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 DXTA200601528Brake · stuckDURING TAXI OUT AT SFO RIGHT BRAKE APPEARED TO BE DRAGGING. ON RETURN TAXI TO FBO GROUND CONTROL REPORTED SMOKE FROM THE BRAKE AREA. AIRCRAFT WAS STOPPED AND ON INSPECTION NRB 4 FUSE PLUG HAD ACTIVATED. REMOVED/REPLACED THE NR 3 AND 4 WHEEL TIRE ASSY AS PERSDR DXTA200601524Acm · leakingAFTER STARTING BOTH ENGINES, COCKPIT AND CABIN FILLED WITH SMOKE COMING FROM OVERHEAD VENTS, VISUAL INSPECTION OF THE TAILCONE COMPARTMENT AND FOUND OIL LEAKING FROM FORWARD PACK. REMOVED AND REPLACED FAULTY FORWARD ACM IAW MM 21-51-00. OPS AND LEAK CHECK GOSDR DXTA200601520Steering Sys · malfunctionedAFTER LANDING TURNING OFF THE RUNWAY ALL CONTROL OF THE NOSEWHEEL STEERING WAS LOST TILLER PLUS PEDALS WERE FROZEN.SDR DXTA200601519Pitot System · contaminatedON TAKEOFF ROLL BETWEEN 60 AND 80 KTS, AMBER "MACH TRIM OFF" AND AMBER "YD OFF LOWER" CAS MESSAGES ILLUMINATED. YD AND M TRIM ANNUNCIATORS ON AUTOPILOT CONTROLLER WENT BLANK. AMBER ARROW APPEARED ON PILOTS PFD AND AP MODES DISAPPEARED. V SPEEDS WERE INTERMISDR DXTA200601514Isolation Valve · inoperativeDURING FLT AT FL450 BAGGAGE DOOR SEAL LIGHT CAME ON APPROX 10 MINS LATER CABIN BEGAN CLIMBING CLOSED ISOLATION VLV AND DESCENDED TO FL410 CABIN ALT KEPT CLIMBING ACCOMP LOSS OF CABIN PRESS CHK LIST DESCENDED TO FL 250 AND CABIN ALT STABILIZED RED CABIN ALT MESSDR DXTA200601511Strut · underservicedUNLOCK LIGHT STAYED ON AFTER GEAR RETRACTION, CYCLED GEAR AND UNLOCK LIGHT WENT OUT AFTER 20 SECONDS. ON POST FLT, FOUND DAMAGE TO A/C AT ENTRY POINT FOR RIGHT MAIN TIRES. DAMAGE TO WHEEL WELL WAS CAUSED BY THE RT OLEO NOT FULLY EXTENDING AFTER TAKEOFF AND TSDR DXTA200601507Computer · failedSHORTLY AFTER TAKEOFF, PRIMARY TRIM STOPPED WORKING. IT WORKED OK FOR THE FIRST 1.5 TO 2 MINUTES. SELECTED STBY TRIM AND IT ALSO DID NOT WORK. STBY TRIM WORKED AFTER 5 MIN OF NOT WORKING. FIRST INDICATION OF PROBLEM WAS NO FLIGHT DIRECTOR MODES COULD BE SELECTSDR DXTA200601508Hose · blownTHERE WAS A COMPLETE (A) SYSTEM HYDRAULIC LOSS WHILE IN FLIGHT. THE EMERGENCY BRAKES AND EMERGENCY NOSEWHEEL STEERING WERE USED FOR LANDING. REMOVED AND REPLACED HYDRAULIC PUMP PRESSURE HOSE ASSY P/N AE1011923H0152, OLD HOSE WAS BLOWN OUT. HOSE REPLACED IAW SDR DXTA200601503Float Valve · defectiveAT FL 320 AND 3100 LBS IN RIGHT TANK AND 0 LBS IN CENTER WING TANK O FULL, RT EICAS MESSAGE APPEARED RIGHT WING WAS VENTING FUEL MOVED CENTER WING X-FER SWITCH TO OFF ABOUT 30-40 SECONDS LATER EICAS MESSAGE DISAPPEARED AND FUEL STOPPED VENTING. REMOVED AND RESDR DXTA200601504Apu · overservicedDURING FLT, APU FAILED IN FLT. PRECEDED BY BURNING ODOR. RAN APU FOR 20 MIN CYCLING BLEED AIR VALVE IN DIFFERENT POSITIONS. APU NEVER SHUTDOWN. NOTICE