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 DXTA2014040405716Rudder · malfunctionedAT FLIGHT LEVEL 210 AND AT 345 KNOTS, THE ACFT HAD A BUZZING SOUND & AIRFRAME VIBRATION FELT IN CONTROLS. SHORTLY AFTER HAD A VIOLENT UNCOMMANDED RUDDER LEFT WITH NO PILOT INPUT. THE ACFT JERKED HARD FOR A FEW SECONDS. PERFORMED A NORMAL LANDING. PERFORMSDR DXTA2014040105710Landing Gear · malfunctionedAFTER TAKEOFF, LT MLG DID NOT LOCK UP DISPLAYED RED HASHES. RAN LANDING GEAR DOES NOT LOCK UP CHECK LIST. GEAR CAME DOWN & BACK UP NORMALLY. VISUALLY INSPECTED THE MAIN LANDING GEAR WIRE HARNESS AND SWITCHES PERFORMED SEVERAL RETRACTION AND EXTENTION CYCLESDR DXTA2014040705720Brake Sys · weakDURING LANDING, THE BRAKES WERE SPONGY WITH THE PEDALS TO THE FLOOR. PERFORMED BLEEDING OF THE BRAKE SYSTEM IAW MM 32-40-20. BRAKE SYSTEM OPS & LEAK CHECKED GOOD.SDR DXTA2014040405715Unknown · vibrationVIBRATION BEGINS AT FL260 AT 290KTS, INCREASED INTENSITY TO 350KTS. FELT IN CONTROL COLUMN & NOT IN RUDDER PEDALS. VIBRATION FELT IN COCKPIT SEATS & IN CABIN SEATS. CHECKED ALL ELEVATOR BELLCRANKS, PUSHRODS, CONTROL COLUMS AND HINGE POINTS FOR CONDITION ANDSDR DXTA2014032705699Landing Gear · unknownDURING MAIN GEAR RETRACTION, FIRST MOVEMENT OF GEAR HANDLE FROM FULL DOWN TO FULL UP, AN ABNORMAL LOUD BANG WAS HEARD COMING FROM THE LOWER FUSELAGE FWD TO CENTER SECTION. RETRACTION SEQUENCE COMPLETELY NORMAL WITH NO ABNORMAL MESSAGES OR INDICATIONS. GEAR SDR DXTA2014032105695Fire Warning · false activationLEFT ENGINE FIRE LIGHT ILLUMINATED AT A VERY FAINT LEVEL DURING CRUISE FLIGHT. REMAINED ON UNTIL POWER WAS REDUCED TO IDLE FOR LANDING. NO OTHER INDICATIONS OF A PROBLEM WERE PRESENT ON THE EICAS OR INDICATORS OR GAUGES. POST FLIGHT INSPECTION DID NOT PROVISDR DXTA2014031705688Engine · vibrationCLIMBING THROUGH FL360, THERE WAS A HARD AIRFRAME BUMP FOLLOWED BY STRONG AIRFRAME VIBRATION & FUMES IN CABIN. RT ENGINE VIBRATION METER SHOWED VIBRATION LEVEL NEAR THE TOP OF THE GREEN BAND. RT ENGINE INDICATIONS WERE NORMAL, N1 & ITT. ALL LT ENGINE INDICSDR DXTA2014031105685Door · damagedEXTERNAL LAVATORY BATTERY DOOR IS BROKEN & LOOSE. FOUR OF THE LATCHES WERE POPPED, DOORS WERE LOCKED. LAVATORY WAS NOT SERVICED DURING LAST STOP. R & R THE DAMAGED LAVATORY BATTERY DOOR & BOTH HINGES WITH NEW. CHECKED GOOD ON THE DOOR LATCHES & LOCKS IAW SDR DXTA2014022805667Display · faultyAT 