GE CF34-3B1

Service difficulty reports · 5,402

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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.

SDR CA020211011Actuator · failed(CAN) AP TRIM RWD CAUTION POSTED ON EICAS. DISCONNECTED AP AND FOUND AILERON SYSTEM JAMMED. OVERPOWERED SYSTEM ACC. CHECKLIST AFTER SEVERAL ATTEMPTS. SUDDENLY SYSTEM GOT FREE AGAIN. VISUALLY INSPECTED AILERON SYSTEM CABLES AND PULLEYS FOR SIGN OF JAMMING NO FIFeb 11, 2002 · Cndair CL6002B19 · Aileron Control SystemSDR ASOA02089Engine · vibrationFLT 4563 - WHILE CLIMBING OUT OF FWA, AT 21,000 FEET, THE LEFT ENGINE N2 VIBRATION SPIKED APPROXIMATELY 2.6 MILS. THE FLIGHT ATTENDANT AND PASSENGERS REPORTED A LOUD NOISE FROM THE LEFT ENGINE. THE LEFT ENGINE SHUT ITSELF DOWN. THE CAPTAIN DECLARED AN EMERGFeb 11, 2002 · N852AS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA020215001Wire Harness · chafed(CAN) DURING TAKE-OFF ROLL, THE POWER SET TO TAKE OFF N1, THE SPEED WERE JUST CALLED ALIVE, WHEN THE LEFT ENGINE ROLLED BACK TO IDLE. THE AIRCRAFT WAS TAXIED CLEAR AND WHILE TAXIING BACK TO FBO LEFT ENGINE SHUT DOWN. THE CAS MESSAGE INDICATED HYD SOV 1 AND ENGFeb 11, 2002 · Cndair CL604 · Fire DetectionSDR CA020221004Wheel · missing(CAN) AFTER FLT. CREW PERFORMED POST FLT INSPECTION AND FOUND LT OB WHEEL ASSY MISSING FROM A/C. THE MISSING WHEEL ASSY RECOVERED IN ATL FROM AIRPORT AUTH. IT OBVIOUSLY DEPARTED WHILE ON TAXI OR TAKEOFF. IT WAS RECOVERED WITH ANTI SKID DRIVE CAP INTACT. NEFeb 11, 2002 · Cndair CL6002B19 · Wheel/Ski/FloatSDR ASOA02089SGear · brokenFLT 4563 - WHILE CLIMBING-OUT OF FWA, AT 21,000 FEET, THE LEFT ENGINE N2 VIBRATION SPIKED APPROXIMATELY 2.6 MILS. THE FLIGHT ATTENDANT AND PASSENGERS REPORTED A LOUD NOISE FROM THE LEFT ENGINE. THE LEFT ENGINE SHUT ITSELF DOWN. THE CAPTAIN DECLARED AN EMERGFeb 11, 2002 · N852AS · Cndair CL6002B19 · Turbine Engine Accessory DriveSDR SWIA200210650Stall Warning · false activationON ROTATION RECEIVED STALL FAIL CAUTION MESSAGE. PERFORMED APPROPRIATE QRH PROCEDURE. RETURNED TO SLC. RESET STALL COMPUTER CIRCUIT BREAKERS CBP-1 Q2 CBP-4 C7 AND CLEARED THE MEMORY. OPS CHECK GOOD.Feb 10, 2002 · N439SW · Cndair CL6002B19 · Stall Warning SystemSDR CA020211010Selector Valve · failed(CAN) LANDING GEAR WOULD NOT EXTEND FOR LANDING. HAD TO PERFORM EMERGENCY GEAR EXTENSION. AIRCRAFT DECLARED AN EMERGENCY. UNEVENTFUL LANDING TOOK PLACE. MAINTENANCE REPLACED MAIN LANDING GEAR SELECTOR VALVE. OPS AND LEAKS CHECKS GOOD.Feb 8, 2002 · Cndair CL6002B19 · Landing Gear SelectorSDR CA020211009Windshield · cracked(CAN) THE WINDSHIELD INSTALLED WAS A POST SERVICE BULLETIN WINDSHIELD. RT WINDSHIELD CORE PLY CRACKED IN CRUISE. CREW INITIATED DESCENT TO 10,000 FEET. (NO EMERGENCY DESCENT). AIRCRAFT LANDED IN BARCELONA, SPAIN AS SCHEDULED. REMOVED AND REPLACED WINDSHIELFeb 7, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020211008Attach