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 CA000209057Control Unit · failed(CAN) FLAPS FAIL AT 0 DEG. RT BPSU AND FCU REPLACED.Jan 18, 2000 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA000120029Smoke Detector · false activation(CAN) IN FLIGHT,CARGO SMOKE MESSAGE ASSOCIATED WITH AURAL WARNING & TRIPLE CHIME. QRH PROCEEDURE CARRIED OUT. ACTIVATED CARGO BAY EXTINGUISHERS. REPLACED BOTH EXTINGUISHER & SMOKE DETECTOR.Jan 18, 2000 · Cndair CL6002B19 · Smoke DetectionSDR CA000209052Panel · broken(CAN) FLIGHT SPOILER DEPLOY MESSAGE, NO SPOILER DEPLOYED ON APPROACH TO WASHINGTON WHEN FLAPS SELECTED AT 45 DEG. A/C ROLLED SHARPLY RIGHT WING DOWN, MANUAL FLIGHT LANDED WITH 30 DEG FLAP. FOUND RIGHT HAND SPOILER PANEL I/B POWER CONTROL ACTUATOR ATTACH HINGE Jan 16, 2000 · Cndair CL6002B19 · Drag Control ActuatorSDR COMA0060055Carbon Seal · leakingRIGHT ENGINE IFSD BECAUSE OF LOW OIL PRESURE. REMOVED AND INSPECTED ALL AGB DRIVE CARBON SEALS. NO DEFECTS FOUND. REASSEMBLED AND C/W OIL CONSUMPTION RUNS. ALL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE.Jan 15, 2000 · N924CA · Cndair CL6002B19 · Turbine Engine Accessory DriveSDR CA000209055Lever · failed(CAN) ON APPROACH FLAP FAIL MESSAGE APPEARED WITH NO MOVEMENT OF FLAP LEVER. FLAPS INSPECTED AS PER AD CF98-14R1, NO FAULT FOUND.Jan 15, 2000 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA000209051Adc · failed(CAN) CAPT & FO PRIMARY FLIGHT DISPLAYS HAD YELLOW INDICATED AIRSPEED FLAGS. CAPT PITOT LINE FOUND CONTAMINATED WITH WATER. LINE PURGED AND BOTH ADC SYSTEM HIGH RANGE LEAK CHECKED. NO FAULTS FOUND.Jan 12, 2000 · Cndair CL6002B19 · Air Data ComputerSDR CA991231037Computer · failed(CAN) UNABLE TO CONTROL CABIN PRESSURE. AIR DATA COMPUTER CHANGED.Jan 11, 2000 · Cndair CL6002B19 · Air Data ComputerSDR CA000209050Brake · failed(CAN) BOTH LT MLG TIRES FOUND DEFLATED ON LANDING. NR 1 BRAKE FOUND AT FAULT. BRAKE, NR 1 AND 2 TIRES REPLACED.Jan 11, 2000 · Cndair CL6002B19 · BrakeSDR CA000209049Bearing · damaged(CAN) GRINDING NOISE FROM NOSE GEAR AREA WHILE TAXING. CREW HALTED A/C TO INSPECT NOSE WHEEL. INNER WHEEL BEARING AND LANDING GEAR AXLE FOUND DAMAGED. WHEEL AND AXLE REPLACED.Jan 8, 2000 · Cndair CL6002B19 · Wheel/Ski/FloatSDR CA000209062Windshield · cracked(CAN) DURING FLIGHT TEST AT FL200, RT WINDSHIELD CRACKED FROM TOP TO BOTTOM, 5 VISABLE LINES. REPLACED.Jan 5, 2000 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA000110067Window · failed(CAN) AFTER LANDING, WHILE TAXING, THE A/C WAS CAUGHT IN SEVERE WIND GUST. LT WING WAS LIFTED OFF THE GROUND, RT WING TIP CONTACTED THE RUNWAY, LT COCKPIT SIDE WINDOW SHATTERED. AWAITING CREW REPORT. UPDATEAS INFO COMES AVAILABLE.Jan 5, 2000 · Cndair CL6002B19 · Wing, Attach FittingsSDR CA000110068Blade · damaged(CAN) IFSD, COMPRESSOR DAMAGEJan 5, 2000 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR CA000209048Sensor · dirty(CAN) CREW REPORTED