37000 HEARD A POP SOUND & THE LT MFD WENT OUT. A BURNING WIRE SMELL STARTED THEN WENT AWAY AFTER SHUTTING OFF THE RT AVIONICS. PERFORMED INSPECTION OF WIRING BEHIND INSTRUMENT PANEL, NO HIDDEN DAMAGE OR DEFECTS NOTED. R & R THE LT MFD ON CO-PILOT'S SIDE SDR 9JLA201402174844Transducer · defectiveFLIGHT CREW REPORTED THAT DURING LANDING ROLL & TAXI THEY RECEIVED A LT ANTI-SKID ANNUNCIATOR FAULT, THEY REPORTED THAT THE LT MAIN BRAKES WERE COLD & THE RT MAIN WERE NORMAL HOT. TROUBLESHOOTING IDENTIFIED THE NR 2 WHEEL SPEED TRANSDUCER TO BE DEFECTIVE & WASDR 9JLA2014030704841Computer · failedTHE FLIGHT CREW REPORTED THAT A EGPWS & TERRAIN FAULT WAS IDENTIFIED ON THE COPILOTS MFD & PFD SCREEN. TROUBLESHOOTING INDICATED THAT THE EGPWS COMPUTER FAILED. THE DEFECTIVE COMPUTER WAS REMOVED & A REPLACEMENT WAS INSTALLED. FUNCTIONAL TEST SATISFACTORY.SDR BKER2014001Starter Gen · defectiveLEFT ENG ABORTED START DUE TO HIGH ITT & NO N1. SECOND START ATTEMPT, NO N2 WITH NO LIMITS EXCEEDED & NO FADEC MESSAGE. INSPECTED LT ENG STARTER-GENERATOR BRUSHES & FOUND BRUSH WIRES BURNT. R & R STARTER- GENERATOR WITH OVERHAULED UNIT. PERFORMED ENG GND RSDR 9JLA2014013004835Altimeter · sluggishCREW REPORTED THAT THE STAND BY ALTIMETER WAS VERY SLUGGISH IN ALL PHASES OF FLIGHT. TROUBLESHOOTING FOUND THE STAND BY ALTIMETER DEFECTIVE. THE DEFECTIVE UNIT WAS REMOVED SN 96258 & REPLACED WITH OVERHAULED UNIT.SDR DXTA2014011705619Actuator · failedAFTER TAKEOFF, RT MLG INDICATED YELLOW & THEN RED. RAN CHECKLIST PROCEDURE TO INCLUDE CYCLING THE GEAR & ALL GEAR RETRACTED NORMALLY. REMOVED FAILED RT MLG ACTUATOR. INSTALLED MODIFIED ACTUATOR. WORK DONE IAW CMP CODE 321004. PERFORMED MLG HYD ACTUATOR BLSDR DXTA2014012805628Structure · damagedTHE MAIN ENTRANCE DOOR AFT LOWER CORNER IS BENT INWARD & SOME PAINT & PRIMER APPEARS TO BE CRACKED OR MISSING. THE DOOR IS 0.168 OUT OF CONTOUR AT THE DEEPEST POINT. ACCOMPLISHED REPAIR TO LOWER AFT CORNER OF MAIN ENTRANCE DOOR. PERFORMED OPERATIONAL & PRESSDR 9JLA2014012404440Outflow Valve · defectiveTHE FLIGHT CREW REPORTED THAT AN AUTO PRESSURIZATION CAS MESSAGE ILLUMINATED. TROUBLESHOOTING OF THE AUTO PRESSURIZATION SYS FOUND THE MAIN OUT FLOW VLV TO BE DEFECTIVE. THE DEFECTIVE OUT FLOW VLV WAS REMOVED & A NEW VLV WAS INSTALLED IAW MM CMP TASK 213008.SDR DXTA2013123005611Fire Warning · false activationENROUTE AT FL390, RECEIVED AN