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 = '200' 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 = '200' 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 CA070514036Engine · noisy(CAN) IN CRUISE THE ENGINE EMITTED A NOISE ACCOMPANIED BY VIBRATION, A FADEC FAULT INDICATION AND FIRE WARNING INDICATION. THE ENGINE WAS SHUTDOWN IN FLIGHT. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514036)SDR DXTA200702039Landing Gear · malfunctionedRT MAIN LANDING GEAR WOULD NOT RETRACT. HAD RED UNSAFE EICAS INDICATION. CONFIRMED DISCREPANCY. TROUBLESHOT AND DISCOVERED CONNECTOR 44G1J TO HAVE AMPLE AMOUNT OF WATER IN IT. CLEANED AND DRIED CONNECTOR AND RECONNECTED. SWUNG GEAR THROUGH SEVERAL CYCLES WITHSDR DXTA200702024Dcu · inoperativeRT MAIN LANDING GEAR WOULD NOT COME UP YELLOW INDICATOR THEN RED. CYCLED ONE TIME DID NOT CHANGE. DCU INOP. REMOVED DCU AND INSTALLED AN INSPECTED UNIT IAW CH 31-50-00 OF THE G-200 MM OPS CHECK GOOD.SDR DXTA200702020Trim System · unknownDURING CLIMB WITH THE AUTOPILOT ENGAGED THE AUTOPILOT DISENGAGED ALONG WITH ILLUMINATION OF THE A/P PITCH TRIM CAUTION MESSAGE 3 TIMES AFTER THE THIRD FAILURE THE PRIMARY PITCH TRIM WOULD NOT FUNCTION. PERFORMED HORIZONTAL TRIM SYSTEM FUNCTIONAL TEST AND RAN SDR DXTA200702005Unknown · unknown30 SECONDS AFTER TAKEOFF WE GOT STALL SYS FAIL ELEV FEEL AND STICK PUSHER FAIL, ALL CB,S WERE IN. REMOVED AND REPLACED THE SPQC WITH AN INSPECTED UNIT AND PERFORMED A COMPLETE FUNCTIONAL TEST I/A/W G200 MM 34-15-00. COMPLIED WITH CMP'S 341601 AND 2703030.SDR CA070220006Actuator · leaking(CAN) AC PERFORMED NORMALLY FOR THE TAKEOFF AND INITIAL CLIMB TO 5000 FEET. APPROX (2) MINUTES INTO THE FLIGHT AFTER CLEARANCE TO 17000 FT WITH CLIMB PWR REAPPLIED TO COMMENCE THE CLIMB, THE RT ENG EXPERIENCED A COMPRESSOR STALL. AFTER (2) OR (3) SURGES THE ENSDR CA070314018Actuator · failed(CAN) ON APPLICATION OF POWER IN CLIMB, THE ENGINE EXPERIENCED A COMPRESSOR STALL ACCOMPANIED BY AN UNCOMMANDED POWER REDUCTION, PARAMETER FLUCTUATIONS AND A FADEC FAULT INDICATION. SUBSEQUENT INVESTIGATION LED TO REPLACEMENT OF THE ENGINE INLET GUIDE VANE ACSDR DXTA200701920Control Unit · malfunctionedRT BLEED AIR LEAK CAME ON IN FLIGHT, WARNING MESSAGE STAYED ON DURING ALL PROCEDURES ON EH-3 OF THE QRH. ENGINE WAS SHUTDOWN INFLIGHT. NO SMOKE OR FIRE REPORTED BY FIRE DEPARTMENT. REMOVED AND INSTALLED NEW RT BLEED AIR CONTROL UNIT IAW G-200 MM / CH 21-61-00SDR DXTA200701915Motor · malfunctionedAUTO PILOT DISENGAGES ON APPROACH IN ALL MODES AND DURING TURNS. ALSO, IN STRAIGHT FLIGHT, YOKE JERKS RT AND LT ROUTINELY ABOVE MACH .78. FOUND THE RUDDER SERVO MOTOR, AUTOPILOT TO BE FAULTY. REMOVED AND REPLACED THE AUTOPILOT RUDDER SERVO MOTOR WITH AN OVERSDR DXTA200802817Ecu · inoperativeDURING APU SHUTDOWN FLAMES WERE COMING OUT OF