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 DXTA200501057Line · undertorquedDURING THE T/R CHECK, WHILE TAXIING THE RIGHT ENGINE FAILED. CHECKED CABLE FOR SHIM, NONE FOUND. CHECKED ALL BLEED CONTROL LINES FOR PROPER TORQUE. REPLACED A+B FADECS IAW RR AE3007C M/M 76-12-00. REPLACED FPMU IAW AE3007C M/M 73-21-00. FOUND TWO FUEL NOZSDR DXTA200501080Relay · failedTRAILING EDGE FLAPS DID NOT DEPLOY FOR LANDING -FLAPS FAIL- WOULD NOT RESET. NO FLAP EMERGENCY LANDING, CHECKLIST USED WITH NO FUTHER EVENTS. REPLACED KZ092 FLAPS POWER RELAY WITH NEW RELAY AND TIGTHENED ALL OTHER TERMINALS IN J-BOX. REINSTALLED FLAP J-BOXSDR 2006FA0000263Wire Harness · disconnectedDURING THE CONDUCT OF THE RECURRING INSPECTION REQUIRED BY AD2005-09-01 AND PHASE 30, THE WIRING BUNDLE FOR THE APU FIRE BOTTLE WAS FOUND WRAPPED AROUND THE APU FUEL TUBE JUST FORWARD OF THE FIRE BOTTLE. THIS WIRE BUNDLE HAS BOTH AN ACTIVATION CIRCUIT (NORMALSDR DXTA200501044Warning System · false activationDURING TAKEOFF ROLL AT APPROXIMATLEY 50 KNOTS, RECEIVED AMBER CAS MESSAGE HP DUCT OVERPRESSURE. TAKEOFF WAS ABORTED. CAS MESSAGE WENT AWAY WHEN POWER WAS REDUCED ON ABORT. RAN ENGS TO MAX POWER N2 OF THE DAY (86 PERCENT) FOR 10 MIN W/ NO DEFECTS. PULLED POSDR DXTA200501043Landing Gear · malfunctionedDURING CLIMB THROUGH FL 250-350 NOSE GEAR THUMPS, NO UNLOCK LIGHT NOTICED. ITEM IS UNDER INVESTIGATION.SDR DXTA200501038Float Valve · failedIN FLIGHT ,WING TANK OFULL R AMBER CAS MESSAGE ILLUMINATED AT FL290 SHORTLY AFTER LEVELING OFF. THE APPROPIATE CHECKLIST WAS COMPLETED FUEL VENTED OUT OF R WING FOR 3 MINUTES (LOST 150 LBS).THEN MESSAGE WENT OUT 2 MINUTES LATER (TOTAL FUEL 4900 LBS/L TANK 235SDR O2G2005F00013Pdu · failedDURING CLIMBOUT OF SDL, WHILE RETRACTING FLAPS THEY FAILED AT 13 PERCENT AND WOULD NOT RESET. REPLACED FLAP PDU AND SOFT START RELAY. (K)SDR 2005FA0001522Hinge Bracket · corrodedDURING RECENT INSPECTION CORRODED HARDWARE WAS FOUND ON AILERON. AFTER AILERON WAS REMOVED HEAVY GALLING WAS FOUND ON OUTBOARD HINGE SUPPORT AND AILERON FITTING. SEVERAL OTHER AIRCRAFT WERE INSPECTED AND 3 OTHERS AND IDENTICAL GALLING. MFG WAS NOTIFIED AND SDR DXTA200501036Link · crackedDURING REMOVAL OF MLG ASSY, EXCESS MOISTURE CAME OUT OF RT OB AXLE WHEN REMOVING HUBCAP ASSY. TRAILING LINK ASSY HAS VISIBLE CRACK APPROX 10 INCHES IN LENGTH, ON TOP SIDE OF TRAILING LINK, CTRD BETWEEN MLG RETRACT ACTUATOR ATTACH LUGS. BORESCOPE INSP FOUND CSDR DXTA200501035Position Switch · out of adjustNOSE GEAR RELEASED FROM LOCK IN FLIGHT CLIMBING THROUGH FL 280 AND FL 320 AND DESCENDING THROUGH FL 230. GEAR DID NOT EXTEND, NOR DID NOT OBSERVE THE GEAR UNLOCK LIGHT. PERFORMED GEAR BUMP TROUBLESHOOTING IAW CESSNA 