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 DXTA200601194Unknown · unknownTEN MILES FROM DESTINATION AIRPORT, BUSS NR 1 WENT TO EMERGENCY POWER. DECLARED EMERGENGY AND LANDED SAFELY. ITEM IS UNDER INVESTIGATION.SDR 2005FA0000273Filter · leakingHYDRAULIC LEAK FROM RT PYLON NOTED DURING POST FLIGHT, CAUSE: RUDDER STANDBY FILTER ASSEMBLY DIFFERENTIAL PRESSURE INDICATOR HAD 1 RETAINING SCREW SHEARED AT THE HEAD P/N AA-2100-11D99. 3000 PSI OF SYSTEM PRESSURE CAUSED O-RING DAMAGE AND THE SUBSEQUENT LEAK.SDR DXTA200500527Downlock Switch · failedON TAKEOFF NOSE GEAR CAME UP NORMAL, THROUGHT 10,000 FT NOTICED NOSE GEAR INDICATED DOWN. LIGHT WAS INTERMITTANT DURING FLIGHT. BLEW GEAR DOWN. UNSAFE LIGHT CAME ON FOR ABOUT 10 SECONDS, THEN WENT OUT. INSPECTED NLG DOWNLOCK SWITCH SG006 AND CONNECTOR PG00SDR DXTA200500524Strut · dischargedAFTER TAKEOFF GEAR HANDLE WOULD NOT COME UP. FOUND NOSE STRUT NOT PROPERLY SERVICED. SERVICED NOSE STRUT IAW CESSNA 750 MM 12-10-38. CYCLED GEAR MULTIPLE TIMES, OPS CHECKS GOOD.SDR DXTA200500521Wheel · vibrationEXPERIENCED EXTREME VIBRATION APPROX 60-80 KTS ON TAKEOFF ROLL. ABORTED TAKEOFF. VIBRATION WAS EXTREME ENOUGH TO DISENGAGE YAW DAMPER AND KNOCK PFD'S OFF LINE. TAKEOFF WAS IN ASPEN, NO SNOW, BUT EXTREME COLD. REMOVED AND REPLACED BOTH LEFT AND RIGHT NOSE WSDR DXTA200500518Water Separator · odorTHERE IS A STRONG OILY SMELL IN THE COCKPIT ONCE THE APU IS RUNNING AND THE BLEED AIR IS SELECTED ON. FOUND BOTH WATER SEPARATOR FILTER SOCKS DIRTY. CLEANED FILTER AND FOUND COCKPIT WATER SEPARATOR VALVE STUCK OPEN. CLEANED AND LUBED VALVE. RE-INSTALLED WASDR DXTA200500513Limit Switch · out of rigGEAR HANDLE WOULD NOT COME UP ON DEPARTURE. GEAR SIGNED DOWN AND LOCKED (THREE GREEN). PERFORMED RIG PROCEDURE ON ALL 3 SQUAT SWITCHES. PERFORMED FUNCTIONAL CHECK ALL OK. OPS CHECKED GOOD IAW CITATION 750 MM 32-30-01.SDR DXTA200500506Pitot Line · obstructedON THE T/O ROLL FGC B FAILED AND LOST THE YD AND MACH TRIM. ABORTED THE T/O AND WHEN EXITING THE RUNWAY THE SYSTEM RESET. TROUBLESHOT AND DISCONNECTED PITOT (PILOT & COPILOT), LINES CLEANED OUT WATER AND / OR DEBRIS, RECONNECTED AND PERFORMED OPS CHECK AND LSDR DXTA200400504Acm · odorAT FL 410, CREW AND PAX SMELLED FUMES IN THE GALLEY AREA AND COCKPIT. SMELL DIMINISHED IN CABIN AREA. SMELL WAS INTERMITTANT FOR 30 MINUTES DURING DESCENT. SMELL WENT AWAY WHEN COCKPIT PAC WAS TURNED OFF. COCKPIT PAC WAS TURNED OFF DUE TO LOSS OF TEMPERATUSDR DXTA200400494Manifold · malfunctionedNOSE GEAR BUMP DURING DESCENT. REPLACED LANDING GEAR MANIFOLD ASSEMBLY AS PER THE CE750 MM CHAPTER 32-30-02. GROUND OPS AND LEAK CHECKS WERE SATISFACTORY.SDR DXTA200400492Window · failedWHILE