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 DXTA200702377Actuator · failedON TAKEOFF, AFTER GEAR UP, BEFORE FLAPS UP, GOT CAS (RUD LIMIT FAIL A), CONTROL PAGE MSG RUDDER LIMIT 99 PERCENT. INSTALLED NEW ACTUATOR IAW 750 M/M 27-23-00 RIG AND OPS CHECK GOOD IAW 750 M/M 27-20-00.SDR DXTA200702373Apu · smokeWHILE RUNNING APU ON THE GROUND WITH COCKPIT PAC ON HIGH GOT SMOKE IN COCKPIT. COCKPIT PAC SUPPLY TEMP ROSE RAPIDLY. COCKPIT PAC OIL RESEVOIR WAS CLEAR ON PREFLIGHT NOW BLACK. REPLACED COCKPIT PAC ACM & COALESCER SOCK OPS CK GOOD REF CE750 M/M 21-51-00.SDR DXTA200702368Bolt · looseON CLIMBOUT AT APPROXIMATELY 1000 FT MSL, A LOUD POP WAS HEARD FROM THE RT NOSE AREA OF THE AIRCRAFT, ACCOMPANIED BY THE AMBER CAS MSG (NOSE DOOR OPEN - R). CHECKLIST WAS DONE AND AN UNEVENTFUL NORMAL LANDING WAS MADE. ON POST FLIGHT, FOUND THAT THE RT NOSE DSDR DXTA200702366Steering Sys · malfunctionedSEVERE NOSE WHEEL SHIMMY ON TAKE-OFF, BELOW 40 KTS. IT STARTED JUST AFTER TAKE-OFF ROLL AND LASTED UNTIL NORMAL TAXI SPEED. REMOVED AND REPLACED POWER STEERING UNIT. OPS CHECK GOOD IAW CE750 M/M 32-50-00SDR DXTA200702365Motor · failedWITH AUTOPILOT ENGAGED, TRIM CLACKER AUDIBLE MORE THAN NORMAL. AFTER DISENGAGING AUTOPILOT, WE DISCOVERED NEITHER YOKE PRIMARY TRIM SWITCH HAD ANY AUTHORITY, NO CAS MESSAGE. WE ENGAGED SECONDARY TRIM SYSTEM AND MADE A PRECAUTIONARY LANDING WITHOUT INCIDENT.SDR DXTA200702362Landing Gear · malfunctionedRT MAIN LANDING GEAR DID NOT SHOW GREEN DOWN AND LOCKED INDICATION WHEN GEAR WAS SELECTED DOWN. IAW CHECKLIST: GEAR DOWN BOTTLE HANDLE WAS PULLED AND MAIN MANUAL RELEASE HANDLE PULLED. [08-23-07] RESET N2 BOTTLE, RESET LANDING GEAR CONTROL MANIFOLD, PURGED SDR DXTA200702359Brake Assy · weakTO GET EVEN BRAKING FROM THE CAPTAINS BRAKE PEDALS, THE RT PEDAL MUST BE PUSHED DOWN APPROX TWICE AS MUCH AS THE LT. THE CO-PILOTS PEDALS ARE THE SAME EXCEPT THE SPLIT IS MUCH LESS. [08-23-07] INSPECTED POWER BRAKE METERING VALVE. NO DEFECTS NOTED. PERFORMSDR DXTA200702421Hose · rupturedIMMEDIATELY AFTER RAISING, THE LANDING GEAR HANDLE AFTER TAKEOFF, ALL (A) SYSTEM HYDRAULIC PRESSURE WAS LOST AND THE EICAS INDICATED 4 PERCENT HYDRAULIC FLIUD REMAINING. THE MAIN LANDING GEAR RETRACTED AND THE NOSE GEAR REMAINED DOWN. FOUND "NWS" CETERING HYSDR DXTA200702419Control Handle · intermittentLANDING GEAR HANDLE WOULD NOT MOVE AFTER TAKEOFF TO RETRACT GEAR. JACKED A/C, HOOKED UP HYD. SERVICE CART, CYCLED LANDING GEAR FOUND GEAR HANDLE OPERATION INTERMITTENT, REMOVED + REPLACED GEAR HANDLE MODULE, OPERATED GEAR HANDLE SEVERAL TIMES OPS CHECK GOOD.SDR DXTA200702356Tire · out of roundDURING TAKE-OFF ROLL WE EXPERINCED A VIOLENT NOSE WHEEL SHIMMY BELOW 70 KNTS INDICATED. FOUND BOTH (LT & RT) NOSE TIRES OUT OF ROUND AND