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 engine_model_key = 'CF343B' 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 engine_model_key = 'CF343B' 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 CA150408028Shaft · failed(CAN) WHILE OPENING THE PASSENGER DOOR, THE AFT COUNTER BALANCE CABLE GUIDE SHAFT FAILED. INSPECTION OF THE DOOR IDENTIFIED NO FURTHER RELATED DEFECTS. NO DEFICIENCIES WERE IDENTIFIED WITH THE GUIDE SHAFT AT THE LAST INSPECTION. THE FAILED GUIDE SHAFT IS BEISDR CA150327005Panel · corroded(CAN) MULTIPLE PANELS IN ACFT WERE FOUND CORRODED. CORROSION REMOVED, SOME OF THE CORROSION HAS GONE ENTIRELY THROUGH THE SURFACE OF THE HONEYCOMB PANEL.SDR CA150304006Flex Drive · cracked(CAN) FOUND DURING INSPECTION, 4 FLEX SHAFT ASSEMBLIES CRACKED ON THE SWAGED FITTING ENDS ON 2 THRUST REVERSERS ON OUR ACFT. 2 WERE FOUND ON THE LT ENGINE AND 2 ON THE RT ENGINE. 3 WERE PN 121754-2 AND ONE 121754-3. LOOKING AT THE FAILED PARTS IT APPEARS THSDR CA150128006Element · damaged(CAN) WE COMPLETED THE PREFLIGHT AND DEPARTED AS SCHEDULED. EVERYTHING WAS NORMAL, UNTIL AROUND 1530Z, ABOUT 10-15 MILES AWAY FROM CALLS (A FIX ON THE ILS 11L IN TUS), WE GOT THE RED L 14TH DUCT, CAS MESSAGE, AND THE OVERHEAD RED 14TH STAGE DUCT FAIL LIGHT. WESDR CA150115003Microwave Oven · malfunctioned(CAN) WHILE IN CRUISE FLIGHT AT 40,000, ONE OF THE PASSENGERS WAS USING THE GALLEY MICROWAVE OVEN. WHILE IN USE, THE MICROWAVE P/N 400-2577-01 STARTED SPARKING AND SMOKING. THE CB TRIPPED STOPPING THIS NOTED ACTION. CB WAS LEFT OUT DURING THE REMAINDER OF THE SDR CA150113028Manifold · failed(CAN) CREW REPORTED ON TAXI CHECK OUT OF VANCOUVER GROUND SPOILERS WOULD NOT RETRACT - TROUBLESHOOTING CARRIED OUT USING CL605 WM 27-61-00 AND ROCKWELLCOLLINS PSEU SENSOR DISCRETE DATA LABEL 271-274, LABEL 274 BIT 28 FOUND AT 0 INDICATING NO RETURN HYDRAULIC PSDR CA141217018Connector · damaged(CAN) WHILE CARRYING OUT TASK AMM 27-34-07-000-801. UPON REMOVAL OF THE TRANSMITTER, WE NOTICED A ROLL PIN/STOP WAS BENT, AND HAD INDICATIONS OF CONTACT WITH ANOTHER STOP PIN. WITH THE UNIT PROPERLY INSTALLED, THERE IS NO INDICATION THAT THESE PINS SHOULD BE SDR CA141219008Windshield · cracked(CAN) LEFT WINDSHIELD SURFACE FACE PLY CRACKED IN CRUISE. AS A RESULT RAPID DELAMINATION OCCURRED, WHICH LEAD TO THE BREAKUP OF THE FACE PLY. FACE PLY PIECES DEPARTED THE WINDSHIELD MAKING CONTACT WITH THE LEADING EDGE OF THE VERTICAL & HORIZONTAL STABILIZERSDR CA141217014Duct · ruptured(CAN) LT ENGINE ANTI-ICE DUCT RUPTURE. DURING