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 = 'CF343B1' 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 = 'CF343B1' 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 SWIA200110063Warning System · activatedWHITE SPOILERON FAULT MESSAGE ON EICAS. RETURN TO GATE AS PER QRH.DEFERRED AS PER MEL 27-65-3. COMPLIED WITH MAINTENANCE PROCEDURE PER MEL. SUPPLEMENTAL REPORT FORTHCOMING. UPDATE 7/26/2001: REMOVED AND REPLACED NR 2 SECU IAW MM 27-60-01. SPOILERS CHECKSDR JBXA000311Engine · failedNR 2 ENGINE OVERTEMPED BEFORE REACHING RATED TAKEOFF POWER. PERFORMED BORESCOPE INSP OF ENGINE IAW 72-00-00-290-02, 72-00-00-290-03, 72-00-00-290-04, 72-00-00-290-05. FAILED INSPECTION, REMOVED AND REPLACED ENGINE IAW 71-00-00.SDR CA010726001Mount · cracked(CAN) DURING AN OPPORTUNITY INSPECTION OF THE ENGINE BEAM, CRACKS WERE FOUND ON THE CENTER SECTION. (REF ASB 601R-53-069.)SDR AUS20010744Windshield · cracked(AUS) LT PILOTS SIDE WINDSHIELD INNER PLY CRACKED DIAGONALLY FROM THE FORWARD LOWER CORNER.SDR JBXA000303Engine · lack of lubeLEFT ENGINE OIL TEMP WAS 168 DEGREES. AFTER RETARDING THROTTLE THE TEMP FELL TO 164 DEGREES. WITH THE THROTTLE AT FLIGHT IDLE THE OIL TEMP DROPPED TO 153 DEGREES. SERVICED NR 1 ENGINE OIL TO PROPER LEVEL IAW CRJ AMM 12-13-00. PERFORMED VISUAL INSPECTION FOSDR CA010725019Mount · cracked(CAN) DURING SUPPORT BEAM INSPECTION, AS PER SB601R-53-059, CRACKS WERE FOUND AT BL0 AND LBL36.SDR CA010726006Mount · cracked(CAN) DURING AN OPPORTUNITY INSPECTION OF THE ENGINE SUPPORT BEAM, CRACKS WERE FOUND ON THE CENTER SECTION. SEE ASBSDR SWIA972662Connector · looseDURING CLIMB OUT THROUGH 18,000 FT LEFT ENGINE HAD UNCOMMANDED ACCELERATION. N1 WENT INTO RED. REDUCED THRUST LEVERS ON LEFT ENGINE SUCESSFULLY AND RETURNED TO SLC. PERFORMED FAN ROTOR N1 OVERSPEED INSPECTION PER RJ MM 71-00-00 PG 504 TABLE 503. NO DEFECTS SDR CA010704024Plate · cracked(CAN) DURING C CHECK, MAINTENANCE FOUND A CRACK LOCATED IN THE PLATE ASSY. RBL 45.00 AT THE JOINT WITH THE FLOOR BEAM SUPPORT ANGLE AT PRESSURE BULKHEAD FS 621.00 THE CRACK WAS CONFIRMED USING NDT INSPECTION.SDR CA010704028Control Unit · failed(CAN) DURING CLIMB PILOT REPORTED EICAS MESSAGE DCU NR 2 AUR AL FAIL, APR FAIL AND FLUCTATION OF ENGINE PARAMET ERS 9N1,N2 & ITT) ON BOTH ENGINES. THEY SELECTED THE APR SWITCH OFF AND THE FLUCTUATIONS WENT AWAY, FLIGHT CONTINUED TO NICE. IT CAME BACK AT 40 NM SDR SWIA972665Pressure Switch · failedINFLIGHT LEFT SCAVENGER EJECTOR CAUTION MESSAGE