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 DXTA200500915Pdu · inoperativeFLAPS FAIL IN FLIGHT, SLATS EXTENDED / FLAPS AT ZERO. ATTEMPTED RESET TO NO AVAIL, DIVERTED. TROUBLESHOT FLAPS WITH TEAM X. TO PDU. REMOVED AND REPLACED PDU WITH OVERHAULED PDU ASSY. RIGGED FLAPS, GOOD. OPS CHECK FLAPS GOOD IAW MM.SDR DXTA200500910A/C Pack · overtempLEFT PACK TEMP 120 DEGREES AND RISING UNCONTROLLABLE BOTH MANUAL OR AUTO FOLLOWED BY BLUE SMOKE IN THE COCKPIT COMING FROM AIR VENTS. ITEM IS UNDER INVESTIGATION.SDR DXTA200500909Wheel · vibratesDURING T/O ROLL, NOSE STRUT VIBRATES EXCESSIVELY. REMOVED AND REPLACED LT AND RT NOSE GEAR TIRE ASSYS IAW 750 MM 32-41-01.SDR DXTA200500913Autopilot Sys · malfunctionedARRIVING 180 KNOTS, AUTO-PILOT REPEATEDLY CAME OFF-LINE. ELEV FELT HEAVY ON CONTROLS. AT 140 KNOTS, PRIMARY TRIM WOULD NOT WORK. NO CAS MESSAGES RECEIVED EXCEPT WHEN SECONDARY TRIM ARMED. SECONDARY TRIM NOT ATTEMPTED. DOWNLOADED FAULT HISTORY FROM IAC NR 1&SDR DXTA200500905Actuator · failedRUDDER LIMIT FAIL A EICAS MESSAGE. CONTROL PAGE SHOWS 43 PERCENT RUD LIMIT. REMOVED UPPER RUDDER -A- LINEAR ACTUATOR DUE TO INTERNAL FAILURE. INSTALLED OVERHAULED UNIT. OPERATIONAL CHECK WAS GOOD. WORK WAS DONE IAW CE-750 MM 27-23-00.SDR DXTA200500897Coalescer Bag · contaminatedAPPROX 2 MINUTES AFTER THE APU WAS STARTED ON THE GROUND, THE COCKPIT AND CABIN BEGAN FILLING WITH ENVIROMENTAL TYPE SMOKE THE COCKPIT PAC WAS IN THE OFF POSTION AS REQUIRED BY THE MEL. THE CABIN PAC WAS ON AND THE ISOLATION VALVE WAS OPEN. THE COCKPIT SUPPLSDR DXTA200500890Brake · stickingWHILE TAXIING, DURING BRAKE TEST, THE LEFT MAIN BRAKES SEEMED TO BE STICKING, AN ABRUPT PULLING TO THE LEFT, COULD NOT HOLD A/C STRAIGHT EVEN WITH DIFFERENTIAL BRAKING . HYDRAULIC PRESSURE NORMAL.SDR DXTA200500888Slat · inoperativeGOT "FLAP FAIL" AMBER EICAS MESSAGE DURING APPROACH. FOLLOWED CHECKLIST BUT COULDN'T CLEAR. GOT SLATS AND NO FLAPS.SDR DXTA200500887Rudder · oscillatesUPPER RUDDER OSCILLATING FULL DEFLECTION WITH IN GREEN ARC AT HIGH SPEED LIMITS CHANGED FGC WITH NO CHANGE.SDR DXTA200500889Landing Gear · unsecureGEAR BUMP WAS EXPERIENCED NUMEROUS TIMES DURING CLIMB TO CRUISE ALTITUDE AND OCCASIONALLY ON DESCENT; NOT AT ALL DURING CRUISE FLIGHT. ACCOMPLISHED "GEAR BUMP" TROUBLESHOOTING IAW 750 TEAM X ENGINEERING CHECKLIST. NO DEFECTS NOTED. SERVICED NLG STRUT IAW CESDR DXTA200500885Computer · inoperativeTAKEOFF ABORTED FOR AMBER MESSAGE WITH CAUTION LIGHT, MACH TRIM INOP, YAW INOP, ALSO HAD CYAN FGC A INOP. PERFORMED OPS CHECKS ON BOTH FGC'S IAW PRIMUS 2000 INTEGRATED