CLIMBING THRU FL300 THE OUTER PORTION OF COPILOTS SIDE COCKPIT WINDOW COMPLETELY SHATTERED. INNER PLASTIC PANEL REMAINED INTACT. REPLACED CO-PILOT'S SIDE, ELEC. HEATED COCKPIT WINDOW WITH A NEW WINDOW PER CE 750 MM 56-12-00. OPS CHECK GOOD. NO LEAKS NSDR DXTA200400491Pdu · malfunctionedFLAPS FAILED WHILE APPROACHING DESTINATION, TRIED TO RESET WITH NO CHANGE. LANDED WITH SLATS EXTENDED AND NO FLAPS. REMOVED & REPLACED FLAP MOTOR (PDU) IAW: CE750 M/M 27-52-00. RIGGED FLAP SYSTEM IAW: CE750 M/M 27-50-00. FLAP SYSTEM OPERATIONALY CHECK'S GOOSDR DXTA200400490Control Cable · out of rigFLAPS FAIL EICAS MESSAGE SLATS DEPLOYED, BUT NO FLAPS. COULD NOT DUPLICATE SQK. C/W MECHANICAL RIG AND ELECTRICAL RIG IAW 750 M/M 27-50-00. FOUND LT INBD FLAP BINDING, RE-RIGGED FLAPS AND OPS CHECKED GOOD.SDR DXTA200400488Fuel Sys · malfunctionedREPEAT - AMBER WING TANK -O FULL R- CAS ON IN FLIGHT. FUEL SPILLING FROM RIGHT WING WITH ONLY 3000 LBS IN WING TANK, SPILLING STOPPED THEN STARTED AGAIN WITH 2700 LBS IN WING TANK AND SAME CAS MESSAGE. ITEM IS UNDER INVESTIGATION.SDR DXTA200400482Pump · failedDURING FLIGHT HYDRAULIC A-PUMP FAILED, HYDRAULIC -B- OVERTEMP BLEW GEAR DOWN AND USED MANUAL BRAKES ON LANDING. ITEM IS UNDER INVESTIGATION.SDR DXTA200400484Landing Gear · malfunctionedDURING CRUISE FLIGHT AT FL390, THE NOSE WHEEL PARTIALLY EXTENDED AT MACH .90, RED UNLOCK LIGHT ILLUMINATED. ITEM IS UNDER INVESTIGATION.SDR DXTA200400481Strut · lowAFTER TAKEOFF LANDING GEAR HANDLE WOULD NOT MOVE OUT OF THE DOWN POSITION. JACKED A/C FOUND NOSE STRUT SERVICE LOW. SERVICED NOSE STRUT AS REQUIRED. PERFORMED GEAR SWING SYSTEM OP'S CHECKS SATISFACTORY AT THIS TIME. ALL WORK DONE IAW CE750 M/M 12-10-38.SDR DXTA200400475Wheel · vibrationVIOLENT SHAKING IN NOSE GEAR ON TAKEOFF ROLL, ABORTED AROUND 30-40 KTS. REMOVED & REPLACED LT & RT NOSE TIRES, AND WHEEL ASSEMBLIES, WORK DONE IAW CITATION 750 M/M 32-41-01.SDR UG8AGM0418Switch · stickingTAKEOFF ABORTED, DURING TAKEOFF ROLL DUE TO HP DUCT O PRESSURE CAS (AMBER) MESSAGE ILLUMINATING. CREW COULD NOT DETERMINE WHICH ENGINE PROBLEM OCCURRED ON. THROTTLE WAS PULLED BACK IMMEDIATELY. TRIP WAS PUT ON ANOTHER AIRCRAFT. SB COMPLIED WITH. MAINT GROSDR DXTA200400473Brake Assy · malfunctionedRIGHT BRAKE VERY SOFT, BRAKE INDICTOR VERY LITTLE REMAINING. INSPECT THE RIGHT HAND SIDE BRAKE SYSTEM, 3 BRAKE INDICATOR HAD .075 INCH REMAINING AND NR 4 BRAKE INDICATOR HAS .068 REMAINING. REMOVED AND REPLACED BOTH NR 3 & NR 4 BRAKE ASSEMBLIES AND SHUTTLE VSDR DXTA200400465Brake Assy · malfunctionedRIGHT BRAKE PRESSURE IS LOCKED, RIGHT BRAKE PEDAL HAS NO PRESSURE. ITEM IS UNDER INVESTIGATION.SDR DXTA200400462Trim Scale · warning lightON TAKEOFF