REPEATELLY ILLUMINATES, INCREASES FREQUENCY WITH VERTICAL SPEED GREATER THAN 1,000 FPM. INSTALLED SCAVENGE EJECTOR PRESSURE SWITCH IAW 28-42-07.SDR CA010704011Beam · cracked(CAN) CRACKS WERE FOUND DURING ENGINE SUPPORT BEAM INSPECTION, AS PER SB601R-53-059.SDR CA010704015Carbon Seal · failed(CAN) BOMBARDIER AEEROSPACE HAS JUST RECEIVED A REPORTABLE SDR EVENT WHICH WE ARE REQUIRED TO REPORT ON. WHILE IN CRUISE FLIGHT THE CREW COULD SMELL AND SEE SMOKE.OXYGEN MASKS WERE DONNED BY THE CREW ANDTHEPAX MASKS WERE DEPLOYED. FLIGHT WAS DIVERTED. UPON INVSDR SWIA972649Controller · inoperativeSHORTLY AFTER TAKE OFF GOT LEFT WINDOW HEAT CAUTION MESSAGE. RETURNED TO FAT. AFTER TROUBLESHOOTING SYSTEM FOUND FORWARD TEMP CONTROLLER INOP AND CANNON PLUGS SWAPPED. PUT CANNON PLUGS IN CORRECT POSITION AND REPLACED FORWARD TEMP CONTROLLER IAW CRJ MM 30-41SDR MASA01058Carbon Seal · failedFLT 6901 - A FERRY FROM AVP-CMH - RETURNED TO THE FIELD IN AVP WHEN THE COCKPIT FILLED UP WITH SMOKE SHORTLY AFTER TAKEOFF. THE CREW WENT ON OXYGEN AND TRIED TO CLEAR THE CABIN OF SMOKE. THE CREW LANDED SAFELY. MAINTENANCE WAS DISPATCHED FROM PHL. MAINTENASDR JBXA000298EngineDiscrepancy: #2 engine borescope inspection task card #021-440-107, HPT stage 1 and 2.Failed inspection.Corrective action: Removed and replaced #2 engine IAW CL-65 AMM 71-00-00.SDR CA010626045Tire · failed(CAN) AFTER TAKE OFF AT GEAR RETRACTION, THE CREW NOTED A LEFT MAIN LANDING GEAR DISAGREEMENT. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL INSPECTED ANDFOUND THAT THE TREADHAD SEPARATED FROM THE LEFT INBOARD MAIN GEAR TIRE DURING TSDR CA010626046Windshield · cracked(CAN) PASSING THROUGH 8,000 FT. THE WINDSHIELD DEVELOPED A CRACK AND SHATTERED. AFTER THE EVENT THE AIRCRAFTIMMEDIATELY RETURNED FORA WINDSHIELD REMOVAL AND REPLACEMENT.SDR CA010627034Oil System · fluctuates(CAN) A/C IN CRUISE AT FL.310, CREW NOTICED FLUCTATION IN OIL PRESSURE WITH A LOSS OF OIL PRESSURE. ENGINE SHUT DOWN BY THE FLIGHT CREW AND LANDED IN PHOENIX. INVESTIGATING AT THIS POINT SHOWS OIL TANK AS GOOD. OIL LEVEL IN GEARBOX IS GOOD. GE ON WING SUPPORT SDR CA010627025Pump · failed(CAN) NR 2 ENGINE OIL PRESSRE BEGAN TO FLUCTATE DURING CRUISE. THE PRESSURE DROP FOLLOWED BY AN INCFREASE IN OIL TEMP. THE PILOT INITIATED AN IN FLIGHT SHUTDOWN. ENGINE OIL PUMP REPLACED.SDR SWIA972641Windshield · failedPASSING THROUGH 10000 FT AT 150 KIAS AND NORMAL RATE OF DESCENT THE CAPTAIN'S FORWARD WINDSHIELD SHATTERED. IT SHATTERED WITH