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 DXTA200400285Odor · detectedAT FL410 STRONG ODOR OF SMOKE IN CABIN AND THE COCKPIT, SMOKE WAS COMING FROM BEHIND THE CAPTAIN’S CIRCUIT BREAKER PANEL AND OUT THE DEFROST HOLES JUST BELOW THE LEFT SIDE WINDOW. DEPLOYED O2 MASKS AND LANDED SAFELY. INSPECTED THE FOLLOWING AREAS FOR SIGNS OFSDR UG82004F00002Smoke Detector · dirtyDURING DESCENT, BAGGAGE SMOKE LIGHT (EICAS) CAME ON. NO SMOKE OR FUMES DETECTED ON INSPECTION AFTER LANDING. BAGGAGE SMOKE DETECTOR FOUND TO BE VERY DIRTY. REMOVED SMOKE DETECTOR AND CLEANED COVER AND MOUNTING AREA. REINSTALLED AND PERFORMED FUNCTIONAL CHESDR GM0409Smoke Detector · dirtyBAGGAGE SMOKE LIGHT(EICAS) CAME ON. NO SMOKE OR FUMES DETECTED ON INSPECTION AFT LANDING. BAGGAGE SMOKE DETECTER FOUND TO BE VERY DIRTY. INITATED A FLEET INSPECTION AND CLEANING OF DETECTERS. REMOVED SMOKE DETECTER AND CLEANED ALSO CLEANED COVER AND MOUNTISDR DXTA200400281Warning Light · illuminatedDURING TAKE-OFF ROLL BELOW 80 KTS, NO TAKE-OFF CAS MESSAGE ILLUMINATED, MACH TRIM OFF, PRIMARY STAB TRIM FAILED, YAW DAMPER FAIL LOWER, YAW DAMPER NOT CENTERED, FGC A FAIL CAS MESSAGES ILLUMINATED. NOSE WHEEL SHIMMY VERY STRONG ALSO, ABORTED TAKE-OFF. PERFOSDR DXTA200400280Release Cable · damagedCLIMBING THROUGH FL250, CREW HEARD A LOUD THUMP FOLLOWED BY A LANDING GEAR UNLOCK LIGHT INDICATION. DURING DESCENT THROUGH 4000 FT, HEARD A THUMP FOLLOWED BY THE “UNLOCK” LIGHT GOING OUT. FOLLOWED CHECKLIST TO LOWER AND BLOW DOWN GEARS, HAD NORMAL GEAR INDICATSDR DXTA200400279Control Valve · leakingUPON GEAR EXTENSION HYDRAULIC FLUID LEVEL DROPPED BELOW 16 PERCENT, DIVERTED AIRCRAFT TO APA AND LANDED SAFELY. FOUND SLAT SPOOL VALVE LEAKING, REMOVED AND REPLACED VALVE, BLED A/B SYSTEM RESERVOIRS WITH (2) GALLONS OF SKYDROL EACH. LEAK CHECKED GOOD IAW THESDR DXTA200400278Pitot Tube · damagedON TAKEOFF ROLL WITH UPPER AND LOWER YAW DAMPERS AND MACH TRIM IN A-CONFIGURATION, THE LOWER YAW DAMPER FAILED BETWEEN 50 AND 70 KTS, AMBER "YD OFF LOWER" EICAS MESSAGE APPEARED. REPLACED PITOT LINE TO NR 1 ADC PER 750 MM CHAPTER 34-11-01 LEAK CHECK GOOD. COMSDR DXTA200400277Squat Switch · out of adjustAFTER TAKE OFF FROM BED AND ESTABLISHED A POSITIVE RATE OF CLIMB, SELECTED GEAR UP AND THE GREEN NOSE GEAR LIGHT REMAINED ILLUMINATED. PLACING GEAR SELECTOR TO THE EXTEND POSITION ALL THREE GREEN GEAR LIGHTS ILLUMINATED AND THE UNLOCKED LIGHTS EXTINGUISHED. THSDR DXTA200400272Downlock Switch · inoperativeWHEN GEAR HANDLE WAS PUT IN DOWN POSITION 3 GREEN AND RED GEAR UNSAFE LIGHT ILLUMINATED. RECYCLED GEAR HANDLE AND CONDITION WAS THE SAME PER EMERGENCY CHECK LIST, GEAR HORN CAME ON WITH FULL FLAPS. DIVERTED TO SWF AND LANDED SAFELY. VISUALLY INSPECTED THE RTSDR CA040323006Roll Pin · damaged(CAN) DURING