AVIONICS SYSTEMS TEST AND FAULT MANUAL, OPS CHECKS SERVICEABLE.SDR DXTA200500884Display · failedNR 1 DU DISPLAY FAILED INFLIGHT. SLIGHT SMELL OF ELECTRIC SHORT OCCURRED BUT DISAPPEARED AFTER DESELECTING NR 1 DU AS THE PFD DISPLAY. VERIFIED DU870 DEAD. REMOVED AND REPLACED NR 1 PFD AND OPS CHECKED FUNCTIONS NORMAL IAW CESSNA 750 MM CHAP 34-25-01.SDR DXTA200500881Wire Harness · inoperativeFUEL FILTER BYPASS LIGHT (R) ILLUMINATED ON T/O ROLL. LOW SPEED ABORT AT 40KTS. REMOVED AND REPLACED RT ENGINE HARNESS IAW RR 30007 MM 73-13-10. REMOVED PN 23051442 S/N OFF NX0466.SDR DXTA200500880Odor · detectedOILY SMELL COMING FROM COCKPIT PAC, MORE SO DURING DESCENT. IT GOT SO BAD, SHUT OFF THE COCKPIT PAC DURING DESCENT INTO SFO, AND THE SMELL WENT AWAY.SDR DXTA200500878Pin · shearedDURING TAXI, TILLER KNOB DEVELOPED SLACK WHEN TURNING THEN FINALLY POPPED AND ROTATES FREELY. UNABLE TO STEER THE AIRCRAFT WITH THE TILLER. ROLL PIN IN TILLER KNOB SHEARED OFF. INSTALLED NEW PIN, P/N MS16562-30. WORK DONE IAW CE-750 MM. CH. 32-50-00. OPS SDR DXTA200500875Filter · bypassingFUEL FILTER BYPASS LIGHT (R) ILLUMINATED ON T/O ROLL. LOW SPEED ABORT AT 40KTS.SDR DXTA200500877Yaw Damper · malfunctionedIN FLIGHT YAW DAMPER DOES NOT APPEAR TO OPERATE IN COORDINATION WITH FLIGHT CONTROLS. LAGS AND OVERCORRECTS. SEVERAL TIMES IN FLIGHT, BOTH ON AUTO-PILOT AND WHEN HAND FLOWN, YAW DAMPER APPEARS TO OPERATE UNCOMMANDED. OVERCOMPENSATING APPEARS WORSE ON B FGC.SDR DXTA200500866Windshield · failedDESCENDING THROUGH APPROXIMATELY 37000 FT WINDSHIELD HEAT INOP RT CAS MESSAGE ILLUMINATED SHORTLY AFTERWARDS A LAMINATE LAYER OF THE RIGHT WINDSHIELD SHATTERED. ITEM IS UNDER INVESTIGATION.SDR DXTA200500864Warning Light · illuminatedPRIMARY STAB TRIM FAIL CAS MESSAGE. ITEM IS UNDER INVESTIGATION.SDR DXTA200500865Hydraulic System · leakingWHILE WAITING FOR CLEARANCE FOR T/O, SMELLED A VERY BAD ODOR FOLLOWED BY THE HYD PRESS B LOW AND THE HYD PUMP B-SYSTEM FAIL, THEN THE RUDDER STANBY SYSTEM FAIL LIGHT. LEAKING APPEARED TO COMING FROM THE PYLON AREA. ITEM IS UNDER INVESTIGATION.SDR DXTA200500860Fitting · loose"RUD STBY SYS FAIL" CAS MESSAGE ILLUMINATED TWICE IN FLIGHT. RSS PRESSURE FLUCTUATED 2200 TO 3800 PSI. DUPLICATED SQK ON GROUND. FOUND RUDDER STANDBY ACCUMULATOR PRESSURE LOW SERVICED ACCUMULATOR IAW 750 MM CHAP 12-10-16. TIGHTENED LOOSE FITTING ON ACCUMULSDR DXTA200500861Handle · lockedGEAR WOULD NOT RETRACT AFTER T/O HANDLE LOCKED IN DOWN POSITION T/O INDICATORS ON N1 STAYED ON AFTER POWER REDUCTION THEY WERE WHITE. ITEM IS UNDER INVESTIGATION.SDR 2005FA0001097Union · looseHYD UNION WAS FOUND TO BE LOOSE ALLOWING O-RING TO FAIL OVER TIME. O-RING WAS REPLACED AND FITTING TORQUED. (K)SDR DXTA200500852Acm · seizedDURING TAXI IN AFTER OPERATIONAL CHECK FLIGHT, SMOKE AND ODOR NOTICED COMING THROUGH COCKPIT GASPERS. BY THE TIME AIRCRAFT WAS PARKED AND SHUTDOWN, SMOKE AND ODOR FILLED THE COCKPIT AND CABIN. ARFF CALLED TO THE SCENE. NO NOTICEABLE FIRE OR FLAMES. TROUBLSDR 2005FA0001257O-Ring · failedNAS1612-6, O-RING LOCATED ON AN814-6K, PLUG INSTALLED IN (A) HYDRAULIC SYSTEM MANIFOLD, PN 6717277-3 FAILED, CAUSING LOSS OF SYSTEM (A) HYDRAULIC FLUID AND SUBSEQUENT PILOT SHUTDOWN OF (A) HYDRAULIC SYSTEM. FOUND TORQUE ON PLUG TO BE LESS THAN 30 INCH POUNDS SDR DXTA200500841Battery Pack · intermittentEMERGENCY LIGHTING SYSTEM NOT WORKING PROPERLY. WITH SWITCH IN ARM, EXTERIOR LIGHTS ILLUMINATE AND BACK HALF OF CABIN LIGHTS ILLUMINATE. FOUND 5G SWITCH ACTIVATED. REPLACED AFT BATTERY PACK DUE TO SW BEING TO SENSITIVE. OPS OK IAW CE750 M/M 33-50-01.SDR DXTA200500849Position Sensor · faultyFLAPS FAIL CAS ILLUMINATED IN CRUISE AT FL450. FLAP INDICATOR CYCLED CONTINOUSLY FROM 0 DEGRRES TO 15 DEGREES INDICATION. FLAPS WERE NOT MOVING. FLAPS WON'T RESET. DUPLICATED DISCREPANCY. NO BITE CODES ON FLAP CONTROLLER. INSTALLED FLAP BREAK OUT BOX. TSDR DXTA200500842Warning Light · false indicationDURING CLIMB-OUT, HAD NOSE DOWN LIGHT NO GEAR UNSAFE LIGHT. THEN WENT OUT. DIVERT TO LAX. POSITIONED AIRCRAFT INTO HANGAR AND JACKED. HOOKED UP HYDRAULIC MULE AND SWING GEAR SEVERAL TIMES. NO FAULTS NOTED. OPERATIONAL CHECK OF GEAR INDICATIONS SATISFACTORYSDR DXTA200500836Bungee Cord · stiffAFTER DEPARTURE, FULL RUDDER TRIM TO LT REQUIRED IN ORDER TO KEEP ACFT COORDINATED. CLIMBING THRU FL 200 AT 250 KIAS, RUDDER KICKED BACK TO NORMAL. HAD TO TRIM RUDDER BACK TO CENTER. OPS CK OF RUDDER SYSTEM ON GROUND REVEALED NO DEFECTS. REMOVED ACCESS PANESDR DXTA200500828Actuator · failedRUDDER LIMIT FAIL -B- CAS MESSAGE ILLUMINATED DURING FLIGHT. RUDDER LIMIT WAS 28 PERCENT T/S TO BAD ACTUATOR REMOVED AND REPLACED LOWER RUDDER LIMIT ACTUATOR SYSTEM OP'S CHECKS SATISFACTORY AT THIS TIME. ALL WORK DONE IAW CE 750 M/M 27-23-00.SDR DXTA200500827Actuator · failedAMBER "RUB LIMIT FAIL B" CAS MESSAGE WITH A AMBER "RUDDER LIMIT 18%" MESSAGE IN EICAS CNTRL POSITION PAGE. EVENT MARKER PUSHED. COULD NOT DUP FLT CREWS DISCREPANCY ON ARRIVAL. RANG OUT WIRING FROM LOGIC MODULE TO LWR RUDDER LIMIT ACT WITH NO DISCREPANCYS FOUNSDR DXTA200500829Cooling Turbine · failedSMOKE BURNT OIL SMELL COMING FROM ENVIRONMENTAL SYSTEM. WORSE ON