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 = '390' 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 = '390' 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 2011FA0000748Engine · failedDURING CRUISE AT 25,000 FEET, DETECTED SMOKE IN THE COCKPIT. SHORTLY AFTER THE LEFT ENGINE INDICATORS SHOWED LOW OIL PRESSURE (IN THE RED) AND THE LOW OIL PRESSURE ANNUNCIATOR. SHUTDOWN ENGINE, AND DIVERTED TO THE NEAREST MAJOR AIRPORT. ON LANDING, OBSERVEDSDR 26N2011F00003Aoa · inoperativeCREW REPORTED THAT LT STALL FAIL ANNUNCIATOR ILLUMINATED. TROUBLESHOT SYSTEM AND FOUND LT AOA HEAT INOPERATIVE. R & R LT AOA ASSY, PN SLZ8060-3, SN AB 0353. SYS OPS CHECKED OK.SDR E81RJW304642Control Unit · failedINVESTIGATED REPORTED FLAP SYS FAILED TO OPERATE. FOUND THE FLAP CONTROL UNIT TO HAVE AN INTERNAL FAILURE, WOULD NOT RESET. REPLACED THE FLAP CONTROL UNIT WITH A SERVICEABLE FLAP CONTROL UNIT AND SYS OPERATIONS FOUND NORMAL. RECOMMEND AIRFRAME AND COMPONENT MSDR E81RJW304426Controller · intermittentINVESTIGATED PILOT REPORT OF INTERMITTENT PITCH TRIM FAIL INDICATION ON CLIMBOUT WITH AUTOPILOT ENGAGED. OPERATIONS REPORTED NORMAL IN OTHER MODES. REPLACED PITCH TRIM CONTROLLER WITH A REPAIRED CONTROLLER. FUNCTIONAL TESTS OF PITCH TRIM SYS NORMAL, NO FAULTSDR ZP7A20110228Wire Harness · out of positionCREW HEARD A LOUD AIR NOISE DURING CRUISE PORTION OF FLIGHT. REPORTED THAT THE GEAR HANDLE ILLUMINATED RED, WHICH INDICATES A GEAR DOOR UNLATCH CONDITION. REDUCED AIRSPEED TO 200 KNOTS AND CYCLED THE LANDING GEAR DOWN THEN BACK UP. NOISE WAS STILL PRESENT AND SDR CA101216001Bearing · corroded(CAN) DURING 200HRS SCHEDULE INSPECTION FOUND NOSE WHEEL BEARING CORRODED.SDR E81RAW301008Display · malfunctionedFLIGHT CREW REPORTED PILOT'S PRIMARY FLIGHT DISPLAY TURNED GREEN FOR APPROX 2 MINUTES DURING FLIGHT, THEN RETURNED TO NORMAL.SDR E81RJW3033120Oxygen Mask · sticking(E81R) DURING FUNCTIONAL TEST OF PAX OXYGEN SYS FOLLOWING SCHEDULED SOLENOID SHUTOFF VALVE O/H. NOTED FLOW INDICATORS IN ALL SIX CABIN PAX OXYGEN MASK ASSY'S, STICKING. FOUND OILY TYPE FILM & EVIDENCE OF MOISTURE CONTAMINATION IN AFFECTED MASK ASSY'S. CAUSINGSDR CA100927004Bearing · corrodedDURING INSP, FOUND BOTH BEARING CORRODED AND BOTH BEARING REPLACED.SDR CA100927003Bearing · corrodedNOSE WHEEL BEARING NOISY DURING TAXI AND GETS LOUDER WITH RUDDER APPLICATION (SIDE LOADING). DURING