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 DXTA200300114Warning Light · illuminatedDURING TAKE OFF "YAW DAMPER LOWER-OFF" CAS MESSAGE CAME ON, ABORTED TAKE OFF. - PURGED OUT PITOT TUBES FOR WATER AND DEBRIS, COMPLIED WITH YAW DAMPER OPS CHECK AND PITOT STATIC SYSTEM LEAK CHECK IAW CESSNA 750 MM CHAPTER 27-24-00 & 27-20-00 AND FAR 91.411.SDR DXTA200300113Window Post · chafedWHILE PERFORMING MAINTENANCE NEAR PILOT'S SIDE WINDOW, NOTICED WINDSHIELD CENTER POST HAS CHAFE DAMAGE, FURTHER EVALUATION SHOWED DAMAGE MEASURED APPROX. .375 INCH LONG BY .100 INCH WIDE AND APPROX. .028 DEEP. THE THICKNESS OF THE POST IS .062 INCH. - ITEM IS SDR DXTA200300111Torque Link · wornAFTER TAKE OFF FROM SWF FOR PHL, LANGING GEAR WOULD NOT RETRACT, ACCOMPLISHED AIT TURN BACK TO SWF. - INSPECTED GEAR & FOUND THE NOSE GEAR TORQUE LINK CAM BOLT HOLE ELONGATED & WORN. REPLACE NOSE GEAR TORQUE LINK CAM WITH NEW PER THE CE 750 MM CHAPTER 32-20-02SDR DXTA200300110Clamp · leakingWHILE IN CRUISE AT FL290 THE "WING O'FULL L" CAS MESSAGE CAME ON. ABOUT 30 SECONDS LATER WE GOT THE SAME MESSAGE FOR THE RIGHT WING, FUEL WAS NOTED TO BE DUMPING OUT OF BOTH WINGS. AFTER WE SHUT OFF THE CENTER TANK TRANSFER SWITCHES IT TOOK ABOUT A MINUTE FOSDR DXTA200300107Control Unit · inoperativeAMBER (FLAPS FAIL) CAS MESSAGE ILLUMINATED IN FLIGHT WOULD NOT RESET. FLAPS WOULD NOT EXTEND, SLATS OPERATED NORMALLY, DIVERTED INTO JFK AND LANDED SAFELY.SDR DXTA200300106Manifold · damagedDESCENDING THRU FL180 AN UNCOMMANDED EXTENSION OF GEAR WAS EXPERIENCED (GEAR DID NOT FULLY EXTEND) GOT UNLOCKED LIGHT THEN GEAR RETRACTED. - TROUBLESHOT AND FOUND HYDRAULIC MANIFOLD DOES NOT HOLD PRESSURE. REMOVED AND REPLACED LANDING GEAR HYDRAULIC MANIFOLD ASDR DXTA200300104Circuit Breaker · trippedDURING CLIMB THRU 7000 FEET " REMOTE CB TRIPPED" CYAN CAS MESSAGE ILLUMINATED AND ELECTRICAL FIRE SMELL WAS NOTED IN COCKPIT, NO SMOKE SEEN IN AIRCRAFT. FOUND PASSENGER SAFETY SIGN ON ESCAPE HATCH SHORTED. REMOVED AND REPLACED PASSENGER SAFETY SIGN WITH NEW SDR DXTA200300103Controller · failedDURING DESCENT AT APPROX 13000 FT, (FGC A FAIL) MESSAGE ON EICAS, FOLLOWED SHORTLY AFTER BY SMOKE ODOR AND (TRIM SW FAIL L) ON EICAS. EVENT BUTTON WAS CYCLED. TROUBLESHOT AND FOUND THE F/O’S FLIGHT GUIDANCE CONTROLLER GC-810 FAILED. REMOVED AND REPLACED F/O CSDR DXTA200300099Valve · stuckUPON APPROACH TO LNK, WITH GEAR HANDLE SELECTED DOWN MAIN GEARS EXTENDED, NO GREEN NOSE GEAR INDICATION. COMPLIED WITH CE-750 CHECKLIST AFTER TOWER FLY BY-VISUALLY CONFIRMED DOWN, USED BLOW DOWN SYSTEM AS PER CHECKLIST, LANDING UNEVENTFUL. TROUBLESHOT AND FOUSDR DXTA200300094Bungee