A VERY LOUD BANG. REMOVED AND REPLACED PILOT'S WINDSHIELD WITH SERVICEABLE WINDSHIELD IAW CRJ MM 56-00-00. PN ON NP-13921-9 SN ON SDR SWIA972625Pump · failed30 SECONDS AFTER GEAR WAS SELECTED DOWN, NR 2 HYDRAULIC PRESSURE MESSAGE HYDRAULIC LEVEL IN NR 2 INDICATED 0 PERCENT FLUID. AFTER SHUTDOWN LEVEL ROSE TO 15 PERCENT. EDP RUNNING DRY FOR 5 MINUTES. REPLACED RIGHT ENGINE HYDRAULIC PUMP IAW MM 29-11-01. PN ONSDR CA010626019Check Valve · failed(CAN) DURING APU BLEED TRANSITION TO ENGINES THE APU LCV FAIL LIGHT CAME ON AND OPEN LIGHT REMAINED ON. ABOUT 15 SECONDS THE RT FIRE INDICATION APPEARED, CREW THROTTLED BACK JUST BELOW 70 PERCENT N1 AND THE FIRE WENT OUT. CREW SHUTDOWN ENGINE AND DECLARED EMERSDR CA010627021Web · cracked(CAN) DURING "C" CHECK, SIX CRACKS WERE FOUND INTHE ENGINE SUPPORT BEAM. TWO CRACKS WERE LOCATED ON THE LOWER WEB AT FS 640.0 BETWEEN LBL 9.5 AND RBL 9.5. FOUR CRACKS WERE LOCATED ON THE UPPER WEB AT FS 640 BETWEEN LBL 9.5 REPAIR PERFORMED PER REO 601R-53-61-3SDR CA010627032Engine · malfunctioned(CAN) DURING CRUISE FLIGHT CREW REPORTED LOW OIL PRESSURE AND ASSOCIATED WITH HIGH OIL TEMPERATURE. ENGINE REPLACED AND A/C RETURNED TO SERVICE.SDR SWIA972601Pcu · malfunctionedLEFT SPOILERONS FAULT STATUS MESSAGE ON PDI2 IN FLIGHT. REMOVE AND REPLACE LEFT SPOILERON OUTBOARD PCU IAW 27-62-00 AND RESET CB4CN THEN CLEARED SECU FAIL LOGS. OPS CHECKS GOOD ON FLIGHT CONTROL. NO DEFECTS NOTED AT THIS TIME. P/N ON 27000-7, S/N ON MAL-34SDR SWIA972567Windshield · crackedRIGHT FIRST OFFICERS WINDSHIELD CRACKED ON FINAL APPROACH. REMOVED AND REPLACED THE RIGHT WINDSHEILD ASSEMBLY IAW RII 56-401 AND MM 56-11-01. LEAK AND OPS CHECKS GOOD. P/N ON PPGNP-13921-10, S/N ON 01095H5012, S/N OFF 00083H3537.SDR CA010706017Engine · failed(CAN) ON TAKEOFF R/H ENGINE N2 VIBRATION EXCEEDED LIMITS, IN FLIGH T ENGINE SHUT DOWN CARRIED OUT AND AIRCRAFT RETURNED FOR TROUBLSHOOTINGSDR CA010706019Windshield · failed(CAN) AT FL330 THE CAPTAIN'S WINDSHIELD SHATTERED. NO CONFIRMATION IF PIECES OF WINDOW DEPARTED AIRCRAFT. REMOVED AND REPLACED CAPTAIN'S WINDSHIELD IN ACCORDANCE WITH AMM 54-11-01.SDR SWIA972564Actuator · defectiveLEFT THRUST REVERSER UNLOCK CAUTION MESSAGE AT 1000 FEET AGL AFTER TAKEOFF. NO AUTO LEVER RETARD AND NO BUFFET. RETURNED TO FIELD. LEFT REV UNLOCK LIGHT CAME ON AT TOP OF DESCENT AND STAYED ON UNTIL ENGINE SHUT DOWN. INSPECTED THE LEFT THRUST REVERSER FOUNSDR SWIA972565Windshield · crackedON DESCENT INTO DEN CAPTAINS WINDSHIELD