TROUBLESHOOTING, FOUND BOTH BEARING CORRODED.SDR E81RJT22870Actuator · failedFLIGHT CREW REPORTED FLAP SYS FAIL INDICATION ON APPROACH. FOUND RT WING NR 3 FLAP ACTUATOR TO BE EXTENDED IN EXCESS OF 0.5 INCHES TOO FAR IN ALL FLAP POSITIONS. REPLACED THE NR 3 RT FLAP ACTUATOR WITH A REPAIRED ACTUATOR AND RIGGED THE FLAP SYS AS REQUIRED, SDR E81RJW302972Power Supply · failedPILOT NOTED "POPPING" NOISES FROM COCKPIT PEDESTAL AREA AT POST-FLT ELECTRICAL SYS SHUTDOWN, FOLLOWED BY SMOKE FROM PEDESTAL AREA. FOUND XL500/5 STANDBY POWER SUPPLY (HBC PN 390-384027-0001) TO INTERMITTENTLY OUTPUT 16-17 VDC AT 5VDC INSTRUMENT LIGHTING OUTPUTSDR E81R_JW30282_3Control Cable · seized(E81R) DURING REPLACEMENT OF RT ENG FWD POWER CONTROL CABLE ASSY FOR EXCESSIVE LEAKAGE IN CONJUNCTION WITH COMPLIANCE WITH SB 76-3907 FOUND NEW REPLACEMENT CABLE ASSY. SEIZED DURING INITIAL POST-INSTALLATION RIGGING CHECKS. REPLACED 1ST REPLACEMENT CABLE ASSSDR E81RJW302753Actuator · malfunctionedON FINAL APPROACH TO MSN PILOT REPORTED RECIEVING SPOILER AND SPEEDBRAKE SYSTEM FAIL INDICATIONS. AFTER LANDING COMMANDED SPEED BRAKES TO LIFT DUMP MODE BUT NOTED ONLY R/H WING PANELS EXTENDING. NOTED LOUDER THAN NORMAL NOISES WHEN CONDUCTING POST-LANDING SPOISDR E81RJW302543Shutoff Valve · failed(E81R) INVESTIGATED PILOT REPORT OF RT ENG ANTI-ICE VALVE FAIL ANNUNCIATOR ILLUMINATED. FOUND NACELLE ANTI-ICE SHUTOFF VALVE ASSY, INOPERATIVE. INSTALLED VALVE WAS INSTALLED NEW 6 WEEKS PREVIOUS. REPLACED SHUTOFF VALVE WITH NEW VALVE, FUNCTIONAL TESTS OK. 4TH SDR E81RJW302511Detector · malfunctionedINVESTIGATED PILOT REPORT OF HORIZ STABILIZER L/E ANTI-ICE SYS FAIL INDICATION. AFTER EXTENSIVE TROUBLESHOOTING, FOUND RT ICE DETECTOR WOULD SHOW A FAIL INDICATION WHEN PROBE WAS LIGHTLY COVERED BY A RAG. IF TESTED IAW STEP 3 OF MM 30-11-00-501 OPS TEST WITH SDR E81RJW302513Relay · failedINVESTIGATED REPORT OF LT ENGINE IGNITION SYS STAYING ACTIVATED AFTER ENGINE START SEQUENCE COMPLETED. VERIFIED COMPLAINT, FOUND LT ENGINE IGNITION STANDBY POWER RELAY 80K7 FAILED. REPLACED RELAY WITH NEW RELAY, IGNITION SYS OPERATIONS NORMAL. HAVE NOTED THSDR E81RJW302431Shutoff Valve · failedINVESTIGATED REPORTED RT ENG ANTI-ICE FAIL ANNUNCIATOR INDICATION. REPLACED INOPERATIVE ENG INLET ANTI-ICE SHUTOFF VALVE WITH NEW SHUTOFF VALVE, ENGINE ANTI-ICE FUNCTIONAL CHECKS OK. HAVE REPLACED SEVERAL LOW TIME NEW