APU FIRE EICAS MESSAGE & AURAL ALARM. RAN CHECKLIST TO INCLUDE BLOWING FIRE BOTTLE. EICAS MESSAGE & ALARM CAME ON INTERMITTENTLY FOR DURATION OF FLIGHT. DECLARED EMERGENCY & LANDED. NO INDICATION OF FIRE WAS FOUND AFTER LANDISDR 9JLA2014011504438Oxygen Mask · leakingTHE FLIGHT CREW REPORTED THAT THE COPILOTS OXYGEN MASK WAS FOUND TO BE LEAKING OXYGEN. THE DEFECTIVE CREW MASK WAS REMOVED FROM SERVICE PN MC10-13-150 & SN 98366. AN OVERHAULED CREW MASK WAS INSTALLED.SDR 9JLA2013123104828Strut · damagedCREW REPORTED THAT AFTER LOADING OF PASSENGERS DURING COLD WEATHER OPERATIONS, THE CREW WAS UNABLE TO CLOSE THE CABIN DOOR & DAMAGED THE AFT DOOR SUPPORT TELESCOPIC STRUT. IT WAS DETERMINED THAT THE AFT DOOR TELESCOPIC TIE ROD AS JAMMED DUE TO FROZEN WATER INSDR Y9PA20140116001Boot · delaminatedRIGHT HORIZONTAL STABILIZER DE-ICE BOOT FAILED, DELAMINATED.SDR DXTA2013121605598Transceiver · faulty35 MINS INTO FLIGHT FROM KTIW TO KLAS, AT FL 390, .76M THE RED GEAR NOT DOWN CASS MSG ILLUMINATED TRIGGERING THE RED MASTER WARNING. THE POWER WAS SET TO 92.8 N1 & GEAR LEVER FULLY SELECTED UP. CASS MSG STAYED ILLUMINATED FOR APPROXIMATELY 15 TO 20 SECONDS TSDR DXTA2013120205587Autopilot Sys · malfunctionedAT FL380 AUTO PILOT KICKED OFF SEVERAL TIMES THEN FAILED. HAND FLYING THE AILERONS WERE STICKING. FLYING AT FL280 AFTER APPROXIMATELY 1 HOUR THE AILERONS STOPPED STICKING & THE AUTOPILOT RESET. APPLIED POWER TO THE AIRCRAFT & PERFORMED FREEDOM OF MOVEMENT CHSDR DXTA2013111805569Wire Harness · corrodedFL 260, CLIMBING AT 300KTS, RT RED BOX SLASH GEAR UNSAFE INDICATION APPEARED. SPEED TAPE TURNED RED. AFTER SLOWING TO ABOUT 270KTS GEAR INDICATION RETURNED TO NORMAL AND REMAINED NORMAL. FLT WAS SMOOTH, NO VIBRATIONS. FOUND CORROSION ON RT MLG PROXIMITY SWSDR DXTA2013111805568Unknown · odorAFT CARGO AREA HAS EXTREMELY STRONG FUEL ODOR INSIDE. THERE IS NO VISIBLE FUEL LEAKING EXTERNALLY. INSPECTED CARGO BAY FOR ANY ODORS OR VISIBLE FUEL LEAKS WITH NO DEFECTS NOTED. FUELED AIRCRAFT TO 9300 LBS OF FUEL AND LEFT OVERNIGHT. REINSPECTED AND FOUND A SDR DXTA2013102205544Converter · contaminatedAFTER TAKE OFF WITH APU SHUTDOWN, FLOW PACK BOTH, 250 KTS, CLIMBING THROUGH 12000FT CABIN FILLED WITH SMOKE. FOUL SMELLING, BAD TASTING SMOKE. IAW QRH OPENED DUMP VALVE WHICH REMOVED MOST OF SMOKE. INSPECTED EOS SYSTEM FOR OIL CONTAMINATION. FOUND THE OZONE SDR