Cylinder · out of adjustAILERON CONTROL BINDING WORSE TO THE RIGHT, TAKES EXCESSIVE RIGHT WING DOWN TRIM AT HIGH SPEEDS. - ADJUSTED LT PCU ACTUATOR INPUT BUNGEE TO ELIMINATE FORCE FIGHT CONDITION. PERFORMED ADJUSTMENT IAW MFG 750 MM CHAPTER 27-10-00, OPS CHECKED GOOD.SDR DXTA200300089Actuator · malfunctionedDURING FLIGHT FROM VNY TO HPN THE RUDDER LIMIT FAIL "A" WARNING LIGHT ILLUMINATED. ACCOMPLISHED AIR TURN BACK TO VNY AND LANDED OVERWEIGHT. REMOVED AND REPLACED UPPER RUDDER LIMITER ACTUATOR WITH A REPAIRED UNIT. OPS CHECKED GOOD, WORK DONE IAW CESSNA 750 MMSDR DXTA200300084Actuator · failedWHEN LANDING GEAR WAS RETRACTED ON TAKEOFF ALL THREE GEAR GREEN LIGHTS EXTINGUISHED BUT RED UNLOCK LIGHT REMAINED ON, GEAR WAS CYCLED , ALL INDICATIONS NORMAL. - TROUBLESHOT AND FOUND NLG ACTUATOR FAILED, REPLACED NOSE LANDING GEAR ACTUATOR IAW CE750 M/M CHAPTSDR DXTA200300082Warning Light · illuminated"WING TANK O' FULL -R" MESSAGE CAME ON AT CRUISE . RT TANK SHOWED APPROX 3100 LBS , LT WING APPROX 200 LBS . TOTAL QUANTITY DECREASED APPROX 300 LBS IN LESS THAN A MINUTE. FUEL OBSERVED DUMPING FROM RIGHT WING OUTBOARD VENT, VENTING STOPPED DURING DECENT. POWSDR 2003F00531Block · defectiveON ROLL OUT, CREW GOT AN FGC A/B FAIL AMGER EICAS MESSAGE. CHECKED ASSOCIATED WIRING AND CONNECTORS. REPLACED BOTH TERMINATING RESISTOR BLOCK. TEST FLEW A/C OPERATIONAL CHECK GOOD. (M)SDR DXTA200300069Downlock Switch · inoperativeRIGHT MAIN LANDING GEAR INDICATION REMAINED GREEN AFTER GEAR WAS RETRACTED, USED EMERGENCY BLOW DOWN GEAR. LANDING WAS UNEVENTFUL. DETERMINED THE RIGHT GEAR ACTUATOR DOWNLOCK SWITCH WAS FAULTY, REMOVED AND REPLACED WITH NEW SWITCH, PERFORMED GEAR OPERATIONSDR DXTA200300068Hydraulic System · leakingIN CRUISE AT FL 410 HYDRAULIC VOLUME LOW CAS MESSAGE ILLUMINATED ON THE A-HYD SYSTEM, VOLUME SHOWED 16 PERCENT. INITIATED EMERGENCY CHECKLIST AND UNLOADED THE A-HYD PUMP, USED THE EMERGENCY BLOWDOWN SYSTEM TO LOWER THE GEAR. GOOD BRAKES AND STEERING AFTER LASDR DXTA200300065Vent Line · out of positionWING TANK "FULL R AMBER CAS" MESSAGE ILLUMINATED IN CRUISE FLIGHT 10 MINS AFTER LEVELING AT FL 290. FUEL GAUGES SHOWED 2460LB BOTH SIDES. VISUAL INSPECTION IN AIR SHOWED FUEL VENTING OUT OF RIGHT WING. INSPECTED INBOARD AND OUTBOARD TRANSFER FLOAT VALVES, SDR DXTA200300058Wheel · inoperativeNOSE WHEEL BEGAN SHAKING VIOLENTLY PASSING THROUGH 60 KNOTS DURING TAKEOFF ROLL. REPLACED LT & RT NOSE TIRE & WHEEL ASSY IAW 750 M/M 32-41-01.SDR DXTA200300054Strut · contaminatedGEAR UNLOCK LIGHT WOULD NOT EXTINGUISH RECYCLED ONCE AND IT STILL DID NOT GO OUT. FOUND PARTICLES IN NLG STRUT FLUID. REMOVED AND REPLACED