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 CA010307027Panel · cracked(CAN) DURING A C CHECK INSPECTION, A CRACK WAS FOUND IN THE LOWER WING PLANK AT WING STATION WS 148.019.AT THE TIME OF REPORT, THE AIRCRAFT WAS STILL IN C CHECK. REPAIR ENGINEERING ORDER (REO) 601R-57-21-130 WILL BE APPLIED PRIOR TO RETURNING THE AIRCRAFT INTOFeb 19, 2001 · Cndair CL6002B19 · Wing, Plate/SkinSDR CA010226010Window · cracked(CAN) THE RT WINDOW CRACKED IN CRUISE. THE MAINTENANCE REPLACED THE WINDOW.Feb 2, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA010308007Apu · damaged(CAN) SMELL OF FUEL AND SMOKE IN AIRCRAFT AFTER APU STARTED ON DESCENT. EMERGENCY RESPONSE CALLED. FLIGHT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. APU REPLACED OPERATION AND LEAK CHECK CARRIED OUT AND SYSTEM CHECKED SERVICEABLE.Feb 2, 2001 · Cndair CL6002B19 · APU Core EngineSDR CA020104013Windshield · failed(CAN) CAPTS WINDSHIELD SHATTERED AT TOP OF DESCENT. WINDSHIELD REPLACED AS PER AMM 30-41-01-710.Jan 21, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA0160128Carbon Seal · leakingLEFT ENGINE OIL PRESSURE FLUCTUATING BETWEEN 30 AND 48 PSI. REPLACED THE ACCESSORY DRIVES CARBON SEALS.Jan 17, 2001 · N949CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR COMA0160110Plug · chafedLEFT ENGINE FAN VIB INDICATED 2.7. FOUND BLADES RUBBING AT ACCESS PLUG. ADJUSTED GAP AT ACCESS PLUG.Jan 14, 2001 · N967CA · Cndair CL6002B19 · Turbine Engine Bypass SectionSDR COMA0160098Spinner · vibrationLEFT ENGINE FAN VIB INDICATED 2.7. REPLACED THE AFT FAN SPINNER (OUT OF BALANCE).Jan 13, 2001 · N954CA · Cndair CL6002B19 · Turbine Engine Bypass SectionSDR CA011113017Support · cracked(CAN) FOUND THREE CRACKS DURING CHECKS. CRACKED AT FS 630 & 640, LT & RT BL 36 & 00.Jan 11, 2001 · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR COMA0160093Engine · vibrationRT ENGINE VIB INDICATION AT .7, ENGINE FAILED. REPLACED ENGINE.Jan 7, 2001 · N709CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA0160057Nozzle · departedVIBRATION FELT DURING FLIGHT, VIBRATION STOPPED DURING DECENT. POST FLIGHT INSP FOUND LEFT ENGINE TAILPIPE AND EXHAUST FAIRING HAD DEPARTED ACFT.REPLACED LEFT ENGINE.Jan 3, 2001 · N933CA · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR CA010116027Windshield · failed(CAN) IN CRUISE, THE F/OS FRONT WINDSHIELD SHATTERED AT 31,000 FEET.THE MAINTENANCE REPLACED THE WINDSHIELD AND RETURNED THE AIRCRAFT TO SERVICE.Jan 3, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA010202011Actuator · failed(CAN) THE CREW REPORTED THE FLAP FAIL CAUTION MESSAGE WHICH APPEARED ON APPROACH (SELECTIION OF 45 DEGREES, STOPPED AT 37). THE MAINTENANCE REPLACED THE RT OUTBOARD FLAP INBOARD ACTUATORJan 