SHATTERED, APPEARED TO BE MIDDLE LAYER. REPLACED CAPTAINS WINDSHIELD IAW CRJ MM 56-11-01 AND SKYWEST CARD RII 56-401. OPS CHECK GOOD ON GROUND. P/N ON: NP-139321-9 S/N ON: 01043H9715 P/N OFF: 601R33033-9 S/N OFFSDR CA010706016Windshield · cracked(CAN) FOUND THE CAPTAIN WINDSHIELD INNER PLY CRACKED ON AN UNSCHEDULED MAINTENANCE INSPECTION. WINDSHIELD REPLACED, AIRCRAFT BACK IN SERVICE.SDR SWIA972547Windshield · crackedAT FL 330, THE CAPT''S WINDSHIELD SHATTERED. REMOVE AND REPLACE CAPTAIN''S WINDSHIELD IAW MM 56-11-01. PRESSURIZED AC IAW 21-31-00 FOR WINDSHIELD REPLACEMENT. OPS CHECK AND LEAK CHECK GOOD. P/N ON 601R33033-9, S/N ON 980048H7587, S/N OFF 00020H8018.SDR CA010511020Gearbox · failed(CAN) RIGHT ENGINE WILL NOT SHUT DOWN USING POWER LEVER.REPLACED THE THROTTLE CONTROL GEAR BOX ASSEMBLY. ENGINE RUNS CARRIED OUT, NO FAULTS FOUND.AIRCRAFT RETURNED TO SERVICE. 2001-05-11 TC: REQUESTING DETAILED INFORMATION FROM ORIGINATOR.SDR CA010511021Harness · inoperative(CAN) CREW ABORTED TAKEOFF DUE TO NR 2 ENGINE OVER TEMPERATURE. MAINTENANCE FOUND ITT THERMOCOUPLE HARNESS PARTIALLY INOPERATIVE. REPLACED HARNESS. NO FURTHER FAULTS FOUND. AIRCRAFT RETURNED TO SERVICE.SDR CA010511014Windshield · cracked(CAN) LT WINDSHIELD CRACKED DURING THE APPROACH. WINDSHIELD REPLACED AND RETURNED TO SERVICE.SDR CA010511016Windshield · fractured(CAN) CAPTAINS WINDSHIELD EXPERIENCED A PLY FRACTURE DURING DESCENT. WINDSHIELD REPLACE, AIRCRAFT RETURNED TO SERVICE.SDR CA010511012Gear · failed(CAN) NR 2 ENGINE OIL PRESSURE DROPPED TO APPROXIMATELY 18 PSI WITH LOW OIL PRESSURE WARNING. ENGINE SHUTDOWN PER QRH. NR 2 ENGINE REPLACED DUE TO GEAR MATERIAL ON THE CHIP DETECTOR.SDR SWIA972527Aileron · jammedAT ABOUT 1000 FT ON FINAL JUST AFTER TURNING AUTOPILOT OFF AILERONS WERE LOCKED UP. AFTER ABOUT 15 TO 20 SECONDS THEY BECAME NORMAL. OPERATED AUTOPILOT WITH ALL 3 HYDRAULIC SYSTEMS, ALSO WITH INDIVIDUAL SYSTEMS ARMED, CONTROL AND INDICATION NORMAL. AP DISCOSDR CA010511026Actuator · failed(CAN) OVERHEAT OF THE ACCUMULATOR, THE ELECTRIC WIING, LOWER ENGINE FAIRING AND THE LOWER CENTRAL PART OF THE NACELLE DUE TO DE-COUPLING OF THE COMPRESSED AIR INTAKE AND THE 10TH STAGE HOT AIR PORTION. THIS COUPLING IS IN A HARD TO READ AREA AND IS HARD TO TIGSDR SWIA972520Warning System · false indicationWING OVERHEAT MESSAGE ON TAKEOFF. ABORTED AT APPROXIMATELY 100 KTS. MESSAGE EXTINGUISHED. OPERATED THE WING ANTI ICE SYSTEM ON THE GROUND AT TAKEOFF POWER. COULD NOT DUPLICATE THE PROBLEM. OPS