FLAT SPOTTED. BOTH NOSE WHEELS ALSO UNDER TORQUE SPECS. REMOVED LT & RT NOSE WHEEL ASSY. INSTALLED NEW L/H & R/H NOSE WHESDR DXTA200702355Oil System · malfunctionedON THE TAKEOFF ROLL WITH POWER (N1) INCREASING THROUGH 86 PERCENT OIL PRESSURE ON THE LT ENGINE ROSE TO 120 PSI AND STAYED THERE. AFTER REJECTING TAKEOFF THE ENGINE WAS RUN UP THROUGH 86 PERCENT TWICE AND BOTH TIMES PRESSURE INCREASED TO ABOVE 120 PSI. RAN ASDR DXTA200702353Packing · out of toleranceGEAR WOULD NOT RETRACT AFTER T.O. GEAR HANDLE LOCKED DOWN. HAD BEEN ACTING UP ON PRIOR FLIGHTS, NOT ALLOWING US TO RETRACT IMMEDIATELY. DISASSEMBLED LOWER NOSE STRUT, REPLACED PACKINGS AND REASSEMBLED, SERVICED PER 750 C/M/M 32-20-02. REPLACED NOSE STRUT ORIFISDR DJFA2007076Acm · seizedTRIP NR 1205032- ON DESCENT CREW NOTED ACM NOT COOLING AND BURNING ODOR IN CABIN. CREW COMPLETED THE APPROACH AND LANDING. MAINTENANCE FOUND THE ACM TURBINE SEIZED. THE ACM WAS REPLACED.SDR DJFA2007075Coalescer Bag · dirtyTRIP NR 1204364- DURING CRUISE, CREW NOTICED A BURNING SMELL FROM THE AIR DISTRIBUTION SYSTEM. CREW ISOLATED PROBLEM TO THE NR 1 PACK. THE PACK WAS SHUT DOWN AND THE FLIGHT CONTINUED TO ITS DESTINATION. MAINTENANCE FOUND THE COALESCER BAG DIRTY; IT WAS CLEASDR DXTA200702342Coalescer Bag · dirtyTHE CABIN PAC TEMP IS UNCONTROLLABLE AND ALSO PRODUCING AN OILY SMELL IN THE CABIN. INSPECTED ACM, OIL, AND SERVICED, REPLACED COALESCER SOCKS PERFORMED APU AND ENGINE RUNS, NO OIL SMELL PRESENT. PERFORMED OPS CHECK OF CABIN TEMP CONTROLER WITH APU AND ENGINSDR DJFA2007073Rib · crackedDURING A SCHEDULED INSPECTION, MAINTENANCE DISCOVERED A RIB IN THE RT PYLON, CRACKED. THE RIB WAS CRACKED AT THE UPPER AND LOWER FLANGES. BOTH CRACKS WERE APPROX 2 INCHES LONG. THE RIB WAS REPLACED.SDR DJFA2007074Rib · crackedDURING A SCHEDULED INSPECTION, MAINTENANCE DISCOVERED A RIB IN THE LT PYLON CRACKED. THE RIB WAS CRACKED AT THE UPPER AND LOWER FLANGES. BOTH CRACKS WERE APPROX. 2 INCHES LONG. THE RIB WAS REPLACED.SDR DXTA200702333Strut · underservicedCOULD NOT RETRACT GEAR AFTER DEPARTURE. GEAR HANDLE WAS LOCKED IN THE DOWN POSITION AND COULD NOT BE MOVED. JACKED A/C, FOUND NLG STRUT DID NOT EXTEND. SERVICED STRUT AND OLEO IAW MM CH 12-10-38. PERFORMED GEAR SWING IAW MM CH 32-30-00. NO DEFECTS NOTED. DOWSDR DXTA200702335Rudder · out of trimRT ELEVATOR ON EICAS SHOWS .3333 DEFLECTION DOWN IN CRUISE FLIGHT. AC YAWS AND THEN EXCESSIVE RUDDER IS NEEDED TO TRIM LEVEL. [07-23-07] ACCOMPLISHED BLEEDING OF HYD. SYSTEM TO ENSURE PROPER OPERATION OF FLIGHT CONTROLS. AFTER BLEEDING & SERVICING OF SYSTESDR DXTA200702330Handle · stuckAFTER TAKEOFF LANDING GEAR HANDLE WAS STUCK IN THE DOWN POSITION. [07-23-07] REMOVED AND REPLACED NOSE LANDING GEAR ASSY WITH SERVICABLE UNIT FROM