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 2008FA0000273Door · damagedAFTER ROUTINE FLIGHT, THE PILOT WAS PERFORMING HIS PREFLIGHT WALKAROUND INSP IN PREPARATION FOR THE NEXT LEG OF THE FLIGHT. HE NOTICED THAT BOTH MLG OUTER DOORS WERE DAMAGED. MECH/ MAINT WENT TO EVALUATE THE DAMAGE TO THE DOORS. RECOMMENDED THAT THE AIRPLANSDR 2008FA0000272Door · damagedAFTER ROUTINE FLIGHT, THE PILOT WAS PERFORMING HIS PREFLIGHT WALKAROUND INSP IN PREPARATION FOR THE NEXT LEG OF THE FLIGHT. HE NOTICED THAT BOTH MLG OUTER DOORS WERE DAMAGED. MECHANIC/MAINT WENT TO EVALUATE THE DAMAGE TO THE DOORS. RECOMMENDED THAT THE AIRPSDR 2008FA0000011Strut · leakingPILOT REPORTED LT AND RT MAIN LANDING GEAR STRUTS LEAKING HYDRAULIC FLUID. DISASSEMBLY LOWER LT MAIN LANDING GEAR STRUT, FOUND PAINT CHIPS CONTAMINATING SEALS. DISASSEMBLED RT LOWER MAIN LANDING GEAR STRUT, FOUND PAINT CHIPS CONTAMINATING SEALS AND METAL FILLISDR 2008FA0000010Strut · leakingPILOT REPORTED LT AND RT MAIN LANDING GEAR STRUTS LEAKING HYDRAULIC FLUID. DISASSEMBLY LOWER LT MAIN LANDING GEAR STRUT, FOUND PAINT CHIPS CONTAMINATING SEALS. DISASSEMBLED RT LOWER MAIN LANDING GEAR STRUT, FOUND PAINT CHIPS CONTAMINATING SEALS AND METAL FILLISDR 2007FA0001043Stop · distortedPILOT REPORTED LANDING GEAR UNLOCKED INDICATION AFTER GEAR RETRACTION AFTER TAKEOFF. FOUND NLG STOPPER ASSY DAMAGED AND PREVENTING NLG ASSY FROM CENTERING AND ENGAGING UPLOCK ASSY. REPLACED STOPPER ASSY AFTER NLG DISASSEMBLY AND INSPECTION, LANDING GEAR OPERSDR JAS2007F00000Packing · failed(CONTROL NR JAS-SDR-OO1) FLUCTION OF HYDRAULIC PRESSURE. DEFECTIVE/DAMAGED PN MS28778-6 PACKING. FLIGHT CREW COMPLETED ABNORMAL CHECKLIST. UPON INSPECTION, FOUND THAT PACKING AT HYDRAULIC PUMP PRESSURE OUTLET FITTING HAD FAILED. THIS COMPONENT WAS WORKED OSDR 2007FA0000945Pump · damagedHYDRAULIC PUMP ASSY, PN 390-389022-0003, INSPECTED AND FOUND NOT DEFECTIVE. FOUND DEFECTIVE/ DAMAGED PART PN MS28778-6, PACKING. FLIGHT CREW COMPLETED ABNORMAL CHECKLIST. UPON INSPECTION FOUND THAT PACKING AT HYDRAULIC PUMP PRESSURE OUTLET FITTING HAD FAILESDR SX42007F00000Controller · malfunctionedFAILURE OF BLEED HEAT TEMP CONTROL SYSTEM LT AND RT. BOTH SIDE ENUNCIATED OVERHEAT. SELECTED BLEEDS OFF, RETURNED TO DEPARTURE. LANDING UNEVENTFUL. (K)SDR GC4N200700001Actuator · faultedAFTER COMPLAINT FROM THE PILOT OF NOT GETTING A NOSE LANDING GEAR DOWN LIGHT STRAIT AWAY, PLACED THE AIRCRAFT ON JACKS AND CARRIED OUT 4 RETRACTIONS WHICH RESULTED IN 100 PERCENT FAILURE OF THE NOSE LANDING GEAR FULLY EXTENDING, AFTER FAULT FINDING WE BELIEVE SDR ERYA200715901Switch · malfunctionedUNCOMMANDED PITCH, ROLL, AND YAW. UNABLE TO ARREST UNCOMMANDED INPUTS OR CORRECT UNCOORDINATED FLIGHT CONTROLS WITH ANYTHING OTHER THAN REDUCTION OF THRUST TO REDUCE FORCE ON FLIGHT CONTROL SURFACES. RUDDER TRIM