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 CA001110021Controller · failed(CAN) UNABLE TO LOWER FLAPS ON APPROACH TO HALIFAX. MONITOR RAISED TO CARRY OUT FLAP INSPECTION AS PER A.D. FLAP SYSTEM RESET, OPERATION CHECKED NORMAL.Oct 20, 2000 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA001101007Control Panel · failed(CAN) DURING TAKEOFF, APU FIRE WARNING BELLS SOUNDED. CREW DISCHARGED FIRE EXTINGUISHER AND APU FIRE WARNING STOPPED. MULTIPLE FIRE FAIL MESSAGES WEREALSO POSTED.MAINTENANCE CREW OBSERVED SPILLED BEVERAGE CONTAINER ON L/H SIDE CONSOLE AND FLUID EVIDENT IN FIREOct 14, 2000 · Cndair CL6002B19 · Fire DetectionSDR CA001107006Switch · intermittent(CAN) AIRCRAFT DEPARTED FARNBOROUGH EN ROUTE TO BEIRUT. CLIMBING THROUGH 45,000 FEET AT 220 KNOTS, THE RT AMBER REVERSER UNLOCK CAPTION ILLUMINATED. CHECK LISTS FOLLOWED, EMERGENCY STOW WAS SELECTED. ENGINE WAS SHUT DOWN AND AIRCRAFT DIVERTED TO STANSTED AIRPOct 13, 2000 · Cndair CL600* · Engine Thrust ReverserSDR COMA0060809Engine · malfunctionedLEFT ENGINE HIGH OIL TEMP, LOW OIL PRESSURE. REPLACED LEFT ENGINE.Oct 7, 2000 · N937CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA001024041Computer · failed(CAN) STALL FAIL CAUTION MESSAGE FOLLOWED BY CONFIG SPOILERS AT APPROX 80 KTS.ABORTED TAKEOFF.SPC RESET PER AMM, AIRCRAFT BACK IN SERVICE.Oct 7, 2000 · Cndair CL6002B19 · Stall Warning SystemSDR CA001024042Engine · overheated(CAN) SHORTLY AFTER TAKEOFF, NR 1 ENGINE OIL TEMPERATURE PARAMETER WENT INTO RED FOLLOWED BY A LOW OIL PRESSURE WARNING. ENGINE SHUT DOWN, EMERGENCY DECLARED AND UNEVENTFULY LANDING. NR 1 ENGINE REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2000-10-31TC: FOLLOW-Oct 7, 2000 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA001024043Actuator · failed(CAN) DURING TAKEOFF, STAB TRIM CAUTION MESSAGE ILLUMINATED. TAKEOFF ABORTED AT 100 KNOTS.RTO INSPECTION, HSTA AND MCU REPLACEMENT CARRIED OUT ON AIRCRAFT BEFORE RETURNING INTO SERVICE.Oct 7, 2000 · Cndair CL6002B19 · Stabilizer ActuatorSDR CA001024046Computer · failed(CAN) DURING TAKEOFF STALL FAIL CAUTION MESSAGE ILLUMINATED. TAKEOFF ABORTED.STALL PROTECTION COMPUTER RESET AS PER AMM, AIRCRAFT RETURNED TO SERVICE.Oct 7, 2000 · Cndair CL6002B19 · Stall Warning SystemSDR CA001024048Computer · failed(CAN) DURING CLIMB OUT, AT 160 KNOTS AND 1500 FEET, STALL FAIL CAUTION MESSAGE ILLUMINATED. STALL PROTECTION COMPUTER RESET AS PER AMM, AIRCRAFT RETURNED TO SERVICE.Oct 7, 2000 · Cndair CL6002B19 · Stall Warning SystemSDR CA001024049Valve · failed(CAN) ON APPROACH UNABLE TO EXTEND NOSE LANDING GEAR. MANUAL EXTENSION USED. NOSE WHEEL STEERING FAILED ON LANDING. NLG EXTEND AND STEERING VALVE REPLACED AS PER AMM. AIRCRAFT RETURNED TO SERVICE.Oct 7, 