Fitting · cracked(CAN) DURING THE NDT INSPECTION OF THE FUEL BOOST PUMP SCREW HOLES 3 CRACKS WERE FOUND. REPAIR IN ACCORDANCE WITH REO 601R-57-21-164.Feb 6, 2002 · Cndair CL6002B19 · Fuel Boost PumpSDR CA020211007Odor · detected(CAN) ON APPROACH, AFTER CREW STARTED APU AND SWITCHED BLEEDS, SMOKE TOILET MESSAGE CAME ON. SMOKE ALARM ALSO SOUNDED FOR SEVERAL MINUTES. F/A REPORTED HAZE FROM ROW 8 AFT. BY THE TIME THE CREW LANDED, HAZE HAD DISAPPEARED. LOCAL MAINTENANCE INSPECTED THFeb 4, 2002 · Cndair CL6002B19 · Air Distribution SystemSDR CA020211006Window · cracked(CAN) CAPTAIN'S SIDE WINDOW CRACKED ON TAXI OUT. REMOVED AND REPLACED RT SIDE WINDOW IAW 56-12-01. AIRCRAFT RETURNED TO SERVICE.Feb 1, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA200210609Selector Valve · malfunctionedMAIN GEAR WARNING ON LANDING. FOLLOWED EMERGENCY PROCEDURE AND MAIN GEAR DID NOT EXTEND. MANUALLY EXTENDED GEAR ON THIRD ATTEMPT. REMOVED AND REPLACED MAIN GEAR SELECTORS VALVE. GEAR SWINGS SATISFACTORY. LEAK CHECK GOOD.Jan 30, 2002 · N905SW · Cndair CL6002B19 · Landing Gear SelectorSDR SWIA200210611Blade · damagedON TAKEOFF ROLL, LARGE VIBRATION/NOISE FELT THROUGHOUT AIRCRAFT FELT ON RUDDER PEDALS AND THRUST LEVERS. FOUND DAMAGE TO LEFT ENGINE NR 8 & 9 FAN BLADES. REMOVED AND REPLACED NR 8, 9, 22 & 23 LEFT ENGINE FAN BLADES WITH SERVICEABLE UNITS. PERFORMED RUN CHECJan 30, 2002 · N405SW · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR SWIA200210617Engine · vibratesNR 1 ENGINE FAN VIB IN YELLOW ARC SHORTLY AFTER TAKEOFF. ON ENGINE RUN UP, COULDN'T DUPLICATE PROBLEM. AT HIGH POWER SETTINGS, VIB NEVER GOT ABOVE .3. INSPECTED FAN BLADES VISUALLY AND INSPECTION GOOD.Jan 30, 2002 · N595SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA020117008Socket · burned(CAN) SHORTLY AFTER TAKEOFF FROM TOULOUSE, FRANCE, SMOKE APPEARED IN CABIN. SMOKE CAME FROM ROW 8DF FROM FINISHING PANEL ABOVE RIGHT EMERGENCY EXIT. ELECTED TO RETURN TO TOULOUSE. SMOKE HOODS IN FORWARD AND AFT POSITION USED BY FLIGHT ATTENDANT. LANDING WEJan 17, 2002 · Cndair CL6002B19 · Passenger Compartment LightingSDR CA020117009Window · cracked(CAN) LEFT WINDOW CRACKED IN CLIMB. PERFORMED UNSCHEDULED LANDING. LEFT WINDOW REPLACED PER AMM.Jan 17, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020117011Window · cracked(CAN) DURING CRUISE AT FL280 / IAS 280, THE RIGHT WINDOW CRACKED. RIGHT WINDOW REPLACED PER AMM.Jan 17, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020117006Sensor · leaking(CAN) CREW GOT L 14TH DUCT MESSAGE. MESSAGE WAS INTERMITTENT AT FIRST. EVENTUALLY, MESSAGE WENT TO STEADY STATE. CREW FOLLOWED QRH 6-2 THEN ABNORMAL 1-2. THEY LANDED AT THE NEAREST SUITABLE AIRPORT. MAINTENANCE WAS SENT. REPLACED THE LEFT LEAK SENSING ELEMENTJan 16, 2002 · Cndair CL6002B19 · Engine Bleed Air SystemSDR CA020117003Window · cracked(CAN) PILOTS SIDE WINDOW CARACKED DURING CRUISE. WINDOW ASSEMBLY REPLACED IAW AMM.Jan 15, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020117004Engine · failed(CAN) AIRCRAFT DEPARTED WASHINGTON DULLES INTERNATIONAL AIRPORT ON FLIGHT 7187, THE FLIGHT CREW DETECTED A SEVERE VIBRATION AND RESULTANT ENGINE SHUTDOWN WITHOUT PILOT'S INPUT. THE AIRCRAFT RETURNED TO THE ORIGINATING AIRPORT AND DECLARED AN EMERGENCY. ENJan 15, 2002 · N629BR · Cndair CL6002B19 · Powerplant SystemSDR CA020124004Controller · faulty(CAN) SMOKE IN CABIN DUE TO RT PACK OVER TEMP IN AUTO, REVERTED TO MANUAL TEMPERATURE CONTROL. FOUND TO BE THE TEMP CONTROLLER AT FAULT. REPLACED THE TEMPERATURE CONTROLLER.Jan 15, 2002 · Cndair CL6002B19 · Cabin Temperature ControllerSDR CA020117002Support · cracked(CAN) FOUND CRACK ON THE ENGINE SUPPORT BEAM. ENGINE SUPPORT BEAM REPAIRED.Jan 14, 2002 · Cndair CL6002B19 · Engine Mount SectionSDR CA020110015Window · cracked(CAN) PILOTS LEFT SIDE WINDOW CRACKED IN CRUISE.REMOVED AND REPLACED LEFT SIDE WINDOW WITH SERVICEABLE UNIT IAW AMM 56-12-01.Jan 10, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020110017Pcu · failed(CAN) FLIGHT 5280 FROM AVP TO CVG ON TAXI OUT SPOILERON FAULT MSG ILLUMINATED AND UNCOMMANDED SPOILERON DEPLOYMENT. CB4CN CIRCUIT BREAKER POPPED IN AVIONICS BAY - SENT MECH & PARTS ON ROAD TRIP. SUBSTITUTED AIRCRAFT 7539. R&R'D LEFT SPOILERON OUTBOARD PCU. AIRJan 10, 2002 · Cndair CL6002B19 · Drag Control SystemSDR CA020114004Window · cracked(CAN) PILOTS RIGHT SIDE WINDOW CRACKED IN CRUISE. REMOVED AND REPLACED RIGHT SIDE WINDOW WITH SERVICEABLE UNIT IAW AMM 56-12-01.Jan 10, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020110008Windshield · cracked(CAN) DESCENDING THROUGH 14,000 FT THERE WAS AN ELECTRICAL FLASH FOLLOWED BY THE F/O'S WINDSHIELD "CRACKING / SHATTERING". THE WINDSHIELD HEAT WAS ON AT THE TIME. R&R'D WINDSHIELD AND HEAT CONTROLLER ACCORDING TO AMM.Jan 9, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020110011Pump · leaking(CAN) DURING FLIGHT THE CREW NOTED SYSTEM NR 2 LEVEL TO BE OWN TO 30 PERCENT. FLIGHT DIVERTED. MAINTENANCE DETERMINED THAT THE NR 2 EDP WAS LEAKING. NR 2 EDP WAS REMOVED AND REPLACED. SYSTEM WAS SERVICED. RUNS AND LEAK CHECKS CARRIED OUT.Jan 9, 2002 · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR CA020110012Carbon Seal · leaking(CAN) AS CREW WAS CLIMBING THROUGH 27,000 FT, RECEIVED RT ENGINE OIL PRESSURE MESSAGE. CREW SHUT DOWN RT ENGINE AND CONTINUED ON TO ATL. ONCE IN ATL, MAINTENANCE FOUND THE ENGINE 6 QUARTS LOW OF OIL. EVENTUALLY, OIL LEAKAGE WAS FOUND IN THE C-SUMP AREA. THEJan 9, 2002 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA020110005Windshield · failed(CAN) AIRCRAFT WAS ENROUTE TO GRR. CREW REPORTED CO-PILOT'S WINDSHIELD SHATTERED JUST BEFORE DESCENT AT 28,000 FEET. MAINTENANCE CREW REMOVED AND REPLACED CO-PILOT'S