REPOSITION FLIGHT, LH ENGINE ANTI-ICE DUCT RUPTURED. THEY HAD IN FLIGHT "L COWL A/ICE" MESSAGE, SO THEY SWITCHED OFF ENG ANTI ICE AND DIVERTED TO AERODIENST. THE AIRCRAFT LANDED SAFELY BUT THE LEFT THRUST REVERSESDR CA141128011Fuel Control · malfunctioned(CAN) ABORTED TAKEOFF DUE TO LEFT ENGINE SHUTDOWN DURING TAKEOFF. DURING TAKEOFF AT ABOUT 20 KNOTS & 60% N1, THE ENGINE BEGAN TO SPOOL DOWN UNCOMMANDED. THE ENGINE GRADUALLY SPOOLED DOWN & THE ENGINE SHUTDOWN. MAINTENANCE INSPECTED THE ENGINE & FOUND THAT ISDR RU3A20141107040Valve · leakingRT 14TH STAGE DUCT LIGHT RED ILLUMINATED WITH RED MASTER CAUTION LIGHT. REPAIRED LEAK AT 14TH STAGE BLEED AIR VLV.SDR CA141107002Line · loose(CAN) DURING A DAILY INSPECTION, A LOOSE LT NR 1 HYD SYS LINE/PIPE WAS NOTED. FURTHER INVESTIGATION REVEALED THE INSERT OF A FAIR LEAD BLOCK WAS WORN, ALLOWING THE PIPE TO VIBRATE, AND THE RUBBER INSERT FOR AN ADEL CLAMP WAS DETERIORATED WHICH ALLOWED HEAVY CHSDR RU3A20141105039Valve · leaking14TH DUCT FAIL LIGHT ILLUMINATED TWICE. RT 14TH STAGE BLEED AIR VLV LEAKING AT ENG SIDE OF VLV, LOOSENED CLAMPS, REPOSITIONED VLV & TIGHTENED CLAMPS.SDR R61A201410271141Bolt · failedABOUT 10 MILES FROM DESTINATION, RECEIVED MULTIPLE E2 FADEC FAULTS AND THE ENGINE DROPPED TO IDLE. ATTEMPTED TO RE-ENGAGE TLA CONTROL BUT THE ENGINE WOULD NOT RESPOND AND THE AUTO THROTTLE TURNED OFF. RAN QRH AND DECLARED AN EMERGENCY. LANDED WITHOUT INCIDSDR CA141028007Trunnion · corroded(CAN) FOUND CORROSION AROUND FWD AND AFT ATTACHMENT BUSHINGS DURING PERFORMANCE OF SB ON MLG MAIN FITTING ASSEMBLIES. REPAIRED.SDR CA141010018Heater · burned(CAN) WHEN DOING MAINTENACE WITH THE EXTERNAL POWER CONNECTED, THE AVIONIC TECHNICIAN SMELLED SMOKE COMING FROM THE CABIN. AFTER DISCONNECTING THE EXTERNAL POWER AND THE SMOKE WAS GONE, THEY FOUND OUT THAT THE CAUSE WAS THE WATER LINE HEATER AND THE SURROUNDISDR CA140915008Engine · flamed out(CAN) AT FL360 IN CRUISE A NOISE SOUNDING LIKE A FAN WAS HEARD. 10 MIN THE ENGINE FLAMED OUT. AIRCRAFT DIVERTED AND LANDED OVERWEIGHT.SDR CA141202031Gear · fractured(CAN) AT FL360 LEFT ENGINE FLAMED OUT. EMERGENCY LANDING CARRIED OUT. FOUND LEFT ENGINE GEARBOX FAILURE. DECIDED TO BORESCOPE THE RIGHT ENGINE. FOUND CRACK IN AXIS P GEAR. REMOVED GEARBOX.SDR CA140910011Tire · damaged(CAN) ON TAKEOFF, THE NR 3 MAIN WHEEL TIRE FAILED AND LOST ITS RUBBER. THE TIRE IS A NEW TIRE NOT A RE-TREAD, AND HAS 152 CYCLES, 258.8 HOURS SINCE IT WAS INSTALLED. THE RUBBER COMING OFF DAMAGED THE AIRCRAFT LANDING GEAR WARNING