THAT AS APU RAN & WARMED UP THAT THERE WAS SOME BLACK SMOKE NOTICE. ALSO, NOTICED BACKSHELL FOR OIL TEMPSDR DXTA200601500Pdu · failedFLAPS FAILED AT 5 DEG AND WOULD NOT RESET SLATS WORKED OK ON GROUND, FLAPS RESET 3 TIMES IN 2 SECS AND FLAPS WOULD GO UP. REMOVED AND REPLACED FLAP POWER DRIVE UNIT, OPERATIONALLY CHECK'S GOOD IAW CE750 M/M 27-50-00.SDR DXTA200601490Odor · detectedDISTINCTIVE OIL ODOR ISOLATED TO COCKPIT PACK AIRFLOW FROM COCKPIT PACK VERY WEAK. RAN APU, NO ODOR NOTED FROM EITHER PACK AND AIRFLOW WAS NORMAL FROM BOTH PACKS. VERIFIED STRONG FLOW AT BOTH ACM INTAKES. STARTED ENGINES AND TURNED OFF APU OIL. AGAIN AIRFLSDR DXTA200601489Yoke · bindingYOKE CONTROL BINDING WHEN DISPLACING LEFT. ADD MORE PRESSURE, YOKE WOULD MOVE. CHECKED CABLE TENSIONS, ALL CHECKED GOOD. REMOVED AND INSPECTED AILERON PUSH RODS AT AILERON FOUND BEARING TO BE TIGHT. CLEANED AND LUBED BEARINGS. REINSTALLED PUSHRODS SYSTEM,SDR DXTA200601482Brake Assy · unknownWITH EQUAL AMOUNT OF PRESSURE APPLIED TO THE BRAKES PEDALS, AIRCRAFT PULLS TO THE LEFT. AIRCRAFT RESPONDS THE SAME WITH LEFT SIDE OR RIGHT SIDE BRAKE APPLICATION. PILOT OR COPILOT BRAKE APPLICATION. PERFORMED POWER BRAKE SYSTEM FUNCTIONAL TEST WITH SATISFACSDR DXTA200601478Unknown · unknownLOUD CLUNKING NOISE HEARD AND FELT ON COCKPIT FLOOR DURING CRUISE FLIGHT. OCCURRED ON SEVERAL OCCASIONS DURING CRUISE FLIGHT 400, NO GEAR INDICATION NOTED.SDR DXTA200601470Actuator · intermittentAMBER "RUD LIMITER FAIL A" CAS MESSAGE, 84 PERCENT INFLIGHT. LOWER RUDDER PERFORMED RUDDER LIMITER OPERATIONAL CHECK. NO DISCREPANCIES NOTED. GAINED ACCESS TO RUDDER LIMITER A ACTUATOR. VISUAL INSPECTION CHECK GOOD. CONTACTED NETJETS WHO ELECTS TO REPLACESDR DXTA200601467Apu · overservicedAFTER T/O, GEAR WOULD NOT RETRACT WITH THE GEAR HANDLE IN THE UP POSITION. RECYCLED DURING FLIGHT FROM TEB TO DAL NOTICED BURNING ODOR COMING FROM COCKPIT GASPERS WHEN DUCT TEMP (COCKPIT) REACHES APPROX 120*. ESPECIALLY NOTICABLE WHEN POWER IS REDUCED ON INISDR DXTA200601464Line · leakingDURING FLIGHT FROM SAV TO HPN, NOTICED OILY ODOR WHEN PAC IS RUNNING, CONTINUED FLIGHT TO HPN WITHOUT INCIDENT. INSPECTED APU AND TAIL COMPT. FOUND APU COMPT TO BE COVERED IN FLUID. DETERMINED FLUID TO BE HYDRAULIC FLUID FROM LEAK AT LWR RUDDER ACTUATOR SEESDR DXTA200601453Acm · failedON GROUND AT PBI, AFTER SELECTING BLEED AIR MAX COOL, NOTICED SMOKE FILLING THE COCKPIT. REMOVED & REPLACED COCKPIT PAC COOLING TURBINE IAW CE 750 MM 21-57-00. OPS AND LEAK CHECK GOOD.SDR DXTA200601451O-Ring · blownIN LEVEL FLIGHT AT FL400, HYD VOLUME LOW A CAS MESSAGE CAME ON. OBSERVED THE VOLUME AT 14 PERCENT AND THE PRESSURE AT 2800 PSI. RAN THE CHECKLIST AND MADE A LANDING. THE EMERGENCY GEAR BLOW DOWN AND BRAKES WERE APPLIED. TROUBLESHOT