DESCENT. REMOVED AND REPLACED FAILED ACM TURBINE. OPERATIONAL CHECK GOOD IAW CE-750 M/M CH 21-51-00.SDR DXTA200500820Control Cable · out of adjustINFLIGHT, CLIMBING THROUGH 35,000 FT, 3 LOUD AUDIBLE THUMPS HEARD AND FELT EMITTNG FROM LT FORWARD NOSE COMPARTMENT. FOUND RT MAIN FREE FALL CABLE W/TENSION CAUSING RT MAIN GEAR HOOK TO BE UNSEATED IN EXTEND POSITION. READJUSTED RT MAIN GEAR FREEFALL TENSIONSDR DXTA200500838Uplock Switch · out of adjustAFTER TAKEOFF, LANDING GEAR FAILED TO RETRACT NORMALLY. UNLOCK LIGHT STAYED ILLUMINATED FOR ABOUT 2 MINUTES. FELT LIKE NOSE WHEEL WAS TRYING TO CYCLE UP. AFTER SEVERAL ATTEMPTS GEAR STOWED AND UNLOCK WENT OUT. PRIOR TO LANDING, GEAR EXTENDED NORMALLY. ADJSDR DXTA200500817Brake · malfunctionedDURING LANDING ROLLOUT BRAKES WERE SOFT AND FELT UNRESPONSIVE WHEN HARD BRAKING WAS APPLIED. ON TAXI IN BRAKES WERE CHECKED BY BOTH PILOTS AND BOTH PILOTS HAD THE SAME PROBLEM AT SLOW SPEEDS AS WELL. ITEM IS UNDER INVESTIGATION.SDR DXTA200500806Landing Gear · malfunctionedWHILE CLIMBING THRU 35,400 FT NOSE GEAR UNLOCK AND BUMP WAS FELT. ITEM IS UNDER INVESTIGATION.SDR DXTA200500834Actuator · failedRUD LIMIT FAIL B AMBER CAS MESSAGE IN CRUISE FLIGHT, FAILED AT 18%. INSTALLED OVERHAULED LWR RUDDER TRAVEL LIMITER ACTUATOR IAW 750 M/M 27-23-00, AND 27-20-00-720. OPS CHECK GOOD.SDR DXTA200500805Connector · contaminatedPRI STAB TRIM FAIL CAS MESSAGES IN FLT AT FL380, PRI STAB TRIM FAIL, A/P FAIL AND MACH TRIM OFF. CHECKED SYSTEM FOR PROPER OPERATION. COULD NOT DUPLICATE SQUAWK. REMOVED LT & RT HORIZONTAL STAB ACTUATOR ACCESS PANELS. FOUND WATER ON ALL CONNECTORS. CLEANESDR DXTA200500798Coalescer Bag · odorAFTER DEPARTING KBED AND RAISING THE LANDING GEAR, A STRONG SMELL OF SMOKE WAS SMELLED IN THE COCKPIT. NO SMOKE WAS PRESENT, BUT THE SMELL OF SMOKE CONTINUED UNTIL LANDING BACK AT KBED. RAN BOTH PACKS WITH APU, NR 1 AND 2 ENGINE. NO OIL SMELL NOTED. COCKPIT SDR DXTA200500796Strut · failedAFTER TO GEAR RETRACTION NORMAL, A FEW MINUTES LATER GEAR MOVEMENT TYPE NOISE HEARD WITH NO LIGHTS OR PARTIAL EXTENSION. NOISES FOLLOWED A FEW SECONDS LATER BY RED 'UNLOCK' LIGHT NO EXTENSION AND HYD PRESSURES AND QTY'S NORMAL THROUGHOUT FLIGHT. GEAR EXTENDSDR DXTA200500793Ground Wire · faultyDURING CLIMB AROUND FL270, OBSERVED AN AMBER "FLAPS FAIL" CAS MESSAGE. IT RESET/WENT OUT WHEN PRESSED THE FLAP RESET BUTTON. THIS HAPPENED 4 TIMES. ON APPROACH AND LANDING THE FLAPS OPERATED NORMALLY. FOUND FAULTY GROUND AT G7048-COMMON GROUND FOR RESOLVERSDR DXTA200500790Limit Switch · inoperativeAMBER TRIM SWITCH FAIL ILLUMINATED