CESSNA ICT RS CNQR918C PER CESSNA 750 MM 32-20-00. GROUND OP'S CHECKED GOOD.SDR DXTA200702329Controller · inoperativeIN CRUISE ALTITUDE OF FL200 MACH NR APPEARED. SELECTED C/O BUTTON ON AUTOPILOT PANEL AND THE BUTTON REMAINED IN THE DEPRESSED POSITION. NO OTHER MODES WERE ALLOWED TO BE SELECTED AND AUTO PILOT WOULD NOT RE ENGAGE. REMOVED AND REPLACED FLIGHT CONTROLLER GC-SDR DXTA200702326Strut · overservicedAFTER TAKEOFF LANDING GEAR HANDLE WOULD NOT MOVE TO ALLOW RETRACTION OF GEAR, ABOUT 40 SECONDS LATER A SMALL THUMP OCCURRED AND WE WERE ABLE TO RETRACT. JACKED AIRCRAFT, FOUND NOSE STRUT TO EXTEND TO FULL LENGTH. PERFORMED GEAR SWINGS. NO DISCREPANCY NOTED. RSDR DXTA200702325Roll Servo · inoperativeAT CRUISE FL 450 WOULD FAIL TRANSFER TO FGB-B AND RESET WITHIN 30 SECONDS THEN FGC B WOULD FAIL TRANSFER TO FGC-A THEN RESET WITHIN 30 SECONDS. THE AUTOPILOT WOULD DISCONNECT SOMETIMES. GAINED ACCESS TO IMT PAGE. INSPECTED AND FOUND FAULT CODE NR 1250 IAC/AISDR DXTA200702322Acm · failedDESCENDING TROUGH FL310 CREW HEARD A VERY LOUD POP SOUND FOLLOWED IMMEDIATELY BY A STRONG SMOKE SMELL. NO SMOKE WAS OBSERVED, THE POP SOUND SEEMED TO COME FROM CABIN AREA. T/S FOUND AFT (COCKPIT) ACM INOP. GAINED ACCESS TO ACM. REMOVED ACM AND INSTALLED A RSDR DXTA200702320Control Cable · stickingAFTER LANDING AND STRONG BREAKING, AIRCRAFT BRAKES FEEL LIKE THEY HAVE NOT RELEASED. BRAKES FINALLY RELEASED WHEN PEDALS WERE QUICKLY PUSHED AS HARD AS POSSIBLE AND THEN RELEASED. REMOVED AND REPLACED BOTH BRAKE CABLES WITH NEW IAW MM 32-42-02 GROUND OPS CHSDR DXTA200702319Air Data Module · intermittentMACH TRIM AND YAW DAMPER DISENGAGED ON TAKEOFF AT 70-75 KTS. (2) ATTEMPTED TAKEOFFS. (M2B) REPLACED NR 2 MADC DUE TO INTERMITENT SPLITS. IAW MM 34-12-00. IAW FAR 91.411 + 91-413. OLD P/N: 7014700-607, OLD S/N: 0316642. NEW P/N: 701-4700-607. NEW S/N: 9909SDR DXTA200702318Wheel · out of roundEXTREMELY NOTICABLE NOSEWHEEL SHIMMY DURING TAKEOFF ROLL BETWEEN 60-70 KNOTS. FOUND NOSE TIRES OUT OF ROUND REMOVED AND REPLACED NOSE WHEEL/ TIRE ASSY'S WITH AN O/H WHEEL AND NEW TIRE IAW MM 32-41-00.SDR DXTA200702317Coalescer Bag · dirtyON 5 MILE FINAL, STRONG BURNING ELECTRICAL SMELL IN COCKPIT, REMOVED BOTH COALESCER SOCKS P/N 746451-3 AND INSTALLED 2 NEW SOCKS P/N 746451-3.SDR DXTA200702315Acm · leakingSTRONG ODOR OF SOMETHING BURNING IN COCKPIT. REMOVED BOTH COALESCER SOCKS P/N 746451-3 AND INSTALLED 2 NEW SOCKS P/N 746451-3. REMOVED THE COCKPIT (AFT) ACM P/N 738384-33 S/N 9808193 AND INSTALLED A REPAIRED UNIT P/N 738384-33 S/N 200207059. PERFORMED AN OPSDR DXTA200702313Controller · malfunctionedAT FL450 LOST CABIN PRESSURE. CABIN CLIMB RATE +5500 FPM. AMBER CABIN ALT FO SAW CABIN AT 9500. INDICATED EMERGENCY DESCENT. DIVERTED INTO KNEW. CABIN