3, 2001 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR COMA0160042Bolt · missingWE WERE REMOVING THE QEC KIT FROM ENGINE 807539 THAT WAS INSTALLED ON A PORTABLE ENGINE STAND. WHEN IT CAME TIME TO REMOVE THE EXHAUST NOZZLE P/N 228-55030-11J WE FOUND 7 BOLTS (OUT OF 30) MISSING. FOUR OF THE BOLTS (P/N NAS6303U4 AND NAS 6303U9) WERE LOCATED Jan 2, 2001 · Cndair CL6002B19 · Turbine Engine Combustion SectionSDR CA010201007Windshield · cracked(CAN) CAPTAINS WINDSHIELD CRACKED ON DESCENT TO TORONTO AT 25,000 FEET. REPLACED CAPTAINS WINDSHIELD.Dec 31, 2000 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA010321007Windshield · cracked(CAN) CAPTAINS WINDSHIELD CRACKED ON DESCENT TO TORONTO AT 25,000 FEET. REPLACED CAPTAINS WINDSHIELD.Dec 31, 2000 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA010116031Windshield · cracked(CAN) THE CAPTAINS WINDSHIELD CRACKED ON TAXI OUT.THE MAINTENANCE REPLACED THE WINDSHIELD.Dec 18, 2000 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA010201010Handle · failed(CAN) AFTER TAKEOFF, AN OPEN DOOR PASSENGER DOOR WARNING MESSAGE APPEARED. THE AIRCRAFT RETURNED TO OTTAWA. AFTER LANDING, THEY FOUND THAT THE OUTER HANDLE WAS POPPED OUT. THE INNER HANDLE STOP WAS ADJUSTED. THE INNER DOOR RIGGING CHECK OK, PASSENGER DOOR SENSDec 13, 2000 · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0061042Fuel Control · malfunctionedLEFT ENGINE N2 COULD NOT BE REDUCED BELOW 85 PERCENT IFSD. REPLACED THE FUEL CONTROL.Dec 11, 2000 · N420CA · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR CA001229024Actuator · failed(CAN) THE L REV UNLOCKED MESSAGE POSTED AFTER TAKEOFF. NO OTHER INDICATION OF T/R DEPLOYMENT. THE MAINTENANCE REPLACE THE LEFT T/R POWER DRIVE UNIT, AIRCRAFT RETURNED TO SERVICE.Dec 11, 2000 · Cndair CL6002B19 · Engine Thrust ReverserSDR COMA0061020Engine · flamed outLEFT ENGINE FLAMED OUT DURING APPROACH. REPLACED ENGINE.Dec 8, 2000 · N971CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA010102002Smoke Detector · malfunctioned(CAN) THE CREW REPORTED A SMOKE TOILET CAUTION MESSAGE DURING CRUISE. THE MAINTENANCE DID AN INSPECTION AND FOUND NO EVIDENCE OF BURNING SMELL. THEY REPLACE THE SMOKE DETECTOR AFTER THEY FERRIED THE A/C TO THE MAIN BASE.Dec 6, 2000 · Cndair CL6002B19 · Smoke DetectionSDR CA010102005Sensor · dirty(CAN) THE CREW REPORTED THAT DURING CLIMB, AT 7000 FT, A PASSENGER DOOR CAUTION MESSAGE (NOT SPECIFIED) CAME ON. AT 11000 FT, THE PASSENGER DOOR WARNING MESSAGE CAME ON. THE MAINTENANCE INTERROGATED THE PSEU, FOUND S76 AND S27 AT FAULTY. THE SENSORS WERE CLEANDec 6, 2000 · Cndair CL6002B19 · Door Warning SystemSDR CA001211019Control Cable · broken(CAN) AFTER SELECTING THE FLAPS TO 8 DEGREE, THE