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 = '1900C' 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 = '1900C' 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 YADA20180426001Lens · detachedLEFT WING TIP NAV STROBE LENS COVER LOST INFLIGHT.SDR EPUA2018042000001Rivet · crackedBS 531 FRAME RIVETS WERE FOUND FAILING WITH RADIAL CRACKS.SDR JDWA201804190001Fuel Control · malfunctionedDURING APPROACH, THE NR 1 POWER OUTPUT REDUCED AND WOULD NOT RESPOND TO INPUT. THE ENGINE WAS SHUT DOWN AND AIRCRAFT LANDED WITHOUT INCIDENT. TROUBLESHOOTING REVEALED NO DAMAGED P3 OR PY LINES. REPLACED FUEL CONTROL UNIT.SDR JIKA2018042000001Panel · shortedTHE PILOT REPORTED AFTER TAKE-OFF, THAT THE CIRCUIT BREAKER PANEL LOCATED ON THE RIGHT SIDE OF THE COCKPIT WAS EMITTING SMOKE AND SAW SPARKS COMING FROM THE PANEL. FOLLOWED PROCEDURES AND WAS ABLE TO STOP THE SPARKS BY DISABLING THE CIRCUIT. RETURNED AND LASDR EPUA20180309001Light · inoperativeNOSE GEAR DOWN ANNUNCIATOR DOES NOT ILLUMINATE AND DOES NOT TEST. FLIGHT CREW DIVERTED AND DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY. MAINTENANCE REPLACED ANNUNCIATOR BULBS, PERFORMED MULTIPLE GEAR SWINGS, OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.SDR YADA20180227001Bolt · failedDURING TAXI OUT FOR DEPARTURE, MADE A 180 DEGREE TURN AT THE TAKEOFF END OF THE RUNWAY. TURNED TO THE LEFT USING NOSE STEERING, DIFFERENTIAL POWER AS WELL AS THE BRAKE TO GET THE NOSE TO CASTER FURTHER AROUND. TRYING TO STRAIGHTEN OUT THE AIRPLANE WAS VERY DSDR YADA2018022218001Gasket · failedRIGHT BLEED AIR ANNUNCIATOR ILLUMINATED INFLIGHT. RIGHT OVERTEMP SENSOR GASKET FAILED MELTING THE EVA TUBING.SDR TIMA20180214003Governor · openPROPELLER DID NOT COME OUT OF FEATHER AFTER A PROPELLER CYCLE CHECK DURING RUN-UP. REPLACING THE OVERSPEED GOVERNOR ELIMINATED THE PROBLEM. THE DUMP VALVE OF THE OVERSPEED GOVERNOR STUCK IN THE OPEN POSITION.SDR TIMA20180206002Trim System · malfunctionedELECTRIC ELEVATOR TRIM ACTUATED UN-COMMANDED. THE PILOT PRESSED THE 'TRIM DISCONNECT' BUTTON WHICH STOPPED THE ELECTRIC TRIM OPERATION.SDR TIMA20180126001Switch · failedLANDING GEAR FAILED TO FULLY EXTEND WHEN SELECTED. THE GEAR WAS PUMPED DOWN MANUALLY. THE LANDING GEAR CONTROL CIRCUIT WAS FOUND OPEN THROUGH THE SWITCH, WHICH DETECTS THAT THE NOSE ACTUATOR IS IN THE EXTENDED TO THE DOWN POSITION. WHEN THIS SWITCH FAILED,SDR YADA20180118001Scavenge Pump · leakingMAINTENANCE DISCOVERED THAT THE NR 2 ENGINE OIL SCAVENGE PUMP HOUSING WAS LEAKING THROUGH THE CASTING. OIL SCAVENGE PUMP HOUSING WAS REMOVED AND REPLACED.SDR JIKA2018011602Valve · bypassingTHE PILOT REPORTED ON APPROACH, WHEN THE LANDING GEAR WAS SELECTED DOWN, DID NOT RECEIVE A THREE GREEN DOWN AND LOCKED GEAR INDICATION AND THE LANDING GEAR CONTROL CIRCUIT BREAKER TRIPPED. THE PILOT RESET THE CIRCUIT BREAKER, CYCLED THE LANDING GEAR AND RECSDR JIKA2018011601Tube · collapsedTHE PILOT REPORTED THAT THE LEFT ENGINE OIL PRESSURE BEGAN FLUCTUATING NEAR THE LOW REDLINE. THE PILOT PERFORMED A PRECAUTIONARY