GE CF34-3A

Service difficulty reports · 174

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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 = 'CF343A'
  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 CA981001009Selector Valve · failed(CAN) GEAR DISAGREE RED NOSE GEAR ICON ON TAKEOFF. AIRCRAFT RETURNED. NOSE GEAR AND DOOR SELECTOR VALVE AND PROXIMITY SENSOR ELEC UNIT REPLACED. . PART TC: 5,867.Sep 15, 1998 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA9860280Actuator · leakingVG ACTUATOR AT THE SEVEN O'CLOCK POSITION ON THE RIGHT ENGINE IS LEAKING FUEL. REPLACED ACTUATOR.Sep 15, 1998 · N915CA · Cndair CL6002B19 · Compressor Bleed ControlSDR CA981001008Sensor · out of adjust(CAN) NOSE GEAR DID NOT RETRACT ON UP SELECTION. GEAR DISAGREE WARNING, WITH NOSE WHEEL STEERING CAUTION LIGHT. OLEO EXTEND PROXIMITY SENSOR TARGET ADJUSTED. . PART TC: 5,865.Sep 14, 1998 · Cndair CL6002B19 · Landing Gear Position and WarningSDR CA980909014Control Unit · malfunctioned(CAN) NR 1 ENGINE SHUTDOWN IN FLIGHT DUE TO 14 STAGE DUCT AND AURAL MESSAGE. POST-FLIGHT INSPECTION FOUND NO DAMAGE TO THE LEFT HAND ENGINE PYLON DUCT. THE LEFT HAND BLEED CONTROLLER AND THE SENSING ELEMENT WERE REPLACED AND THE ENGINE WAS GROUND RUN SERVICEAug 22, 1998 · Cndair CL6002B19 · Compressor Bleed ControlSDR CA980909010Stop · cracked(CAN) PASSENGER DOOR NOISY AND LEAKING AIR DURING FLIGHT. AIRCRAFT RETURNED TO BASE. DOOR STRIKER FOUND CRACKED ON FRAME. DOOR FRAME WEB SPLICED PER ENGINEERING ORDER DRAWING NUMBER 600-31535. PART TC: 5,964.Aug 19, 1998 · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA980909017Bpsu · failed(CAN) FLAPS FAILED AT 33 DEGRESS WHEN SELECTED TO 45 DEGREES. REPLACED LEFT HAND BRAKE AND POSITION UNIT.. PART TC: 3,567.Aug 18, 1998 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA980827026Line · failed(CAN) NR 3 HYDRAULIC PRESSURE SYSTEM INDICATING LOW FOLLOWED BY LANDING GEAR DISAGREE. HYDRAULIC PRESSURE AT ZERO. NECESSARY TO DO ALTERNATE GEAR EXTENSION. LANDING NORMAL. HYDRAULIC PUMP 3A AND 3B PRESSURE LINE LEAKING.. PART TC: 5,683.Aug 5, 1998 · Cndair CL6002B19 · Hydraulic System, MainSDR CA980814015Lever · failed(CAN) EN ROUTE FLAPS FAIL CAUTION MESSAGE AFTER SELECTING FLAPS TO 8 DEGREES ON APPROACH. FLAPS INDICATED EXTENDED. REPLACED FLAP CONTROL POSITION LEVER.. PART TC: 5,470.Jul 29, 1998 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA980720023Circuit Breaker · tripped(CAN) ON APPROACH, FLAPS FAIL CAUTION ON WITH FLAPS SELECTED AT ZERO. OVERSPEED CLACKER ON TILL SPEED REDUCED BELOW 230. FLAP FAIL MESSAAGE STAYED ON. ISOLATION GUIDE CIRCUIT BREAKER RESET CARRIED OUT. FLAP FAIL MESSAGE CLEARED. FECU CHECKED OK.. PART TCJul 5, 1998 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR JBXA980040Fcp · inoperativeAUTOPILOT FAILED TO ENGAGE IN FLIGHT, HAD FCC INDICATIONS, APC FLASHES, NO FLIGHT DIRECTOR INDICATIONS ON CAPT SIDE AND 1/2 BANK CAME ON. LIGHT ON NAV LT SIDE, RT SIDE ON HEADING MODE, LT SIDE ON SPEED. REMOVED AND REPLACED FCP IAW CRJ MM CHP 22-11-07 OPERATJun 2, 1998 · N573ML · Cndair CL6002B19 · Autopilot SystemSDR COMA9860124Control Unit · malfunctionedLEFT ENGINE DOES NOT RESPOND TO POWER LEVER MOVEMENT, ABORTED TAKEOFF AND RETURNED TO THE GATE. DEFERRED THE ELECTRONIC SPEED CONTROL SYSTEM. AIRCRAFT RETURNED TO SERVICE.May 31, 1998 · N933CA · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR CA980608023Support · out of adjust(CAN) CABIN MAIN PASSENGER DOOR DIFFICULT TO OPEN. AFT UPPER FRAME, FIXED BEARING SUPPORT FOR ROTARY LATCH CAM ADJUSTED. PART TC: 6,698.May 23, 1998 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA980608022Valve · failed(CAN) GEAR DISAGREE WARNING AT RETRACTION AFTER TAKEOFF. REPLACED MAIN LANDING GEAR SELECTOR VALVE. PART TC: 6,940.May 21, 1998 · Cndair CL6002B19 · Landing Gear SelectorSDR CA980512016Fcu · failed(CAN) FLAP SYSTEM FAILED AFTER TAKEOFF. LANDED OK WITH ZERO DEGREE FLAPS. FLAP ELECTRONIC CONTROL UNIT RESET. PART TC: 6,973.Apr 23, 1998 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA980512018Control Box · inoperative(CAN) CREW REPORTED STEERING INOPERATIVE, SYSTEM RESET, UNSUCCESSFUL. AIRCRAFT LANDED WITHOUT NOSEWHEEL STEERING AND HAD TO BE TOWED TO GATE. ELECTORNIC CONTROL UNIT AND SERVO VALVE REPLACED. PART TC: 5,075.Apr 21, 1998 · Cndair CL6002B19 · Landing Gear Steering SystemSDR CA980417010Detector · malfunctioned(CAN) AURAL RED WARNING CARGO SMOKE AFTER TAKEOFF. ON APPROACH, WARNING REAPPEARED. NORMAL AND STANDBY CARGO BOTTLES DISCHARGED. SMOKE DETECTORS AND RELAY K11HL REPLACED.Apr 3, 1998 · Cndair CL6002B19 · Smoke DetectionSDR CA980309013Warning System · activated(CAN) WHILE SLOWING THROUGH 215 KNOTS, FLAPS SELECTED TO 8 DEGREES, FLAP FAIL CAUTION MESSAGE ON, FLAPS REMAINED AT 0 DEGREES. LANDING UNEVENTFUL. FLAP ECU SHOWS BOTH CHANNELS FAIL, RESET OK.Feb 24, 1998 · Cndair CL6002B19 · Central WarningSDR CA980305009Warning System · activated(CAN) TAKEOFF REJECTED AT APPROXIMATELY 90 KNOTS AS ELECTRONIC FLIGHT INSTRUMENT SYSTEM HEADING REFERRING FLAG UP. RESET ARINC COMMUNICATIONS AND REPORTING SYSTEM.Feb 16, 1998 · Cndair CL6002B19 · Integrated Flight SystemSDR CA980220010Transmitter · leaking(CAN) DURING CRUISE, LEFT ENGINE LOW OIL PRESSURE CAUTION AND AURAL WARNING, NECESSITATING ENGINE SHUT DOWN. FOUND OIL COMING OUT OF THE ENGINE DRAIN MAST, BUT NO OTHER LEAK. TRANSMITTER REPLACED.Feb 3, 1998 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA971125008Winglet · broke