AND O/H ANTI-ICE VALVES ON ACFT THIS FALL/SDR E81RJT227504Display · inoperativePILOT REPORTED COPILOT'S PRIMARY FLIGHT DISPLAY SCREEN WENT BLANK FOR APPROX 1 SECOND IN FLIGHT. UNABLE TO DUPLICATE DURING ON-GROUND CHECKS. REPLACED FLIGHT DISPLAY WITH AN O/H EXCHANGE UNIT, NO FAULTS OBSERVED. REMOVED UNIT O/H 8/26/2005.SDR E81RJT227501Shutoff Valve · malfunctionedTROUBLESHOT INOPERATIVE RT ENG NACELLE INLET HEAT INDICATION AT IDLE. FOUND RT NACELLE INLET HEAT PRESSURE REGULATING/SHUTOFF VALVE FAILED. VALVE WAS INSTALLED 1/19/2010, AFTER O/H, REPLACED VALVE ASSY WITH ANOTHER O/H VALVE ASSY AND FUNCTIONAL CHECKS ON ENG GSDR E81RJW3022513Fmc · malfunctionedINVESTIGATED REPORT OF FLIGHT MANAGEMENT SYS LOSING LAST SAVED POSITION, THEN GOING TO NORTH ZERO DEGREES AND EAST ZERO DEGREES. REPLACED NR 1 FMC-3000 FLIGHT MANAGEMENT COMPUTER CARD WITH AN O/H REPLACEMENT CARD AND RELOADED DATABASE. FMS OPS NORMAL. RECOMMENSDR E81RJW3022512Adc · malfunctionedINVESTIGATED REPORT OF RT (COPILOT'S) SIDE PITCH TRIM FAIL INDICATION. ALSO SHOWING RED "X" INDICATIONS FOR AIRSPEED, ALTITUDE, AND VERTICAL SPEED. ALTITUDE PRESELECT TURNS RED, THEN BLUE. REPLACED NR 2 AIR DATA COMPUTER WITH AN O/H UNIT, DISPLAY INDICATIONSSDR E81RJW30230Switch · out of adjustINVESTIGATED, VERIFIED REPORTED INOPERATIVE IN FLIGHT OPERATION OF SPEED BRAKE SYS. FOUND LT POWER LEVER 80 PERCENT SPOILER SYS SWITCH S1 OUT OF ADJUSTMENT. ADJUSTED S1 SWITCH AS REQUIRED, SPOILER/SPEED BRAKE SYS OPS NORMAL. TRANSIENT ACFT, MX HISTORY NOT AVASDR E81RJW30228Fuel Control · malfunctionedINVESTIGATED REPORTED LT ENG SURGING AND "POPPING" AFTER START. REPLACED FUEL CONTROL ASSY. (HMU) WITH REPAIRED EXCHANGE UNIT, ENGINE OPERATIONS NORMAL. RECOMMEND ACCY MFG INVESTIGATE AT TEARDOWN FOR FAULTS TO DETERMINE IF ONE-TIME PROBLEM, OR FURTHER INVESTIGSDR E81RJW302212Relay · closedINVESTIGATED REPORT OF LT ENG IGNITION SYS NOT SHUTTING OFF AFTER ENG START SEQUENCE. FOUND LT IGNITION SYS STANDBY POWER RELAY 80K7 NOT FUNCTIONING. REPLACED 80K7 RELAY WITH NEW RELAY, IGNITION SYS OPS NORMAL. HAVE REPLACED NUMEROUS PN M83536/10-028L IGNITIOSDR E81RJW302211Anti-Ice Valve · malfunctionedINVESTIGATED REPORT OF VIBRATION FELT THROUGH ACFT AFTER REPLACEMENT OF RT ENGINE NACELLE INLET ANTI-ICE SHUT-OFF VALVE ASSY. WITH AN O/H VALVE ASSY. SUSPECT VIBRATION CAUSED BY RAPID MODULATION OF ANTI-ICE SHUTOFF VALVE. VALVE