FLAP FAIL CAUTION MSG APPEARED. FLAPS REMAINED AT 0 DEGREE.REPLACED THE LEFT EPSU REPLACED THE RIGHT BPSU FOUND RIGHT FLEXDRIVE SEVERAL STRANDS WERE BROKEN & TWISTED AROUND THE FLEX DRIVE.Nov 24, 2000 · Cndair CL6002B19 · Stabilizer Control SystemSDR COMA0060936Engine · vibrationLEFT ENGINE N2 VIB WARNING. REPLACED THE LEFT ENGINE.Nov 22, 2000 · N712CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA001212011Controller · failed(CAN) FLAPS FAILED AT 20 DEGREE'S ON APPROACH TO TORONTO. FLAPS RETRACTED TO 8 DEGREES ON GROUND, AND FAIL MESSAGE CLEARED.Nov 20, 2000 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA001212009Power Unit · failed(CAN) FLAP FAIL FROM ZERO DEGREE FLAP POSITION 10,000 FEET ALTITUDE LEVEL. SPEED 210 KNOTS. REPLACED FLAP POWER DRIVE UNIT AND BRAKE POSITION SENSING UNIT (BPSU) P/N 865D100-9.Nov 19, 2000 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA001129024Flex Coupling · failed(CAN) AT CRUISE ALTITUDE OF 23,000, THE LT REV UNLOCKED CAUTION MESSAGE APPEARED WITH THE REV ICON ON THE N1 GAUGE AND THE T/R REV EMERGENCY STOW LIGHT ILLUMINATED. EMERGENCY DECLARED. THE MAINTENANCE REPLACED THE THRUST REVERSER / PDU FLEXSHAFT LOCK OUT UNIT.Nov 19, 2000 · Cndair CL6002B19 · Engine Thrust ReverserSDR CA001212010Actuator · failed(CAN) FLAPS FAIL MESSAGE WHEN FLAPS SELECTED TO 8 DEGREES. FLAPS WENT TO 2 DEGREES. FOUND LEFT HAND INBOARD ACTUATOR WITH A HIGH RUNNING TORQUE.LEFT HAND INBOARD ACTUATOR REPLACED, OPERATION CHECK CARRIED OUT.Nov 18, 2000 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CA001212008Actuator · failed(CAN) FLAPS FAILED AT ZERO. REPLACED RIGHT HAND WING NR4 FLAP ACTUATOR, ADJUSTMENT AND TEST CARRIED OUT NIL FAULT.Nov 17, 2000 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CA001129025Actuator · failed(CAN) FLAPS FAILED ON APPROACH AT ZERO. FLAPLESS LANDING CARRIED OUT NORMALLY.SYSTEM RESET IN CHICAGO. CHANGED NR 4 FLEX SHAFT AND NR 1 FLAP ACTUATOR, FLAPS SYSTEM RIGGED OPERATION CHECKED NORMAL. WINTERIZATION TASK COMPLETED.Nov 14, 2000 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CA001129026Control Unit · failed(CAN) FLAPS FAIL ON APPROACH TO OTTAWA. INTERROGATED FECU, FOUND FLAPS JAM MESSAGE. NR 5 CABLE LEFT AND RIGHT BENT. CHANGED NR 5 CABLE, CHECKED FLAP TORQUE, NO FAULT.Nov 13, 2000 · Cndair CL6002B19 · Trailing Edge FlapsSDR CA001129032Control Unit · failed(CAN) ON APPROACH TO OTTAWA, FLAP FAIL MESSAGE ON ENGINE INDICATING AND CREW ALERT SYSTEM, WHEN FLAPS SELECTED TO 8 DEGREES. FLAPS INSPECTED, SYSTEM RESET AND OPERATION CHECKED NORMAL.Nov 10, 2000 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA001129030Switch · faulty(CAN) AFTER DEPARTURE, STAB TRIM AND MACH TRIM MESSAGE APPEARED, STABILIZER