SWITCH REPLACED.SDR 2007FA0000699Shutoff Valve · jammedPILOT REPORTED RT ENGINE HYDRAULIC SHUTOFF VALVE WOULD NOT CLOSE FOLLOWING PREFLIGHT CHECKS. FOUND VALVE ASSY STUCK OPEN. REPLACED VALVE ASSY WITH NEW VALVE ASSY, OPERATIONS NORMAL. VALVE ASSY (PN 45AS65014003) HAVE NOTICED THESE VALVE ASSY TENDING TO FAIL SDR 2007FA0000626Valve · stickingPILOT REPORTED RT HYDRAULIC SHUTOFF VALVE INITIALLY STUCK DURING PREFLIGHT TEST, THEN OPENED. REPLACED VALVE WITH NEW UNIT, FUNCTIONAL TESTS, OK. REMOVED VALVE ASSY, PN 39045AS65014-003, MANUFACTURED 11/2005. (K)SDR 2007FA0000460Connector · faultyTROUBLESHOT INTERMITTENT ANTI-SKID SYSTEM FAIL ANNUNCIATION, CABIN DOOR SEAL STAYING INFLATED ON GROUND, AND LIFT DUMP HANDLE OPERATION. FOUND BAD CRIMP ON PIN (L) FOR WIRE G117B24 IN LT MLG SQUAT SWITCH CONNECTOR. FUNCTIONAL CHECKS OK. (K)SDR 2006FA0000942Flap Track · damagedDURING 200/600 HR PHASE INSPECTION FOUND THE RT IB AFT FLAP TRACK UPPER 3 ATTACH FASTENERS PN: MS90354S0609 WORKING. RECOMMEND ADDITIONAL ATTENTION TO FLAP RIGGING AND ALL ATTACHING HARDWARE DURING PHASE INSPECTION. (K)SDR 2006FA0000941Flap Track · damagedDURING 200/600 HR PHASE INSPECTION FOUND THE RT IB AFT FLAP TRACK UPPER 3 ATTACH FASTENERS PN: MS90354S0609 WORKING. RECOMMEND ADDITIONAL ATTENTION TO FLAP RIGGING AND ALL ATTACHING HARDWARE DURING PHASE INSPECTIONS. (K)SDR 2006FA0000940Flap System · misriggedDURING PHASE INSPECTION FOUND THE LT IB AFT FLAP TRACK ATTACH BOLT CHAFED 3 LAYERS OF CARBON FIBER INTO THE FUSELAGE. FOUND FLAP MISRIGGED AND TOP 3 FLAP TRACK FASTENERS WORKING. RECOMMEND ADDITIONAL ATTENTION TO FLAP RIGGING AND ALL ATTACHING HARDWARE DURINSDR 2006FA0000831Washer · misinstalledDURING WHEEL DISASSEMBLY FOR TIRE REPLACEMENT FOUND WHEEL TIE BOLT CHAMFERED WASHERS INSTALLED INCORRECTLY, WITH CHAMFERED SIDES TOWARDS WHEEL HALF. NOTED WASHERS TO BE BENT, WHEEL TIE BOLT HEADS UNDERSIDE RADIUSES DAMAGED. SUSPECT TECHNICIAN ASSEMBLY WHEELSSDR 2006FA0000830Washer · misinstalledDURING WHEEL DISASSEMBLY FOR TIRE REPLACEMENT FOUND WHEEL TIE BOLT CHAMFERED WASHERS INSTALLED INCORRECTLY, WITH CHAMFERED SIDES TOWARDS WHEEL HALF. NOTED WASHERS TO BE BENT, WHEEL TIE BOLT HEADS UNDERSIDE RADIUSES DAMAGED. SUSPECT TECHNICIAN ASSEMBLING WHEESDR DEBA401PP2Switch · malfunctionedON ACCELERATION FOR TAKEOFF THE CREW RECEIVED A TAKEOFF CONFIGURATION WARNING HORN AT 100KTS, PRIOR TO ROTATION. TAKEOFF WAS ABORTED WITHOUT INCIDENT. THE AIRCRAFT RETURNED TO THE RAMP. WHILE TROUBLESHOOTING THE PROBLEM CORRECTED ITSELF. DETERMINED THAT TSDR 2005FA0001584Hose · chafedDURING INITIAL 200 HOUR INSPECTION FOUND LT ENGINE MOTIVE FLOW FUEL LINE HOSE ASSY CHAFED BY ADJACENT COWL LATCH. REPLACED HOSE ASSY. AND REROUTED, SECURED AS REQUIRED FOR CLEARANCE. AIRCRAFT ABOVE SN RANGE OF AD AND MSB. (K)SDR DEBA401PP1Unknown · unknownAIRCRAFT