INFLIGHT SHUT DOWN OF THE LEFT ENGINE AND DIVERTED. LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE LEFT ENGINE AND FOUND OIL SDR YADA20180102001Actuator · failedPILOT REPORTED THAT THE LANDING GEAR FAILED TO FULLY RETRACT, AIRCRAFT RETURNED TO HOME STATION. MAINTENANCE REMOVED AND REPLACED RIGHT MAIN LANDING GEAR ACTUATOR, OPERATIONAL CHECK SUCCESSFUL.SDR YADA20171226001Actuator · crackedWHILE PERFORMING HEAVY MAINTENANCE INSPECTION AND SCHEDULED X-RAY OF NLG ACTUATOR CAP, TEST RESULTS SHOWED NOSE LANDING GEAR ACTUATOR CAP TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR ACTUATOR WITH SERVICEABLE.SDR YADA20171218001Unknown · odorCLIMBING THROUGH 10,000 FT, SMELLED A BURNING PLASTIC SMOKE, UP TO 20,000 FT. DURING DESCENT THROUGH 14,000 FT, THE ODOR DISAPPEARED. MAINTENANCE PERFORMED TROUBLESHOOTING OF SURROUNDING AREAS AND CHECKED WIRES FOR ANY BURN INDICATIONS, UNABLE TO SEE ANY BUSDR YADA20171205001Rib · crackedWHILE PERFORMING HEAVY MAINTENACE VISUAL INSPECTION FOUND LARGE CRACK ON LEFT HAND WING INBOARD LEADING EDGE RIB P/N: 114-120033-45. MAINTENANCE REMOVED AND REPLACED LEADING EDGE RIB IAW BEECH SRM.SDR EPUA20171116001Light · intermittentNOSE WHEEL LOCK LIGHT INTERMITTENT, BULB WORKS FINE. EMERGENCY GEAR EXTENSION COMPLETED. AIRCRAFT LANDED SAFELY WITH NO DAMAGE TO AIRCRAFT. MAINTENANCE IS CURRENTLY TROUBLESHOOTING LANDING GEAR SYSTEM FOR CAUSE OF NOTED DEFECT.SDR EPUA20171110001Cabin Pressure · failedDURING FLIGHT AT 18,000 FEET THE CABIN ALTITUDE WARNING INDICATOR ILLUMINATED. CABIN PRESSURIZATION HAD FAILED. MAINTENANCE IS CURRENTLY WORKING ON RESOLVING THIS DEFECT. NO OTHER INFORMATION AVAILABLE AT THIS TIME.SDR JIKA2017102401Unknown · malfunctionedTHE PILOT WAS ON APPROACH TO KCRP AND WHEN THE LANDING GEAR SELECTOR WAS SELECTED TO THE GEAR DOWN POSITION, THE GEAR WOULD NOT EXTEND. THE HANDLE ILLUMINATED RED AND THE LANDING GEAR CONTROL CIRCUIT BREAKER TRIPPED. THE PILOT RESET THE CIRCUIT BREAKER ONCE ANSDR YADA20171020001Control Head · smokeON ENGINE SHUTDOWN, THE PILOT NOTICED AN ELECTRICAL ODOR, ACCOMPANIED WITH SMOKE COMING FROM THE CENTER CONSOLE AUTO-PILOT CONTROL HEAD. MAINTENANCE CONFIRMED THE SMOKE WAS FROM AUTO-PILOT CONTROL HEAD BOX, AND REMOVED THE COMPONENT.SDR YADA20171018001Door Frame · crackedDURING MAINTENANCE VISUAL INSPECTION OF AIRSTAIR DOOR, FOUND A CRACK ON AIRSTAIR DOOR FRAME TO BE OUT OF LIMITS IAW SRM 53-90-08. AIRSTAIR DOOR FRAME WAS REPLACED.SDR EPUA20171201001Engine · contaminatedSTRONG ODOR FROM ENVIRONMENTAL SYSTEM DURING TAKE OFF AND CLIMB. AIRCRAFT ENGINES RAN, ODOR SEEMED TO BE RESIDUAL ENGINE WASH PRODUCT. RAN ENGINES TO CLEAR ODOR. NO FURTHER DEFECTS NOTED.SDR YADA20170926002Door Frame · crackedWHILE PERFORMING MAINTENANCE INSPECTION DURING A,B,C CHECK FOUND CRACK ON CARGO DOOR FRAME P/N:114-430125-5 AT F.S.: 509.50 . CRACK IS 1.6 INCHES LONG AND BEYOND LIMITS. FRAME SECTION WILL BE REPLACED AND DOUBLER INSTALLED.SDR YADA20170926001Door Frame · crackedWHILE PERFORMING MAINTENANCE INSPECTION DURING A,B,C CHECK FOUND MULTIPLE