UPPER & LOWER NLG BARREL ASSY. LANDING GEAR FUNCTIONAL TEST NORMAL, WORK IAW CE-750 MM CHAPTER 32-20-02.SDR DXTA200300055Acm · seizedAT TEB DURING GROUND OPS OF APU NORMAL APU BLEED SELECTED WITH NORMAL APU EGT TEMPS, ISOLATION VALVE OPEN, PILOTS NOTED GRINDING NOISE. ACM SEIZED CAUSING CABIN TO FILL WITH SMOKE. REMOVED SEIZED FORWARD ACM AND INSTALLED OVERHAULED UNIT, OPS & LEAK CHECK GOSDR CA030703004Wire Harness · shorted(CAN) RT WINDSHIELD HEAT INOPERATIVE ON ENGINE INDICIATING AND CREW ALERT SYSTEM POPPED. SB HK062 AC POWER TO RT WINDSHIELD. WIRE BUNDLE PQ020 AND JE004 TOUCHING AND HEAT SHRINK FAILURE CAUSING SB HK 062 TO POP.REPLACED HEAT SHRINK PROBLEM ELIMINATED.SDR DXTA200300052Pitot Tube · contaminatedYAW DAMPER & MACH TRIM DISENGAGED DURING TAKEOFF ROLL, ABORTED TAKEOFF. FOUND WATER SITTING IN RT PITOT TUBE. REMOVED RT PITOT TUBE AND CLEANED AND REINSTALLED PITOT TUBE, PERFORMED OPERATIONAL CHECK OF AIR DATA SYSTEMS AND YAW DAMPENER SYSTEMS IAW HONEYWELLSDR 2003F00511Starter · failedRIGHT ENGINE REPORTED AS SMOKING BY TOWER AND OTHER AIRCRAFT DURING TAXI OUT. RIGHT ENGIEN STARTER FAILED TO DISENGAGE AFTER START. STARTER WAS REPLACED, SERVICED AND OPERATIONALLY CHECKED. RIGHT ENGINE STARTER CHECK GOOD PER CESSNA CITATION X MM AND THE AISDR 2003F00425Actuator · inoperativeTAKING OFF FROM CLT, CREW GOT A CYAN FGC FAIL MESSAGE. THE FGC B REVERTED AUTOMATICALLY, IN AN ATTEMPT TO CHANGE FGC SOURCE BACK, GOT THE SAME MESSAGE. LANDED AT GSO. (M)SDR DXTA200300048Uplock Switch · out of rigGEAR UNLOCK LIGHT WOULD NOT EXTINGUISH AFTER GEAR RETRACTION FOR SEVERAL MINUTES. RIGGED LANDING GEAR UPLOCK SWITCHES IAW THE CESSNA CITATION 750 M/M CH 32-30-05. FUNCTIONAL TEST OF LANDING GEAR SYSTEM REVEALED NO DEFECT PER CESSNA MM CH 32-00-01.SDR 2003F00392Transfer Valve · failedRT TANK O'FILL, VENTED FUEL OPERATED IAW CESNA LETTER QTY WAS LESS THAN 32000 LBS. A FUEL TRANSFER CHECK WAS PERFORMED BY MAINTENANCE PER CESSNA MM. NO DEFECTS FOUND, SYSTEM FUNCTIONED NORMALLY. (M)SDR DXT2003F00000Manifold · shortedAFTER TAKEOFF LANDING GEAR FAILED TO RETRACT AND OPENED LEFT MLG BREAKER. RSETTING BREAKER OPEN AGAIN. EMERGENCY GEAR BLOW-DOWN INITIATED AND LANDED AT AIRPORT HANGER. OPERATIONAL CHECK CONFIRMED DISCREPANCY. FOUND SHORTED SOLENOID IN GEAR CONTROL MODULE. SDR DXTA200300043Squat Switch · failedAFTER TAKEOFF LANDING GEAR FAILED TO RETRACK, GEAR HANDLE WOULD NOT MOVE. ACCOMPLISHED AIR TURNBACK TO SAN AND LANDED SAFELY. REMOVED AND REPLACED NOSE LANDING SQUAT SWITCH DUE TO INTERNAL FAILURE. OPERATIONAL CHECKED GOOD, WORK DONE IAW 750 MM CHAPTER 32-6SDR DXTA200300042Manifold · failedLANDING GEAR WOULD NOT RETRACK UPON RETRACTION, LT GEAR C/B POPPED, RESET ONCE TRIED ONE TIME, GEAR WOULD NOT RETRACT. USED GEAR BLOW DOWN BOTTLE TO ENSURE DOWN AND LOCKED. REMOVED AND REPLACED LANDING GEAR CONTROL MANIFOLD IAW 750 M/M 32-30-02, OPS AND LEAKSDR 2003F00391Computer · failed'A' CHANNEL OF FGC (FLIGHT GUIDANCE COMPUTER) FAILED DURING FLIGHT. 