WOULD NOT PASS THE BIT CHECK ON PREFLIGHT. CONTACTED NEAREST AUTHORIZED RAYTHEON SERVICE CENTER FOR SERVICE OF THE NITROGEN BOTTLE, BOTTLE WAS JUST AT THE BOTTOM OF THE GREEN. THE THOUGHT WAS THAT IT CAUSED A LOW PRESSURE INDICATION AND MADE THE BITSDR 2005FA0001557Tube · chafedINVESTIGATED HYDRAULIC FLUID LEAKAGE FROM RT ENGINE AREA. FOUND RT ENGINE HYDRAULIC PUMP TO DAMPER TUBING ASSY CHAFED BY ADJACENT CLAMP AND SEEPING FLUID. REPLACED TUBE AND SECURED AS REQUIRED KIT INSTALLED 5.9 HRS PREVIOUS FOR COMPLIANCE WITH AD. (K)SDR 2005FA0001488Actuator · failedINSTALLED .0 TIME SINCE FACTORY, MODIFIED NR 1L FLAP ACTUATOR AS PART OF COMPLIANCE WITH MFG MSB. (FLAP FAIL) ANNUNCIATOR ILLUMINATED AFTER INSTALLATION. FLAP SYSTEM TROUBLESHOOTING SHOWED FAULT CODES 2,8 AND THEN 1,2, 8. ANNUNCIATOR NOT ILLUMINATED AFTER RSDR 2005FA0001487Actuator · failedINSTALLED .0 TIME SINCE FACTORY MODIFIED NR 2R FLAP ACTUATOR AS PART OF COMPLIANCE WITH MFG MSB. (FLAP FAIL) ANNUNCIATOR ILLUMINATED AFTER INSTALLATION. FLAP SYSTEM TROUBLESHOOTING SHOWED FAULT CODES 3, 8 AND THEN 1,3, 8. ANNUNCIATOR NOT ILLUMINATED AFTER RSDR V2J2005F00000Flap System · failedTHE FLAP/SPOILER SYSTEM ON THIS AIRCRAFT IS PLAGUED WITH FAILURES, THERE ARE MORE OF THESE REPORTS TO FOLLOW. (EA25200510358) (K)SDR V2J2005F00001Flap System · inoperativeTHE FLAP/ SPOILER SYSTEM ON THIS AIRCRAFT IS PLAGUED WITH FAILURES. THERE ARE MORE OF THESE REPORTS TO FOLLOW. (EA25200510359) (K)SDR 2005FA0001107Solenoid · seizedREF: (PT1838110) DOOR SOLENOID FAILED IN OPEN POSITION. WITH EITHER ENGINE RUNNING, THE DOOR COULD NOT BE OPENED/CLOSED DUE TO INFLATED SEAL. SOLENOID REPLACED, OPERATIONAL CHECK GOOD. (K)SDR 2005FA0000835Bolt · chafedUPON REMOVAL OF FLAP ACTUTORS FOUND NR 3 LT AND RT FLAP ACTUATORS WERE DEEPLY GOUGED, DUE TO FLAP TRACK BOLTS INSTALLED BACKWARDS. PN OF BOLT NAS6205-18D. REMOVED BOLT AND INSPECTED AND REINSTALLED IN THE CORRECT DIRECTION. (K)SDR 2005FA0000468Tuning Unit · brokenDURING REPLACEMENT OF LT BI-FLOW CONTROL VALVE IN CONJUNCTION WITH A SCHEDULED INSPECTION, FOUND PNEUMATIC TUBE IN LT PYLON AREA BENT AND CRACKED IN HALF. SUSPECT MAY BE CAUSED DUE TO PREVIOUS ROUGH HANDLING OR FORCING TUBING DURING BI-FLOW VALVE REPLACEMENT SDR E8I2004F00000Control Valve · inoperativePILOT REPORTED NO BRAKING ACTION WITH HARD PEDAL PRESSURE, AIRCRAFT STOPPED ON ROLL-OUT WITH EMERGENCY BRAKING SYSTEM. TROUBLESHOT POWER BRAKE SYSTEM. REPLACED PN 3903843000003 (CRANE-HYDRO AIRE PN 388111) POWER BRAKE/ ANTISKID SYSTEM CONTROL VALVE WITH REPASDR 2004FA0000781Circuit Breaker · wrong partREPORTED THAT THE WING ICE LIGHT C/B SWITCH TRIPS AFTER BEING IN (ON) POSITION FOR 3-4 MINUTES. TROUBLESHOOTING REVEALED THAT A 3 AMP C/B HAD BEEN INSTALLED IN A 7 AMP CIRCUIT AT POSITION 33CB15. INSPECTING THE OTHER C/B SWITCHES REVEALED