PASSENGER DOOR WARNING MESSAGE SHORTLY AFTER TAKE OFF, A/C RETURNED TO CHIGAGO. CLEANED SENSORS AND BITE CHECK CARRIED OUT OK.Dec 29, 1999 · Cndair CL6002B19 · Door Warning SystemSDR CA000110080Seal · fouled(CAN) PASSENGER DOOR HANDLE MESSAGE DURING CLIMB THROUGH FL220. WHILE PERFORMING QUICK REFERENCE HANDBOOK PROCEDURE, PASSENGER DOOR WARNING MESSAGE CAME ON.REMOVED GRAVEL FROM DOOR SEAL, DEPRESSOR AND SILL AREA, DOOR CLOSED AND CONFIRMED STOWED AND LOCKED.Dec 22, 1999 · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA9960777Seal · failedLEFT ENGINE OIL PRESSURE WARNING. REPLACED AGB DRIVE SEALS FOR THE EDP AND ATS.Dec 18, 1999 · N962CA · Cndair CL6002B19 · Engine Oil Distribution (Airframe Furnished)SDR CA000110079Rheostat · burned(CAN) ON INITIAL FLOOD LIGHT SELECTION AN ELECTRICAL ARC AND SMOKE EMERGED FROM THE FIRST OFFICER SIDE PANEL. CB POPPED AND SMOKE STOPPED. FOUND RHEOSTAT BEHIND PANEL BURNED, HEAT DAMAGE FOUND ON WIRES. ALL EFFECTED PARTS REPLACED.Dec 17, 1999 · Cndair CL6002B19 · Flight Compartment LightingSDR COMA9960764Filter · cloggedRIGHT HAND ENGINE OIL PRESSURE AT 130 PSI. REPLACED CLOGGED OIL FILTER, AND CLEANED THE OIL PUMP SCAVENGE SCREENS.Dec 14, 1999 · N948CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA991231041Latch · out of rig(CAN) PASSENGER DOOR LATCH MESSAGE ON CLIMB FROM WASHINGTON, THEN RED PASS DOOR AND AURAL WARNING. DOOR RE-RIGGED AND A/C PRESSURIZED.Dec 8, 1999 · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA9960749Engine · lack of lubeRIGHT ENGINE LOW OIL PRESSURE WARNING IFSD. REPLACED RIGHT ENGINE.Dec 5, 1999 · N713CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA000209061Windshield · cracked(CAN) DURING TEST FLIGHT ON APPROACH FOR AUTO PILOT MOD, RT WINDSHIELD CRACKED. REPLACEDDec 4, 1999 · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA971617Target · looseAFTER GEAR RETRACTION GEAR DISAGREE WARNING ON LEFT MAIN GEAR. RETURNED TO SLC. NOTED FAULT IN PSEU FOR LEFT GEAR UPLOCK, (FAR). TIGHTENED UPLOCK TARGET AND CHECKED GAP PER MM 32-32-05. CYCLED GEAR NORMALLY AND PEFORMED FREE FALL CHECK. GEAR INDICATIONS CNov 30, 1999 · N416SW · Cndair CL6002B19 · Landing Gear Position and WarningSDR CA991210075Connector · corroded(CAN) ON APPROACH FLAP FAIL MESSAGE AFTER 20 DEG. R/H BPSU CANNON PLUG FOUND CORRODED ALONG WITH PINS AT BPSU. L/H CANNON PLUG REPLACED AS PRECAUTIONNov 28, 1999 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA991210076Actuator · failed(CAN) ON APPROACH FLAPS FAIL WHEN SELECTED FROM 30 TO 45. FLAPS WOULDN''T RETRACT AFTER LANDING. MAINT COLD SOAKED FLAP ACTUATORS NR4 LH AND 2&3 RH. A/C TEST FLEW U/S. PDU REPLACED SERV.Nov 28, 1999 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR COMA9960719Engine · malfunctionedDURING TAKEOFF, NR 2 ENGINE N1 HUNG AT 38 DEGREES. COULD NOT DUPLICTE. ACCELERATION TEST WAS NORMAL.Nov 26, 1999 · N971CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA971613Sensor · malfunctionedPITOT BASE OVERHEAT WARNING ILLUMINATED AFTER TAKEOFF. RETURNED TO FIELD. POWERED AIRCRAFT DOWN AND BACK UP. NO DEFECTS NOTED AT THIS TIME. AIRCRAFT GOOD FOR CONTINUED SERVICE. REMOVED AND REPLACED AIR DATA SENSOR CONTROLLER AFTER ARRIVAL IN SLC. OPS CHENov 26, 1999 · N410SW · Cndair CL6002B19 · Air Data ComputerSDR CA991210053Secu · failed(CAN) ON DESCENT, FLIGHT SPOILERS DEPLOYED, IMMEDIATE SHARP BANK TO THE RIGHT. SPOILERS RETRACTED. NR 2 SPOILER ECU REPLACED.Nov 20, 1999 · Cndair CL6002B19 · Drag Control SystemSDR CA991210052Bpsu · failed(CAN) FLAPS FAIL ON APPROACH AT 8 DEGREES. RT BPSU REPLACED.Nov 18, 1999 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA991210045Te Flap · failed(CAN) FLAP FAIL MESSAGE ON APPROACH. SYSTEM RESET.Nov 17, 1999 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA991210046Te Flap · faulty(CAN) FLAP FAIL ON APPROACH. RESET CARRIED OUT.Nov 17, 1999 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA991210047Actuator · failed(CAN) FLAPS FAIL ON APPROACH. NR 1AND NR 2 LT ACTUATORS, NR'S1, 3, 4 FLEX SHAFTS REPLACED.Nov 17, 1999 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CA991210050Latch Cam · failed(CAN) UNABLE TO OPEN PASSENGER DOOR ON ARRIVAL. DOOR LATCH MECHANISM CAM AND HOUSING RELOCATED, DOOR RIGGING CARRIED OUT AND DOOR SEAL CHANGED.Nov 17, 1999 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA991210051Sensing Unit · failed(CAN) FLAP FAILED AT 8 DEGREES ON APPROACH. BPSU REPLACED.Nov 11, 1999 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA971599unknownEN ROUTE CLIMB THROUGH FL340 N2 VIB ICON CAME ON. WOULD NOT GO OUT UNTIL N1 REDUCED TO 80 PERCENT. ON DESCENT, N2 ICON AGAIN CAME ON AT FL300. REDUCED N1 TO 79 PERCENT. N2 VIB ICON OUT. RETURNED TO SLC. REPLACED ENGINE VIBRATION TRANSDUCER RIGHT ENGINE ANov 10, 1999 · N403SW · Cndair CL6002B19 · Engine Vibration AnalyzerSDR CA991103049Throttle Cable · seized(CAN) RIGHT THROTTLE FROZE AT FL 370 AFTER APPROXIMATELY 3.5 HOURS. THROTTLE CABLE CLEANED WITH DRY NITROGEN. AIRCRAFT RETURNED TO SERVICE.Nov 9, 1999 · Cndair CL6002B16 · Power LeverSDR CA991210048Pseu · failed(CAN) AFTER TAKEOFF, MLG INDICATED UNSAFE AFTER GEAR UP SELECTION. PROX IMITY TARGET ADJUSTED AND PSU REPLACED.Nov 8, 1999 · Cndair CL6002B19 · Landing Gear Position and WarningSDR CA991210049Handle · worn(CAN) AFTER TAKEOFF, EXPERIENCED A BANG TYPE NOISE AND PASSENGER DOOR MESSAGE. EXCESSIVE WEAR ON PASSENGER DOOR HANDLE. HANDLE REPLACED AND PRESSURE CHECK CARRIED OUT.Nov 8, 1999 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA991210044Drive Unit · failed(CAN) FLAP FAIL AT ZERO. ZERO FLAP LANDING CARRIED OUT. FLPA PDU REPLACED.Nov 7, 1999 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA971592De-Ice Sys · malfunctionedANTI-ICE DUCT MESSAGE WITH -A/I+ ON LEFT WING LEADING EDGE RED ON ANTI-ICE SYNOPTIC PAGE. RETURNED TO SLC. LEFT WING