750 MM 32-30-00. FOUND NOSE GEAR UPLOCK SSDR DXTA200501034Acm · failedSTRONG ODOR LIKE OIL BURNING COMING FROM PACKS IRRITATING EYES AND SHORTNESS OF BREATHING. REMOVED COCKPIT ACM/COMP TURBO. CLEANED SECONDARY HEAT EXCHANGER. INSTALLED ACM/COMP. TURBO OVERHAULED BY HAMILTON SUNDSTRAND CRS SI3R842L IAW CESSNA 750 M/M CHAP 21SDR DXTA200501047Strut · dirtyDURING FLIGHT GEAR RETRACTS HEARD AND FELT BUMP IN THE NIGHT FOUR (4) TIMES DURING FLIGHT. MEASURED EXTENSION OF NOSE STRUT, MEASURED 9.80 INCHES DISASSEMBLED AND CLEANED LOWER BARREL ASSEMBLY. RESEALED AND REASSEMBLED. MEASUREMENT NOW 9.75 INCHES IAW MM. SDR DXTA200501029Warning Light · illuminatedWHILE DESCENDING TO LAND, WITH NO FLAPS OR SLATS EXTENDED, RECEIVED AN AMBER FLAP FAIL MESSAGE ALONG WITH THE FLAPS INDICATING FLAPS 15 DEGREES WHEN UP. FOLLOWED EMERGENCY CHECKLIST. LANDED WITH SLATS EXTENDED ONLY. COULDN'T RETRACT AFTER LANDING. ITEM IS SDR DXTA200501028Yaw Damper · malfunctionedABORTED T/O IN TEB DUE TO EXCESSIVE VIBRATION DURING T/O AND YAW DAMPER OFF LOWER CAS MESSAGE. ITEM IS UNDER INVESTIGATION.SDR DXTA200501026Float Valve · leakingWING TANK OVERFILL "R" CAS MESSAGE ILLUMINATED INFLIGHT AND VENTED ABOUT 300LBS. OF FUEL IN ABOUT A MINUTE. THE RIGHT TANK CONTINUED TO VENT FUEL INTERMITTENTLY DURING DESCENT AND STILL VENTED FUEL WITH 2900LBS. - TROUBLESHOT SYSTEM, DEFUELED A/C AND FOUND (1SDR DXTA200501022Odor · detectedREMOTE CB TRIPPED CYAN CAS MESSAGE CAME ON DURING DESCENT. BURNING ODOR WAS NOTICED FOR ABOUT 30 -45 SEC. ITEM IS UNDER INVESTIGATION.SDR DXTA200501020Warning Light · illuminatedAFTER TAKEOFF, GREEN NOSE WHEEL DOWN INDICATOR LIGHT REMAINING ON. NO RED UNLOCK INDICATOR, AND NO AUDIBLE GEAR OR GEAR DOOR NOISE. GEAR EXTENDED NORMALLY, NORMAL LANDING. ITEM IS UNDER INVESTIGATION.SDR DXTA200501011Landing Gear · noisyBANG CAN BE FELT AND HEARD FROM NOSE AREA DURING FLIGHT ABOUT EVERY 10 MINS IN CLIMB & DESCENT EVERY 15-20 IN CRUISE. REQUIRING TEST FLIGHT OCF FOR FURTHER EVALUATION. PERFORMED GEAR SWING MULTIPLE TIMES AND COULD NOT DUPLICATE PROBELM. CONFIRMED THE GEAR BSDR CNQ2005F00000Line · chafedFLEXIBLE HYDRAULIC HOSE CHAFED THROUGH ALLOWING HYDRAULIC FLUID TO BE LOST IN THE (B-SYSTEM). HOSE WAS CONTACTING LT ELEVATOR POWER CONTROL UNIT. REPLACED HOSE AND VERIFIED ROUTING UNIT. REPLACED HOSE AND VERIFIED ROUTING TO PREVENT CHAFING. MFG IS ISSUINGSDR DXTA200501001Hose · chafedAFTER TAKEOFF, LOST ALL HYDRAULIC FLUID ON THE -B- SYSTEM WITH ASSOCIATED HYD PRESS LOW -B- AND HYD FLUID LOW -B- AMBER CAS MESSAGES. AFTER LANDING, COULD SEE FLUID DRIPPING DOWN FROM THE TAIL. REMOVED LEFT ELEVATOR OUTBOARD PCU HOSE ASSEMBLY DUE TO BEING CHSDR DXTA200500995Landing Gear · vibrationLANDING