GE CF34-3A1

Service difficulty reports · 1,372

Newest first. General aviation reporting is voluntary.

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 = 'CF343A1'
  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 COMA0060349Transmitter · leakingFUEL LEAKING FROM LEFT ENGINE. REPLACED THE FUEL FLOW TRANSMITTER.Apr 15, 2000 · N915CA · Cndair CL6002B19 · Fuel Flow SensorSDR CA000501028Window · failed(CAN) CAPTAINS SIDE WINDOW SHATTERED DURING FLIGHT. WINDOW REPLACED.Apr 11, 2000 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA000501025Sensor · failed(CAN) EICAS MESSAGE FAILURE OF THE PASSENGER DOOR UNSAFE, AFTER TAKE OFF FLIGHT RETURNED TO ORD. SENSOR FOUND TO BE FAR. CLEANED SENSORS, PERFORMED SELF TEST.Apr 9, 2000 · Cndair CL6002B19 · Door Warning SystemSDR CA000501026Sensor · failed(CAN) SMOKE IN COCKPIT AND CABIN AND LT A/C PACK HIGH TEMPRATURE WARNING ON. PACK SHUT DOWN. CLEANED COCPIT TEMP CONTROL SENSOR.Apr 9, 2000 · Cndair CL6002B19 · Cabin Cooling SystemSDR CA000501027Windshield · cracked(CAN) ON CLIMB-OUT FROM YHZ CAPTAINS WINDSCREEN OUTTER PANE CRACKED.Apr 9, 2000 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA000410038Element · failed(CAN) 14TH STAGE DUCT WARNING MESSAGE IN CRUISE. SENSING ELEMENT REPLACED.Apr 5, 2000 · Cndair CL6002B19 · Overheat DetectionSDR COMA0060286Harness · defectiveRIGHT HAND ENGINE N1 FLUCTUATES. REPLACED THE ENGINE BROWN WIRE HARNESS.Mar 24, 2000 · N948CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA000320017Carbon Seal · leaking(CAN) AN OIL SMELL COULD BE DETECTED FROM THE AIR DISTRIBUTION SYSTEM. THE NR 1 ENGINE, 1 AND 3 CARBON SEALS WERE REPLACED.Mar 20, 2000 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR CA000410033Separator · contaminated(CAN) SMOKE IN CABIN ON TAKEOFF AND AT CLIMB ALTITUDE. AIRCRAFT TURNED AROUND AND LANDED SAFELY WITHOUT INCIDENT. OIL RESIDUE WAS FOUND IN THE WATER SEPARATOR SYSTEM. NR 1/3 CARBON SEALS WERE PREVIOUSLY CHANGED PRIOR TO THIS FLIGHT ON BOTH ENGINES. ALL DUMar 20, 2000 · Cndair CL6002B19 · Humidity Control SystemSDR CA000410025Windshield · failed(CAN) WINDSHIELD SHATTERED IN FLIGHT. WINDSHIELD REPLACED.Mar 20, 2000 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA000410023Separator · failed(CAN) SMOKE IN CABIN, ABORTED TAKE-OFF. REPLACED BOTH WATER SEPERATORS BAGS AND CLEANED SEPERATOR HOUSING AND RAIN LINE RESTRICTORS.Mar 15, 2000 · Cndair CL6002B19 · Cabin Cooling SystemSDR CA000410028Amplifier · failed(CAN) LOW POWER ON RIGHT ENGINE, ABORTED TAKEOFF AT 80 KNOTS. ENGINE WOULD ONLY DEVELOP 76 PERCENT OF N1. N1 SPEED CONTROLLER AMPLIFIER REPLACED.Mar 14, 2000 · Cndair CL6002B19 · Turbine GovernorSDR CA000410032Carbon Seal · failed(CAN) OIL SMOKE IN COCKPIT FOR 20 SECONDS. NR 1 AND NR 2 CARBON SEALS WERE REPLACED.Mar 14, 2000 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA000328011Engine · vibrates(CAN) ENGINE VIBRATED ON TAKE OFF, TAKE OFF ABORTED. REPORT REQUIRED.Mar 8, 2000 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA000328019Blade · failed(CAN) OPERATOR HAS EXPERIENCED T2 BLADE FATIGUE FAILURE AND HAS IMPLEMENTED A 6,000 HOUR LIFE LIMIT.Mar 8, 2000 · Cndair CL6002B19 · Turbine SectionSDR CA000328014Smoke Detector · malfunctioned(CAN) SMOKE CARGO FIRE DETECTION INDICATION IN COCKPIT. SMOKE MASTER WARNING ON LANDING. BOTH BOTTLES DISCHARGED, NO FIRE. BOTH SMOKE DETECTORS REPLACED.Mar 5, 2000 · Cndair CL6002B19 · Smoke DetectionSDR COMA0060238Light · contaminatedFORWARD SECTION OF EMERGENCY FLOOR PATH LIGHT IS INOPERABLE. CLEANED WATER FROM FLOOR LIGHT, SYSTEM TEST SATISFACTORY.Mar 4, 2000 · N739CA · Cndair CL6002B19 · Emergency LightingSDR COMA0060232Eec · malfunctionedRIGHT ENGINE N1 DROPPED FROM 87 PERCENT TO 78 PERCENT. DEFERRED THE ENGINE ELECTRONIC CONTROL SYSTEM PER MEL.Mar 2, 2000 · N948CA · Cndair CL6002B19 · Fuel Controlling SystemSDR COMA0060234Pcu · malfunctionedCONFIG SPOILER WARNING DURING TAKEOFF. REPLACED THE LEFT FLIGHT SPOILER PCU.Mar 2, 2000 · N716CA · Cndair CL6002B19 · Drag Control ActuatorSDR COMA0060240Mask · deployedPASSENGER 02 MASK DEPLOYED AT 12,000 FT. RESTOWED PASSENGER 02 MASK.Mar 1, 2000 · N810CA · Cndair CL6002B19 · Passenger Oxygen SystemSDR CA000320027Pcu · out of adj(CAN) THE CREW RECEIVED A SPOILER CONFIG EICAS WARNING ON TAKEOFF AND ABORTED. MAINTENANCE DETERMINED THAT THE SPOILER POWER CONTROL UNITS OUT WERE OUT OF ADJUSTMENT.Feb 29, 2000 · Cndair CL6002B19 · Drag Control SystemSDR CA000320028Control Unit · failed(CAN) ON TAKE-OFF THE CREW RECEIVED A SPOILER CONFIG WARNING, BUT THE WARNING WENT OUT AFTER LIFT OFF (WOW). SPOILER ELECTRONIC CONTROL UNIT NR 1 AND NR 2 INTEROGATED AND FOUND THAT THE NR 2 MODULE B WAS DEFECTIVE. THE SECU WAS REPLACEDFeb 29, 2000 · Cndair CL6002B19 · Drag Control SystemSDR CA000320023Pcu · failed(CAN) THE CREW RECEIVED A SPOILER CONFIG EICAS WARNING ON TAKEOFF AND ABORTED. MAINTENANCE DETERMINED THAT THE SPOILER PCU WAS AT FAULT AND REPLACED IT.Feb 26, 2000 · Cndair CL6002B19 · Drag Control SystemSDR CA000320032Fcu · failed(CAN) THE CREW RECEIVED A FLAPS FAIL WARNING. MAINTENANCE REPLACED THE FECU AND THE BPSU P/N 855D100-9.Feb 25, 2000 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA000224046Ballast · smoke(CAN) FLIGHT CREW REPORTED DURING TAXI TO THE ARRIVAL GATE THAT THE CABIN BEGAN TO FILL WITH ELECTRICAL SMOKE. THE FLIGHT ATTENDANT REPORTED THE SOURCE OF SMOKE INITIATED AT ROW 5A SIDE PANEL LIGHTING. SIDE WALL LIGHTING BALLAST REPLACED.Feb 24, 2000 · Cndair CL6002B19 · Passenger Compartment LightingSDR CA000320021Indicator · failed(CAN) DURING TAKEOFF, THE CREW RECEIVED A SPOILER CONFIG EICAS WARNING AND A MASTER CAUTION. THE TAKEOFF WAS ABORTED. THE PROBLEM WAS TRACED TO THE THROTTLE POSITION SENSOR AND IT WAS REPLACED.Feb 23, 2000 · Cndair CL6002B19 · Engine ControlsSDR CA000222010O-Ring · failed(CAN) LOW OIL PRESSURE EXPERIENCED. EMERGENCY LANDING AFTER ENGINE SHUT DOWN. AIR STARTER O-RING REPLACED TO CORRECT OIL LOSS.Feb 19, 2000 · Cndair CL6002B19 · Turbine Engine Accessory