DXTA2013101405542Strut · failedALL PROBE HEAT INOPERATIVE, COMES ON WHEN OVERRIDE IS SELECTED. TROUBLESHOT TO A FAULTY NOSE GEAR STRUT NOT FULLY EXTENDING. REMOVED AND REPLACED NOSE LANDING GEAR SHOCK STRUT ASSEMBLY IAW CMP 322016, 322002. OPS AND LEAK CHECKED GOOD.SDR DXTA2013101405539Window · crackedPILOT SIDE WINDSREEN, SPIDER WEB CRACKED, COVERING ENTIRE PANEL. REMOVED CRACKED WINDOW, PERFORMED WINDSHIELD AND SIDE WINDOW TEMP SENSING ELEMENT RESISTANCE CHECK AND HEATING ELEMENTS RESISTANCE CHECK PER 56-10-00. INSTALLED NEW WINDOW AND PERFORMED ALL LESDR 9JLA2013120404814Probe · defectiveTHE FLIGHT CREW REPORTED THAT THE TAT CB DISENGAGED DURING FLIGHT. TROUBLESHOOTING IDENTIFIED THE TAT PROBE AS DEFECTIVE. THE PROBE WAS REMOVED SN A41306 & REPLACED WITH A REPAIRED PROBE. OPERATIONS CHECKED SATISFACTORY.SDR DXTA2013100705529Engine · smokeAFTER TAKEOFF, HAD SMOKE IN COCPIT AND CABIN. WENT THROUGH EMERGENCY PROCEDURE DUMPED CABIN AND WENT TO RAM. SMOKE STOPPED AND LANDED IMMEDIATELY. REMOVED AND REPLACED ENGINE. ALL WORK PERFORMED IAW G200 AMM 71-00-00 AND PW306 EMM 71-00-00.SDR DXTA2013092305516Warning Message · illuminatedWHILE AT FL400 AND ONE HOUR INTO THE FLIGHT, RT ENG OIL PRESSURE HIGH EICAS ILLUMINATED. OBSERVED RED 111PSI AND IMMEDIATELY RETARDED THROTTLE TO IDLE. ATTEMPTED TO INCREASE POWER BUT OIL PRESSURE INCREASED PROPORTIONATLEY TO THROTTLE MOVEMENT.SDR 9JLA2013111806425Cable · brokenFLIGHT CREW REPORTED THAT THE MAIN ENTRY DOOR LIFTING SYSTEM WAS INOPERATIVE. TROUBLESHOOTING IDENTIFIED THE DOOR LIFT CABLE BROKE. THE SYSTEM WAS DISABLED WHILE MFG SEARCHED THE WORLD FOR A REPLACMENT CABLE. POOR PARTS SUPPORT, 6 WEEKS FOR REPLACEMENT CABLESDR DXTA2013082805487Control Box · inoperativeNORMAL BRAKING SYS INTERMITTENT. AFTER LANDING, WITH NORMAL BRAKING, LOST BRAKING. INCREASED PEDAL FORCE AND APPROXIMATLEY 2 TO 3 SECONDS BRAKING RETURNED. HAPPENED TWICE ON TAXI TO RAMP. REMOVED AND REPLACED ANTISKID CONTROL BOX IAW CMP 324501. PERFORMED SDR DXTA2013082605485Wheel · vibrationWHEN RETRACTING GEAR AFTER NORMAL TAKEOFF, NOSE WHEEL WOBBLES AND CAUSES A VIBRATION ON NOSE OF ACFT FOR 10-12 SECONDS.SDR DXTA2013081605477Valve · failedNORMAL BRAKING SYS INTERMITTENT. AFTER NORMAL LANDING WITH NORMAL BRAKES, LOST ALL BRAKING POWER WHILE TAXIING. CAME BACK WITH TWO LOUD THUMPS. AFTER RELEASING AND REAPPLYING THE BRAKES, SAME EVENT HAPPENED