WAS STUCK AT 8 UNITS. UNABLE TO TRIM, AIRCRAFT RETURNED TO TORONTO. FOUND FIRST OFFICER DISCONNECT SWITCH AT FAULT. CHANGED FIRST OFFICER STAB DISCONNECT SWITCH, FUNCTIONAL CHECK OF HONov 9, 2000 · Cndair CL6002B19 · Stabilizer Control SystemSDR CA001110039Blade · damaged(CAN) AFTER TAKEOFF OUT OF MANCHESTER NH (MHT) GOT N1 VIB ICON. FOLLOWED BY SMOKE IN CABIN. CREW SHUT DOWN THE ENGINE AND RETURNED TO BLOCKS. PRELIMINARY REPORT OF EXTENSIVE FAN BLADE DAMAGE. ROAD CREW BEING ARRANGED TO GO TO MHT FOR POSSIBLE ENGINE CHANGE. AVNov 7, 2000 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR CA001110040Engine · failed(CAN) INBOUND FLIGHT FROM RALIEGH / DURHAM, NC (RDC). PILOT FELT SLIGHT VIBRATION IN SEAT. OIL PRESSURE WENT TO ZERO. ENGINE AUTO-SHUTDOWN. AIRCRAFT MADE AN UNEVENTFUL LANDING. CHIP DETECTOR HAS LARGE AMOUNT OF DEBRIS ON IT.ENGINE HAS APPROXIMATELY 9000 HOURS Nov 7, 2000 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA0060893Engine · failedRIGHT ENGINE FAILED, HIGH N1 VIB AND ZERO OIL PRESSURE. REPLACED ENGINE.Nov 6, 2000 · N983CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA0060894Engine · failedLEFT ENGINE LOW OIL PRESSURE WARNING, AND THEN LEFT ENGINE FAILED. REPLACED ENGINE.Nov 6, 2000 · N963CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA001129027Actuator · failed(CAN) BOTH STABILIZRER TRIM CHANNELS FAILED, BOTH WENT BACK TO NORMAL, THEN REOCCURRED ON LANDING. ATTEMPTED TO RESET, MESSAGE DISAPPEARED MOMENTARILY, THEN FAULT REOCCURRED. HISTORY FAULT.STABILIZER MOTOR CONTROL UNIT (P/N 7062-3) AND HORIZONTAL STABILIZER TRNov 6, 2000 · Cndair CL6002B19 · Stabilizer ActuatorSDR CA001129029Computer · failed(CAN) ON APPROACH, FUEL IMBALANCE CAUTION MESSAGE, QUICK REFERENCE HANDBOOK PROCEDURE CARRIED OUT, EXCEPT GRAVITY FLOW DUE TIME CONSTRAINT ON APPROACH.COULD NOT TRANSFER ON AUTOMATIC OR MANUAL MODE. FLIGHT CREW DECLARED EMERGENCY. CHANGED 3 TANKS CONFIGURATIONov 6, 2000 · Cndair CL6002B19 · Fuel Quantity IndicatorSDR CA001110038Duct · cracked(CAN) AFTER FLIGHT 5401 FROM CVG TO TOL, WHILE PARKED AT THE GATE WITH APU RUNNING GOT A SMOKE TOILET WARNING MSG & LAV SMOKE DETECTOR WAS BEEPING. ALSO SMOKE IN THE CABIN. PERFORMED QRH, SMOKE DETECTOR STOPPED BEEPING & WARNING MSG CLEARED, AND CALLED FOR FIRNov 4, 2000 · Cndair CL6002B19 · Air Distribution SystemSDR CA001110032Relay · failed(CAN) APR INOP CAUTION MESSAGE ON TAKEOFF ROLL, ABORTED TAKEOFF. REMOVED AND REPLACED APR ARM RELAY (K1KL) IN JB-5. OPS CHECKED, SYSTEM NORMAL.Nov 2, 2000 · Cndair CL6002B19 · Electrical Power SystemSDR CA001110034Compressor · damaged(CAN) CREW REPORTED NR 1 ENGINE VIBRATION AFTER TAKEOFF FOLLOWED BY AN UNCOMMANDED ENGINE STOPPAGE. MAINTENANCE REPORTED THAT A BORESCOPE INSPECTION REVEALED EXTENSIVE COMPRESSOR DAMAGE. 