DriveSDR CA000320019Fcu · failed(CAN) DURING APPROACH, THE FLAPS WERE SET TO 45 DEGREES AND THE CREW GOT A FLAPS FAIL WARNING. THE FLAPS STOPPED AT 34 DEGREES. A RESET WAS ATTEMPTED WITHOUT SUCCESS. MAINTENANCE TRACED THE PROBLEM TO A FAILED FLAP ELECTRONIC CONTROL UNIT AND REPLACED IT.Feb 19, 2000 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA000222016Window · failed(CAN) CAPT SIDE WINDOW SHATTERED DURING FLIGHT. EMERG DECLARED. WINDOW REPLACED.Feb 13, 2000 · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA0060146Carbon Seal · failedSTRONG OIL SMELL IN AIRCRAFT. SUSPECT FAILED CARBON SEALS. REPLACED LEFT ENGINE.Feb 8, 2000 · N912CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA0060143Valve · leakingLEFT, 10TH STAGE BLEED AIR DUCT, MESSAGE. REPLACED THE LEFT HAND 14TH STAGE BLEED AIR VALVE.Feb 7, 2000 · N912CA · Cndair CL6002B19 · Compressor Bleed ValveSDR CA000222015Apu · failed(CAN) STRONG SMELL OF FUEL IN CABIN AND COCKPIT. BOTH ON GROUND AND INFLIGHT. FUEL RESIDUE IN APU BAY AREA. CLEANED AND TIGHTENED APU FUEL SUPPLY LINE TO FUEL CONTROL UNIT. LEAK CHECKED, CHANGED BOTH COALESCER BAGS.Feb 6, 2000 · Cndair CL6002B19 · APU Engine Fuel and ControlSDR CA000404033Handle · cracked(CAN) CRACKS FOUND IN HOUSING AROUND DOOR SHAFT HANDLE 100 PERCENT OF ITS CIRCUMFERENCE. CAMPAIGN WAS DONE TO VERIFY ALL A/C AND TO REPLACE ALL HANDLE ASSEMBLIES AFFECTED. NEW HANDLE INSTALLED.Feb 4, 2000 · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR CA000404034Handle · cracked(CAN) CRACKS FOUND IN HOUSING AROUND DOOR SHAFT HANDLE 100 PERCENT OF ITS CIRCUMFERENCE. CAMPAIGN WAS DONE TO VERIFY ALL A/C AND TO REPLACE ALL HANDLE ASSEMBLIES AFFECTED. NEW HANDLE INSTALLED.Feb 4, 2000 · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR CA000404035Handle · cracked(CAN) CRACKS FOUND IN HOUSING AROUND DOOR SHAFT HANDLE 100 PERCENT OF ITS CIRCUMFERENCE. CAMPAIGN WAS DONE TO VERIFY ALL A/C AND TO REPLACE ALL HANDLE ASSEMBLIES AFFECTED. NEW HANDLE INSTALLED.Feb 4, 2000 · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR CA000404036Handle · cracked(CAN) CRACKS FOUND IN HOUSING AROUND DOOR SHAFT HANDLE 100 PERCENT OF ITS CIRCUMFERENCE. CAMPAIGN WAS DONE TO VERIFY ALL A/C AND TO REPLACE ALL HANDLE ASSEMBLIES AFFECTED. NEW HANDLE INSTALLED.Feb 4, 2000 · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR CA000404037Handle · cracked(CAN) CRACKS FOUND IN HOUSING AROUND DOOR SHAFT HANDLE 100 PERCENT OF ITS CIRCUMFERENCE. CAMPAIGN WAS DONE TO VERIFY ALL A/C AND TO REPLACE ALL HANDLE ASSEMBLIES AFFECTED. NEW HANDLE INSTALLED.Feb 4, 2000 · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR CA000404038Handle · cracked(CAN) CRACKS FOUND IN HOUSING AROUND DOOR SHAFT HANDLE 100 PERCENT OF ITS CIRCUMFERENCE. CAMPAIGN WAS DONE TO VERIFY ALL A/C AND TO REPLACE ALL HANDLE ASSEMBLIES AFFECTED. NEW HANDLE INSTALLED.Feb 4, 2000 · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR CA000404041Handle · cracked(CAN) CRACKS FOUND IN HOUSING AROUND DOOR SHAFT HANDLE 100 