O/H 12/21/2009 ON WO R82102. RECSDR E81RJW302236Shutoff Valve · failedREPLACED FAILED RT ENG INLET ANTI-ICE SHUTOFF VALVE ASSY WITH "0 TSOH" VALVE. NEWLY O/H VALVE CAUSED VIBRATION FELT THROUGH AIRFRAME, BELIEVED TO BE CAUSED BY RAPID VALVE MODULATION. VALVE O/H WO NR R79693 DATED 10/27/2009. THIS IS THE SECOND RECENTLY O/H VALSDR CWQA04292010Unknown · malfunctionedPRIOR TO TAXI RUDDER TRIM ALL THE WAY LEFT AND WILL NOT (UNABLE) RETRIM. INSTALLED NEW RUDDER TRIM INDICATOR AND RUDDER TRIM INTERRUPT RELAY. TEAR DOWN REPORTS STILL NOT AVAILABLE, SPECIFIC PART CAUSE AND RESOLUTION STILL NOT CONFIRMED.SDR E81RJW30194Roll Pin · migratedCONFIRMED FLIGHT CREW REPORT OF THE SPOILER SYSTEM NOT PASSING THE PREFLIGHT BIT TEST PER THE AFM. REQUIRED ADJUSTING THE LT AND RT ROLL ACTUATOR LVDT'S AND LT AND RT SURFACE POSITION SENSORS LVDT'S VOLTAGES TO WITHIN SERVICE LIMITS. REQUIRED ADJUSTMENT OF THESDR E81RJW301904Control Module · out of toleranceDURING TROUBLESHOOTING FOR SIMULTANEOUS "ROLL FAIL" AND "SPEED BRAKE FAIL" ANNUNCIATOR INDICATIONS REPLACED HBC P/N 390-384011-0019 SPOILER SYSTEM ELECTRONIC CONTROL MODULE WITH AN ELECTRONIC CONTROL MODULE REPAIRED BY MANUFACTURER'S FACILITY 8/04/2009. DURINGSDR E81R_JW30193Controller · malfunctionedVERIFIED FLIGHT CREW WRITE-UP OF INOPERATIVE PITCH TRIM AT AIRPORT. TROUBLESHOT WITH MFR'S TECH. REPLACED HBC PN 390-384028-0009 PITCH TRIM CONTROLLER WITH REPAIRED UNIT, FUNCTIONAL CHECKS OK. TRANSIENT ACFT, RECORDS NOT AVAILABLE. RECOMMEND COMPONENT AND/ORSDR E81R_JW30190_1Control Module · malfunctionedFLIGHT CREW REPORTED "ROLL FAIL" AND "SPEED BRAKE FAIL" ANNUNCIATOR INDICATIONS. REQUIRED EXTENSIVE TROUBLESHOOTING WITH MANUFACTURER SUPPORT. REPLACED SPOILER CONTROL UNIT CONNECTOR 27P1 NO. 5 AND NO. 7 CONTACTS DUE TO LOW MOUNTING TENSION. CLEANED AND REASSESDR CA091002006Line · leaking(CAN) PILOT NOTED FUEL LEAKING OUT OF LT ENG LWR COWLING DURING WALKAROUND INSP. REMOVED COWLING, CLEANED FUEL RESIDUE FROM LT ENG ASSY, THEN ACFT GROUND RUN FOR LEAK CHECK. DURING LEAK CHECK THE AME OBSERVED A STEADY, HIGH PRESSURE FUEL SPRAY EMANATING FROM SDR GSPA2190001Line · leakingA HYDRAULIC LEAK WAS FOUND ON THE LEFT MLG DOOR HYDRAULIC UP LOCK TUBE ASSEMBLY P/N 390-581953-0013. THE LEAK WAS COMING FROM THE BEND RADIUS ON THE TUBE DO TO A VERY SMALL CRAK OR PIN HOLE. THE LEAK WAS ENOUGH TO LEAVE PUDDLE OF FLUID ON THE HANGAR FLOOR.SDR E81RJW3018133Hose · chafedDURING SCHEDULED INSP, FOUND LT ENG COMPARTMENT FUEL HOSE ASSY CHAFED PAST SERVICE LIMITS FROM CONTACT WITH ADJACENT COWLING STRUCTURE. REPLACED HOSE ASSY WITH NEW HOSE ASSY AND SECURED AS REQUIRED. 