2000-11-14TC:Nov 2, 2000 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR CA001129034Sensor · failed(CAN) AT 1,000 FTAGL PASSENGER DOOR LATCH CAUTION MESSAGE CAME ON. IN CLIMB, THROUGH 6,000 FEET, PASSENGER DOOR WARNING CAME ON. MESSAGE DISAPPEARED IN DESCENT, PRESURIZATION WAS NORMAL.AIRCRAFT RETURNED.INTEROGATED PROXIMITY SENSING ELECTRONIC UNIT, FOUND S26Nov 1, 2000 · Cndair CL6002B19 · Door Warning SystemSDR CA001107008Fuel Control · malfunctioned(CAN) DURING CRUISE, NR 2 ENGINE N2 NOTED DROPPING TOWARDS ZERO AND ITT RAPIDLY INCREASING INTO THE RED.FAULTY MFC CONFIRMED DURING GROUND RUN. MFC REPLACED AND A SUCCESSFUL GROUND RUN FOLLOWED.Oct 29, 2000 · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR CA001107009Compressor · damaged(CAN) CREW REPORTED NR 1 ENGINE VIBRATION AFTER TAKEOFF FOLLOWED BY UNCOMMANDED ENGINE STOPPAGE.BOROSCOPE INSPECTION REVEALED EXTENSIVE COMPRESSOR DAMAGE.Oct 29, 2000 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR SWIA972063Relay · failedAPR INOP ON TAKEOFF ROLL. ABORTED TAKEOFF FAT - DEFERRED APR. REMOVED AND REPLACED APR ARM RELAY (KIKL) IN JB5 MM 76-13-01. RAN BOTH ENGINES APR TESTS NR 1, 2, 3, FUNCTION NORMALLY.Oct 28, 2000 · N405SW · Cndair CL6002B19 · Fuel Controlling SystemSDR CA001110006Shaft · failed(CAN) FLAP FAILED ON APPROACH TO OTTAWA, THROUGH 10,500 FEET, 190 KNOTS, WITH SPOILERS EXTENDED WHEN FLAPS SELECTED AT 8 DEGREES. FOUND LT & RT ACTUATORS AND FLEX LT NR 1 AT FAULT. ACTUATORS AND FLEX CHANGED, SYSTEM RIGGING AND OPERATION CHECK CARRIED OUT.Oct 26, 2000 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA001110011Actuator · failed(CAN) APPROXIMATELY 30 MINUTES AFTER TAKEOFF, STABILIZER TRIM MESSAGE ON ENGINE INDICATING CREW ALERT SYSTEM, NO CHANGE WITH AUTO PILOT ON/OFF. ATTEMPTED TO RESET MESSAGE DISAPPEARED MOMENTARILY, THEN FAULT REOCCURRED. AIRCRAFT RETURNED TO TORONTO. CHANGED Oct 25, 2000 · Cndair CL6002B19 · Stabilizer ActuatorSDR CA001110010Bpsu · failed(CAN) FLAPS FAIL ON APPROACH AT FLAP AND SELECTION, FLAPS FAILED AT ZERO. AIRCRAFT LANDED FLAPLESS. LEFT AND RIGHT FLEX CABLES LUBRICATED, BRAKE POSITION SENSING UNITS CHANGED. SYSTEM RIGGED, FLAP ELECTRONIC CONTROL UNIT TEST CARRIED OUT, SYSTEM OPERATION CHECOct 21, 2000 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA001110022Shaft · broken(CAN) FLAP FAIL MESSAGE WHEN FLAPS SELECTED TO 8 DEGREES. AIRCRAFT DIVERTED TO WASHINGTON.FOUND RIGHT HAND OUTBOARD FLAP FLEX SHAFT TORN AND BROKEN. REPLACED FLEX SHAFT, SYSTEM RIGGED AND OPERATION CHECKED NORMAL.Oct 21, 2000 · Cndair CL6002B19 · Trailing Edge Flap Control System
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