WINDSHIELD.Jan 7, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020110006Window · failed(CAN) ON LANDING ROLL, THE LEFT SIDE WINDSHIELD SHATTERED. MAINTENANCE WAS SENT. THEY REMOVED AND REPLACED THE PILOT'S SIDE WINDOW. CHECKS CARRIED OUT AND AIRCRAFT RETURNED TO SERVICE.Jan 7, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020110014Aileron · failed(CAN) DURING AILERON DEFLECTION TEST ON GROUND, THE PILOT FOUND THAT THERE WAS ONLY 15 DEG DEFLECTION. MAINTENANCE FOUND THAT THE SEAL RETAINER ON THE WING TRAILING EDGE HAD CAUGHT WITH THE AILERONS LEADING EDGE AND INHIBITED AILERON FUNCTION. THIS CAUSED STJan 1, 2002 · Cndair CL6002B19 · Wing, Control SurfacesSDR ASOA01303Carbon Seal · leakingFLT 4698 - WHILE CLIMBING THROUGH FL270 FROM ATL-SWF, THE CAPTAIN REPORTED RECEIVING A RIGHT ENGINE OIL PRESSURE MESSAGE FOLLOWED BY AN AURAL WARNING. THE OIL PRESSURE WAS FLUCTUATING BETWEEN 30 AND 49 PSI. THE CAPTAIN SECURED THE RIGHT ENGINE AND RETURNED TDec 28, 2001 · N826AS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA020103010Oil Cooler · leaking(CAN) A/C ON APPROACH WHEN CREW NOTED LEFT OIL PRESSURE FLUCTUATING. CREW RPTED PRESSURE FLUCTUATING UP TO 25 PSI&AVERAGING 30 PSI LOWER THAN RIGHT ENGINE. NO MENTION OF WARNINGS OR OTHER ACTION TAKEN. MAINT FOUND LEFT ENGINE TO BE 5 QTS LOW OF OIL. ENGINE SERDec 20, 2001 · Cndair CL6002B19 · Engine Oil CoolerSDR CA011221006Pump · failed(CAN) WHILE EXTENDING THE GEAR DURING APPROACH GEAR DISAGREE AND HYD 3 LOW PRESSURE CAUTION MESSAGES. CHECKED HYDRAULIC SYNOPTIC PAGE. VERIFIED NR 3 HYD PRESSURE QUANTITY 0 PERCENT. REMOVED AND REPLACED HYD. PUMP 3A WITH SERVICEABLE UNIT. PERFORMED LEAK CHEDec 19, 2001 · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR CA020103008Windshield · cracked(CAN) DURING FLIGHT AT FL 190, THE RIGHT WINDSHILED CRACKED. RIGHT WINDSHIELD REPLACED.Dec 19, 2001 · Cndair CL6002C10 · Flight Compartment WindowsSDR CA011219001Seal · damaged(CAN) CLIMBING THROUGH 2,000 FEET R 14TH DUCT WARNING MESSAGE WAS GENERATED. RETARDED PL AS PER QRH. MESSAGE WENT OUT. RT 14TH DUCT LIGHT AND RT14TH DUCT MESSAGE ILLUMINATED WITH RED FLOW LINE BETWEEN RT 14TH STAGE SOV, NOSE COWL AND WING SOV AT POWER ABOVDec 18, 2001 · Cndair CL6002B19 · Air Intake Anti/De-Ice SystemSDR CA011217023Windshield · cracked(CAN) WHILE AIRCRAFT PARKED AT THE GATE, WINDSHIELD CRACKED APPEARED ON CAPTAIN SIDE. AIRCRAFT FERRIED FROM EDINBURGH TO EXETER FOR REPLACEMENT.Dec 17, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020103009Computer · failed(CAN) STAB TRIM / MACH TRIM WILL NOT STAY ENGAGED. REMOVED AND REPLACED THE HORIZONTAL STABILIZER COMPUTER.Dec 16, 2001 · Cndair CL6002B19 · Stabilizer ActuatorSDR CA011217007Window · cracked(CAN) RT WINDOW CRACK IN CRUISE. RIGHT WINDOW REPLACED.Dec 12, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA011218008Windshield · cracked(CAN) DURING DESCENT AIRCRAFT 7522 THE CO-PILOT'S WINDSHIELD CRACKED. MAINTENANCE REMOVED AND REPLACED THE PILOT'S WINDSHIELD.Dec 7, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA011217010Windshield · cracked(CAN) THE PILOT REPORTED THE LT FLIGHT DECK WINDSHIELD CRACKED AT APPROX. 