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 CA030619002Relay · failed(CAN) WHEN THE LANDING GEAR WAS SELECTED DOWN ON APPROACH THE GEAR FAILED TO EXTEND. A MANUAL EXTENSION WAS CARRIED OUT. MAINT JACKED THE AIRCRAFT AND SELECTEDGEAR UP AND THE GEAR AGAIN WOULD NOT MOVE. TROUBLESHOOTING FOUND THAT THE ABOVE RELAY WAS EXTREMELY HSDR 06092003Relay · failedLANDING GEAR FAILED TO EXTEND USING GEAR SELECTOR - HAND PUMPED GEAR DOWN.SDR 051603Diaphragm · rupturedLOW PSI FUEL PUMP FOUND LEAKING ON RAMP - RUPTURED DIAPHRAGMSDR CA030516002Circuit Board · inoperative(CAN) DURING TAKE-OFF ROLL, PILOT NOTICED THAT AUTO-FEATHER SYSTEM DID NOT ILLUMINATE TO IDENTIFY ARM FUNCTION. PILOT INITIATED REJECTED TAKE-OFF, ADVISED ATC & SUBSEQUENTLY RETURNED TO AIRPORT. MAINTENANCE WAS CONTACTED TO INSPECT AND TROUBLESHOOT AUTO FEATSDR 051003Circuit Breaker · inoperativePILOT REPORTED THAT HE HAD TO MANUALY EXTEND THE LANDING GEAR.SDR 040503Switch · wornPILOT REPORTED HAVING TO CYCLE THE LANDING GEAR TO GET THE LEFT MAIN TO INDICATE DOWN AND LOCKED (GREEN) - MAINTENANCE REPLACED THE LEFT MAIN GEAR DOWN AND LOCK SWITCH.SDR NSVA200300022Smoke · detectedAFTER NR 2 ENG START AND TAXI OUT OF GATE CREW NOTICED THE APPEARANCE OF SMOKE IN THE COCKPIT AND IN CABIN. AIRCRAFT RETURNED TO GATE AND MAINTENANCE DISPATCHED. MAINTENANCE INSPECTED RT GENERATOR AND FOUND RESIDUAL OIL. CLEANED OIL AS REQUIRED. PERFORMED SDR 2004F00000Engine · making metalPILOT REPORTED NR 1 ENGINE OIL PRESSURE SLOWLY DROPPED TO RED LINE AND THE LOW OIL PRESSURE LIGHT CAME ON. ENGINE WAS SECURED AND THE AIRCRAFT WAS LANDED AT ANCHORAGE WITHOUT INCIDENT. INSPECTION REVEALED HEAVY METAL CONTAMINATION IN THE OIL FILTER, FERROUS SDR ACE030320031Diaphragm · rupturedFUEL WAS FOUND LEAKING FROM NR 1 ENGINE GANG DRAIN - REPLACED LOW PSI FUEL PUMP. DETERMINED THAT DIAPHRAGM WAS RUPTUREDSDR NSVA200300016Door Latch · seizedLEB-Crew reported door handle stiff with door open or closed and button stuck on handle for airstair door. MX R&R Airstair door latch and lock assembly IAW Beech AMM 52-10-00. Op's check good.SDR NSVA200300015Smoke · detectedDURING IN FLIGHT FUNCTIONAL CHECK-CREW NOTED SMOKE IN COCKPIT AND CABIN DURING CLIMB OUT FROM HEF. CREW TURNED OFF BLEED AND ENVIRON MODE TO OFF. APPROACH AND LANDING WAS UNEVENTFUL. MX PERFORMED COMP WASH, INSPECTED OIL FILTER, RAN ENGINE TO CHECK FOR ANY SDR NSVA200300011Downlock Switch · inoperativeFINAL INTO BKW-PILOT REPORTED DURING GEAR EXTENSION, DID NOT GET GREEN LIGHT INDICATION FOR NOSE GEAR DOWN AND LOCKED. CREW RETRACTED GEAR AND PERFORMED A MANUAL EXTENSION IAW WITH CHECKLIST, STILL NO LIGHT FOR NOSE GEAR. CREW DECLARED IN FLIGHT EMERGENCY (IFSDR NSVA200300006Odor · detectedDURING FLIGHT THE LIGHTS/FLIGHT CIRCUIT BREAKER POPPED OUT. CIRCUIT BREAKER WAS RESET AND THEN POPPED AGAIN. THEN A STRONG ODOR OF ELECTRICAL DISCHARGE. THE BACKLIGHTING OF THE CAPTAIN AND CO-PILOTS INSTRUMENTS