GEAR BUMP OCCURS REPEATEDLY DURING CLIMB. PERFORMED GEAR BUMP TROUBLESHOOTING CHECKLIST IAW 750 MM 32-30-00. ALL CHECKS GOOD. PERFORMED NUMEROUS GEAR SWINGS, FAST AND SLOW. COULD NOT DUPLICATE DISCREPANCY. NO PREVIOUS HISTORY OF SQUAWK. OPS CHECKSDR DXTA200500994Bleed Valve · failedON INITIAL POWER UP FOR TAXI, RIGHT ENGINE MADE A LARGE THUMP AND SHUT ITSELF DOWN. REMOVED UPPER, LOWER BLEED AIR VALVES & ACCELERATION BLEED VALVE. INSTALLED NEW VALVES. OPS CKED GOOD. WORK DONE IAW ROLLS ROYCE AE3007C MM CH 75-31-10 & 75-31-15.SDR DXTA200500993Manifold · faultyWHILE IN FLIGHT AT 43000 FT, THERE WAS A BANG OR NOISE WITH VIBRATIONS FELT THROUGH THE FLOOR. IT APPEARED TO BE FROM THE NOSE COMPARTMENT, POSSIBLY THE NOSE GEAR. REMOVED AND REPLACED GEAR MANIFOLD IAW CE750 M/M CHAPTER 32-30-02. SYSTEM OPS CHECK GOOD.SDR DXTA200500989Acm · faultyAFTER LANDING AT TEB, CABIN FILLED WITH SMOKE. OVERHEAD GASPERS ON RIGHT SIDE, TOO HOT TO TOUCH. TAILCONE COMPARTMENT SHOWED FORWARD PAC OIL BOWL BLACK WITH FOAM INSULATION WAS LOOSE ON LEFT SIDE. HEAT FROM OVERHEAD TOILET AREA EXTREMLY HOT. REMOVED AND RESDR DXTA200500986Pcu · bindingDURING ALL PHASES OF FLIGHT, AIRCRAFT HAD EXTREME RIGHT ROLL REQUIRED ABNORMAL LEFT AILERON TRIM WITH AUTO PILOT ENGAGED RETRIM L WING DOWN CAS MESSAGE ILLUMINATED WHICH REQURED MORE LEFT AILERON TRIM TO EXTINGUISH MESSAGE. TESTED AND FOUND TRIM SYSTEM BINDINSDR DXTA200500983Limit Switch · out of adjustNOSE GEAR MAKES CLUNKING SOUND DURING CRUISE FLIGHT. APPROXIMATELY EVERY 15 MINUTES IT SOUNDS LIKE NOSE GEAR IS BEING RETRACTED. ADJUSTED NOSE GEAR UPLOCK CABLE IAW 750 MM 32-30-06. ADJUSTED NOSE GEAR UPLOCK SWITCH IAW 750 MM 32-30-05, NOSE GEAR OPS CK GOODSDR DXTA200500979Smoke · detectedAFTER ENGINES WERE STARTED, THE COCKPIT FILLED UP W/ SMOKE. SHUTDOWN ENGINES AND APU AND EVACUATED AIRCRAFT, NO PAX ONBOARD.SDR DXTA200500974Wheel · looseTAKEOFF ABORTED UNDER 80 KTS DUE TO SEVERE VIBRATION FROM NOSEWHEEL. INSPECTED BOTH NOSE WHEELS AND TIRES, FOUND LEFT WHEEL LOOSE. REMOVED BOTH WHEELS, CHECKED BALANCE, BALANCE CHECKS GOOD. REINSTALLED BOTH NOSE WHEELS AND RETORQUED WHEELS. INSPECTED WHEELSDR DXTA200500972Acm · unserviceableUNABLE TO CONTROL TEMP RISE FOR CABIN PACK. SMOKE ENTERED CABIN ON LEFT SIDE OF CABIN AND TAIL CONE AREA SMELLED LIKE SOMETHING HAD BEEN BURNING. ACM WOULD NOT TURN. REMOVED AND INSTALLED AN OVERHAULED ACM. OPS AND LEAK CHECKS GOOD AT THIS TIME ALL WORK DOSDR DXTA200500971Acm · failedWHILE DESCENDING OUT OF 410, HEARD A LOUD BANG AND SMELLED SMOKE. THE SMOKE CLEARED, UNABLE TO CONTROL COCKPIT TEMP. SUSPECT COCKPIT ACM BROKEN. ITEM IS UNDER INVESTIGATION.SDR DXTA200500970Rudder · malfunctionedUPON CLIMBOUT THROUGH 7000 FT