SUFFICIENT OVERHEAT SENSOR CHANGED. OPS CHECK GOOD.Nov 7, 1999 · N416SW · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR CA991210067Throttle · failed(CAN) CREW REPORTED THE LEFT ENGINE POWER LEVER WAS UNABLE TO RETARD TO IDLE CUTOFF. ENG SHUT DOWN BY FIRE PUSH BUTTON.Nov 5, 1999 · Cndair CL6002B19 · Power LeverSDR CA991210043Controller · failed(CAN) LEFT WINDSHIELD HEAT MESSAGE WITH BURNING SMELL IN COCKPIT. WINDSHIELD TEMPERATURE CONTROLLER REPLACED.Nov 4, 1999 · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR CA991210042Bpsu · failed(CAN) FLAPS FAIL AT 40 DEGREES DURING TAXI. LEFT NR 5 FLEX SHAFT CLEANED AND LUBED AND LT BPSU REPLACED.Nov 3, 1999 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA971591Engine · low powerCLIMBING THROUGH 33,000 N2 VIB WARNING ON N2 GAUGE ILLUMINATED (NR 2 ENGINE). REDUCED POWER UNTIL VIB WARNING CLEARED (84 PERCENT N1). DESCENDED TO 27,000 TO MAINTAIN FLYABLE AIRSPEED. ADVANCED NR 2 ENGINE POWER AND VIB WARNING CAME ON AGAIN AT 80 PERCENT N1Nov 3, 1999 · N403SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA991210041Te Flap · failed(CAN) FLAPS FAIL AT 38 DEGREES ON APPROACH. SYSTEM RESET.Nov 2, 1999 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA991231001Ram Air Turb · failed(CAN) DURING PRODUCTION FLT. ADG WOULD NOT DEPLOY IN FLIGHT. BLADES WERE FOUND STUCK BETWEEN THE FUSELAGE AND ADG DOOR. NOT PROPERLY STOWED.Nov 2, 1999 · Cndair CL6002B19 · AC Generation SystemSDR CA991210038Ecu · failed(CAN) DURING CRUISE , CAUTION MESSAGE FLIGHT SPOILER AND SPOILERONS. NR 2 SECU REPLACED.Nov 1, 1999 · Cndair CL6002B19 · Drag Control SystemSDR SWIA971588Power Lever · malfunctionedLEFT ENGINE POWER LEVER UNABLE TO RETARD TO IDLE OR CUT OFF. SHUT LEFT ENG DOWN USING LEFT FIRE PUSH BUTTON. LANDED AT SLC UNEVENTFUL. N1 STUCK AT 90 DEGREES. REMOVED AND REPLACED LEFT ENGINE GEAR BOX ASSY FOR POWER THROTTLE LEVER PER MM 76-11-17. PERFORMOct 31, 1999 · N411SW · Cndair CL6002B19 · Power LeverSDR CA991210037Pin · sheared(CAN) ON CLIMB-OUT, UNABLE TO PRESSURIZE AIRCRAFT. PASSENGER DOOR FLAPPER DOOR OPENED WITH SHEAR PINS ON VENT DOOR SHEARED.Oct 30, 1999 · Cndair CL6002B19 · Air Distribution SystemSDR SWIA971587Oil Sys · reqd serviceEN ROUTE TO HLN CLIMBING THROUGH 28,000 FT, RECEIVED AN APU LOW OIL PRESSURE LIGHT ON EICAS ONE. RETURNED TO SLC. SERVICED APU OIL TO CORRECT LEVEL. INSPECTED APU AND OBSERVED NO LEAKS OR OTHER ABNORMALITIES. OPS CHECKS GOOD AT THIS TIME.Oct 27, 1999 · N405SW · Cndair CL6002B19 · APU Oil SystemSDR CA991210029Indicator · malfunctioned(CAN) FLAP FAIL MESSAGE WHEN SELECTING FLAPS FROM 35 TO 45 DEG. SYSTEM RESET.Oct 26, 1999 · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR CA991103078Windshield · failed(CAN) ON APPROACH, CAPTAIN'S WINDSHIELD SHATTERED. NEW WINDSHIELD INSTALLED.Oct 24, 1999 · Cndair CL6002B19 · Flight Compartment Windows
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