2000 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR CA001024026Engine · failed(CAN) DURING CLIMB, NR 1 ENGINE EXPERIENCED AN UN-COMMANDED SHUT DOWN. FLIGHT CREW DECLARED AN EMERGENCY LANDING (UNEVENTFUL). THE AIRPORT FIRE DEPARTMENT FOAMED THE ENGINE AFTER LANDING BECAUSE OF VISIBLE SMOKE COMING OUT OF THE JET PIPE. THE ENGINE LPT HAD DOct 6, 2000 · Cndair CL6002B19 · Turbine SectionSDR CA001024028Control Unit · failed(CAN) CREW REPORTED SEVERAL STAB AND MACH TRIM CAUTION MESSAGES INTERMITTENT IN CLIMB AND CRUISE. REPLACED THE HSTCU, AIRCRAFT BACK IN SERVICE.Oct 6, 2000 · Cndair CL6002B19 · Stabilizer Control SystemSDR CA001024030Control Unit · malfunctioned(CAN) CREW REPORTED A CONFIG STAB WARNING MESSAGE DURING TAKEOFF ROLL AND STAB NOSE UP BY ITSELF. ABORTED TAKEOFF AT 97 KNOTS.NO FAULTS ON HSTCU NOR ON THE MDC. PERFORMED FULL OPERATIONAL CHECK OF STAB. NO FAULTS FOUND. AIRCRAFT RETURNED TO SERVICE.Oct 6, 2000 · Cndair CL6002B19 · Stabilizer Control SystemSDR CA001024031Filter · failed(CAN) CREW REPORTED A RT FUEL TO PRESSURE CAUTION MESSAGE IN DESCENT. MESSAGE WENT AWAY WHEN THE THRUST LEVERS WERE PUSHED FORWARD.MAINTENANCE REPLACEDTHE RT ENGINE FUEL FILTER ELEMENT AND RT ENGINE FUEL LO PRESS SWITCH. AIRCRAFT BACK IN SERVICE.Oct 6, 2000 · Cndair CL6002B19 · Engine Fuel PumpSDR CA001024034Idg · lack of lube(CAN) UPON TAKEOFF, NR 1 IDG DROPPED OFFLINE, ABORTED TAKEOFF. FOUND LEFT IDG OIL LEVEL LOW. SERVICED IDG PER AMM. AIRCRAFT BACK IN SERVICE.Oct 6, 2000 · Cndair CL6002B19 · AC Generator-AlternatorSDR CA001024036Handle · failed(CAN) CREW REPORTED A CARGO DOOR CAUTION MESSAGE DURING CLIMB. CREW RETURNED TO FIELD.LUBED CARGO DOOR HANDLE AND OPS CHECK PER AMM.AIRCRAFT BACK IN SERVICE.Oct 6, 2000 · Cndair CL6002B19 · Cargo/Baggage DoorsSDR CA001024037Warning System · activated(CAN) CREW REPORTED A CARGO DOOR CAUTION MESSAGE AFTER TAKEOFF. CREW RETURNED TO FIELD. OPS CHECKED PER AMM.Oct 6, 2000 · Cndair CL6002B19 · Door Warning SystemSDR CA001024039Computer · failed(CAN) STALL FAIL CAUTION MESSAGE POSTED FOLLOWED BY CONFIG SPOILERS MESSAGE AT APPROX. 80 KTS.ABORTED TAKEOFF, AND RETURNED TO BLOCKS.SPC MEMORY RESET PER AMM. AIRCRAFT BACK IN SERVICE.Oct 6, 2000 · Cndair CL6002B19 · Stall Warning SystemSDR COMA0060788Engine · failedLEFT ENGINE FAILED DURING CLIMB. TURBINE SEIZED. REMOVED AND REPLACED LEFT ENGINE.Oct 4, 2000 · N946CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA001024017Control Unit · failed(CAN) FLAP FAIL MESSAGE APPEARED ON FLIGHT (CRUISE) WHEN FLAPS AT 0 DEGREES.RESET THE FLAP SYSTEM, AIRCRAFT BACK IN SERVICE.Sep 30, 2000 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA001024018Actuator · failed(CAN) WHEN OPERATING THE PILOT/CO-PILOT STAB TRIM