390 SERIES POWERPLANT INSTALLATIONS HAVE TIGHT CLEARANCES BESDR GSPA LS092146Starter Gen · damagedDURING NR 2 ENG START THE PILOT REPORTED ENGINE ACCELERATED FAST AND MADE STRANGE NOISES. START SEQUENCE WAS TERMINATED. INVESTIGATION REVEALED THE NR 2 STARTER GEN SMELLED OF SMOKE WAS HARD TO TURN AND BRUSHES HAD HEAT DISCOLORATION AND WERE CHIPPED.SDR CA090206004Throttle Cable · frozen(CAN) PREMIER 1A ACFT, NR 2 THROTTLE CABLE FROZEN (MOISTURE) IN FLIGHT. THROTTLE CABLES BOTH FORE AND AFT SHEATHING BLOWN THROUGH WITH PRESSURIZED DRY NITROGEN AND FOUND SIGNIFICANT MOISTURE PRESENT. ACFT CABLES TO BE REPLACED PRIOR TO NEXT FLIGHT IAW MM.SDR 2009FA0000033Fcu · malfunctionedPILOT REPORTED FLAPS WOULD NOT RETRACT AFTER LANDING. TROUBLESHOT SYS IAW THE MM 27-50-00-101 AND HBC TECH SUPPORT RECOMMENDATIONS. RECEIVED NUMEROUS FAULT CODES NOT FOUND IN TROUBLESHOOTING MATRIX. REPLACED FLAP CONTROL UNIT WITH REPAIRED FLAP CONTROL UNIT IASDR BKE2008F00004Torque Link · looseON THE RUNWAY WHEN POWER WAS ADVANCED AND ACFT +/- 45 KTS. THERE WAS A VIBRATION SENSED IN THE FRONT. EXITED THE RUNWAY AND RETURNED TO FBO TO ASCERTAIN PROBLEM. TIGHTENED TORQUE LINK CENTER BOLT IAW AMM 32-20-02-401. PERFORMED HIGHT SPEED TAXI, NO DEFECTS SDR 2008FA0000901Damper · wrong partINVESTIGATED PILOT REPORT OF MLG DOORS NOT CLOSING INDICATION FOLLOWING GEAR RETRACTION. FOUND RUBBER BUMPER MISSING FROM LT MAIN GEAR UPLOCK DAMPER ASSY, LT MAIN GEAR UPLOCK DAMPER ASSY CAUSING LT MN GEAR UPLOCK HOOK NOT TO RESET AND ENGAGE ROLLER FOLLOWINGSDR 2008FA0000662Seal · dislodgedPRESSURE REFUELING CONNECTION CAP FOUND WITH SEALING RING DISLODGED AND HOLDING THE CHECK VALVE OPEN WHEN THE CAP IS INSTALLED. FUEL LEAKING FROM CAP CAUSING FUEL TO FLOW FROM IT UP THE SIDE OF THE AIRCRAFT. THE FUEL FLOWING UP THE OUTSIDE OF THE AIRCRAFT HAS SDR 2008FA0000573Float Valve · separatedDURING 1200 HR INSP WHICH REQUIRES OPENING ALL WING AND FUSELAGE FUEL TANK ACCESS PANELS FOR INTERNAL INSPECTION IN BOTH LT & RT CTR FUSELAGE TANKS, FWD FLOAT VENT VALVES FLOAT SECTION OF VALVE ASSY WAS FOUND SEPARATED AND LAYING LOOSE INSIDE FUEL TANK AREA. SDR 