CHECK GOOD.SDR SWIA972521Switch · faultySTABILIZER TRIM AND MACH TRIM CAUTION MESSAGE CAME ON AFTER TAKEOFF. FOLLOWED QRH, WOULD NOT RE-ENGAGE. AIRCRAFT RETURNED TO THE FIELD. CAT II. REMOVED AND REPLACED FIRST OFFICER''S PITCH TRIM DISCONNECT SWITCH IAW MM 27-41-30. PERFORMED STABILIZER TRIM OSDR SWIA972519Windshield · crackedON DESCENT THROUGH 17,000, LEFT WINDSHIELD SHATTERED. NO LOSS OF PRESSURIZATION AND NO OTHER STRUCTURAL DAMAGE NOTED. REMOVED AND REPLACED LEFT WINDSHIELD IAW RII 56-401 AND MM 56-11-01. OPS CHECKS GOOD. P/N ON PPG-WP-139321-9, S/N ON 0103248940, P/N OFF SDR CA010511005Rod · loose(CAN) AIRCRAFT ENROUTE TO MONTERREY, THE CREW WERE UNABLE TO RETARD THE LEFT HAND THROTTLE LOWER THAN 95 PERCENT. THE CREW RETURNED TO MEMPHIS AND CARRIED OUT QRH ABNORMAL 1-14. MECHANICS FOUND THE HOLD OPEN STRUT OF THE LT ENGINES UPPER CORE COWL JAMMED BETWSDR CA010511008Line · chafed(CAN) UPON CLIMBING, CREW RECEIVED A HYDRAULIC NR 1 LOW PRESSURE MESSAGE, ASSOCIATED WITH A NR 1 SYSTEM, QUANTITY INDICATING ZERO PERCENT. AIRCRAFT DIVERTED TO BIRMINGHAM. MAINTENANCE FOUND A CHAFED STEEL BRAIDE HYDRAULIC LINE IN AFT FUSE. THE LINE IS THE PESSSDR SWIA972510Control Cable · out of adjAT TAKEOFF N1 SETTING NOTICED HIGHER THAN NORMAL ITT TEMPS ON RIGHT ENGINE. ALSO AT GROUND IDLE, NOTICED HIGHER THAN NORMAL N1 SPEEDS AT 28 PERCENT. ADJUSTED RIGHT ENGINE VG ACTUATOR FEED BACK CABLE IAW 72-00-00 SPECIAL PROCEDURE 07. RAN CHECK A/C, ALL RAN SDR SWIA972513Sensor · malfunctionedDISPLAY COOL MESSAGE CAME ON CLIMBING THROUGH 12,000 FEET. TRIED FLT ALT AND STBY POSITIONS ON DISPLAY FAN. MESSAGE REMAINED FOR ABOUT 10 MINUTES. VERIFIED FAN OPERATION IN ALL POSITIONS AND AIR FLOW GOOD, NO LEAKS. REPLACED AIRFLOW SENSOR. OPS CHECK GOODSDR CA010501015Windshield · cracked(CAN) UPON TOUCH DOWN, CAPTAINS WINDSHIELD INNER PLY CRACKED. WINDSHIELD REPLACED.SDR CA010626020Access Door · missing(CAN) AFTER AIRCRAFT LANDED AT CHICAGO O'HARE, IT WAS NOTICED T HAT THE NOSE COWL LOWER ACCESS PANEL (228-50081-142) WAS ON THE RUNWAY. OTHER DAMAGED PARTS WERE NOSE COWL UPPER ACCESS PANEL 228-50080-158 AND COVER ASSEMBLY 228-50793-120. PRIOR TO THIS EVENT THSDR CA010501002Bushing · failed(CAN) WHEN THE AIRCRAFT ARRIVED IN THE HANGAR THE MECHANICS WERE UNABLE TO OPEN THE PASSENGER DOOR. THE BUSHING FROM THE CASTING FOR THE TORQUE TUBE WERE FOUND TO BE MIGRATED. THE BUSHING WERE RE-INSTALLED AND THE DOOR RIGGING C/OUT.
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