SWITCHES, THE STAB TRIM CHANNEL NR 1 INOP MESSAGE APPEARS.REPLACED THE HSTA AND MCU. SERIAL NUMBERS NOT AVAILABLE AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.Sep 30, 2000 · Cndair CL6002B19 · Stabilizer ActuatorSDR CA001024010Computer · malfunctioned(CAN) STALL FAIL MESSAGE POSTED ON THE EICAS IN FLIGHT AT 250 KTS.STALL COMPUTER RESET. AIRCRAFT RETURNED TO SERVICE.Sep 27, 2000 · Cndair CL6002B19 · Stall Warning SystemSDR CA001024011Computer · malfunctioned(CAN) STALL FAIL CAUTION MESSAGE POSTED UPON TAKEOFF, ASSOCIATED WITH CONFIG SPOILERS WARNING.ABORTED TAKEOFF AT 80 KTS.RESET STALL COMPUTER. SYSTEM OPS CHECKED GOOD.AIRCRAFT BACK IN SERVICE.Sep 27, 2000 · Cndair CL6002B19 · Stall Warning SystemSDR CA001024012Computer · malfunctioned(CAN) STALL FAIL CAUTION MESSAGE POSTED UPON TAKEOFF, ASSOCIATED WITH CONFIG SPOILERS WARNING.ABORTED TAKEOFF AT 80 KTS.RESET STALL COMPUTER. AIRCRAFT BACK IN SERVICE.Sep 27, 2000 · Cndair CL6002B19 · Stall Warning SystemSDR COMA0060783Check Valve · failedINFLIGHT, BUFFET VIBRATION COMING FROM CABIN. REPLACED THE RIGHT HAND ENGINE 10TH STAGE BLEED AIR CHECK VALVE.Sep 24, 2000 · N981CA · Cndair CL6002B19 · Engine Bleed Air SystemSDR CA001024005Computer · malfunctioned(CAN) A STALL FAIL CAUTION MESSAGE APPEARED ON TAKEOFF ROLL AT 70 KTS, FOLLOWED BY A CONFIG SPLRS WARNING MESSAGE (THE TAKEOFF WAS NOT ABORTED).THE STALL COMPUTER WAS RESET (EICAS 2000 INCORPORATED ON THIS A/C).Sep 23, 2000 · Cndair CL6002B19 · Stall Warning SystemSDR CA001024009Actuator · failed(CAN) CREW REPORTED FLAP FAIL MESSAGE AND FLAPS MOVEMENT STOPPED AFTER SELECTION FROM 0 TO 8 DEGREES DURING APPROACH. (NOTE: SB 601R-27-111 WAS CARRIED OUT 3 WEEKS AGO.) THE MAINTENANCE FOUND THE FLEXSHAFT BETWEEN NR 3 & NR 4 ACTUATORS TWISTED/KINKED. CABLES RSep 23, 2000 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CA001003018Computer · malfunctioned(CAN) STALL FAIL CAUTION MESSAGE POSTED UPON TAKEOFF. RESET STALL COMPUTER, A/C BACK IN SERVICE.Sep 22, 2000 · Cndair CL6002B19 · Stall Warning SystemSDR CA001003023Actuator · failed(CAN) STAB TRIM CHANNEL NR 2 WILL NOT ENGAGE & MACH TRIM CATUION MESSAGE AT THE GATE. REPLACED THE HSTA AND THE MCU ON SPEC.NOTE: DURING REPLACEMENT, FOUND THE STABILIZER SURFACE TO BE EXCESSIVELY STIFF TO MOVE. STABILIZER PIVOT LUBRICATED. A/C BACK IN SERVICESep 22, 2000 · Cndair CL6002B19 · Stabilizer Control SystemSDR CA001003013Control Unit · failed(CAN) STAB TRIM CHANNEL NR 2 MESSAGE ON EICAS POSTED PRIOR TO DEPARTURE.MAINTENANCE REPLACED THE MCU (MOTOR CONTROL UNIT). A/C RETURNED TO SERVICE.Sep 20, 2000 · Cndair CL6002B19 · Stabilizer Control SystemSDR CA001003016Engine · damaged(CAN) DURING MORNING CREW PRE-FLIGHT WALK AROUND, RT ENGINE INTAKE, FAN & GUIDE