OXYGEN MASKS USED. VISUALLY INSPECTED INSIDE TAIL COMPT FOR ANY LOOSE DUCTS, BLOWN DUCTS, LOOSE COUPLINGSDR DXTA200702312Acm · leakingEXTREME SULPHUR FUMES IN COCKPIT AND CABIN AT FL390, BOTH PACS IN NORM, BOTH TEMP SELECT IN AUTO, ENROUTE TIME 60 MINUTES. FUMES DISIPATED DURING DESCENT. DECLARED AN EMERGENCY. NORMAL APPROACH AND LANDING. REMOVED AND REPLACED AFT ACM IAW MM 21-51-00. OPSSDR DXTA200702310Wheel · out of balanceAPPROXIMATELY 70 KNTS, HAD STRONG NOSE WHEEL VIBRATION AND YD OFF LOWER CAS MESSAGE. ABORTED TAKEOFF AND MESSAGE DISAPPEARED. ONLY DEFECT NOTED WAS LOWER TORQUE LINK HARDWARE WAS VERY LOOSE, ALLOWING SOME PLAY IN LOWER LINK. RETIGHTENED HARDWARE IAW MM AND ISDR DXTA200702307Bungee · inoperativeLT RUDDER TRIM EXCESSIVE IN DIFFERENT PHASES OF FLIGHT. IN CLIMB OUT LT RUDDER TRIM INSIDE OF T ON TRIM INDICATOR, WITH AUTO PILOT ON AND DESCENDING THRU 20,500 AT 300 KTS, THE AIRPLANE SWERVED/SMALL JOLT AND IT IMMEDIATELY SHOWED MORE RUDDER TRIM REQUIRED. TSDR O2G2007F00002Relay · failedELECTRONIC FLIGHT DISPLAY NR1, NR2, AND NR3 DISPLAY RED (X). LEFT SIDE BEING POWERED BY BATTERY ONLY. LT BATTERY NOT CHARGING. REPLACED START LOGIC RELAY. (K)SDR DXTA200702305Position Sensor · out of adjustRUDDER OSCILLATED IN CRUISE FLIGHT (FL270 - 340KTS IAS) FOR APPROX 10 SECS FOLLOWED BY BLUE YD FAIL - B MSG FOLLOWED APPROX 20 SECS LATER BY YELLOW (YD FAIL - AB) MSG OSCILLATIONS. UPPER RUDDER POSITION SENSORS FOUND TO BE OUT OF ADJUSTMENT, AND RUDDER PEDAL SDR DXTA200702301Landing Gear · inoperativeNOSE GEAR FAILED TO RETRACT ON TAKEOFF, RED UNLOCK AND GREEN NOSE INDICATORS ILLUMINATED. [07-13-07] OPERATED GEAR OPERATIONALLY 30 CYCLES AND FOUND NO DEFECTS. REMOVED, REPLACED, OPS CK GOOD OF RENTAL ACTUATOR IAW 750MM 32-30-03.SDR DXTA200702299Sensor · malfunctionedWHEN THE POWER LEVERS ARE ADVANCED TO THE TAKEOFF POSITION AND THE AIRCRAFT BEGINS TO ACCELERATE THE NO TAKEOFF MESSAGE AND CHIMES COME ON. THE TAKEOFF WAS ABORTED. [07-13-07] THE NO TAKE OFF BOX ON THE NR 2 MFD WAS CHECKED BUT DISPLAYED NO MESSAGES . TAKE OSDR DXTA200702298Rudder · oscillatesRUDDER OSCILLATED IN CRUISE FLT AND THROUGHOUT DESCENT. YD FAIL UPPER B CAME ON DURING THE FLIGHT AND REMAINED ON, OSCILLATION STOPPED AFTER SLOWING BELOW 300KTS. [07-13-07] REMOVED AND REPLACED THE UPPER RUDDER CHANNEL B POSITION SENSOR. OPS CHECKED GOOD ISDR DXTA200702297Hydraulic System · failedDURING CRUISE AT FL480, THE B SIDE HYDRAULIC SYSTEM FAILED. AMBER CAS MESSAGE B PUMP FAIL, THE B QTY LOW, B PRESSURE DROPPED TO 0 PSI, QTY DROPPED TO 2 PERCENT, BTEMP AT 60 DEGREES. [07-13-07] FOUND RT ENGINE DRIVEN HYD PUMP FAILED INTERNALLY. REMOVED PUMSDR DXTA200702295A/C Pack · odorUPON LANDING, CABIN A/C PACK BEGAN PRODUCING AN OILY ODOR AND HAZE. [07-12-07] REMOVED