'A' CHANNEL OF FGC TRIPPED OFF LINE. FLIGHT CREW WAS ABLE TO RESET SYSTEM. IMT WAS INTERROGATED AND NO FAULTS WERE FOUND. PERFORMED OPERATIONAL CHECK PER HONEYWELL MM. SYSTEM SELF TEST OKSDR 2003F00393Latch · unsecureNOSE DOOR OPEN R, CAS MESSAGE ILLUMINATED AFTER TAKEOFF. INSPECTED RIGHT NOSE DOOR AND FOUND LATCH OPEN. INSPECTED LATCH AND TEE BOLT FOR DEFECTS AND FOUND NONE. RELATCHED DOOR IAW PROCEDURES OUTLINED IN CESSNA MM. CAS MESSAGE EXTINGUISHED AND AIRCRAFT WASSDR DXTA200300040Resolver · inoperativeFLAPS FAIL AMBER CAS MESSAGE ILLUMINATED AND FLAPS INDICATOR JUMPED FROM 0-35 DEGREES IN LEVEL CRUISE FLIGHT ABOVE 250 KIAS ON 3 DIFFERENT OCCASIONS. - INSPECTED AND FOUND RESOLVER GROUND (GT048) LOOSE. TIGHTENED GROUND TERMINAL.SDR DXTA200300037O-Ring · failedON LANDING ROLL, HAD A COMPLETE LOSS OF SYSTEM HYD FLUID AND EMERGENCY BRAKE WAS USED, AIRCRAFT HYDROPLANED BUT STOPPED SAFELY, NO VISIBLE DAMAGE TO AIRCRAFT. REPLACED ORING PLUG, ON "A" HYDRAULIC MANIFOLD, AND OPERATIONALLY TESTED, BLED SYSTEM AND LEAK CHECKSDR 2003F00359Limiter · failedDURING PILOT'S PREFLIGHT, WITH APU RUNNING, THE 'RUDDER LIMIT FAIL' RED CAS MESSAGE ANNUNCIATED. ANOTHER AIRCRAT WAS UTILIZED FOR THE TRIP. THE RUDDER LIMITER FAILED TO ACTUATE DUE TO A FAULT IN THE ELECTRICAL COMPONENTS OF THE SYSTEM. AIRCRAFT WAS DE-POWERSDR 2003F00290Indicator · malfunctionedATTITUDE AND HEADING STUCK IN THE TEST MODE. NR 1 AHRS HAD FAILED. REPLCED NR 1 AHRS AND OPERATION WAS NORMAL. (M)SDR 2003F00294Computer · failedDURING FLIGHT, Y/D FAILED, AUTOPILOT DISENGAGED, AND FGC 'A' AND FGC 'B' FAILED. AIRCRAFT CONTINUED ON TO DESTINATION AS SCHEDULED. NR 1 IAC (INTEGRATED AVIONICS COMPUTER) FAILED. REPLACED THE NR 1 IAC AND OPERATION WAS NORMAL. (M)SDR DXTA200300022Landing Gear · vibrationREJECTED TAKEOFF DUE TO SEVERE NOSE WHEEL SHIMMY.SDR DXTA200300021Warning Light · illuminatedON TAKEOFF MASTER CAUTION LIGHT CAME ON FOR FGC B-CHANNEL FAIL, ABORTED TAKEOFF.SDR DXTA200300019Controller · malfunctionedJUST AFTER STARTING A DESCENT FROM FL 410 CABIN RAPIDLY OVERPRESSURIZED . PRESSURE WENT TO BELOW ZERO AND CABIN DPSI WAS RIGHT AT REDLINE. DUE TO RATE AND PRESSURE, CHOSE TO CABIN DUMP. AS A RESULT OXYGEN MASKS DEPLOYED. OPS CHECKED PRESSURISATION SYSTEM OSDR 2003F00300Tire · deflatedDEPARTING DENVER THE NO