CRACKS AT AIRSTAIR DOOR FRAME. ONE LOCATED ON FRAME P/N:114-420041-37 AND ONE LOCATED ON AIRSTAIR DOOR CHANNEL P/N:114-420041-41. BOTH CRACKS ARE BEYOND LIMITS AND PARTS WILL BE REPLACEDSDR JIKA2017092501Connector · unsecureTHE PILOT REPORTED ON TAKEOFF THAT THE GEAR SELECTOR SAFETY J HOOK DID NOT AUTOMATICALLY RETRACT AFTER LIFTOFF, MANUALLY RETRACTED THE J-HOOK AND SELECTED THE LANDING GEAR SELECTOR TO THE UP POSITION. THE RIGHT MAIN GEAR DOWN INDICATION (GREEN LIGHT) EXTINGUSDR YADA20170905001Control Cable · contaminatedPILOT REPORTED THAT THE ELEVATOR (PITCH) FROZE OR BOUND UP WHILE IN CRUISE FLIGHT FROM (ANC) FLYING INTO (SDP). MECHANIC REMOVED FLOOR BOARDS IN TAIL SECTION AND INSPECTED PULLEYS AND CABLES. FOUND PUDDLES OF WATER IN ZONES 5&6 AND ALSO BY ELEVATOR PULLEYS JUSSDR YADA20170821001Windscreen · crackedPILOTS WINDSCREEN CRACKED IN FLIGHT.SDR EPUA20170817001Skin · corrodedDURING SCHEDULED INSPECTION, DEFECTS WERE NOTED AT STRINGER 15R AT BS 355.75 FOUND TO BE DEBONDED FROM THE SKIN WITH CORROSION.SDR TIMA20170816012Tire · separatedPOST FLIGHT INSPECTION REVEALED A SECTION OF TREAD MISSING FROM THE LEFT INBOARD TIRE. THE MISSING TREAD WAS A STRIP MEASURING APPROXIMATELY 2 X 16 INCHES. IT IS ASSUMED THAT THE TREAD SEPARATED DURING LANDING SINCE THE PRE FLIGHT INSPECTION REVEALED NO DAMASDR YADA20170812001Tcas System · malfunctionedPILOT REPORTED- "HE RECEIVED A CLEARANCE FROM RADIO, THAT WAS PASSED FROM ATC, "ON DEPARTURE TURN LEFT HEADING 090 AND MAINTAIN 4,000 FT." AS WE CLIMBED THROUGH 2,000 FT, CHECKED IN WITH CENTER AND WAS GIVEN A NEW ALTITUDE OF "CLIMB AND MAINTAIN FL21000." AS WSDR TIMA20170811011Line · chafedAFTER A NORMAL TAKEOFF, THE PILOT WAS UNABLE TO MAINTAIN CLIMB POWER AND TORQUE ON THE LT ENGINE. AS POWER CONTINUED TO DECREASE, THE PILOT SHUT DOWN THE LT ENGINE AND RETURNED TO DEPARTURE FOR AN UNEVENTFUL LANDING. INSPECTION REVEALED THAT THE PRIMARY FUSDR YADA2017081100001Arm · wornON LANDING, THE NR 2 ENGINE FAILED TO GO INTO REVERSE AFTER LANDING.SDR JIKA2017270702Warning System · activatedTHE PILOT REPORTED HE WAS EN-ROUTE FROM KCRP TO KMAF WHEN THE RIGHT ENGINE OIL PRESSURE WARNING LIGHT BEGAN TO ILLUMINATE ON AND OFF WITH NO CHANGE IN OIL PRESSURE INDICATION. THEN AFTER A MINUTE OF FLIGHT THE OIL PRESSURE WARNING LIGHT CAME ON STEADY WITH A SDR YADA20170727001Indication Sys · malfunctionedAFTER TAKEOFF, THE AIRCRAFT EXPERIENCED A GPS, VOR, AND ADF ERROR THAT LASTED APPROXIMATELY 7-8 MINUTES. THE COURSE LINE ON THE NR 2 GPS WAS OFF TO THE RIGHT BY APPROXIMATELY 2 MILES FROM THEIR POSITION. THE NR 1 GPS WAS INDICATING A COURSE LINE IN THE OPPOSITSDR TIMA20170628010Skin Panel · corrodedDURING A MAINTENANCE INSPECTION OF THE FUSELAGE EXTENSIVE CORROSION WAS DISCOVERED IN THE LOWER FUSELAGE SKIN ASSEMBLY. THE CONDITION WAS CORRECTED BY THE INSTALLATION OF NEW FUSELAGE SKIN PANELS.SDR YADA20170621001Sensor · failedPILOT REPORTED THE LEFT ENVIRONMENTAL FAIL DURING CLIMB OUT, PILOT CYCLED ENVIROMENTAL SYS OFF THEN OPEN AND RECEIVED THE RIGHT ENVIROMENTAL