THE RUDDER NEEDED MORE AND MORE TRIM TO REMAIN CENTERED. CONTINUED TO ADD LEFT RUDDER TRIM UNTIL THE HALF WAY POINT. IT TOOK MORE RUDDER TRIM AND WOULD NOT CENTER. THE RUDDER THEN VIOLENTLY SWUNG BACK THE OTHER DIRECTION. OPERSDR DXTA200500961Pitot System · warning lightAMBER 'P/S-RAT HEAT OFF' CAS MESSAGE ILLUMINATED DURING TAKEOFF ROLL. T/O ABORTED. SWITCHES WERE IN THE ON POSITION THE ENTIRE TIME. CHECKED FOR MESSAGE ON MAINTENANCE PAGE 60TLS, CHECKED CONNECTION ON LT/RT P/S SWITCHES S1030 AND S1063. SHOOK DOWN ALL ACSDR DXTA200500960Acm · failedABOUT 1 HOUR INTO OUR FLIGHT AT FL410, DETECTED AN ODOR IN THE COCKPIT THAT SMELLED ELECTRICAL IN NATURE. SYSTEMS WERE OPERATING NORMALLY AND THE SMELL DISSIPATED AFTER ABOUT 5 MINUTES THEN AFTER LANDING WITH THE APU RUNNING, DETECTED THE SAME SMELL. THE A/CSDR DXTA200500959Handle · dirtyFLAPS FAILED AT 15 DEGREES. FLAPS FAILED AT 15 DEGREES HAD BITES NR 2 AND NR 6 ON CONTROLER REMOVED FLAP HANDLE, REMOVED COVER AND CLEANED LINT FROM INSIDE HANDLE IAW: CE750 M/M 27-50-00. FLAPS OPERATIONALY CHECK GOOD.SDR DXTA200500956Unknown · unknownAT FL400 IN CRUISE A LOUD THUMP WAS HEARD AND FELT IN THE NOSE AREA. ITEM IS UNDER INVESTIGATION.SDR DXTA200500955Actuator · failedAT FL 320 AND .88 MACH THE UPPER RUDDER YD STARTED BOUNCING OFF THE LEFT SIDE OF THE RUDDER LIMITER WITH THE UPPER YD IN THE B-CHANNEL, IT WOULD NOT HAPPEN ON THE A-CHANNEL. AT SPEED & ALTITUDE THE RUDDER HAD TO BE TRIMMED TO THE LEFT EXCESSIVELY. REMOVED UPSDR DXTA200500949Acm · stiffNOTICED A PUNGENT SUFFER ODOR IN THE COCKPIT WHILE AT FL410 IN CRUISE POWER, ODOR SEEMS TO COME AND GO. ACCOMPLISHED AN EMERGENCY DESCENT AND LANDING W/O FURTHER INCIDENT. FOUND COCKPIT ACM VERY STIFF TO TURN. REPLACED ACM IAW 750 MAINTENANCE MANUAL CHPT 21SDR DXTA200500950Brake Assy · malfunctionedBRAKE PEDALS ON LEFT AND RIGHT GO ALL THE WAY TO THE STOPS WHEN PRESSURE IS APPLIED, BRAKES FELT SPONGEY. PERFORMED VISUAL INSPECTION OF BRAKES, NO DEFECTS NOTED. PERFORMED BLEEDING PROCEDURES, PERFORMED POWER BRAKE PRESSURE CHECK, PRESSURE CHECKS NORMAL. PSDR DXTA200500939Controller · faultyAMBER FLAPS FAIL CAS MESSAGE ON FLAP EXTENSION FROM 15-35 DEGREES. RESET AND THEN WORKED NORMAL FOR SECOND APPROACH. FOUND BITE 3 SHOWING ON CONTROLLER. TROUBLESHOT SYSTEM TO A FAULTY CONTROLLER. REMOVED AND REPLACED W/REPAIRED UNIT. OPERATIONAL CHECK NORSDR DXTA200500942Striker · out of adjustDURING T/O ROLL AMBER EICAS MSG. BAGGAGE DOOR SEAL AND MASTER CAUTION ILLUMINATED BEFORE 80 KIAS. ABORTED T/O. ADJUSTED BAGGAGE DOOR SEAL SWITCH AND STRIKER PLATE DUE TO BAGGAGE DOOR SEAL CAS MESSAGE ON T/O ROLL. SYSTEM OPS CHECKED GOOD IAW CE-750 MM CH 52SDR DXTA200500941Ground Stud · looseEMERGENCY