PERCENT OF ITS CIRCUMFERENCE. CAMPAIGN WAS DONE TO VERIFY ALL A/C AND TO REPLACE ALL HANDLE ASSY AFFECTED. NEW HANDLE INSTALLED.Feb 4, 2000 · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR CA000404042Handle · cracked(CAN) CRACKS FOUND IN HOUSING AROUND DOOR SHAFT HANDLE 100 PERCENT OF ITS CIRCUMFERENCE. CAMPAIGN WAS DONE TO VERIFY ALL A/C AND TO REPLACE ALL HANDLE ASSEMBLIES AFFECTED. NEW HANDLE INSTALLED.Feb 4, 2000 · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR CA000404040Handle · cracked(CAN) CRACKS FOUND IN HOUSING AROUND DOOR SHAFT HANDLE 100 PERCENT OF ITS CIRCUMFERENCE. CAMPAIGN WAS DONE TO VERIFY ALL A/C AND TO REPLACE ALL HANDLE ASSY AFFECTED.NEW HANDLE INSTALLED.Feb 4, 2000 · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR COMA0060115Element · malfunctionedANTI-ICE DUCT WARNING MESSAGE. REPALCED BLEED AIR LEAK DETECTION LOOP A 40 WK.Jan 31, 2000 · N941CA · Cndair CL6002B19 · Engine Bleed Air SystemSDR CA000201021Selector Valve · failed(CAN) CREW REPORTED GEAR DISAGREE FOR NLG. A/C RTB AND PILOT DECLARED EMERGENCY. MAINT UNABLE TO DUPLICATE ON GROUND. NLG SELECTOR VALVE REPLACED AS PRECAUTIONARY MEASURE.Jan 31, 2000 · Cndair CL6002B19 · Landing Gear SelectorSDR COMA0060124Fcu · malfunctionedRIGHT ENGINE OVER SPEED. REPLACED RIGHT ENGINE FUEL CONTROL.Jan 29, 2000 · N797CA · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR CA000209060Rod · out of adj(CAN) AFTER DEPARTURE, PASSENGER DOOR WARNING CAME ON. DOOR STOW HANDLE LATCH MESSAGE AT FL200. CABIN PRESS REMAINED NORMAL. DOOR INDICATION TARGET CLEANED, DOOR MECHANISM LATCH ROD ADJUSTED, OPERATION CHECKED NORMALJan 24, 2000 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA000209059Cam · overserviced(CAN) DURING T/O PASS DOOR INDICATION CAME ON. UNABLE TO PRESSURIZE. AIRCRAFT RETURNED TO BASE. FOUND DOOR UPPER LATCH CAM OVERGREASED, UNABLE TO MAKE CAM FULL ROTATION.Jan 21, 2000 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA000209058Bracket · broken(CAN) FOUND LT ENGINE UPPER THRUST REVERSER FORWARD AND AFT BRACKET BROKEN. CHANGED BRACKETS AND REINSTALLED PANEL.Jan 20, 2000 · Cndair CL6002B19 · Engine Thrust ReverserSDR CA000120030Apu · failed(CAN) IN FLIGHT THE CREW NOTICED SMOKE IN THE COCKPIT AND CABIN. THE APU EGT WAS IN THE YELLOW RANGE AND SHUT DOWN AS PER QRH. ONCE APU STOPPED, THE SMOKE EVACUATED. MAINTENANCE REMOVED WATER SEPERATOR TO CLEAN COALESCER BAG. APU DID LOOSE MOST OF THE OIL.Jan 20, 2000 · Cndair CL6002B19 · APU Oil SystemSDR CA000120031Engine · malfunctioned(CAN) HIGH OIL PRESSURE AND HIGH ITT EXPERIENCED AT T/DOWN. FDR,CVR AND MDC TO BE DOWN LOADED. ENG REACHED 1026 C FOR 3.5 SECONDS.BJan 20, 2000 · Cndair CL6002B19 · Engine Oil PressureSDR CA000209056Controller · failed(CAN) ON FINAL APPROACH, SELECTED FLAPS TO 30 DEGREES AND HAD FLAP FAIL MESSAGE. RESET FLAP CONTROL 1&2, CYCLED FLAPS SEVERAL TIMES. NO FAULT FOUND.Jan 18, 2000 · Cndair CL6002B19 · Trailing Edge Flap Control System
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