2008FA0000603Ring · dislodgedPRESSURE REFUELING CONNECTION CAP FOUND WITH SEALING RING DISLODGED AND HOLDING THE CHECK VALVE OPEN WHEN THE CAP IS INSTALLED. FUEL LEAK FROM CAP CAUSING FUEL TO FLOW FROM IT UP THE SIDE OF THE AC. THE FUEL FLOWING UP THE OUTSIDE OF THE ACFT HAS BEEN DRAWN INSDR 2008FA0000512Switch · failedPILOT REPORTED SPOILER FAIL INDICATION IN CRUISE FLIGHT. ALL SPOILER PANELS DEPLOYED UPON LANDING. SCU FAULT CODE 44R4RV3V INDICATED. ADJUSTED LT & RT SPOILER FINAL POSITION LVDT`S AS REQUIRED IAW MM 27-60-00-501. REPLACED LT THROTTLE SWITCH S1, SPOILER SYSDR E812008F00001Valve · stuckINVESTIGATED PILOT REPORT OF UNCOMMANDED RT ENGINE ANTI-ICE OPERATION DURING TAKEOFF AND CRUISE FLIGHT. FOUND RT ENGINE ANTI-ICE VALVE STICKING OPEN. REPLACED VALVE WITH SERVICEABLE O/H VALVE, FUNCTIONS NORMAL. HAVE NOTED SEVERAL FAILURES OF ANTI-ICE VALVESSDR 2008FA0000456Valve · stuckREPLACED FAILED RT ENGINE ANTI-ICE VALVE WITH 0 TSOH VALVE ASSY SUPPLIED BY HBC/RAPID; O/H BY MFG, WO R73432, DATED 5/22/2008. VALVE ASSY FAILED IN STUCK IN OPEN POSITION, WHEN INITIALLY TESTED FOLLOWING INSTALLATION. REPLACED VALVE WITH ANOTHER RAPID-SUPPLISDR 2008FA0000455Relay · stuckINVESTIGATED PILOT REPORT OF RT ENG STARTER/GEN NOT DISENGAGING FROM START FUNCTION AFTER ENG START. FOUND 80K5 RT ENG START LATCH RELAY STUCK IN START FUNCTION. RT STARTER/GEN TERMINAL COVER AND COOLING AIR INLET DUCT SHOW SIGNS OF OVERHEATING. INSPECTED STASDR 2008FA0000348Actuator · malfunctionedIN CONJUNCTION WITH REPAIRS FOR UNCOMMANDED ROLL, TRIM ACTUATION AT KMDW REPLACED RT ROLL TRIM ACTUATOR (HBC PN 390-3810090010) WITH RAPID SUPPLIED REPAIRED UNIT. ATTEMPTED TO PERFORM ROLL TRIM FUNCTIONAL CHECKS IAW THE 390 MM 27-10-00-501 AFTER ACTUATOR REPLASDR 2008FA0000275Wire · brokenAFTER LANDING, THE PILOT WAS INFORMED BY FUEL TRUCK DRIVER THAT LT MLG IB DOOR WAS NOT PROPERLY LOCKED IN THE UP POSITION, AND THE OB PORTION OF THE DOOR HAD MADE CONTACT WITH THE RUNWAY DURING LANDING. ENGINEERING DEPT RECOMMENDED THAT THE AC BE FLOWN BACK USDR 2008FA0000274Door · damagedTHE PILOT WAS INFORMED BY THE FUEL TRUCK DRIVER THAT THE LT MLG IB DOOR WAS NOT PROPERLY LOCKED IN THE UP POSITION, AND THE OB PORTION OF THE DOOR HAD MADE CONTACT WITH THE RUNWAY DURING LANDING. ENGINEERING DEPT RECOMMENDED THAT THE AIRPLANE BE FLOWN BACK UN
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