RETURN DUE TO NUMEROUS FAILURES & CAS MESSAGES. IRS 2 FAULT/ FOLLOWED BY SUSPECTED IAC 2 FAILURE. FMS 2, RMU 2, DU 4 & DU 5 FAILED. AMBER CAS MESSAGES ASSOCIATED WITH IAC 2 FAILURE. CAS MESSAGES FADEC REV ADC L, FADEC FAULT LB, PRI-STAB TRIM FAISDR DXTA200500940Actuator · malfunctionedLOWER YAW DAMP DISENGAGED TWICE DURING TAKEOFF ATTEMPTS. PERFORMED TEST OF LINEAR ACTUATORS FOR YAW DAMP SYSTEM IAW CESSNA 750 MM 27-24-00. OPS CHECK NORMAL. NO MESSAGES.SDR DXTA200500931Acm · inoperativeIN FLIGHT HEARD A LOUD POP IN THE CABIN FOLLOWED BY AN ELECTRICAL BURNING ODOR, ALSO IN THE CABIN SHEDDING THE CABIN ELECTRICAL LOAD WITH THE INTERIOR MASTER TO THE OFF POSITION TOOK CARE OF THIS ISSUE INTERIOR MASTER WAS LEFT OFF. REMOVED AND REPLACED FWD AISDR DXTA200500926Line · leakingEXCESSIVE BRAKE PEDAL PRESSURE NEEDED ON LANDING ROLL OUT. REQUIRED LARGER THAN NORMAL INPUT TO STOP AIRCRAFT. THIS WAS A DRY RUNWAY NOT CONTAMINATED. PERFORMED VISUAL INSPECTION OF BRAKES AND PLUMBING. PERFORMED POWER BRAKE BLEEDING IAW CITATION 750 MM CHSDR DXTA200500927Sensor · malfunctionedON DESCENT, PYLON BLEED LEAK, ILLUMINATED EMERGENCY PROCEDURES COMPLETED, WARNING LIGHT EXTINGUISHED WHEN IDLE, BUT CAME BACK ON WHEN POWER WAS ADDED. REMOVED PANEL 412DB TO GAIN ACCESS TO SENSOR TT018 AND TT020 VISUALLY INSPECTED BOTH SENSORS, NO DEFECTS NOTSDR UG82005F00007Sensor · intermittentHYDRAULIC SYSTEM, A TEMPERATURE FLUCTUATED BETWEEN 80-130 DEGREES C WITH SMALL VARIATION IN PRESSURE. UNLOADED A HYDRAULIC SYSTEM AND TEMPERATURE DECREASED TO 90 DEGREES C BUT CLIMBED TO 119 DEGREES AT SHUTDOWN ON THE RAMP. REPLACED DEFECTIVE TEMPERATURE SENSDR DXTA200500922Flap System · malfunctionedWHEN FLAPS SELECTED TO FIVE, FLAP FAIL CAS MESSAGE APPEARED. FOLLOWED CHECKLIST, ATTEMPTED RESET, FLAPS FALLEN AGAIN IN THE FLAP FIVE POSITION.SDR DXTA200500923Odor · detectedDURING CRUISE AT FL 400, A VERY STRONG ACRID BURNING ODOR WAS DETECTED BY CREW AND PAX. PRECAUTIONARY LANDING MADE. STRONG ODOR ON GROUND WAS AROUND BAGGAGE AND HELL HOLE AREA. NO VISABLE SMOKE.SDR DXTA200500920Landing Gear · malfunctionedCLIMBING THROUGH APPROX FL270, THE LANDING GEAR UNLOCK LIGHT BEGAN CYCLING ON AND OFF ACCOMPANIED BY THE LANDING GEAR SLAMMING INTO THE UP AND LOCKED POSTION CONTINUOUSLY 1 TO 2 TIMES PER SECOND BEGAN A DESENT AND THE CYCLING STOPPED AT APPROX FL200 WHEN LOW ESDR DXTA200500918Downlock Switch · faultyON GEAR RETRACTION GREEN LT MAIN GEAR DOWN LIGHT REMAINED ILLUMINATED. GEAR APPEARED FULLY RETRACTED. GEAR EXTENDED NORMALLY FOR LANDING. REMOVED FAULTY DOWN LOCK SWITCH FROM LT POSITION. INSTALLED NEW SWITCH. OPS CHECKS GOOD IAW CESSNA 750 MM 32-30-04.
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