TAKEOFF WARNING ANNUNCIATED AND THE TAKEOFF WAS ABORTED. THE RIGHT LANDING GEAR WHEELS, BOTH INBOARD AND OUTBOARD, DEFLATED AFTER TAXI IN DUE OT HEAT BUILD UP CAUSED BY HEAVY BRAKING. MAINTENANCE CREW DISPATCHED FROM AACI MAIN BASE AT SDR 2003F00315Switch · brokenDURING TAXI TO TAKEOFF, THE NO TAKEOFF CAUTION APPEARED ON THE EICAS. SIMULTANEOUSLY, THE PARK BRAKE PRESS LOW MESSAGE WAS ILLUMINATED. THE CREW TAXIED BACK TO GM BASE AND ANOTHER AIRCRAFT WAS UTILIZED FOR THE FLIGHT. UPON TROUBLESHOOTING, THE PARK BRAKE SWSDR 2003F00313Switch · brokenDURING TAXI TO TAKEOFF, THE NO TAKEOFF CAUTION APPEARED ON THE EICAS. SIMULATNEOUSLY, THE PARK BRAKE PRESS LOW MESSAGE WAS ILLUMINATED. THE CREW TAXIED BACK TO GM BASE AND ANOTHER AIRCRAFT WAS UTILIZED FOR THE FLIGHT. UPON TROUBLESHOOTING, THE PARK BRAKE SWSDR DXTA200300016Landing Gear · failedAFTER TAKE OFF GEAR WOULD NOT RETRACT. - SERVICED NOSE STRUT AND PERFORMED GEAR SWING, SYSTEM OPS CHECKED GOOD.SDR 2003F00230Transmitter · inoperativeUPPER RUDDER A-B FAILED TWICE. ABLE TO RESET TO B-CHANNEL. REPLACED UPPER RUDDER POSITION TRANSMITTERS. RIGGED AND TESTED PER CESSNA MM. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR DXTA200300005Windshield · crackedDURING FLIGHT AT 31,000 FT THE RIGHT WINDSHIELD CRACKED.SDR 2003F00232Regulator Valve · malfunctionedON APPLICATION OF TAKEOFF POWER, AMBER EICAS MESSAGE 'HP DUCT 'O' PRESS R' CAME ON. ABORTED TAKEOFF. RIGHT HIGH PRESSURE REGULATING VALVE FAILED TO REGULATE PROPER BLEED AIR PRESSURE. REPLACED RIGHT HP BLEED AIR REGULATOR VALVE. OPERATION NORMAL. (M)SDR 2003FA0000212Hose · deterioratedAT 19,000 FT, NOSE GEAR TRIED TO EXTEND. HYDRAULIC PRESSURE SLAMMED GEAR BACK UP. WITHIN 30 SECONDS HYDRAULIC QUANITY ON "A" SYSTEM RESERVOIR STARTED DROPPING. AIRCRAFT WAS SLOWED AND NORMAL GEAR EXTENSION WAS MADE. HYDRAULIC QUANITY ON A SYSTEM RESERVOIR WENSDR 2003F00227Bearing · seizedMAIN CABIN DOOR IS HARD TO OPEN FROM THE INSIDE. REPLACED AFT CABLE ASSEMBLY, SPRING PIVOT BEARINGS ANDLONG SHAFT. RIGGED THE DOOR PER CESSNA MM. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR 2003F00217Battery Pack · failedEXIT LIGHT OVER EMERGENCY EXIT INOPERATIVE ON BATTERY. REPLACED AFT EMERGENCY LIGHT BATTERY PACK. OPERATIONAL TEST IN GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR 2003F00214Throttle · stuckAFTER LANDING AT CYYZ, THE RIGHT THROTTLE THRUST REVERSER LEVER WOULD NOT STOW. LEVER STUCK IN THE UP POSITION. ADJUSTED RIGHT THRUST REVERSER LEVER DETENT IAW CESSNA CITATION 750 MM. OPERATIONAL CHECK OF RIGHT THRUST REVERSER, THRUST REVERSER LEVER AND RIG
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