AGAIN. SELECTED EMERGENCY BRAKES AND TAXIED TSDR 9JLA2013090506419Regulator Valve · defectiveEICAS DISPLAYED DE-ICE SYS AND DE-ICE SYS ALT, WHEN PNEUMATIC BOOT DEICING SYS WAS SELECTED ON NORM AND ALTERNATE. MX TROUBLESHOOTING IDENTIFIED THE PRESSURE REGULATOR VALVE AS DEFECTIVE. VALVE WAS REMOVED AND REPLACED WITH NEW VALVE. FUNCTIONAL CHECKED SASDR DXTA2013080605471Frame · damagedDURING DESCENT THRU 17,000 FT, THE ACFT HAD A BIRD STRIKE AT 300 KTS JUST BELOW THE RT WINDSCREEN. THERE IS A DENT THE SIZE OF A SOFTBALL WITH A LARGE HOLE IN IT. INSPECTED AREA AND FOUND BS 2669 FRAME DAMAGED. REMOVED DAMAGE FRAME SECTION IAW DWG SEB51011SDR DXTA2013071805451Engine · shutdown10 MINUTES AFTER DEPARTURE, LEFT ENGINE SHUTDOWN INFLIGHT, CLIMBING THROUGH 12,400 THE LT FADEC FAULTY ICAS ILLUMINATED. LT N2 INDICATOR TURNED RED BRIEFLY AND THE ITT HAD A 100 DEGREE SPLIT (L750/R850). 10-15 SECONDS LATER THE LT ENGINE SHUTDOWN. LT ENGINSDR DXTA2013071705449Unknown · leakingDURING CLIMB THROUGH 5000', RECEIVED A LT ENG OIL LEVEL LOW MESSAGE. CONFIRMED WITH IDICATOR AT 22 PSI. OIL INCREASED SLIGHTLY TO 33-36, RAPIDLY DROPPED TO 0 PSI. PERFORMED ENGINE SHUTDOWN AND RETURNED TO DEPARTURE. ON GROUND SAW OIL ON THE LOWER THRUST RSDR DXTA201307175549Oil System · leakingDURING CLIMB THROUGH 5000', RECEIVED A LT ENGINE OIL LEVEL LOW MESSAGE. CONFIRMED WITH IDICATOR AT 22 PSI. OIL INCREASED SLIGHTLY TO 33-36, THEN RAPIDLY DROPPED TO 0 PSI. PERFORMED ENGINE SHUTDOWN AND RETURNED TO DEPARTURE. ON THE GROUND SAW SOME OIL ON THSDR DXTA2013071105440Tire · deflatedLEFT OTBD MAIN TIRE FLAT, WENT FLAT AFTER LANDING AND ANTI-SKID LIGHT CAME ON AND STAYED ON AFTER LANDING. REPLACED NR 1 & 2 WHEEL ASSY IAW MM 32-42-02. R & R NR 1 MLG WHEEL TRANSDUCER IAW CMP 324502 AND OPS TESTS GOOD IAW MM 32-40-30.SDR DXTA2013061005413Hydraulic Line · leakingFL390, RT HYD LOW LEVEL, HYD EICAS MESSAGE CAME ON. QTY SHOWING 24. RAN CHECKLIST. RT HYDRAULIC LOW PRESSURE EICAS MESSAGE CAME ON. RAN CHECKLIST, DECLARED AN EMERGENCY, DIVERTED. HYD FLUID LEAKING FROM THE BELLY. REPLACED CHAFED HYD LINES IN AFT COMPARTMSDR DXTA2013053105408Outflow Valve · malfunctioned15 MINUTES INTO FLIGHT AT 31,000 FT, CABIN ALTITUDE REACHED 8500 & DISPLAY TURNED YELLOW. KEPT SLOWLY CLIMBING. RAN CHECKLIST & PUT IN MANUAL MODE, BUT STILL UNABLE TO CONTROL. CABIN ALTITUDE REACHED 10,000 FT, DESCENDED TO 15,000 FT. REACHING