28000 FEET, THE FLIGHT SEQUENCE WAS COMPLETED WITHOUT FURTHER INCIDENCE THE WINDSHIELD WAS REPLACED.Dec 5, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA011218007Windshield · failed(CAN) THE AIRCRAFT WAS DESCENDING. THE RT WINDSHIELD SHATTERED. INSPECTION REVEALED THAT THE RT WINDSHIELD CORE PLY HAD SHATTERED. THE RT WINDSHIELD IS BEING REPLACED.Nov 30, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA011210005Gearbox · failed(CAN) APPROXIMATELY 20 MINS AFTER TAKE OFF, THE CREW NOTICED THE NR 2 ENGINE N2 DROP TO ZERO RPM WITHIN 2-3 SECONDS. ALL OTHER NR 2 ENGINE PARAMETERS ALSO REDUCED AND THE ENGINE FLAMED OUT. THIS OCCURRED DURING THE CLIMB AT APPROX. FL 310. THE OIL PRESSURE Nov 29, 2001 · Cndair CL6002B19 · Accessory GearboxesSDR CA011130008Bearing · loose(CAN) RT ENGINE - VARIABLE GUIDE VANE SHAFT AFT SUPPORT BEARING MIGRATION.SUBJECT MSN WAS UNDERGOING AN A-CHECK.MAINTENANCE FOUND THAT THE BEARING ON THE VG SHAFT AFT SUPPORT HAD MIGRATED.VG SHAFT AFT SUPPORT WAS REPLACED WITH A NEW ONE.Nov 28, 2001 · Cndair CL6002B19 · Engine Air Intake SystemSDR CA011130009Handle · failed(CAN) AIR TURNBACK DUE TO PASSENGER DOOR WARNING AND PAX DOOR STOW CAUTION MSG POSTED. AT 1,500 FT AGL PASSENGER DOOR UNSAFE CAUTION MESSAGE CAME ON. AT 10,000 FT RED PASSENGER DOOR WARNING MESSAGE WAS POSTED. RETURNED TO AIRPORT. INSPECTED PASSENGER DOOR FORNov 28, 2001 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA011210006Display · overheated(CAN) SMELL OF SMOKE. FMS CDU WAS HOT TO TOUCH AND LOSS OF COLORS ON SCREEN.Nov 28, 2001 · Cndair CL6002B19 · Flight Management Computing Hardware SystemSDR CA011217009Windshield · cracked(CAN) LT WINDSHIELD STARTED CRACKING DURING TAXI OUT. REMOVED AND REPLACED LEFT WINDSHIELD LEAK CHECK GOOD.Nov 23, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA011128002Mount · cracked(CAN) CRACKS FOUND ON THE RIGHT SIDE (2.5 INCHES) AND LEFT (TWO CRACKS = CUMULATIVE MEASUREMENT OF APPROXIMATELY 2 INCHES )ACCESS PANEL CUT-OUT.Nov 22, 2001 · Cndair CL6002B19 · Engine Mount SectionSDR CA011128003Support · cracked(CAN) DURING THE INSPECTION OF THE ENGINE SUPPORT BEAM IAW SB A601R-53-059, TWO CRACKS WERE FOUND. ONE ON THE UPPER WEB AT RBL 9.5 AND LEFT LOWARD ACCESS PANEL LEFT FORWARD CORNER.Nov 22, 2001 · Cndair CL6002B19 · Engine Mount SectionSDR CA011128005Windshield · cracked(CAN) LT COCKPIT WINDSHIELD CRACKED NEARING TOP OF CLIMB - FL335. AIRCRAFT CONTINUED ON WHERE THE WINDSHIELD WAS REPLACED.Nov 22, 2001 · Cndair CL6002B19 · Flight Compartment Windows
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