WEIGHT OFF WHEEL PROX SWITCH, SDR J7SA201408250147Cabin Pressure · malfunctionedOVER PRESSURIZATION OCCURED AT FL400. SWITCHED TO MANUAL MODE WITH NO CONTROL ON CABIN PRESSURIZATION.SDR CA140702014Cowl Door · departed(CAN) ON DEPARTURE CREW FELT ACFT SHUDDER SLIGHTLY. ACFT HANDLED NORMALLY ALL INDICATIONS WERE NORMAL. AT DESTINATION, DISCOVERED RT ENGINE UPPER CORE COWL WAS MISSING.SDR 2014FA0000293Hose · rupturedTHE SILICONE RUBBER HOSE, THAT ATTACHES THE ECU WATER SEPARATOR TO A RESTRICTOR IN THE DRAIN LINE, RUPTURED PREMATURELY. THE REPLACEMENT PART, SUPPLIED BY MFG, HAS A SEAM IN THE HOSE, INTRODUCED DURING MFG. THE HOSES ARE SPLITTING ON THIS SEAM AND CREATING ASDR CA140423012Blade · loose(CAN) ENGINE WAS REMOVED FROM THE ACFT AFTER BORESCOPE INSPECTION REVEALED SUBSTANTIAL DAMAGE IN THE COMPRESSOR. ONCE INSPECTED IN THE SHOP, IT WAS NOTED THAT APPROXIMATELY 6 COMPRESSOR BLADES IN THE 12TH STAGE WERE MISSING, CAUSING DAMAGE FROM STAGES 12-14. SDR CA140408001Engine · smoke(CAN) SMOKE FROM ENGINE NR 1 AFTER START.SDR CA140521007Light · burned(CAN) WHILE WORKING ON THE ACFT, MAINTENANCE CREW FOUND THAT THE CIRCUIT BREAKER FOR THE FLOODLIGHTS WAS DISENGAGED, RESETTING THE BREAKER JUST RESULTED IN IT POPPING AGAIN. THE CUSTOMER WAS INFORMED AND THEY GAVE THE GO AHEAD TO FAULT FIND THE PROBLEM. THE SDR CA140227001Flap Track · broken(CAN) DURING A DAILY INSPECTION ON THE 24TH OF FEBRUARY A HEAVY WRINKLE WAS FOUND ON THE LT INBD FLAP. FURTHER INVESTIGATION FOUND THE FAIRING OVER THE FLAP TRACK PULLED DOWN AT THE FRONT. UPON REMOVAL OF THE FLAP TRACK FAIRING THE FORWARD ATTACH BRACKET FORSDR CA140225010Sensor · burned(CAN) THE ACFT WAS POWERED BY APU GENERATOR ONLINE. AFTER 30 MINS, WHEN THE HYDRAULIC PUMP TURNED ON, THE FOLLOWING CIRCUIT BREAKER WAS POPPED OUT, 115 VAC ESS FEED, ESSAC TRANSFER CONT). THE SMOKE CAME FROM BEHIND THE CAPTAIN SIDE CIRCUIT BREAKER PANEL CBP-SDR CA140217020Manifold · failed(CAN) PROXIMITY SYS FAULT, STATUS MESSAGE ON POWER UP. R & R GROUND SPOILER MANIFOLD. PERFORMED BLEED LEAK AND OPS CHECK OF GROUND SPOILER SYSTEM.SDR CA140214001Thrust Reverser · unwanted deploy(CAN) LEFT THRUST REVERSER UNCOMMANDED DEPLOYMENT ON THE TAKEOFF ROLL AT 70 KTS. LT ENGINE OVERHEAT MESSAGE ALSO PRESENT. TAKEOFF ABORTED, ENGINE SHUTDOWN AND ACFT RETURNED TO STAND.SDR CA140120020Wire · failed(CAN) DURING A DAILY INSPECTION, IT WAS NOTED THAT THE TAIL LOGO LIGHTS WOULD NOT ILLUMINATE. INVESTIGATION OF THE SYS FOUND BOTH BULBS SERVICEABLE WITH NO POWER AT THE LIGHT ASSEMBLIES. FURTHER