DURING CLIMB-OUT (FL180-FL200). TROUBLE SHOT AND FOUND FAULTY TRIM SWITCH ON PILOT CONTROL WHEEL. REMOVED & REPLACED SWITCH SWITCH OPS CHECKS GOOD IAW 750 M/M 27-40-00.SDR DXTA200500787Controller · inoperativeCABIN ALTITUDE AMBER EICAS MSG CAME ON AS WE CLIMBED THRU 12,000 FT CABIN ALTITUDE SHOWED 9000 FEET 1.4 DIFFERENTIAL AND RATE OF CLIMB OF 1000 FEET. LEVELED AT 14000 FEET AND SELECTED FULL HOT ON PAC TEMP SEL RATE OF CLIMB WENT TO ZERO AND CABIN STAYED AT 900SDR DXTA200500786Landing Gear · malfunctionedLANDING GEAR BUMP THROUGH 15,000 FT, NO UNLOCK LIGHT INDICATED. COULD NOT DUPLICATE PROBLEM ON GROUND. CARRIED OUT T/S. MADE ADJUSTMENTS TO R/S CLEAR UPLOCK SWITCH. MLG SYSTEM OPS CHECK GOOD. COMPLIED WITH GEAR BUMP TROUBLESHOOTING IAW CE 750 MM. INSTRUCTED SDR DXTA200500785Converter · malfunctioned"FLAPS FAIL" CAS MESSAGE DISPLAYED IN CRUISE AND RESET PER CHECKLIST WHEN FLAPS WERE DEPLOYED FROM 5-15 DEGREES, A MOMENTARY ROLL OCCURRED. FLAPS EXTENDED NORMALLY BEYOND 15 DEGREES. OPS CHECKED FLAPS WITH FLAP BREAKOUT BOX. TESTED AT DIFFERENT FLAP ANGLES WISDR DXTA200500784Controller · malfunctionedFLIGHT CONTROL FAULT CAS AND AILERON CONTROL LIGHT FLASHING. INSTALLED DMU . FOUND FORCE FIGHT BETWEEN PCU'S. ALL 4 TRANSDUCERS FUNCTION NORMALLY, ADJUSTED PCU'S. OPS CHECK NORMAL. WORK IAW CESSNA 750 MM CHAPT 27-10-01SDR DXTA200500799Dmu · malfunctionedAT CRUISE ALTITUDE, HEARD CLICK OR SNAP AND FELT ABRUPT JERK OF NOSE TO LT . RUDDER TRIM RAN AWAY WITH 50 PERCENT DEFLECTION AND STOPPED RETRIMMED RUDDER WITH NO FURTHER INCIDENT. CHECKED RUDDER CABLE TENSIONS AND DMU FOR A PCU FORCE FLIGHT. CONNECTED DMU ANSDR DXTA200500783Computer · malfunctionedNR 1 IAC FAILED IN FLIGHT, DU 1, 2, 3, RED X THROUGH SCREENS, NR 1 FMS INOP, NR 1 RMU STILL WORKS, NO HEADING BUG OR ALTITUDE SETTING CAPABILITY EITHER. REMOVED AND REPLACED HONEYWELL PRIMUS 2000 IC800 WITH A REPAIRED UNIT FROM HONEYWELL NR LV2R992K S/N ON : SDR DXTA200500782Manifold · failedON DESCENT TWO LOUD BANGS CAME FROM THE SAME AREA IN THE NOSE GEAR. - REMOVED LANDING GEAR CONTROL MANIFOLD DUE TO INTERNAL FAILURE. INSTALLED SERVICEABLE MANIFOLD IAW CE750 M/M CH 32-30-02. OPS CHECKED AND LEAK CHECKED GOOD. MANIFOLD WAS MODIFIED AND RETURNESDR DXTA200500777Trim System · frozenSTABILIZER TRIM JAMMED DURING FLIGHT AT -2.3 POSITION ON EICAS TRIM CLACKER WAS HEARD AT FIRST INTERMITTENTLY THEN ALMOST CONTINUOUSLY WHILE STAB REMAINED AT -2.3 POSITION. ONCE DESCENT WAS INITIATED STABILIZER UNFROZE AND SUDDEN PITCH CHANGE OCCURRED SOME SC
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