THAT ALTITUSDR DXTA2013052005396Brake Sys · malfunctionedBRAKES REQUIRE EXCESSIVE PRESSURE TO ACTIVATE, WHEN THEY DO ACTIVATE THEY GRAB THEN FADE TO A HARD PEDAL WITH LITTLE BRAKING ACTION. DUPLICATED DISCREPANCY DURING TAXI CHECK & FOUND AIR TO BE IN BRAKE SYS. PROCEDED TO PERFORM BRAKE BLEEDING ACTIONS IAW MM 32SDR 9JLA2013052206410Sensor · defectiveCREW REPORTED APU HAD AN UNCOMMANDED SHUTDOWN. TROUBLESHOOTING IDENTIFIED THE APU OIL TEMP SENSOR AS DEFECTIVE. A NEW SENSOR WAS INSTALLED, FUNCTIONAL AND LEAK CHECKS WERE SATISFACTORY.SDR 9JLA2013061104429Fuel Cell · leakingTHE FLIGHT CREW REPORTED THAT PRIOR TO DEPARTURE THEY NOTED FUEL LEAKING FROM AROUND THE RT WING ROOT AREA. TROUBLESHOOTING IDENTIFIED THE FUEL LEAK WAS COMING FROM THE RT FUEL VENT TUBE ELBOW ATTACHMENT ON THE FUSLAGE FUEL CELL. THE FUEL CELL WAS REMOVE FOR SDR 9JLA2013051506408Fms · failedDURING CRUISE, CREW REPORTED THE NR 1 FMS SHUTDOWN, AUTOPILOT DISENGAGED AND VISIBLE SMOKE APPEARED FROM THE LT SIDE OF THE INSTRUMENT PANEL. AFTER EVALUATION, DIVERTED. AN EMERGENCY WAS DECLARED, & LANDED. THE NR 1 FMS WAS FOUND TO BE DEFECTIVE AND WAS RSDR DXTA2013050605372Unknown · unknownDURING FLIGHT, CREW FELT UNCHARACTERISTICALLY FATIGUED, AND HAD HEADACHES AND TUNNEL VISION. SELECTED DIFFERENT ECS POSITIONS FROM LT TO RT ENGINE AND DISCOVERED THAT RT ENGINE ECS WAS ALLOWING FUMES INTO CABIN AND COCKPIT. CLEARED CABIN AND COCKPIT OF FUMESSDR DXTA201305060569Fire Detector · out of positionAPU FIRE MESSAGE AND BELL CAME ON AFTER STARTING NR 2 ENGINE. NO FIRE OR ABNORMAL TEMPERATURE. TRIED POWERING DOWN EVERYTHING AND RESET BUT FIRE MESSAGE AND BELL STILL ON WHEN POWER WAS ON. POWERED ACFT AND CHECKED EICAS. NO MESSAGE. CHECKED APU SENSING ESDR DXTA2013042905364Uplock Switch · failedAFTER SELECTING GEAR UP THE LT GEAR INDICATION SHOWED RED HASH LINES. THE ACFT DID FEEL LIKE THE GEAR WAS DOWN. NO DRAG OR PULL TO ONE SIDE. WE CYCLED THE GEAR 3X DID NOT FIX THE PROBLEM. JACKED A/C AND SWUNG GEAR SEVERAL TIMES. VERIFIED DISCREPANCY. DISCONSDR DXTA2013042905362Diode · failedSHORT 15 MINUTES FLIGHT FROM T82 TO SAT AT 5000 FEET, WITHIN 5 MINUTES WE ENCOUNTER AN ELECTRIC BURNING SMELL IN THE COCKPIT. CONTINUED AND THE SMELL GOT STRONGER AND STRONGER. DURING THAT FLIGHT WE ALSO GOT AMBER RT AND LT ICE DETECT FAIL EICAS MESSAGES. T
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