INVESTIGATION REVEALED A CHAFED WIRE THRU A BULKHEAD GROMMET LOSDR CA131118016Selector Valve · failed(CAN) PILOT REPORT: FUEL ON BOARD DURING OCCURRENCE: 9.100 LBS PAX ON BOARD: 2 CREW ON BOARD: 3 SPEED AT OCCURANCE: 170 KTS WEATHER CONDITIONS DURING OCCURRENCE: 1430Z ILS26 V260-320/1MS 10KM OVC 1200M 5/-1 QNH 1029 NOSIG "GEAR DISAGREE" WHEN CLEARED FOR THSDR CA131111013Throttle Cable · seized(CAN) LEVEL AT 12,000 FT INBOUND, THRUST WAS BROUGHT TO IDLE FOR DESCENT. PRONOUNCED RT YAW AND CREW OBSERVED LT ENGINE STILL AT CRUISE THRUST. CREW ADVANCED LT THRUST LEVER AND N1 INCREASED. BROUGHT TO IDLE AGAIN, AND THRUST STAYED AT THE INCREASED LEVEL. SDR CA131113007Selector Valve · failed(CAN) AIRCRAFT COMING IN FOR LANDING, AFTER LANDING, GEAR HANDLE MOVED TO DOWN POSITION, ONLY NLG EXTENDED, DOWN, BOTH MLG REMAIN IN RETRACTED, UP, POSITION. PILOTS FOLLOWED THE CHECKLIST WHERE IT STATES TO CYCLE THE LANDING GEAR HANDLE, BUT IT WAS NOT POSSIBSDR EBVR20130618001Support · crackedFOUND CRACKS LOCATED IN THE SWITCH SUPPORTS ON BOTH LT AND RT THRUST REVERSERS.SDR CA130531011Engine · flamed out(CAN) DURING FLIGHT AT CRUISE FL360 .78M, ALL ENGINE INDICATIONS WERE NORMAL WHEN A CLIMB WAS INITIATED TO FL380. CLIMBING THROUGH FL370 THE RIGHT ENGINE ROLLED BACK TO IDLE. CONTINUOUS IGNITION WAS ACTIVATED BUT THE ROLL BACK CONTINUED. IN-FLIGHT ENGINE FAILSDR CA140613002Drain Valve · failed(CAN) THE AUTOMATIC DRAIN VALVE, INSTALLED IN THE LOWER GALLEY OF CL-605, A/C FAILED ALLOWING WATER TO LEAK OUT OF ITS VENT HOLE AND INTO THE GALLEY AND UNDER THE FLOOR INTO THE AVIONICS BAY AND SOAKED THE INSULATION BLANKETS INSTALLED BETWEEN FS 280R AND FS 3SDR CA130502007Engine · bird ingestion(CAN) DURING CLIMB, ACFT EXPERIENCED STRONG VIBRATION ON RT ENGINE, CREW RETURN TO GROUND SAFE AND DISCOVER RT ENGINE HAD A BIRD STRIKE.SDR CA130313005Angle · misinstalled(CAN) DURING THE FLIGHT SPOILER SPECIAL DETAILED INSPECTION, PROCEDURE ET-57-70-001, DUE AT 1200 CYCLES IT WAS FOUND THAT THE ANTI-ROTATION PLATE INSTALLED AT APPROXIMATELY RWS 218.00 , THE OTBD BOLT ON THE RT FLIGHT SPOILER WAS THE INCORRECT PN A 600-10343-43SDR CA130118004Oil System · low pressureLEFT ENGINE OIL PRESS, CAS MESSAGE ON THE START OF THE DESCENT A RED, LT ENGINE OIL PRESSURE, CAS MESSAGE POSTED ON EICAS. CREW BROUGHT LT ENGINE BACK TO IDLE AND FOLLOWED THE AFM PROCEDURES. CREW KEEP AN EYE ON THE ENGINE OIL PRESSURE. WHEN OIL PRESSUE DROSDR CA130111002Engine · malfunctioned(CAN) ALTITUDE FL210, AIRSPEED 210 KIAS TEST POINT ATS RELIGHT