THEN WENT OUT.SDR GLBA2003018TransmitterHIGH OIL PRESS RT ENG, R&R LH OIL PRESS TRANSMITTER OPS CKE LEAK CKE GOODSDR NSVA200300010Skin Panel · wornDetail inspection: Captains partition lug receptacle (in cabin area) elongated and cracked. MX - Removed damaged area and installed doubler repair IAW Field repair FR-CO-00816 REV, dated 02/13/03.SDR FFS2003F00017Skin · corrodedEXTERIOR SKIN OF AIRSTAIR DOOR SHOWED CORROSION BLISTERS UNDER PAINT. COIN TAP INSPECTION REVEALED AREAS OF DISBOND FROM HONEYCOMB CORE. INTERNAL INVESTIGATION FOUND MISSING, CORRODED PATCHES OF HONEYCOMB APPARENTLY CAUSED BY MOISTURE INTRUSION THROUGH THE HSDR CA030214005Switch · failed(CAN) PUSH TO TALK SWITCH REPLACED AFTER FAILURE. NEW PUSH TO TALK SWITCH FAILED WITH 4.7 HOURS USED. SWITCH COMPLETELY BROKEN TO PIECES. ONLY CREW ACTION WAS TO USE HAND MICROPHONE AND HAVE CAPTAIN SIDE DO THE MAJORITY OF COMMUNICATION.SDR OIZ2003F00002Angle · crackedDURING THE ACCOMPLISHMENT OF THE A.D., A SMALL CRACK WAS FOUND IN THE LEFT VERTICAL TO HORIZONTAL STABILIZER FAIRING ANGLE. THE CRACK WAS LOCATED IN THE APPROXIMATE CENTER OF THE ANGLE AND ALONG THE UPPER SECTION (HORIZONTAL STABILIZER SIDE) OF THE BEND RADIUSDR OIZ2003F00001Angle · crackedDURING THE ACCOMPLISHMENT OF AD, A SMALL CRACK WAS FOUND IN THE LEFT VERTICAL TO HORIZONTAL STABILIZER FAIRING ANGLE. THE CRACK WAS LOCATED IN THE APPROXIMATE CENTER OF THE ANGLE AND ALONG THE UPPER SECTION (HORIZONTAL STABILIZER SIDE) OF THE BEND RADIUS. THSDR FFS2003F00016Manifold · brokenWHEN TRANSFERRING FUEL FROM ONE MAIN TANK TO ANOTHER, THERE WAS A SOUND LIKE A HAMMER HITTING THE PIPES. NARROWED IT DOWN TO THE RIGHT MAIN FUEL TANK, FUEL MANIFOLD CHECK VALVE SPRING WAS BROKEN AND THE VALVE WAS CHATTERING, WHEN PRESSURE WAS APPLIED.SDR CA030130002Seal Ring · stuck(CAN) AFTER ENGINE START, THE TORQUE READING INDICATED APPROX 3000 FT/LBS. POWER INCREASES OR DECREASES HAD LITTLE EFFECT. TROUBLESHOOTING WAS PERFORMED. A TORQUE INDICATION SYSTEM CALIBRATION TESTER WAS CONNECTED AND INDICATION WAS NORMAL. A TEST GAUGE WAS SDR 2004F00027Bulkhead · crackedMAINTENANCE DISCOVERED MULTIPLE CRACKS ON THE FORWARD PRESSURE BULKHEAD, LOWER RT CORNER OF P/N 114-410026-6 WEB ASSY, AT THE UPPER END OF STIFFENER P/N 114-410026-55 AND AT STATION 84. THIS CRACK WAS APPROX 2 INCHES LONG. ANTICIPATE FINDING THAT THERE WAS ASDR NSVA200300003Handle · looseIN FLIGHT, INSIDE DOOR HANDLE FELL OFF.SDR 2004F00019Spring · brokenLOW FUEL PRESSURE LIGHT CAME ON IN FLT, ELECTRIC BOOST PUMP WAS TURNED ON AND EXTINGUISHED LIGHT. MAINTENANCE REMOVED THE LOW PRESSURE FUEL PUMP AND FOUND THE DRIVESHAFT HAD SHEARED. THE PUMP WAS REPLACED. DISASSEMBLY OF THE PUMP DISCLOSED THAT THE POPPET VSDR FFS2003F00012Rivet · looseSLIGHT MOVEMENT DETECTED BETWEEN TORQUE ADAPTER AND TORQUE TUBE WHEN ELEVATORS WERE LOADED IN OPPOSITE DIRECTIONS.SDR 2004F00011Bulkhead · crackedON OPERATIONAL CHECK FLIGHT FOR