VANES FOUND DAMAGED.ENGINE CHANGED, A/C BACK IN SERVICE.TC: SUSPECT FOD NO - FURTHER ACTIONSep 20, 2000 · Cndair CL6002B19 · Turbine Engine Air Inlet SectionSDR CA001003017Transducer · failed(CAN) STALL FAIL CAUTION MESSAGE ON EICAS FOLLOWED BY INBD SPOILERS MESSAGE ON TAKE OFF ROLL. REPLACED AOA NR 1 TRANSDUCER AND AOA NR 2 TRANSDUCER (STIFF WHEN ROTATING). A/C BACK IN SERVICE.Sep 20, 2000 · Cndair CL6002B19 · Stall Warning SystemSDR COMA0060758Engine · overservicedTHE LEFT ENGINE INCREASED TO 160 DEGREES DURING CLIMBOUT. FOUND THE LEFT ENGINE OVER SERVICED WITH OIL, SERVICED TO PROPER LEVEL.Sep 19, 2000 · N936CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA001003010Computer · failed(CAN) STALL FAIL MESSAGE POSTED ON THE EICAS AFTER TAKEOFF. A/C MADE AN AIR RETURN TO THE BASE. AOA CHECKED, NO CODES FOR SPC IN MDC, PUSHER CHECKED GOOD. STALL COMPUTER RESET. A/C RETURNED TO SERVICE.Sep 19, 2000 · Cndair CL6002B19 · Stall Warning SystemSDR CA001003011Computer · failed(CAN) STALL FAIL MESSAGE POSTED ON THE EICAS AFTER TAKEOFF. A/C MADE AN AIR RETURN TO THE BASE. REPLACED STALL COMPUTER AND TESTED PER AMM. A/C BACK IN SERVICE.Sep 19, 2000 · Cndair CL6002B19 · Stall Warning SystemSDR CA001019032Control Unit · failed(CAN) FLAP FAIL MESSAGE IN ROUTE TO MCI. FLAP AT 0 DEGREE FOR LANDING. REPLACED THE FLAP ELECTRONIC UNIT AND PERFORMED FLAP INSPECTION AS PER AMM 27-51-10.Sep 14, 2000 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA001212015Selector Valve · failed(CAN) WHILE TOWING AIRCRAFT TO HANGER, THE NOSE LANDING GEAR COLLAPSED AND RETRACTED, CAUSING CONSIDERABLE DAMAAGE TO THE AIRCRAFT. NOSE LANDING GEAR SELECTOR VALVE FAILURE AND PREVIOUS BRAKE SYSTEM PROBLEMS.STRUCTURE REPAIR CARRIED OUT, NOSE LANDING GEAR CHANSep 10, 2000 · Cndair CL6002B19 · Landing Gear SelectorSDR COMA0060726Engine · overservicedLEFT ENGINE OIL TEMP IN RED ZONE. ENGINE WAS OVERSERVICED WITH OIL. DRAINED EXCESS OIL AND REPAIRED OIL REPLENISHMENT SYSTEM.Sep 4, 2000 · N835CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA001002003Spring · failed(CAN) FLIGHT CREW REPORTED THE PRESSURIZATION VALVE ON THE MAIN CABIN DOOR WILL NOT CLOSED. MAINTENANCE FOUND THE ROD SPRING WEAK, THEY REPLACED THE ROD ASSY.Sep 4, 2000 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA001002015Bpsu · failed(CAN) FLAPS FAIL EICAS MESSAGE AFTER SWITCHING NR 2 GENERATOR ON LINE AFTER ENGINE START. FERRIED A/C TO MAIN BASE. REPLACED LT & RT BRAKE POSITION SENSOR UNIT (BPSU). A/C RETURNED TO SERVICE.Sep 1, 2000 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA000919005Handle · failed(CAN) CREW REPORTED PAX DOOR OUTER HANDLE MSG POSTED AFTER TAKEOFF. A/C RETURNED TO FRESNO, CA. MAINTENANCE CONFIRMED GROUND CHECKS NORMAL.Aug 