MX, FOUND 1 ROLL PIN LOOSE AND ONE ROLL PIN MISSING ON THE LT OUTPUT SECTOR OF THE ROLL SPOILER MIXER UNIT. - STILL HAD ISSUES WITH RIGGING AND REMOVED AND OPENED UP THE SPOILER MIXER UNIT. FOUND ANOTHER ROLL PIN MISSING AND ONE LOOSE ON THE L/H OSDR DXTA200400262Warning Light · illuminatedDURING TAKEOFF ROLL MASTER WARNING AND NO TAKEOFF CAS MESSAGE CAME ON AT APPROX 90 KNOTS, ABORTED TAKEOFF. ITEM IS UNDER INVESTIGATION.SDR CNQD20040001Window · crackedTHE COCKPIT LEFT SIDE WINDOW OUTER PLY SHATTERED ON CLIMB OUT FROM LAX. THE CREW DEPRESSURIZED THE AIRCRAFT AND DIVERTED TO LGB.SDR 2004F00333Hose · leakingDURING WALK-AROUND AFTER PARKIGN CREW NOTICED HYDRAULIC FLUID ON TAIL AND MADE WRITE UP ON SHUT DOWN AT LAS HYDRAULIC FLUID WAS POURING OUT OF THE LEFT ELEVATOR HINGE POINT CLOSEST TO THE VERTICAL STAB. MAINTENANCE FOUND ELEVATOR ACTUATOR HOSE HAD BEEN RUBBEDSDR DXTA200400246Hydraulic System · leakingSHORTLY AFTER TAKEOFF OBSERVED AMBER HYDRAULIC SYSTEM-A LOW QUANTITY CAS MESSAGE, DISCOVER A-SYSTEM DECREASING IN QUANTITY. UNLOADED A-HYDRAULIC PUMP, HYDRAULIC QUANTITY DECREASED TO -0- AND ELECTED TO LAND IMMEDIATELY. DURING DESCENT PTU FAILED, NOTICED STRSDR 2004F00165Limiter · damagedCREW REPORTED A 'FAILED RUDDER LIMITER B' MESSAGE ON THE CAS. THE LOWER RUDDER LIMITER LINEAR ACTUATOR B-CHANNEL, FAILED AT 25 PERCENT. REPLACED RUDDER LIMITER ACTUATOR 'B' IAW CHAPTER 27-23-00 OF CESSNA MM, OPERAITON CHECK GOOD OK FOR SERVICE. (M)SDR 2004F00166Actuator · inoperative'RUDDER LIMIT FAIL B' CAS MESSAGE ILLUMINATED IN FLIGHT. AIRCRAFT LANDED WITH NO FURTHER DISCREPANCIES. LINEAR ACTUATOR OF LOWER RUDDER LIMITER 'B' FAILED AT 16 PERCENT. REPLACED LOEWR RUDDER LIMITER ACTUATOR ASSEMBLY AND PERFORMED APPROPRIATE RIGGING PROCESDR DXTA200400239Filter · bypassingON TAKEOFF ROLL THE FUEL FILTER BYPASS L AMBER MESSAGE ILLUMINATED, REJECTED TAKEOFF. REMOVED AND REPLACED FUEL FILTER AND O-RING, RAN ENGINE FOR OPS CHECK AND LEAK CHECK. ALL WORK DONE IAW ROLLS ROYCE AE3007C MM CHAPTER 73-30-00.SDR DXTA200400237Warning Light · illuminatedON TAKEOFF ROLL MASTER WARNING LIGHT AND AUDIO INDICATIONS APPEARED WITH NO OTHER CAS INDICATIONS. WARNINGS WENT OFF AFTER 1 CYCLE THEN REAPPEARED WITH NR 2 ENGINE ITT EXCEEDANCE. ITT EXCEEDANCE INDICATION LASTED 2 SECONDS. DOWNLOADED ALLISON TRENDS AND EICASDR 02Roll Pin · shearedSTEERING TILLER DOES NOT STEER NOSE WHEEL.SDR 2004F00088Actuator · inoperativeBLUE YAW DAMPER, FAIL LOWER 'B' CAS MESSAGE, AMBER YAW DAMPER OFF LOWER CAS MESSAGE AND PRI STAB TRIM FAIL AND MACH TRIM OFF CAS MESSAGE CAME ON DURING FLIGHT. CHANNEL 'B' YAW DAMP ACTUATOR FAILED TO OPERATE. REPLACED CHANNEL 'B' YAW DAMP ACTUATOR. OPERATIOSDR 2004F00157Pump · failed'FUEL BOOST ON' AMBER CAS MESSAGE CAME ON IMMEDIATELY AFTER LANDING. LEFT ENGINE FUEL BOOST PUMP FAILURE. REMOVED FAULTY PUMP AND INSTALLED NEW SERVICEABLE UNIT. PERFORMED RUN-UP LEAK CHECK PER CESSNA MM. AIRCRAFT RETURNED TO SERVICE. (M)SDR DXTA200400235Control Handle · malfunctionedAFTER TAKEOFF GEAR HANDLE STUCK IN THE DOWN POSITION, COULD NOT RETRACT GEARS, ACCOMPLISHED AIR TURNBACK. TROUBLESHOT NOSE GEAR SQUAT SWITCH, ALL WIRING CHECKED GOOD. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE, AIRCRAFT REQUIRES OCF FOR LANDING GEAR COSDR DXTA200400227Wire Harness · disconnectedDURING THE TAKEOFF ROLL, A NO TAKEOFF MESSAGE APPEARED. ABORTED TAKEOFF, A-PITCH ROLL DISCONNECT MESSAGE CAME ON, ONCE CLEAR OF THE RUNWAY ALL SYSTEMS CHECKED NORMAL. GAINED ACCESS TO PITCH/ROLL DISCONNECT, FOUND DATA LOADER HARNESS INTERFERING BY PITCH/ROLLSDR DXTA200400225Acm · odorCOCKPIT TEMP SELECTOR CANNOT CONTROL TEMP IN EITHER MANUAL OR AUTO MODE, COCKPIT TEMP (SUPPLY) REMAINS AT APPROX 140 DEGREES DURING FLIGHT. TEN MINUTES AFTER LANDING SUPPLY TEMP ROSE TO APPROX 235 DEGREES ACCOMPANIED BY STRONG ODOR, SIMILAR TO AN OVERHEATED OSDR DXTA200400222Proximity Switch · out of adjustON GEAR RETRACTION THE THREE GREEN LIGHTS WENT OUT, UNLOCK LIGHT STAYED ON AT 195 KNOTS, VIBRATION IN YOKE AND AN INCREASE IN NOISE. CYCLED GEAR WITH SAME RESULT. RIGGED NLG UPLOCK SWITCH AND ADJUSTED ROUTING OF NLG STEERING HOSES. PERFORMED LANDING GEAR OPSDR UG8AGM0414Fuel Tank · leakingWING TANK (0) FILL ON AND VENTING FUEL FOR 3 MIN. 3400 LBS. FUEL. CREW REMINDED OF SL750-28-02 LETTER IN ALL AIRCRAFT LOG BOOKS REGARDING THIS CONDITION AND WHAT STEPS ARE NEEDED TO CORRECT THIS CONDITION. NO ACTION TAKEN. CONDITION IS NORMAL REGARDING THE SDR DXTA200300209Wheel · out of balanceON TAKEOFF ROLL AT 80 KNOTS FELT STRONG VIBRATION AT THE NOSE GEAR AREA, ABORTED TAKEOFF. REMOVED AND REPLACED BOTH NOSE WHEEL ASSEMBLIES DUE TO OUT OF BALANCE. OPS CHECK GOOD, WORK DONE IAW 750 MAINTENANCE MANUAL CHAPTER 32-41-00.SDR DXTA200300207Strut · dischargedAFTER TAKE-OFF ATTEMPTED TO RETRACT GEARS AND FOUND LANDING GEAR HANDLE WOULD NOT GO UP. ACCOMPLISHED AIR TURN BACK. FOUND NOSE STRUT NITROGEN PRESSURE LOW, NOT ALLOWING STRUT TO FULLY EXTEND TO MAKE SQUAT SWITCH. SERVICED NOSE STRUT AS REQUIRED IAW CESSNA SDR DXTA200300206Bleed Valve · failedDURING TAXI OUT ENGINE (FAILED L) RED CAS MESSAGE ILLUMINATED. LT ENGINE ROLL BACK FROM IDLE AND HAD UNCOMMANDED SHUTDOWN. REMOVED & REPLACED ENGINE BLEED VALVE IAW ALLISON/ROLLS-ROYCE MM CHAPTER 75-31-15, GROUND RUNS & OPS CHECKS GOOD.SDR DXTA200300199Tire · failedON LANDING AT TXKF BOTH MAIN TIRES BLEW DAMAGING HARDWARE ON STRUT, GEAR DOOR AND FLAP TRACK FAIRINGS. ITEM IS UNDER INVESTIGATION.SDR DXTA200300180Pitot Line · malfunctionedON TAKEOFF ROLL AMBER CAS MESSAGE CAME ON FOR