PRESSURIZATION CHECKOUT, AIRCRAFT FAILED TO MAINTAIN MAXIMUM CABIN PRESSURE ON SINGLE ENGINE BLEED AIR. MAINT DISCOVERED MULTIPLE CRACKS ON FORWARD PRESSURE BULKHEAD, LOWER RT CORNER OF P/N 114-410026-6, WEB ASSY AT UPPER END OFSDR 2004F00018Downlock Switch · inoperativeAT LANDING IN ANCHORAGE, THE GEAR GREEN SAFE LIGHT DID NOT ILLUMINATE. THE LANDING WAS COMPLETED WITHOUT INCIDENT. MAINTENANCE CONFIRMED THE PROBLEM WAS THE NOSE GEAR ACTUATOR DOWNLOCK SWITCH. (M)SDR 2003FA0000211Torque Tube · excess playFOUND LOOSE RIVETS ON HORN ADAPTER ATTACHED TO LT ELEVATOR TORQUE TUBE PN 1016100195.SDR VFGR435LRivet · looseFOUND LOOSE RIVETS ON FLANGE ADAPTER ATTACHED TO L/H ELEVATOR TORQUE TUBE ASSEMBLY P/N 101-610019-5.SDR NSVA200300002Torque Tube · wornOn or about 12/20/2002 aircraft N51031 (ACTT 24504.0, ACTC 39671) was in for scheduled maintenance (# 6 Detail). Mechanics found that the LH elevator torque tube (crank)was worn where the rivets secure the inner and outer portion of the torque tube together. TSDR CA030112008Seal · failed(CAN) DURING MAINTENANCE CHECK FLT, BEECHCRAFT 1900 HAD AN UNCOMMANDED DEPRESSURIZATION. DESCRIPTION OF THE EVENT WERE AS FOLLOWS, WHILE CLIMBING THROUGH AN ALTITUDE OF 10500 FT. FORWARD CABIN DOOR ENUNCIATOR LIGHT ILLUMINATED AND WHILE COMPLETING THE EMERGSDR 2004F00017Indicator · failedAIR RETURN DUE PILOTS ENCODING ALTIMETER FAILURE, FLAGGED. (M)SDR FFS2003F00008Seal · misalignedFOUND BAFFLE SEALS BETWEEN FORWARD AND AFT NACELLE BULKHEADS, BOTH ENGINES TO BE TRAPPED BETWEEN BULKHEADS, NOT ALIGNED WITH THEM. THIS WILL CAUSE BULKHEADS TO CRACK.SDR YAD2003F00000Pump · failedIN CRUISE FLIGHT, RT ENGINE LOW FUEL PRESSURE ANNUNCIATOR CAME ON AND THE ENGINE SHUT DOWN (FLAMEOUT)-THE AIRCRAFT MADE AN UNEVENTFUL LANDING AT AN ALTERNATE AIRPORT. POST LANDING VISUAL INSPECTION AND GROUND RUNS DID NOT IDENTIFY ANY ABNORMALITIES. ENGINE ASDR 2004F00023Actuator · failedON LANDING IN AKN, NOSE GEAR DOWN AND LOCK LIGHT FAILED TO ILLUMINATE. FERRY TO ANCHORAGE AFTER VERIFYING GEAR DOWN AND LOCKED, GREEN LIGHT CAME ON DURING TAXI OUT. COULD NOT DUPLICATE FAILURE ON GROUND. REPLACED NOSE GEAR ACTUATOR FOR T/S. (M)SDR AUS20021466Governor · faulty(AUS) LT ENGINE PROPELLER GOVERNOR FAULTY. SUSPECT CAUSED BY STICKING PILOT VALVE.SDR FFS2003F00006Seal · misalignedDURING INSPECTION OF THE RT FORWARD COWLING ASSEMBLY, IT WAS FOUND THAT THE AFT BULKHEAD HAD CRACKED AT THE LOWER MOUNT HOLES. WHEN THIS BULKHEAD IS BOLTED TO THE CORRESPONDING BULKHEAD FOR THE REAR COWLING ASSY, A SEAL INCORPORATED IN THE COWL ASSEMBLY. FSDR CA030112006Skin · delaminated(CAN) ON DECEMBER 20, 2002 UPON ARRIVAL OF THE AIRCRAFT AT THE OTTAWA BASE, THE FLIGHT CREW REPORTED THE CABIN DOOR HINGE COVER CRACKED. SUBSEQUENTLY, OUR CONTRACTED AMO INFORMED US OF LOOSENESS FOUND AT THE ATTACHING POINT OF THE MAIN CABIN DOOR HINGE. FURTHESDR OIZ2003F00000Socket · damagedON 12/15/02 DURING TAKEOFF ROLL OUT OF