OF LT ENGINE PREAMBLE: FOLLOWING A SUCCESSFUL WINDMILL RELIGHT OF THE ACFT LT ENGINE IT WAS AGAIN SHUTDOWN IN THE FIRST STEP OF THE ATS RELIGHT PROCEDURE. DURING THE WINDMILL RELIGHT PROCEDURE ITSDR CA121207005Windshield · cracked(CAN) DURING CRUISE WINDSHIELD CRACKED TOP TO BOTTOM.SDR CA130110010Engine · failed(CAN) DURING A QUICK TURN AT THE OPERATORS HOMEBASE, CREW SMELLED SMOKE IN THE CABIN FOLLOWED BY A RED, APU FIRE, CAS MESSAGE ON EICAS. APU AUTO SHUTDOWN AND CREW SET OFF THE APU FIRE BOTTLE. TRIP WAS CANCELLED. TALK WITH MFG, BELIEVE THE APU COMPRESSOR LET SDR CA121019002Spring · broken(CAN) FOUND BROKEN SPRING ON LT AND RT ENGINE THRUST LOWER REVERSER BLOCKER DOOR LINK ASSY DURING 48 MONTHS INSPECTION.SDR CA120921007Lock Fastener · sheared(CAN) INSPECTION REVEALED A SHEARED LOCK FASTENER PIN ON THE FWD ROW OF FASTENERS OF THE INBD FLAP HINGE FITTING 600-10317-6, INSTALLED AT WS 76.50.SDR KKYA20120919001Engine · overtemp"ENGINE" EICAS ON TAKEOFF ROLL. LEFT ENGINE OVERTEMP.SDR CA130131001Wire Harness · exposed(CAN) THE COCKPIT TOUCH SCREEN SUPPLIES THE ELECTRONIC CHARTS, AIRPLANE DOCUMENTATION AND MANUALS, WEATHER INFORMATION, AND ACCESS TO THE CABINS ELECTRONICS SYSTEM CONTROLS. ELECTRICAL HARNESS IS DAMAGED AT INSTALLATION OR/IN SERVICE. THE HARNESS WAS CRUSHEDSDR CA120505002Cowl Door · detached(CAN) THE RT ENGINE UPPER NOSE ACCESS COWL BECAME DETACHED FROM THE ACFT IN FLIGHT. THE CREW DID OBSERVE SOME BUFFET EFFECT BUT DID NOT KNOW THE CAUSE AT THE TIME. THE MISSING PART WAS DISCOVERED POST LANDING. THE ACFT DID HAVE MAINTENANCE CONDUCTED DURING ANSDR U5QA2012040206038Engine · malfunctionedAPPROXIMATELY 13:15 EDT EN ROUTE FROM TOL TO FXE AT FL390. EXPERIENCED MULTIPLE COMPRESSOR STALLS AND THEN A FLAME OUT OF THE RIGHT ENGINE. THE FLIGHT CREW DECLARED AN EMERGENCY AND INITIATED DRIFT DOWN PROCEDURES TO FL180 (APPROXIMATLEY) AND THEN SUCCESSFSDR CA120404001Compressor · stalled(CAN) DURING CLIMB, FROM FL380 TO FL400, THE RT ENGINE BEGAN TO COMPRESSOR STALL 5-6 TIMES QUICKLY AND BRIEFLY, AS THE CREW, INCREASING POWER AT A SLOW RATE PROPORTIONAL TO THE CLIMB RATE OF THE ACFT. THEIR INDICATED MACH NR WAS APPROXIMATELY .80 AND ENGINES WSDR 2012FA0000278Bracket · crackedTHRUST REVERSER WOULD NOT INDICATE EXTENDED. FOUND BRACKET THAT HOLDS THE RETRACT AND EXTEND SWITCHES TO BE CRACKED AROUND THE EXTEND SWITCH WHICH ALLOWED THE SWITCH TO MOVE WHEN THE THRUST REVERSER CONTACTED IT DURING EXTENSION. CAUSE APPEARS TO BE CRACKING
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