31, 2000 · Cndair CL6002B19 · Door Warning SystemSDR CA000919002Sensor · failed(CAN) FLIGHT NR 5805 FROM CVG TO ISP, THE FLIGHT CREW REPORTED. STALL FAIL MSG AT 80 KTS, ON TAKEOFF ROLL. (ABORTED TAKEOFF BELOW 80 KTS). AIRCRAFT RETURNED TO THE GATE FOR INVESTIGATION. MAINTENANCE CREW REPLACED THE AOA SENSOR AND THE AIRCRAFT RETURNED IN SEAug 31, 2000 · Cndair CL6002B19 · Stall Warning SystemSDR CA000919004Torque Link · failed(CAN) FLIGHT NR 5122 FROM MSY TO MCO, THE FLIGHT CREW REPORTED: THE NOSE GEAR STEERING DISCONNECTED ON TAXI OUT (SCISSORS). MAINTENANCE RECONNECTED THE NOSE GEAR STEERING TORQUE LINK (SCISSORS).Aug 31, 2000 · Cndair CL6002B19 · Landing Gear Steering SystemSDR CA000919011Engine · leaking(CAN) FLIGHT NR 5737 FROM CVG TO MSN, THE FLIGHT CREW RPORTED: THE RIGHT ENGINE OIL PRESSURE WARNING ILLUMINTED IN FLIGHT. ENGINE WAS SHUT DOWN AS PER QRH PROCEDURE: DECLARED EMERGENCY LANDING AND RETURNED TO THE DEPARTURE AIRPORT. THE LANDING WAS UNEVENTFUL. Aug 31, 2000 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA001019031Door · out of adj(CAN) MAIN PASSENGER DOOR DIFFICULT TO CLOSE. PASSENGER DOOR LUBED AND RIGGED AS PER MAINTENANCE MANUAL 52-11-02. DOOR FOUND SERVICEABLE.Aug 28, 2000 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA000919012Engine · failed(CAN) FLIGHT NR 6047 FROM (LGA) TO (BUF) CLIMBING THROUGH 17,000 FT LEFT ENGINE FAILED. MADE A SINGLE ENGINE LANDING WITHOUT INCIDENT. CREW DECLARED AN EMERGENCY AND MADE AN UNSCHEDULED LANDING INTO (AVP).SENT MECHANICS, FOUND BLADES MISSING ON LPT. STILL INVEAug 24, 2000 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA000919013Sensor · failed(CAN) FLIGHT NR 5979 FROM (CVG) TO (GRR), THE FLIGHT CREW REPORTED: DURING TAKEOFF ROLL AT APPROXIMATELY 80 KTS, THE STALL FAIL MSG ILLUMINATED (TAKEOFF ABORTED)(SECOND ATTEMPT).MAINTENANCE REPLACED LT AND RT AOA SENSORS.Aug 24, 2000 · Cndair CL6002B19 · Stall Warning SystemSDR CA000919015Engine · failed(CAN) IN FLIGHT. ENCOUNTERED EXTREME TURBULENCE, BOTH L/R ENGINE OIL PRESS WARNING MESSAGES APPEAED. IT WAS NEAR IMPOSSIBLE TO CONTROL THE AIRCRAFT. THE LANDING WAS UNEVENTFUL. SEVERE TURBULENCE INSPECTION CARRIED OUT, NO DAMAGE RPORTED (FDR WAS REMOVED FOR RAug 24, 2000 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA000830025Handle · out of rig(CAN) MAIN PAX DOOR HANDLE WAS STUCK. DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE.PAX DOOR RIGGED AS PER AMM 52-11-02-820-801 AND SL 52-010.Aug 23, 2000 · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0060682Engine · failedLEFT ENGINE FAILED DURING FLIGHT. REPLACED LEFT ENGINE.Aug 22, 2000 · N987CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)
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