VGT, BOTH TORQUE GAUGES BEGAN SPINNING. CREW ABORTED TAKEOFF, TAXIED BACK TO RAMP. AID OF CREW, MAINT HAD ENG RUN UP TO POWER AND NOTED: ALL INDICATIONS WERE NORMAL. A/C WAS GROUNDED AND TROUBLESHOOTING OF TORQUE INDISDR YAD2003F00001Switch · inoperativePILOT REPORTED NO NOSE GEAR DOWN INDICATION FOR LANDING. MAINTENANCE VERIFIED FAILURE OF THE NOSE GEAR ACTUATOR DOWN LOCK SWITCH-REPLACED NOSE GEAR ACTUATOR.SDR 2004F00014Annunciator · inoperativePILOT REPORTED THAT THE NOSE GEAR DOWN AND LOCK GREEN LIGHT WAS INTERMITTENT. MAINTENANCE REPLACED THE GEAR DOWN AND LOCK ANNUNCIATOR. (M)SDR 2004F00022Connector · dirtyAT LANDING IN ANCHORAGE, THE GEAR GREEN SAFE LIGHT DID NOT ILLUMINATE FOR 30 SECONDS AFTER THE SECOND EXTENSION ATTEMPT. THE LANDING WAS COMPLETED WITHOUT INCIDENT. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM AND CLEANED CONNECTORS AND PERFORMED A SATISFACTOSDR 2004F00021Wire · corrodedAT LANDING IN ANCHORAGE, THE GEAR UNSAFE LIGHT CAME ON AT LANDING FLARE. THE GREEN SAFE LIGHT REMAINED ON. THE LANDING WAS COMPLETED WITHOUT INCIDENT. MAINTENANCE REPAIRED BROKEN/CORRODED WIRES AT THE NOSE GEAR DOWN SWITCH BY REPLACING THE SWITCH. (M)SDR 2004F00016Relay · contaminatedON APPROACH TO LANDING IN ANCHORAGE, THE PILOT SELECTED LANDING GEAR DOWN TWICE WITH NO EFFECT. THE GEAR WAS EXTENDED MANUALLY AND THE LANDING WAS WITHOUT INCIDENT. MAINTENANCE CONFIRMED THAT THE HYDRAULIC PUMP RELAY WAS FREEZING, HIGH MOISTURE CONTENT IN UNSDR 2004F00026O-Ring · displacedRIGHT THROTTLE FROZE AT ALTITUDE. MAINTENANCE FOUND THE NR 2 AIR SEAL, AT CENTER CONSOLE DISPLACED. REPLACED CONTROL ASSEMBLY. (M)SDR 2004F00020Connector · dirtyAT LANDING IN ANCHORAGE, PILOT REPORTED HAD TO PUMP THE LANDING GEAR HAND PUMP TO RECEIVE A GREEN SAFE NOSE GEAR ILGHT, HANDLE WARNING WAS NOT ILLUMINATED. MAINTENANCE COULD NOT DUPLICATE, CLEANED NOSE GEAR ACTUATOR AND DOWNLOCK SWITCH CONNECTORS, CHECKED NOSSDR 2004F00013Connector · damagedAT LANDING IN ANCHORAGE, PILOT REPORTED MLG WAS SLOW TO GO DOWN, THE LANDING GEAR WARNING HORN WOULD NOT SILENCE AND INTRANSIT LIGHTS REMAINED ON WITH THREE GREEN SAFE LIGHTS ALSO ON. MAINTENANCE COULD NOT DUPLICATE. REPLACED PCB FOR WARNING HORN FAULT, RESESDR AUS20021332Wire · loose(AUS) LANDING GEAR CONTROL CIRCUIT BREAKER WIRE P270D8 LOOSE.SDR ACE1115021Diaphragm · leakingMAINTENANCE REPLACED THE LOW PRESSURE FUEL PUMP DUE FUEL LEAKING FROM PRESSURE RELIEF PUMP DUE FUEL LEAKING FROM PRESSURE RELIEF CRANE SB. 101SB023 CONCERNING RELIEF COVER SCREW TORQUES AND LEAKS. POST REMOVAL TEARDOWN REVEALED A RUPTURED CONTROL DIAPHRAGM. SDR FFS2002F00008Latch · brokenLOWER AFT AIRSTAIR DOOR LATCH CABLE BROKE, PREVENTING DOOR BEING OPENED. PASSENGERS HAD TO EXIT THRU CARGO DOOR. WHEN THE AIRSTAIR DOOR IS CLOSED, ANY DIRT OR MOISTURE ON THE TREADS IS FUNNELLED TOT HE LOWER PULLEY FOR THIS CABLE. THIS CABLE IS BLENDED AND
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