FAIL LIGHT. MAINTENANCE REMOVED AND REPLACED CENTER TEMPATURE SENSOR AND OPERATIONAL CHECKS WERE SUCCESSFUL.SDR EPUA20170531001Fire Loop · defectiveRIGHT ENGINE FIRE DETECT ILLUMINATED FOR APPROXIMATELY 10 SECONDS IN FLIGHT. PILOT RETURNED TO BASE AND MAINTENANCE DETERMINED THAT THE RIGHT ENGINE FORWARD FIRE LOOP WAS DEFECTIVE THUS GIVING A FALSE FIRE WARNING. MAINTENANCE REPLACED DEFECTIVE FIRE LOOP ANSDR YADA20170515001Fcu · unresponsivePILOT REPORTED THAT THE LEFT HAND ENGINE WAS UNRESPONSIVE TO POWER LEVER INPUT AND WOULD NOT COME OUT OF IDLE. MAINTENANCE PERSONAL REMOVED AND REPLACED THE LEFT HAND ENGINE FUEL CONTROL UNIT, PERFORMED RIGGING, OPERATIONAL AND LEAK CHECKS OF THE LEFT HAND ENGSDR YADA20170430001Bulb · inoperativePILOT REPORTED THE LEFT FIREWALL FUEL VALVE FIRE WARNING LIGHT IS INOPERATIVE, AIRCRAFT RETURNED TO HOME STATION, MAINTENANCE REPLACED BULB IN LEFT SIDE TEE HANDLE, OPERATIONAL CHECK OF FIRE WARNING SYSTEM WAS SUCCESSFUL.SDR TIMA20170321006Seat Track · corrodedDURING A SCHEDULED STRUCTURAL INSPECTION OF THE FUSELAGE, THE RT AFT SEAT TRACK WAS FOUND TO BE CORRODED IN SEVERAL AREAS.SDR TIMA20170321005Seat Track · corrodedDURING A SCHEDULED STRUCTURAL INSPECTION OF THE FUSELAGE, THE LT AFT SEAT TRACK WAS FOUND TO BE CORRODED.SDR YADA20170320001Door Frame · crackedAIR STAIRS DOOR FRAME CRACKED ALONG BOTTOM AFT SECTION.SDR YADA20170315001Door Frame · crackedFORWARD AIR STAIRS DOOR FRAME CRACKED ALONG BOTTOM AFT SECTION BEHIND FUSELAGE HALF OF THE HINGE.SDR JIKA2017031300001Hydraulic System · inadequateLANDING GEAR FAILED TO EXTEND AFTER PLACING THE LANDING GEAR CONTROL DOWN. LANDING GEAR CIRCUIT RELAY CIRCUIT BREAKER TRIPPED AND GEAR HANDLE UNSAFE LIGHT REMAINED ILLUMINATED. THE PILOT PERFORMED MANUAL EXTENSION PROCEDURES AND THE AIRCRAFT LANDED WITHOUT FUSDR YADA20170308002Frame · crackedWHILE AIRCRAFT WAS IN SCHEDULED HEAVY MAINTENANCE, MECHANIC WAS PERFORMING VISUAL C-CHECK AND FOUND A CRACK IN FRAME AT FS 509.50, WL 96 APPROXIMATELY (JUST AFT OF CARGO DOOR). P/N:114-430125-5SDR YADA20170308001Frame · crackedWHILE AIRCRAFT WAS IN SCHEDULED HEAVY MAINTENANCE, MECHANIC WAS PERFORMING VISUAL C-CHECK AND FOUND A CRACK IN FRAME P/N:114-430121-33 AT FS 456.00 APPROXIMATELY WL 96(JUST FORWARD OF CARGO DOOR).SDR YADA20170303001Exhaust Duct · disconnectedPILOT REPORTED THAT THE RIGHT ENGINE FIRE LIGHT FLICKERS DURING TAXI. MAINTENANCE FOUND THAT THE RIGHT ENGINE INBOARD EXHAUST STACK TUBE WAS DISCONNECTED. MAINTENANCE RE-CONNECTED TUBE, OPERATIONAL CHECK SUCCESSFUL.SDR YADA20170224001Intake Duct · unsecurePILOT REPORTED THE RIGHT HAND ENGINE FIRE LIGHT ILLUMINATED DURING TAKEOFF ROLL, ORIGINAL TAKEOFF WAS ABORTED. MAINTENANCE FOUND #2 ENGINE INBOARD NACELLE INTAKE HEAT DUCT WAS UNSECURED. SECURED DUCT AND OPERATIONAL TEST WAS SUCCESFULL.SDR TIMA20170223003Switch · failedDURING TAKEOFF ROLL BAGGAGE DOOR ANNUNCIATION ILLUMINATED. PILOT ABORTED TAKEOFF. INSPECTION REVEALED THE NOSE BAGGAGE DOOR SWITCH HAD FAILED.
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