YAW-DAMPER AND FADEC FAILURE. ABORTED TAKEOFF. TROUBLESHOT AND PURGED OUT BOTH PITOT SYSTEMS, RAN AIRSPEED TO BOTH ADC’'S TO COMPARE AIRSPEED AS REQUIRED AFTER PURGING LINES. CARRIED OUT ENGINE RUNS AND NO FAULTSDR DXTA200300177Bulb · malfunctionedAFTER GEAR RETRACTION UNLOCK LIGHT STAYS ON. GEAR EXTENDS NORMALLY WITH NORMAL INDICATIONS, PILOT STATED, EN ROUTE TO HOU FROM DAL. DIVERTED INTO SAT AS A PRECAUTION. THERE WERE NO PASSENGERS ON BOARD AND NO EMERGENCY ACTION TAKEN. REMOVED 1 INOP BULB AND SDR DXTA200300174Control Module · failedUPON DESCENT INTO SMO CREW OBSERVED THE GEAR UNLOCK LIGHT ILLUMINATED AND A DISTINCTIVE SOUND FROM NOSE GEAR AREA. THIS OCCURRED AT FL 26, FL 20 AND FL 11.5. REMOVED AND REPLACED INOP LANDING GEAR CONTROL MANIFOLD. PERFORMED OPERATIONAL AND LEAK CHECK IAW CESDR DXTA200300171Acm · failedDURING DESCENT HAD SMOKE IN COCKPIT TURNED OFF LEFT CABIN PAC AND SMOKE CLEARED, LANDED SAFELY AT GSO. TROUBLESHOT AND FOUND FAULTY COCKPIT ACM TURBINE, REMOVED AND REPLACED ACM, SYSTEM OPS CHECKED GOOD IAW CESSNA 750 MM CHAPTER 21-51-00.SDR DXTA200300165Pitot Tube · obstructedON TAKEOFF ROLL AT 70 KTS THE FOLLOWING EICAS MESSAGES APPEARED: YD OFF LOWER, MACH TRIM OFF, FGC ADC MISCOM, ABORTED TAKEOFF. DURING VISUAL INSPECTION NOTED A BLOCKAGE IN THE RT PITOT TUBE, PURGED RT PITOT LINE AND PITOT TUBE, NOTED MUD LIKE SUBSTANCE WAS RSDR DXTA200300160Landing Gear · malfunctionedON APPROACH AFTER GEAR EXTENDED, GOT THREE GREEN AND THEN RED UNSAFE LIGHT ILLUMINATED. BLEW GEAR DOWN BY PNEUMATIC BOTTLE. ITEM IS UNDER INVESTIGATION.SDR DXTA200300156Float · stuckAFTER TAKEOFF, AMBER CAS MESSAGE WING O FULL RT ILLUMINATED. FUEL CAN BE VISUALLY SEEN DUMPING OUT OF RIGHT WING FROM VICINITY OF SURGE TANK VENT. FUEL IMBALANCE BECAME EVIDENT AT A RATE OF APPROX 100 LBS PER MIN. PRESSURIZED RIGHT WING, FOUND NO LEAKS IN DSDR DXTA200300152Engine · flamed outDURING TAKE-OFF LT ENGINE CHIP DETECTOR AMBER CAS MESSAGE CAME ON. ABORTED TAKE-OFF. REMOVED AND REPLACED LEFT HAND ENGINE IAW CESSNA 750 MAINTENANCE MANUAL CHAPTER 71-00-03.SDR 2003FA0001137Warning Light · illuminatedWHILE AT CRUISE ALTITUDE, THE CREW NOTED BAGGAGE DOOR SEAL ON LIGHT. CREW BEGAN MAKING PREPARATIONS TO DESCEND TO A LOWER ALTITUDE AS REQUIRED BY AFM INSTRUCTIONS WHEN THE LIGHT (BAGGAGE DOOR SEAL) WENT OUT. INFORMED MFG TECH SUPPORT. WAITING RESOLVE.SDR DXTA200300148Audio Video Unit · failedWHILE ON GROUND AT ASE PRIOR TO BOARDING PASSENGERS, CREW NOTICED SMOKE COMING OUT FROM THE AFT CLOSET AREA, CREW DISCHARGED FIRE BOTTLE INTO AREA. TROUBLESHOT AND FOUND AIRSHOW SYSTEM INOPERATIVE AND AUDIO VIDEO AMP BREAKER POPPED, INSPECTED MONITORS AND FOUSDR DXTA200300147Spacer · missingAFTER TAKE-OFF DURING GEAR RETRACTION ONLY THE LEFT MAIN RETRACTED, AN ATTEMPT