TO BLOWN O-RING ON -A- SSDR DXTA200601450Acm · seizedAPPROX 10 MIN AFTER POWER UP AND STARTING THE APU A VERY DETECTABLE AMOUNT OF SMOKE WAS FILLING THE CABIN. IMMEDIATELY SHUT A/C DOWN, NO OTHER NOTABLE PROBLEMS. ENVIRONMENTAL NOT ELECTRICAL SMOKE. COULD NOT DUPLICATE DISCREPANCY. HOWEVER WHEN MAX COOL SELESDR DXTA200601447Strut · lowGEAR WOULD NOT RETRACT AFTER TAKEOFF. CHECKED OPERATION AT ALL PINS WITH OHMMETER AT NOSE AND MAIN GEAR SQUAT SWITCHES. CHECKED GOOD. JACKED A/C. CHECKED GEAR FOR FULL EXTENSION. FOUND NOSE GEAR NOT FULLY EXTENDING. SERVICED NOSE STRUT WITH HYDRAULIC FLUSDR DXTA200601440Uplock Switch · out of adjustIN CLIMB, NOSE GEAR UPLOCK RELEASED, GEAR UNLOCK LIGHT ILLUMINATED. ACCOMPLISHED NETJETS GEAR BUMP CHECKLIST, FOUND NOSE GEAR UPLOCK SWITCH ADJUSTED OUT OF SPEC. ADJUSTED AND CHECKED UPLOCK SWITCH IAW CESSNA 750 M/M CHPT 32-30-05.SDR DXTA200601433Odor · detectedDURING FLIGHT, A STRONG BURNING ODOR SMELLED THROUGH OUT AIRPLANE ON SHORT FINAL AND TAXI IN. THE ODOR APPEARS TO BE COMING FROM THE PACS. ITEM IS UNDER INVESTIGATION.SDR DXTA200601434Connector · not seatedAFTER TAKEOFF, THE GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. FOUND NOSE GEAR CENTERING SWITCH CONNECTOR PLUG NOT SEATED. INSPECTED AND RESEATED PLUG IAW MM CH 32-30-00. OPS CHECK GOOD.SDR DXTA200601435Fadec · failedAMBER (ENGINE O SPEED SHUTDOWN L) ILLUMINATED AFTER TO. AT APPROXIMATELY 400 FT. ALL ENGINE INDICATIONS WERE NORMAL EXCEPT (L) ITT WAS ERRATIC IN TO THROTTLE POSITION. TROUBLESHOT TO BAD LT (B) FADEC, REMOVED AND REPLACED FADEC, OPERATIONAL CHECKS GOOD. PSDR DXTA200601431Display · failedNR 1 PFD VIBRATION ON TAKEOFF ROLL MOMENTARILY WENT BLANK. REMOVED AND REPLACED NR 1PFD WITH SERVICEABLE UNIT FROM MFG RS NR LV2R992K IAW MM CHAP.34-25-01- OP'S CHECKED GOOD.SDR DXTA200601423Fuel Sys · leakingAT FL 330, WING OVER FULL LT CAS MSG ILLUMINATED. SHORTLY AFTER FUEL BEGAN STREAMING FROM WING. CONDUCTED A RT 360 DEGREE TURN AND VENTING STOPPED. 5 MINS LATER FUEL BEGAN TO VENT AGAIN AND THEN STOPPED. THIS OCCURRED A TOTAL OF 3 TIMES WITH A LOSS OF 400 LBS SDR CA060608009Windshield · failedAIRCRAFT IN CRUISE AT 41000 FT, SMALL CRACK STARTED AT BOTTOM OB LOWER CORNER. WITHIN 15 SECONDS THE CRACK EXTENDED ABOUT 3 INCHES THEN WITHIN ABOUT 30 SECONDS THE OUTER PANE SHATTERED. THE AIRCRAFT WAS FLOWN TO A AIRPORT AND LANDED WITHOUT INCIDENT. THE ASDR DXTA200601407A/C Pack · failedDURING ENGINE START WE SMELLED A VERY STRONG, PUNGENT ENVIROMENTAL ODOR. SUSPECT COCKPIT PAC FAILURE. VERIFIED COCKPIT PAC FAILED.REMOVED AND REPLACED COCKPIT ACM IAW MM 21-51-00. OPERATIONAL AND LEAK CHECK GOOD.SDR DXTA200601401Brake · malfunctionedBRAKES GRAB EXCESSIVELY, ESPECIALLY THE RT BRAKE. ON THE RT BRAKE WHEN SLOWING