REDUCED IN MANUAL MODE OR AUTO, 35 DEGREES CHECK GOOD 43.5K OHMS. CLEANED RT COALESCER IAW CE750 MM CHAPTER 12-10-01-160. SDR DXTA200601273Float Valve · stuckDURING FLIGHT "WING O-FULL L" CAS MESSAGE ILLUMINATED, LOST 300 LBS IN 5 MINUTES. DURING POST FLIGHT INSPECTION, THE FUEL WAS STILL LEAKING OUT ON THE GROUND. INVESTIGATED AND FOUND LT FUEL VENT SYSTEM FLOAT TO BE STUCK IN VENT POSITION FREED FLOAT TO ALLOW SDR DXTA200601266Acm · seizedGOT PACK OIL SMELL IN COCKPIT AND CABIN AT FL 410. TROUBLESHOT AND FOUND AFT PACK TURBINE SEIZED. REMOVED AND REPLACED TURBINE IAW HAMILTON SUNDSTRAND CMM 21-51-16.SDR DXTA200601243Servo · failedDURING CLIMB AT LOW ALT A/C SEAMED TO SLOWLY FISHTAIL. RUDDER TRIM INPUTS CAUSED LARGE CHANGES TO OCCUR. AT HIGH ALTITUDES, MACH .87 OR GREATER THE INCLINATOR WOULD SWING WAY OUT TO ONE SIDE AND THEN BACK TO THE OTHER LIKE A DUTCH ROLL. THE CONTROL PAGE SHOWSDR DXTA200601233Strut · underservicedUNABLE TO MOVE GEAR HANDLE TO RETRACT (UP) POSITION AFTER TAKEOFF. TROUBLESHOT FOUND NOSE GEAR STRUT WAS NOT FULLY EXTENDING AND NOT MAKING NOSE GEAR SQUAT SWITCH. SERVICED NOSE STRUT WITH NITROGEN AND EXTENSION AND RETRACTION, OPS CHECKS GOOD.SDR DXTA200601227Electrical Sys · unknownALL INTERIOR ELECTRICS INOPERATIVE. STRONG ELECTRIC SMELL IN AFT CLOSET.SDR DXTA200601226Actuator · inoperativeRUDDER LIMIT FAIL -A-, 15 PERCENT OF RUDDER AVAILABLE AT LANDING. REMOVED AND REPLACED UPPER RUDDER LIMITER IAW CE750 M/M CHAPTER 27-23-00. OPERATIONAL CHECK GOOD.
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