ROLL JUST BELOW V1, RED MASTER WARNING ILLUMINATED WITH RED NO TAKEOFF EICAS MESSAGE. AFTER ABORTING T/O AND EXITING RUNWAY, NO ABNORMALITIES NOTED ON T/O PAGE, OR ANYWHERE ELSE. FOUND STAB TRIM OUT OF T/O ARC LIMITS. SET STAB TO WITHIN T/O LIMITSDR DXTA200400463Window · failedDURING CRUISE FLIGHT AT FL 410, WINDSHIELD HEAT INOP R CAS MESSAGE ILLUMINATED. TEN SECONDS LATER, LEFT WING SHIELD OUTER PANE SHATTERED, ELECTIRICAL ARCING WAS OBSERVED BETWEEN PANE. PERFORMED EMERGENCY DESCENT AND DIVERSION TO KFLO. ITEM IS UNDER INVESTIGSDR DXTA200400459Check Valve · failedWING TANK OVERFILL RT CAS MESSAGE FOLLOWED BY FUEL VENTING OUT OF RIGHT WING TIP, 6000 LBS OF FUEL TOTAL IN AIRCRAFT. FOUND RT WING SURGE TANK CHECK VALVE TO EXCESSIVE SIDE PLAY. REMOVED AND REPLACED CHECK VALVE WITH NEW. CLOSED ACCESS PANELS AND FUELED A/CSDR DXTA200400456Fuel Filter · cloggedFUEL FILTER BYPASS-R CAS MESSAGE CAME ON DURING THE T/O ROLL. INSPECTED PER ROLLS ROYCE MM 73-30-00200-801 AND FOUND THAT FUEL FILTER NEEDED TO BE REPLACED. REMOVED & INSTALLED NEW FUEL FILTER AND O-RINGS WITH KIT P/N 23061826 RESET BYPASS INDICATOR PERFORMESDR DXTA200400454Autopilot Sys · malfunctionedDURING GO AROUNDS (AFTER A COUPLE APPROACHES) THE AUTO-PILOT DISENGAGED MULTIPLE TIMES AFTER IT WAS RE-ENGAGED IN STABILIZED CLIMB/LEVEL OFF AND IN LEVEL FLIGHT. ON SECOND MISSED APPROACH BOTH FMS UNITS FAILED FOR ABOUT 30 SECONDS ALONG WITH THE AUTO-PILOT DISDR DXTA200400453Warning System · activatedAFTER TAKEOFF, SELECTED FLAPS UP, FLAPS WERE AT ZERO. THE AMBER YD FAIL A-B, CAS MESSAGE ILLUMINATED ON THE CONTROL PAGE. IT SHOWED THE UPPER FAILED TO THE RIGHT OF THE AVAILABLE GREEN LIMIT. SELECTED THE UPPER BUTTON AND THE CAS WENT OUT, UPON LANDING DID SDR DXTA200400450Computer · malfunctionedIN FLIGHT AT 17,000 FT AND 320 KTS FELT A SHARP RUDDER KICK WITH THE AUTOPILOT ON, YD FAIL UPPER -B- AMBER CAS MESSAGE ILLUMINATED. REMOVED AND REPLACED -B- YSAC (UPPER) IAW 750 MM 27-24-01. OPS CHECKED GOOD.SDR DXTA200400449Pitot System · obstructedAT APPROX 80 KTS ON TAKEOFF ROLL THE MACH TRIM CAS MESSAGE ILLUMINATED, FOLLOWED BY THE LOWER RUDDER FAIL CAS MESSAGE. FOLLOWED CHECKLIST FOR LOWER RUDDER FAIL, CAS MESSAGE WERE NORMAL. FOUND BUGS IN PITOT LINES FROM ADC. CLEANED LINES. C/W PITOT SYTEM LEASDR DXTA200400446Landing Gear · malfunctionedAFTER TAKEOFF LANDING GEAR HANDLE PLACED IN THE UP POSITION A LOUD CLUNK WAS HEARD, GOT THE RED UNSAFE AND GREEN NOSE GEAR LIGHT. PLACED GEAR IN THE DOWN POSITION AND GOT 3 GREEN LIGHTS THE GEAR HANDLE WOULD NOT MOVE UP OR DOWN. ITEM IS UNDER INVESTIGATION.SDR UG8AGM0417Sensor · failedSTAB TRIM FAILED ON PREFLIGHT INSPECTION. REPLACED STAB TRIM POSITION