TO A STOP YOU HAVE TO PUSH HARD TO OVERCOME A STICKY SPOT, THEN IT GRABS. TAXIED AIRCRAFT AND CYCLED BRAKES SEVERAL TIMES. USING NORMAL TAXI SPEEDS. APPLIED BRAKES VARYING FROM SDR DXT2006F00000Hose · rupturedAC TOOK OFF AND ATTEMPTED TO RETRACT THE LANDING GEAR. THE CREW THEN NOTICED THAT THE NOSE GEAR DID NOT RETRACT AND THE AIRCRAFT LOST HYDRAULIC FLUID FROM THE (A) RESERVOIR. THE FLIGHT CREW THEN DECLARED AN EMERGENCY. AT THIS TIME THEY PNEUMATICALLY (BLEW) SDR DXTA200601396Hose · rupturedHYD VOLUME LOW (A) CAS MESSAGE. HYD QUANTITY INDICATES ZERO AFTER GEAR RETRACTION. NOSE GEAR DID NOT RETRACT. REPLACED NOSE STEERING UNIT CENTERING HOSE DUE TO RUPTURE WITH NEW HOSE. SERVICED A HYDRAULIC SYSTEM IAW THE MM CHAPTER 32-50-00 AND 12-10-15. OPERATSDR DXTA200601402Battery · overtempBATT 2 O'TEMP MASTER WARNING MESSAGE ILLUMINATED IN CRUISE FLIGHT BATT NR 2 TEMP WAS OVER 70DEG AND CONTINUED TO RISE TO 100 DEG AFTER BATT NR 2 WAS TURNED OFF. REMOVED DEFECTIVE BATTERY AND INSTALLED NICAD BATTERY. NICAD SENT FOR NR 2 POSITION, WORK DONE ISDR DXTA200601394Valve · deterioratedRT WING VENTED FUEL IN FLIGHT. RT WING OVERFILL EICAS MESSAGE RAN PROCEDURES 4 TIMES WITH AIRCRAFT YAWING BEFORE IT STOPPED. REMOVED PANELS ON OB RT WING AND IB RT SURGE TANK. INSPECTED SURGE TANK DRAIN FLOAT, APPEARED GOOD. INSPECTED CHECK VALVE ON DRAIN FSDR DXTA200601388Engine · failedDURING TAXI, RIGHT ENGINE SHUT DOWN, HAD JUST ADVANCED TLA TO CROSS A RUNWAY AND RIGHT ENGINE FAILED. CHECKED THE RIGHT ENGINE FADECS FOR FAULTS, NO FAULTS INDICATED. RAN THE RIGHT ENGINE NUMEROUS TIMES WITH NORMAL STARTS AND ACCELERATION EACH TIME. INSPECTSDR DXTA200601387Acm · seizedON GROUND WITH APU RUNNING AFTER SELECTING MAX COOL THERE WAS A LOUD POP FOLLOWED BY SMOKE IN THE COCKPIT. RAN AIRCRAFT. FOUND COCKPIT ACM TURBINE SEIZED. REMOVED COCKPIT ACM IN REF TO CE750 M/M CH 21-51-00 MAY 11, 2006. INSTALLED NEW ACM AS REQ OPS CHECK SDR DXTA200601390Pump · failedDURING CLIMB OUT RT HYD PRESSURE INDICATED AMBER AT 3300 LBS. LOW HYD VOLUME AND LOSS OF SYSTEM PRESSURE FOLLOWED. RT HYDRAILIC PUMP HAS FAILED, REMOVED PUMP AND INSTALLED OVERHAULED PUMP. PURIFIED (B) HYDRAULIC SYSTEM AND INSTALLED NEW PRESSURE, RETURN AND CSDR DJFA2006246Acm · seizedTHE CREW REPORTED THAT THE LEFT AIR CONDITIONING UNIT CREATED BLUE SMOKE IN THE COCKPIT WHILE RUNNING AT MAXIMUM COOLING WITH VERY LITTLE CONTROL OVER THE COCKPIT AND CABIN TEMPERATURE. MAINTENANCE FOUND THE AFT AIR CYCLE MACHINE FAN TO BE SEIZED. THE AFT ACSDR DXTA200601376Landing Gear · noisyAFTER TAKEOFF THREE GREEN GEAR LIGHTS EXTINGUISHED BUT UNLOCK LIGHT DID NOT GO OUT UNTIL 3000AGL. DURING THIS TIME LOUD NOISES HEARD FROM THE NOSE GEAR. SERVICED NOSE STRUT AND CYCLED GEAR MANY TIMES WITH NO DEFECTS AT THIS