EXHAUST, NO FIRE WARNING LIGHTS OR MSG OF ANY KIND. OPENED UP APU FIRE SWITCH AND DISCHARGED RT FIRE BOTTLE INTO APU, FIRE EXTINGUISHED. M2B- INSPECTED APU AND TAIL CONE AREA FOR DAMAGE NONE NOTED. PERFORMED ALERSDR DXTA200701896Unknown · unknownELEVATOR FEEL FAIL LIGHT CAME ON IN CLIMBOUT. REMAINED ON, THE ENTIRE FLIGHT. UPON A/C ARRIVAL VERIFIED DISCREPANCY AND NOTED THAT THE SPQC WAS NOT FULLY INSTALLED IN RACK, RERACKED SPQC AND MESSAGE EXTINGUISHED. PERFORMED A SPQC DOWNLOAD AND OPS CHECK WITHSDR DXTA200701876Warning System · activatedL BLEED AIR MESSAGE ILLUMINATED IN FLIGHT AS DIRECTED BY THE CHECKLIST THE LT ENGINE WAS SHUTDOWN BY CREW BECAUSE THE MESSAGE REMAINED ON AFTER X-LIST ITEMS WERE COMPLETED SIDE NOTE ENGINE EVENT BUTTONS WERE PRESSED ABOUT 45 SECONDS AFTER MESSAGE ILLUMINATED. SDR DXTA200701874Trim System · failedAUTOPILOT PITCH TRIM FAILED AFTER TAKEOFF WE WERE UNABLE TO CONTROL TRIM W/YOKE THUMB SELECTOR AUTOPILOT WAS FUNCTIONAL AFTER WE TRIMMED AIRCRAFT IN SECONDARY DISCONNECT POSITION TRIM BECAME SEMI FUNCTIONAL UPON ARRIVAL. TROUBLESHOT SYSTEM AND DETERMINED THATSDR DXTA200701853Float Valve · leakingINFLIGHT NOTICED FLUID TRAILING OFF OF THE RT AILERON. ON THE GROUND THE VISIBLE TRAIL DISAPPEARED BUT THERE IS RESIDUAL FUEL POCKET ON THE RT AILERON. REMOVED FUEL PANELS 640NT, 640MB. REMOVED FLOAT VALVE P/N D25W652004-507 S/N 214. INSTALLED NEW FLOAT VASDR DXTA200701850Fire Loop · failedRT ENG FIRE DETECT CAS MSG ILLUMINATED RT AFTER ENGINE START. REPLACED RIGHT ENGINE ZONE 2 DETECTOR & FIRE LOOP CMP 261102 W/O REF FL008823SDR 2007F00009Windshield · crackedTAKEN FROM AIR TAXI TURBINE DAILY RECORD SHEET/MANIFEST. RT COCKPIT WINDSHIELD IS SHATTERED. REMOVED AND REPLACED RT COCKPIT WINDSCREEN IAW G-200 M/M 56-10-05. NO LEAKS NOTED. WINDSHIELD HEATING SYSTEM OPS OK. AIRCRAFT RECORD TAKEN FROM GENERAL DYNAMICS ASDR DXTA200601809Screw · wrong partAFTER DEPARTURE SLATS WOULD NOT RETRACT FULLY. THEY STOPPED AT THE HALFWAY POINT. WE ALSO GOT THE SLAT/FLAP MAINTENCE EICAS. WE SLOWED THE AIRCRAFT AND LEVELED THE AIRCRAFT AND EXTENDED THE SLAT AND KRUGERS THEN RETRACTED THEM. WE TRIED THIS 4- 5 TIMES WITH THSDR DXTA200601798Handle · lack of lubeEMERGENCY EXIT EICAS MESSAGE CAME ON CLIMBING THROUGH 10,000 FT AND WENT OUT DESCENDING THROUGH 4,000. FOUND EMERGENCY EXIT HANDLE OUT OF ADJUSTMENT. READJUSTED E-EXIT HANDLE AND LUBED HANDLE IAW G200 MM 52-20-00. OPS CHECKED GOODSDR CA070103007Pump · malfunctioned(CAN) ENGINE OIL PRESSURE WAS REPORTED TO GRADUALLY DECREASE AND THE ENGINE WAS SHUTDOWN IN FLIGHT. THE AIRCRAFT DIVERTED FOR AN UNSCHEDULED LANDING. THE ENGINE OIL PRESSURE PUMP WAS SUBSEQUENTLY REPLACED. (TC NR 20070103007)SDR DXTA200601794Bleed Valve · stuckAT 4000 FT AND 250 KTS AT APPROXIMATELY 75% NI WE HEARD A BANG FROM THE REAR OF THE AIRCRAFT .ADDITIONALLY THE LEFT ENG VIBRATION GAGE INDICATION SIGNIFICANTLY HIGHER THAN THE RIGHT ENG. AFTER LANDING WE NOTED EXCESSIVE OIL ON THE LEFT WING. INSTALLED (1) 2.5SDR DXTA200601753Control Cable · lack of lubeGEAR HANDLE IS VERY HARD TO MOVE UP OR DOWN. IT ALMOST TAKES TWO HANDS TO RETRACT GEAR UP. NOT AS BAD SELECTING GEAR DOWN BUT STILL HARDER TO DO THAN NORMAL. REMOVED LANDING GEAR CONTROL CABLE AT GEAR CONTROL HANDLE AND LANDING GEAR SELECTOR VALVE. CLEANED ANDSDR DXTA200601744Unknown · odorAFTER TAKEOFF HAD A SMOKE OIL ODOR IN THE COCKPIT FOR ABOUT 10- 20 SECONDS, THEN IT WENT AWAY. LATER INFLIGHT THE PASSENGERS CAME UP AND SAID THAT THEY SAW A SMOKE HAZE BEHIND THE GALLEY IN THE MAIN CABIN . INSPECTED AMPLIFIER AND CONNECTIONS BEHIND GALLEY. NOSDR DXTA200601738Control Valve · inoperativeAFTER TAKEOFF GEAR HANDLE WOULD NOT COME UP. TRIED TO PRESS DOWNLOCK OVERIDE AND GEAR HANDLE WOULD NOT MOVE. REPLACED LANDING GEAR CONTROL ASSY. PERFORMED DOWNLOCK SOLENOID / OVERIDE OPERATIONAL CHECK IAW G200 MAINT. MAN CH. 32-30-00. NO DEFECTS NOTED AT THISDR DXTA200601734Fire Loop · shortedWE WERE LEVEL AT FLIGHT LEVEL 350 WHEN THE (APU FIRE LIGHT) AND BELL CAME ON. WE FIRED THE BOTTLE AND THE FIRE LIGHT STAYED ON. REMOVED AND REPLACED RT FIRE BOTTLE IAW MM 26-20-05. FIRE LOOP FOUND BAD AND REPLACED. APU FIRE DETECTION SYSTEM WAS OPS CHECKED SDR DXTA200601736Audio/Video Unit · failedWITH THE AIRCRAFT ON THE GROUND, CABIN DOOR OPEN, APU ON , APU BLEED AIR ON CABIN UPPER LTS ON, LOWER CABIN LTS ON , AIRSHOW ON, A STREAMING PUFF OF SMOKE EMITTED FROM THE LT UPPER SIDEWALL ABEAM, SEAT NR 3 AND THE SEAT NR 3 ENTERTAINMENT CONTROL PANEL. CABISDR DXTA200601686Door Seal · leakingVERY LOUD DOOR SEAL SQUEAL AFTER TAKEOFF C ALT 200, DIFF 2.3 RATE. REMOVED AND REPLACED PRIMARY DOOR SEAL AND INSPECTED MED VENT DOOR FOR PROPER CLOSING AND STICKING, VENT DOOR WAS STICKING CLEANED SEALING SURFACE AND PERFORMED PRESS CK TO 4.0 PSI NO SQUEAL. SDR DXTA200601663Fire Detector · failedDURING DESCENT ( R ENG FIRE DETECT) AMBER MESSAGE ILLUMINATED AND REMAINED ON. TROUBLESHOT RT ENG- FIRE DETECT SYSTEM, FOUND ZONE 2 FIRE LOOP INOP. REMOVED AND REPLACED RT ENGINE ZONE 2 FIRE LOOP WITH (NEW) UNIT IAWMM 26-10-10 AND CMP'S 261102, 783010, 714202 SDR DXTA200601653Apu · odorWITH APU RUNNING - ECS IN APU NOTED FUEL ODOR IN AFT CABIN IN LAV AREA. FURTHER INSPECTION FOUND ODOR TO BE MOST PRONOUNCED IN SMALL CABINET BELOW LAV CLOSET HOUSING AIRSHOW BOXES - A/C HAD APPROX 1600 LBS OF FUEL ON BOARD. NO FUEL ODOR FROM GASPERS. RAN APSDR DXTA200601549Actuator · failedLEFT MAIN GEAR DID NOT RETRACT UP AND LOCK, GEAR INDICATOR SHOWED AMBER TRANSIT FOLLOWED BY A RED BOX. OBSERVED BY CONTROL TOWER TO BE DOWN. RECYCLED GEAR AND IT CAME UP NORMALLY. REMOVED L/H MLG ACUATOR & INSTALLED A REPAIRED UNIT, OPS & LEAK CHECKED GOOD SDR DXTA200601538Fire Detector · brokenRT ENG FIRE DETECT ILLUMINATED DURING CRUISE FLIGHT. TROUBLESHOT AND CONFIRMED DISCREPANCY. FOUND RT ENGINE ZONE 2 OVERHEAT DETECTOR BROKEN. REMOVED AND REPLACED RT ENGINE ZONE 2 OVERHEAT DETECTOR WITH NEW DETECTOR IAW G-200 M/M CHAP 26-10-10. OPS CHECK GOODSDR CA060905010Bearing · fractured(CAN) DURING CRUISE THE ENGINE EMITTED A LOUD NOISE ACCOMPANIED BY AN INCREEASE IN INTER-TURBINE TEMPERATURE AND VIBRATIONS AND A CHIP DETECTOR INDICATION. THE ENGINE WAS SHUTDOWN IN FLIGHT AND AN UNSCHEDULED LANDING CARRIED OUT. SUBSEQUENT INSPECTION REVEALSDR DXTA200601533Engine · failedAT 41000 FEET, THE RIGHT ENGINE MADE A VERY LOUD BANG FOLLOWED BY HIGH ITT ON THE RIGHT ENGINE WITH SEVERE VIBRATION. THE RT ENGINE HAS UNCOMMANDED SHUT DOWN. ACCOMPLISHED EMERGENCY LANDING AT CID. ON GROUND FOUND ENGINE HD SEVERE INTERNAL FAILURE. REMOVEDSDR DXTA200601494Amplifier · smokeTWO HRS INTO A THREE HR FLIGHT FROM SUN TO HOU, NOTICED A VERY STRONG ELECTRICAL SMOKE SMELL. CONTROL PANEL IN GALLEY WAS OFF. NO COFFEEPOT HEAT, MONITOR ECT WAS ON. TURNED OFF THE CABIN GALLEY, PHONE, CABIN N/C BUTTONS ON THE PEDESTAL IN COCKPIT AND SMELLSDR DXTA200601425Capsule · out of positionR ENGINE DETECT CAS MESSAGE IS ON AND THE RT ENGINE OVERHT LIGHT WILL NOT TEST. UPON INVESTIGATION SUSPECTED EITHER A BAD OVERHEAT DETECT LOOP OR A BAD FIRE DETECT LOOP ON THE NR 2 ENGINE. TROUBLESHOT BOTH LOOPS FOUND BOTH LOOPS TO BE GOOD AS WELL AS THE WISDR DXTA200601410Computer · pilot errorDURING TAKE OFF ROLL ENGINE SET PARAMETER DID NOT MATCH TAKE OFF CONDITTION. - OBSERVED TAKE OFF POWER FOR THE DAY, NOTICED TEMPERATURE ROSE SIGNIFICANTLY. RECALCULATED PERFORMANCE USING CURRENT TEMPERATURE AND ENGINE PERFORMED NORMALLY IAW GULFSTREAM G200 AFMSDR DXTA200601368Coffeemaker · overheatedDURING DESCENT, STARTED GETTING BURNING ELECTRIC SMELL, SMELL SEEMS TO COME FROM BEHIND TOP DRAWER BELOW COFFEE POTS. CABIN POWER WAS TURNED OFF AND SMELL DISAPPEARED COFFEE POT WAS EXTREMELY HOT. REMOVED COFFEE POT. ITEM IS UNDER INVESTIGATION.SDR DXTA200601356Warning Light · illuminatedAFTER TAKEOFF RT MAIN GEAR INDICATOR HAD AMBER BOX, CYCLED GEAR AND WAS NORMAL BUT THEN STARTED FLASHING AMBER. RETURNED FOR LANDING WITH NORMAL GEAR INDICATION. ITEM IS UNDER INVESTIGATION.SDR CA060403016Engine · making metal(CAN) DURING CLIMB, THE ENGINE EMITTED A LOUD NOISE FOLLOWED BY AN UNCOMMANDED POWER REDUCTION. THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED METAL DEBRIS IN THE ENGINE EXHAUST. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCSDR DXTA200601202Warning Light · illuminatedDURING TAKEOFF ROLL EMERGENCY EXIT LIGHT MASTER CAUTION CAME ON AND STAYED ON RESULTING IN ABORTED TAKEOFF. PERFORMED EMERGENCY EXIT DOOR OPERATIONAL TEST. OPS CHECKED GOOD. ALL WORK DONE IAW G200 MM CHAPTER 52-20-00.SDR DXTA200501148Oil System · overservicedAT ABOUT 300' AFTER DEPARTURE SMOKE STARTED ENTERING COCKPIT & CABIN FROM ENVIRONMENTAL SOURCES. SMOKE HAD OILY ODOR & STRONG OILLY ODOR SENSED AROUND LT ENG. CHECKED LT & RT ENGINES FOR OIL LEAKS, NONE NOTED. CHECKED ENGINE BLEED AIR & ECS DUCTS FOR EXCESSIVESDR DXTA200501107Structure · crackedFORWARD 2 INCHES OF FUEL DIVERTER ON AFT UNDERSIDE OF AIRCRAFT IS SEPARATED FROM FUSELAGE. THERE APPEARS TO BE CRACKS IN FUSELAGE RADIATING FROM BOTH SIDES OF SEPARATED AREA. ITEM IS UNDER INVESTIGATION.SDR DXTA200501049Fire Loop · failedDURING CLIMB THRU RECEIVED LT ENG FIRE DETECT MSG ON EICAS. RETURNED WITH NO PROBLEM. ACCESS EXTERNAL AND INTERNAL BYPASS DUCT ON LT ENGINE VISUALLY INSPECTED INTERNAL ZONE 2 FIRE DETECTOR ALSO EXTERNAL ZONE 1 FIRE DETECTOR. NO DEFECTS FOUND. REMOVED LOWESDR DXTA200501008Actuator · inoperativeAFTER TAKEOFF FROM SUX, SLATS AND FLAPS WOULD NOT RETRACT. SLAT/FLAP MAINTEN ICAS MESSAGE CAME ON. TRIED TO RECYCLE SEVERAL TIMES BUT THE PROBLEM WOULD NOT CLEAR. REPLACED NR 3 RT FLAP (OUTBD) ACTUATOR. IAW A/C MM CHAPTER 27 AND CMP 275215 COMPLETED FLAP/SSDR DXTA200501005Latch · out of rigUPON TAKEOFF RIGHT MAIN LANDING GEAR DID NOT RETRACT. SUSPECT GEAR DOOR. ONLY NOT CLOSING FULLY. CYCLED GEAR PER G-200 QRH, GEAR DOOR DID NOT CLOSE FULLY EACH TIME. INSPECTION REVEALED RIGHT FWD MAIN GEAR DOOR LATCH TO BE OUT OF RIG. ALSO FOUND RIGHT GEARSDR DXTA200500998Landing Gear · failedRIGHT MAIN LANDING GEAR WILL NOT RETRACT. CYCLED GEAR IAW G200 QRH, BUT RT MAIN WOULD NOT COME UP.SDR DXTA200500933Transducer · inoperative" ANTI-SKID OFF " LIGHT ILLUMINATED DURING TAXI OUT, PRESSED TO RESET AND APPROX 1 MIN LATER IT ILLUMINATED, CYCLED ANTI-SKID CB'S AND IT AGAIN ILLUMINATED AND CONTINUED TO CYCLE ON /OFF APPROX EVERY MIN. REMOVED TRANSDUCER ON NR 4 WHEEL P/N: 606568 S/N: OLT0SDR DXTA200500932Control Box · hotAT FL410, CREW DETECTED A STRONG ODOR OF ELECTRICAL BURNING. CABIN MASTER ISOLATED IT AND ODOR WENT AWAY. FOUND AIRSHOW BOX (BLUE) BEHIND DRAWER WITH PLATES WAS VERY HOT.SDR 2005FA0001217Control Valve · bypassingWHEN THE THRUST REVERSERS WERE DEPLOYED ON THE AIRCRAFT. A VERY LOUD SQUEALING NOISE CAME FROM THE NOSE LANDING GEAR STEERING CONTROL VALVE. THIS IS THE 4TH REPLACEMENT UNIT INSTALLED ON THE AIRCRAFT. THE 5TH UNIT SERIAL NO. IL0138 RESOLVED THE PROBLEM. AND THSDR 2005FA0001219Control Valve · bypassingWHEN THRUST REVERSERS WERE DEPLOYED ON THE AIRCRAFT, A VERY LOUD SQUEALING NOISE CAME FROM THE NOSE LANDING GEAR STEERING CONTROL VALVE.SDR 2005FA0001218Control Valve · bypassingWHEN THE THRUST REVERSERS WERE DEPLOYED ON THE AIRCRAFT, A VERY LOUD SQUEALING NOISE CAME FROM THE NOSE LANDING GEAR STEERING CONTROL VALVE.
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