THAT POSITION 33CB6, SDR E8I2004F00001Actuator · jammedPILOT REPORTED UNABLE TO RETRACT OR EXTEND FLAPS FROM 10 DEGREES EXTENDED POSITION. TROUBLESHOT SYSTEM, FOUND RT IB FLAP IB ACTUATOR JAMMED. REPLACED ACTUATOR WITH NEW PN 3903814020013 ACTUATOR IAW 390 MM 27-50-03-401 AND RIGGED FLAPS AS REQUIRED IAW MM 27-5SDR 2004FA0000887Skin · crackedTHE RT WINGTIP HAS A CRACK APPROXIMATELY 7 INCHES LONG ON THE FAR OB END, AFT HALF OF THE WINGTIP. THE CRACK RUNS FORE / AFT ON THE WINGTIP.SDR RB570001Position Switch · out of adjustJUST NORTH OF PXR CLIMBING THROUGH FL310, GOT A "CABIN DOOR UNLOCKED" CAUTION LIGHT. RAN THE CHECKLIST, COMMUNICATED WITH ATC AND ASKED FOR LOWER (12000 FT). BRIEFED THE PAX, AND PROCEEDED ON TO VNY. ON ENGINE SHUTDOWN, VISUALLY INSPECTED THE CABIN DOOR ANDSDR CGO2003F00004Relay · inoperativeTROUBLESHOT COMPLAINT OF LT ENGINE NOT CRANKING. FOUND 80K1 LT ENGINE START RELAY COIL NOT ENERGIZING OR CLOSING CONTACTS WITH POWER TO COIL INPUTS. REPLACED RELAY, STARTER CRANKING OPERATIONS NORMAL. HAVE NOTED THIS SAME COMPONENT TO BE CAUSE OF SIMILAR FASDR CGO2003F00000Transmitter · leakingINVESTIGATED FUEL LEAK, FOUND IN RT ENGINE COMPARTMENT DURING ROUTINE 200 HR INSPECTION. FOUND FUEL TO BE LEAKING INTERNALLY INTO TRANSMITTER ELECTRICAL CONNECTOR AREA. OVERHAULED REPLACEMENT PART RECEIVED HAD SAME FAULT . PART MFG, SUSPECT PART HAS DESIGN SDR MGO2002F00000Line · splitPNEUMATIC LINE PROVIDES FOR A MOISTURE DRAIN POINT FOR THE PNEUMATIC MANIFOLD WHICH PROVIDES REGULATED AIR PRESSURE TO THE HYDRAULIC PACKAGE THE PRIMARY OUTFLOW VALVE, THE COCKPIT ALTERNATE AIR VALVE AND PASSENGER DOOR SEAL. LINE IS BULGED AND SPLIT 1.250 INCSDR CGO2002F00007Transducer · leakingINVESTIGATED PILOT COMPLAINT OF FUEL PUDDLING IN BOTTOM OF LT COWLING. FOUND FUEL FLOW INDICATING TRANSDUCER LEAKING INTERNALLY. FIRST TRANSDUCER REPLACED AT 132.8 HRS FOR SAME FAULT. INSTALLED OVERHAULED UNIT, LEAK CHECKED OK. NOTED ON TEAR DOWN REPORT FOSDR 2002FA0001321Switch · inoperativeHIGH RESISTANCE (8 OHMS) IN RIGHT LOW NR THROTTLE LEVER SWITCH. 6 OHMS MAX PER SPEC SHEET. SPOILER CONTROL UNIT RECEIVES ELECTRICAL SIGNAL FROM LOW N1 THROTTLE SWITCH AS A SUBSYSTEM TO SATISFY LIFT DUMP EXTEND AND RETRACT LOGIC. SCU WILL NOT EXTEND OR RETRASDR RB23Squat Switch · disconnectedUPON DEPARTURE FROM ADDISON TX LANDING GEAR HANDLE WAS UP BUT RED LIGHT WAS ILLUMINATED. GEAR APPEARED TO NOT HAVE RETRACTED. GEAR SUBSEQUENTLY RETRACTED, BUT UPON FURTHER TESTING WOULD NOT EXTEND. DIVERTED TO SAN ANTONIO SAT AND USED ALTERNATE GEAR EXTENSISDR 2002F00781Fitting · brokenTHE FITTING IS PLASTIC WITH A .8750 INCH FUEL HOSE ATTACHED, THE HOSE IS AT AN ANGLE WHICH PUTS A SIDE LOAD ON THE FITTING AND THE FITTING BROKE WHERE THREADS END THAT SCREW IN TO THE CHECK VALVE.
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