WAS MADE TO CYCLE THE GEAR AND WHEN HANDLE WAS PUT IN THE DOWN POSITION THREE GREEN AND NO RED INDICATION NOTED, FOLLOWING GEAR HANDLE COULD NOT BE MOVED TO THE UP POSITION. JACKEDSDR DXTA200300139O-Ring · leakingLT HYDRAULIC QUANTITY DROPPED TO ZERO 10 MINUTES AFTER TAKE-OFF. (A) SYSTEM UNLOADED, GEAR BLOW DOWN AND EMERGENCY BRAKE SYSTEMS ACTUATED. ACCOMPLISHED AIR TURN BACK TO CMH. - FOUND PLUG O-RING ON HYDRAULIC MANIFOLD LEAKING. REMOVED AND REPLACED O-RING, LEAK SDR CNQ2003F00002Controller · shortedWHILE DESCENDING THROUGH FL330, THE COCKPIT TEMPERATURE CIRCUIT BREAKER TRIPPED. COCKPIT DISPLAY UNITS NR 1 AND NR 2 WENT INOPERATIVE. UPON FURTHER DESCENT, COCKPIT DISPLAY UNITS NR 4 AND NR 5 WENT INOPERATIVE. ALL DISPLAY UNITS WORKED OK AFTER COOLING OFFSDR DXTA200300131Controller · failedWHILE CLIMBING THROUGH FL330 THE COCKPIT TEMP CIRCUIT BREAKER POPPED, COCKPIT AIR-CONDITIONING PAC WOULD NOT STOP BLOWING HOT AIR. EICAS WARNING “DU-HOT” ILLUMINATED, AFTER LOSING DU 1 & 2 ELECTED TO DIVERT INTO LBL. DURING DESCENT INTO LBL STARTED LOSING DU 4SDR DXTA200300127Bolt · failedCLIMBING THROUGH FL360 THE NLG ATTEMPTED TO EXTEND & RETRACT ITSELF REPEATEDLY. GEAR UNSAFE RED LIGHT CAME ON & OFF EACH TIME, BLEW GEAR DOWN PNEUMATICALLY ON APPROACH. PERFORMED VISUAL INSPECTION TO EMERGENCY GEAR EXTENSION SYSTEM IAW CE 750 MM FOR A ONE TIMESDR DXTA200300126Valve · malfunctionedWHILE IN LEVEL CRUISE FLIGHT AT 29,000 FT THE (WING TANK O'FULL L-R) AMBER CAS MESSAGE ILLUMINATED. BOTH WING TANKS OBSERVED TO BE DUMPING FUEL FOR 2 MINUTES. - TROUBLESHOT AND FOUND BOTH WING VENT VALVES INOP. REMOVED AND REPLACED LEFT AND RIGHT WING VENT VSDR DXTA200300122Bungee Cylinder · loosePITCH VIBRATION IN FLIGHT CONTROLS WITH AUTO PILOT ON, VIBRATION INCREASED AS SPEED INCREASED. NOTICED AT 250 KTS AND 10000FT, VIBRATION ALSO COULD BE HEARD AS LOW FREQUENCY SOUND. TIGHTENED LT ELEVATOR BUNGEE AND ADJUSTED ELEVATOR CABLE TENSION IAW CESSNA 75SDR DXTA200300118Warning Light · illuminatedAT FL 340 CREW HEARD THE NOSE GEAR EXTEND AND OBSERVED THE GEAR UNLOCK LIGHT ILLUMINATED, UPON WHICH IT RETRACTED BACK AND INDICATIONS WENT OUT. ITEM IS UNDER INVESTIGATION.SDR DXTA200300117Filter · cloggedFUEL FILTER BYPASS L CAS MESSAGE CAME ON ABOUT 5 SECONDS AFTER TAKEOFF POWER APPLIED. TAKEOFF ABORTED. INSTALLED NEW FUEL FILTER & RESET BYPASS INDICATOR IAW AE3007C MM CHAPTER 73-30-00, LEAK AND OPS CHECKED GOOD.SDR DXTA200300116Bleed Valve · malfunctionedUPON CLEARED FOR TAKEOFF, ADVANCED THROTTLES AND THE RED CAS MESSAGE, ENGINE FAIL R APPEARED. ENGINE AUTO SHUTDOWN. EXCEEDS PAGE SHOWED IT WAS TRIGGERED BY R ITT 1020 DEGREES COMPARED TO LEFT ITT OF 644 DEGREES. BORESCOPED COMBUSTION SECTION & TURBINE ASSEM
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