SENSOR.SDR DXTA200400444Wheel · noisyDURING FLIGHT, LOUD BANGING NOISE FROM NOSE WHEEL. NOSE WHEEL DROPS A LITTLE AND THEN IS SLAMMED BACK UP MAKING LOUD CLUNK. HAPPENED APPROX 8 TIMES IN A 4 HR FLIGHT. ITEM IS UNDER INVESTIGATION.SDR 2005FA0000684Hose · rupturedHYDRAULIC HOSE RUPTURED IN AREA ADJACENT TO SLEEVE ALLOWING LOSS OF HYDRAULIC FLUID TO (SYSTEM A). HOSE BEING SENT TO MFG FOR EVALUATION. (GL13200505055) (K)SDR DXTA200400447Position Sensor · inoperativeYD FAIL UPPER A CAS MESSAGE DURING CLIMB. DETERMINED UPPER RUDDER POSITION SENSOR -A- WITH FAULT. REPLACED SENSOR -A-, DUE TO CAS MESSAGE DURING CLIMB, WITH FAULT. INSTALLED NEW SENSOR UNIT INTO -A- POSITION. DETERMINED UPPER RUDDER POSITION SENSOR "A" WITSDR DXTA200400440Flapper Valve · failedINFLIGHT THE WING TANK OVERFILL L CAS MESSAGE CAME ON. THE LEFT WING TANK SHOWED 3200 LBS OF FUEL IN IT AND FUEL STARTED TO VENT OVERBOARD, VENTING STOPPED AT ABOUT 2970 LBS INDICATED IN L WING TANK. AFTER LANDING (20 MIN LATER) CREW NOTICED THE UNDERSIDE OFSDR DXTA200400438Strut · damagedAFTER GEAR RETRACTION, RED UNLOCK GEAR LIGHT REMAINED ILLUMINATED. AFTER TOUCHDOWN NOTICED MODERATE VIBRATION COMING FROM GEAR. PERFORMED GEAR SWING COULD NO DUPLICATE DISCREPANCY. MEASURED NOSE STRUT FOUND OVER EXTENDED. REMOVED LOWER BARREL ASSY AND REPASDR DXTA200400434Pitot Tube · obstructedABORTED TAKEOFF AT LESS THAN 80 KTS DUE TO AMBER FADEC REV ADC R CAS MESSAGE. OPERATED AIRCRAFT & NOTED NO FAULTS FOR A OR B FADEC. ENTERED MAINT PAGE & CHECKED LOGGED FAULTS. ONE FAULT CODE OF 3106 LISTED, ADC SENSOR MISCOMPARE FOR 30 OCT 04. ACCOMPLISHEDSDR DXTA200400433Pressure Switch · defectiveAT POWERING UP FOR TAKEOFF THE AMBER FUEL FILTER BYPASS R CAS MESSAGE CAME ON, ABORTED TAKEOFF. TROUBLESHOT AND FOUND FUEL FILTER DPI SWITCH DEFECTIVE. REMOVED WITH NEW SWITCH. OPS CHECK AND LEAK CHECKED GOOD. WORK DONE IAW ROLLS ROYCE AE3007C MM CHAPTER 7SDR DXTA200400429Pressure Switch · malfunctionedDURING TAKEOFF ROLL THE RIGHT HP DUCT OVERPRESSURE WARNING LIGHT CAME ON, ABORTED TAKEOFF. REMOVED & INSTALLED A NEW RT OVER PRESSURE SWITCH IAW CESSNA-750 MM CHAPTER 36-11-00. OPS AND LEAK CHECKED GOOD.SDR DXTA200400430Door Seal · leakingAFTER CRUISING AT FL 410 FOR APPROXIMATELY 1 HR, BAGGAGE DOOR SEAL CAS MESSAGE DISPLAYED. 15 MINUTES LATER, CABIN BEGAN TO CLIMB AT A RATE OF 1000' PER MIN WITH IN 1 MINUTE CABIN RATE INCREASED TO APPROX 6000' PER MINUTE. AMBER AND RED CABIN ALTITUDE CAS MESSDR DXTA200400426Warning Light · illuminatedAFTER TAKE-OFF GEAR WAS SELECTED UP, GREEN LIGHTS WENT OUT, RED LIGHT STAYED ON (GEAR WAS CYCLED BUT THE OUTCOME WAS THE SAME. ) ITEM IS UNDER INVESTIGATION.SDR DXTA200400425Controller · malfunctionedWITH AUTOPILOT ENGAGED, IN A LT TURN, LVL FLIGHT MASTER WARNING ILLUMINATED + CAS MESSAGE RETRIM RT WING DOWN WAS DISPLAYED. THIS HAPPENED TWICE, IN EACH CASE THE AUTOPILOT WAS DISENGAGED BY PILOT. WINGS LEVELED AND LIGHTS EXTINGUISHED. COMPLETED INSPECTIOSDR DXTA200400424Fuel Filter · inoperativeFUEL FILTER BYPASS L CAS MESSAGE CAME ON AT POWER APPLICATION FOR TAKE-OFF ( NO NOTICABLE CHANGE IN ENGINE OPERATION, ABORTED TAKE OFF. INSTALLED NEW FILTER ELEMENT. TEST RAN ENGINE WITH NO FURTHER DEFECTS NOR LEAKS. WORK PERFORMED IAW MM CHAPTER 71-00 ANDSDR DXTA200400423Actuator · failedUPON GEAR RETRACTION ALL GREEN LIGHTS OUT RED UNLOCK LIGHT ON. RECYCLED GEAR AND GOT THE SAME RESULT. A LOT OF AIR/WIND NOISE FROM NOSE OF PLANE, SOUNDED LIKE NOSE GEAR WAS EXTENDED. REMOVED & REPLACED NOSE GEAR ACTUATOR WITH RENTAL UNIT. SENT LINE NOSE GESDR DXTA200400421Solenoid · failedDURING INITIAL DESCENT WITH POWER REDUCTION, THE CABIN BEGAN TO CLIMB AT A RATE OF APPROX 2000 FPM. THE CABIN CONTINUED TO CLIMB AND CONTINUED TO DESCEND, THE CABIN ALT RED CAS ILLUMINATES, INITIATED EMERGENCY DESCENT FOR LOWER ALTITUDE. TROUBLESHOOT TO FAULSDR DXTA200400417Warning Light · illuminated"WING O FILL R" AMBER LIGHT CAME ON IN FLIGHT, LOST ABOUT 400 LBS OF FUEL. INSPECTED RIGHT WING OUTBOARD TRANSFER VALVE. NO DEFECTS NOTED. PERFORMED FUEL TRANSFER SYSTEM SHUTOFF TEST. FOUND ALL OPERATION NORMAL. NO FURTHER ACTION TAKEN. WORK PERFORMED IASDR DXTA200400420Wheel · vibrationDURING TAKEOFF ROLL SEVERE NOSE GEAR SHIMMY / VIBRATION RESULTED IN ABORTED T/O AT 65 KTS. VIBRATION WAS REDUCED, NOT ELIMINATED, WITH APPLICATION OF ELEVATOR BACK PRESSURE. REMOVED AND REPLACED BOTH NOSE WHEEL AND TIRE ASSY WITH OVERHAUL ASSY IAW 750 M/M 32SDR DXTA200400418Wheel · wornLT BRAKE NOISY AND GRABS AFTER LANDING, LT OUTER BRAKE ASSY SMOKES AFTER COOL DOWN. AFTER SHORT TAXI BRAKE CONTINUES TO SMOKE, INNER TIRE IS CONSIDERABLY COOLER THAN OUTER. INITIAL INSPECTION OF LT WHEELS AND BRAKES SHOWS LT OUTER TIRE TO HAVE 8 TO 10 INCH WESDR DXTA200400413Circuit Board · contaminatedDURING FLIGHT, NOTICED ELECTRICAL BURN ODOR IN THE COCKPIT, FOLLOWED BY DISCOVERY OF WATER SEEPING OUT FROM BEHIND RT CIRCUIT BREAKER PANEL, BELOW THE 3 APU CIRCUIT BREAKERS. REMOVED AND INSPECTED CO-PILOT CIRCUIT BREAKER PANEL, CLEANED WITH CONTACT CLEANER, SDR DXTA200400415Warning Light · illuminatedDURING DESCENT, PASSING THROUGH 14000 FT, AT 345 KIAS, AT 3000 FPM, GO TRANSIENT GEAR UNLOCK-FELT NOSE GEAR UNLOCK AND DROP MOMENTARILY BEFORE RE-LOCKING, THE REST OF FLIGHT NORMAL. JACKED AIRCRAFT AND PERFORMED GEAR SWING, CHECKED UPLOCK HOOK AND SWITCH RIGG
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