TIME. WORK DONE IAW MM CH.12-10-38.SDR DXTA200601371Fuel · warning lightWING TANK O FULL R AMBER CAS MESSAGE ILLUMINATED IN FLIGHT , FOLLOWED BY VENTING OF FUEL OUT THE RT WING FOR APPROXIMATELY 4 MINUTES. ITEM IS UNDER INVESTIGATION.SDR DXTA200601363Landing Gear · malfunctionedLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF, ALL OTHER INDICATIONS NORMAL. ITEM IS UNDER INVESTIGATION.SDR DXTA200601360Acm · failedON FULL POWER TAKEOFF ROLL, AFTER 5 SECONDS OR SO A BURNING RUBBER SMELL WAS SENSED. TAKEOFF DISCONTINUED. POST FLIGHT INSPECTION NORMAL. T/S TO DEFECTIVE ACM, FWD PAC. REMOVED FAULTY FORWARD ACM AND INSTALLED OVERHAULED UNIT. REMOVED OIL FROM WATER SEPARATOSDR DXTA200601358Pitot System · contaminatedYAW DAMP, MACH TRIM DISENGAGED TWICE ON TAKEOFF ROLL. PITOT HEAT WAS ON FOR 5 MINUTES PRIOR TO SECOND TAKEOFF ROLL. PERFORMED OPS CHECK OF YAW DAMPNER ON FGC A AND B SIDES, FOUND NO DISCRECPENCIES. DOWNLOAD AFCS FAULTS AND MADC FAULTS AND MAILED TO TEAM X PROSDR DXTA200601373Resolver · inoperativeWHEN THE FLAP HANDLE WAS PLACED TO 15 DEGREES IN PREPARATION FOR TAXI THE FLAPS STOPPED AT APPROX 5 DEG. AND THE AMBER FLAPS FAIL CAS ILLUMINATED. THE FLAP RESET SWITCH WAS PRESSED BUT HAD NO EFFECT. REMOVED AND REPLACED LT FLAP RESOLVER, MM 27-52-00 C/W RIG SDR DXTA200601354Actuator · faultyAFTER LANDING GEAR RETRACTION , RED UNLOCK LIGHT REMAINED ON. WHEN GEAR WAS LOWERED , RED UNLOCKED WENT OUT , ALL GREEN ON. REMOVED AND REPLACED NOSE LANDING GEAR ACTUATOR IAW MM CH 32-30-03. OPS AND LEAK CHECKED GOOD.SDR DXTA200601353Hose · leakingDURING FLIGHT (HYDRAULIC VOLUME LOW B) CAS MESSAGE CAME ON. VOLUME INDICATED 16 PERCENT. SYSTEM UNLOADED IAW CHECKLIST, UNEVENTFUL LANDING. - FOUND RT ELEVATOR PCU HOSE LEAKING. TIGHTENED LINE, AND RAN SYSTEM LEAK CHECK GOOD. IAW MM CHP 27-34-00.SDR DXTA200601351Nut · looseAFTER TAKEOFF CLIMBING THROUGH FL 250 NOTICE A BUMP OR THUMP APPARENTLY COMING FROM NOSE GEAR AREA FOLLOWED BE GEAR UNLOCKED RED LIGHT. CYCLED GEAR ON APP & LIGHT WENT OUT. LOWER GEAR & NORMAL LAND. FOUND STRUT EXTENSION EXCEEDING MAX. LIMITS. FOUND RETAININSDR DXTA200601344Pitot Head · inoperativeON TAKEOFF ROLL AMBER CAS MESSAGE PITOT HTR FAIL SB. MES, CYCLED SEVERAL TIMES. T/O REJECTED APPRO 50-60 KTS. CONFIRMED SQUAWK CAS MES STAYS ON CONTINUOUSLY WHEN PITOT HEAT IS SELECTED ON. TROUBLESHOT USING BREAKOUT BOX FOUND 28VDC GOING TO HEATER, BUT STANDBSDR DXTA200601348Actuator · intermittentRED GEAR UNSAFE LIGHT ILLUMINATES UPON RETRACTION ( WITH GEAR UP ) AFTER TAKEOFF. RECYCLED GEAR AND LIGHT ILLUMINATED AGAIN OBVIOUS AIR NOISE FROM GEAR AREA. REMOVED AND REPLACED NOSE GEAR ACTUATOR IAW MM CH 32-30-03. ADJUSTED NOSE GEAR CASTER AND CYCLED GEA
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