AND REPLACED COCKPIT PAC. ACM LEAK CHECK AND OPS CHECK GOOD IAW CE750 M/M 21-51-00.SDR DXTA200702290Wheel · vibrationSEVERE NOSE WHEEL VIBRATION ABOVE 40 KNOTS ON TAKEOFF ROLL. ABORTED TAKEOFF. [07-12-07] REMOVED AND REPLACED LT AND RT NOSE TIRE ASSEBLIES WITH OVERHAULED ASSY. ALL WORK ACCOMPLISHED IAW CE-750 MM 32-41-02.SDR DXTA200702289Fuel Filter · bypassingLT FUEL FILTER BYPASS AMBER CAS MESSAGE AS POWER WAS APPLIED FOR TAKEOFF. [07-12-07] ACCOMPLISHED INSPECTION OF BYPASS INDICATORS IAW 3007C MM 73-30-00-200-801. REMOVED & REPLACED FUEL FILTER IAW SAME. LEAK CHECK GOOD. OPS CHECK GOOD.SDR DXTA200702287Unknown · unknownMASTER WARNING ILLUMINATED DURING TAKEOFF ROLL JUST ABOVE 80 KTS. [07-12-07] REPLACED LOWER YAW DAMP "B" ACTUATOR AND OPS CHECKED IAW 750 M/M 27-24-00.SDR DXTA200702283Unknown · unknownPCU MONITOR CB POPPED AND FLIGHT CONTROL FAULT EICAS MESSAGE APPEARED DESENDING THROUGH 6000 FT RUDDER FLT CONTROL SHUT OFF SW ALSO ILLUMINATED. [07-12-07] T/S TO BAD ELEVATOR OUTOBARD PCU ("B" SYS) REMOVED AND REPLACED PCU. PERFORMED RIG CHECKS. SYSTEM LEAKSDR DXTA200702281Handle · inoperativeAFTER TAKEOFF, THE LANDING GEAR HANDLE COULD NOT BE MOVED TO THE UP POSITION. [07-12-07] JACKED A/C FOUND NOSE STRUT DID NOT FULLY EXTEND. SERVICED STRUT PER 750 MM. CH. 12-10-38. GEAR HANDLE OPERATIONAL CHECK GOOD. GEAR SWING CLEARANCE CHECK GOOD.SDR DXTA200702277Unknown · unknownAIRCRAFT CONSTANTLY ROLLS LT AND RT IN LEVEL CRUISE. WORSE AT HIGHER ALTITUDE AND HIGHER SPEED. [07-11-07] RESET RT AILERON DROOP TO SPEC. AND ADJUSTED AILERON SERVO CABLES. IAW 750 MM. 22-10-01. ADJUSTED FEEL BUNGEE IAW 750 MM. 27-11-05. ADJUSTED UPPER RUDSDR DXTA200702269Unknown · vibrationABORTED TAKEOFF, DUE TO VERY BAD NOSE WHEEL VIRBRATION. KNOCKED OFF YAW DAMP AND FGC. [07-09-07] REMOVED AND REPLACED BOTH NOSE WHEEL ASSY'S DUE TO VIBRATION CHECKED BALANCE OF NEW WHEEL ASSY. COMPLIED WITH NETJETS NOSE GEAR SHIMMY LIST NO DEFECTS NOTED ALLSDR DXTA200702275Roll Servo · inoperativeDURING DESCENT FROM CRUISE AUTOPILOT ROCKS WINGS BACK AND FORTH BETWEEN FL410 AND FL360 WITH A/P DISCONNECTED AIRCRAFT FLIES LEVEL WITH NO ROLL. REMOVED AND REPLACED THE ALLERON SERVO MOTOR WITH A MODIFIED SERVO MOTOR IAW CESSNA CITATION 750 AMM 22-10-01. OPESDR DXTA200702267Unknown · unknownRUD LIMIT FAIL B CAS MESSAGE IN FLIGHT / RUDDER LIMITED TO 20 PERCENT. [07-09-07] REMOVED AND REPLACED LOWER RUDDER LIMITER ACTUATOR IAW CE-750 M/M 27-23-00. OPS CHECKED GOOD IAW CE-750 M/M 27-20-00.SDR DXTA200702265Unknown · warning lightPRIOR TO 80KTS (PRI STAB TRIM FAIL) AMBER CAS, CAUSED TO ABORT TAKEOFF. [07-09-07] PERFORMED OPS CHECK OF THE STAB TRIM SYTEM NO DEFECTS FOUND I/A/W CE750 M.M. CH 27-40.
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