off(CAN) AIRCRAFT HIT BY LIGHTNING AND RIGHT WINGLET BROKE OFF. UPPER PORTION OF WINGLET REPLACED. NO OTHER DAMAGE OR FAULTS FOUND. PART TC: 3,858.Oct 31, 1997 · Cndair CL6002B19 · Wing, Control SurfacesSDR CA971125007Bpsu · misrigged(CAN) FLAPS LOCKED AT 5 DEGREES. FLAP FAIL MESSAGE INDICATIONS AND CREW ALERT. RIGHT HAND OUTBOARD FLAP RERIGGED. FLAP DRIVE SYSTEM FRICTION CHECK CARRIED OUT, NO FAULT. LEFT AND RIGHT BRAKE POSITION SENSING UNITS RERIGGED AND FLAP ELECTRONIC CONTROL UNIT POct 29, 1997 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA971110012Bpsu · failed(CAN) ON APPROACH FLAPS FAILED AT ZERO DEGREES. AIRCRAFT WENT AROUND AND LANDED OK. BRAKE POSITION SENSING UNIT REPLACED. THIS WAS A REPEAT SNAG.Oct 20, 1997 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA971110011Shaft · failed(CAN) FLAPS FAILED AT EIGHT DEGREES ON APPROACH. CIRCUIT BREAKER RESET NO GOOD. REPLACED RIGHT HAND INBOARD FLAP INBOARD DRIVE FLEX SHAFT AND JACKSCREW ASSEMBLY. PART TC: 4,473.Oct 19, 1997 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA971106006Loop · failed(CAN) LEFT ENGINE 14TH STAGE OVERHEAT WARNING DISPLAYED, THROTTLE RETARDED AND MESSAGE REMAINED, ENG SHUT DOWN AND AIRCRAFT RETURNED TO BLOCKS. 14TH STAGE LOOP SHORTED TO GROUND. LOOP REPLACED.Oct 16, 1997 · Cndair CL6002B19 · Overheat DetectionSDR CA971031013Adc · failed(CAN) REJECTED TAKEOFF AT 70 KNOTS IAS (INDICATED AIR SPEED) DUE TO ELECTRONIC FLIGHT INSTRUMENT SYSTEM (EFIS) COMPUTER MONITOR CAUTION ON AND INDICATED AIR SPEED AMBER SYMBOL ON CAPTAIN'S PRIMARY FLIGHT DISPLAY. REPLACED NR1 AIR DATA COMPUTER.Oct 14, 1997 · Cndair CL6002B19 · Air Data ComputerSDR CA971106005Brake Sensing · out of rig(CAN) ON APPROACH WHEN SELECTED 8 DEGREE FLAP, ENGINE INDICATION CREW ALERTING SYSTEM (EICAS) FLAPS FAIL CAUTION MESSAGE CAME ON. FLAPLESS LANDING CARRIED OUT. RIGGING OF THE BRAKE POSITION SENSING UNIT COMPLETED AS PER TASK 27-51-10-830-801. NO FAULTS FOUNDOct 9, 1997 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA971021020Power Drive Unit · failed(CAN) ON APPROACH, CREW SELECTED 8 DEGREE FLAP, FAIL MESSAGE CAME ON ENGINE INDICATING AND CREW ALERTING SYSTEM AT 0 DEGREE FLAPS. LANDED FLAPLESS. POWER DRIVE UNIT REPLACED.Oct 1, 1997 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA970922021Flap · failed(CAN) ON APPROACH PILOTS GOT A FLAP FAIL INDICATION WHEN THEY TRIED TO SELECT MORE THAN 8 DEGREES FLAPS. FLIGHT DID GO AROUND AND THEN LANDED FLAPLESS AND OK. FLAP ELECTRONIC CONTROL UNIT TEST CARRIED OUT AS PER FAULT MANUAL. SYSTEM RESET AND NO FAULT FOUND AFSep 3, 1997 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA970903017Tire Tread · separated(CAN) LEFT INBOARD TIRE TREAD SEPARATION ON TAKEOFF. LEFT INBOARD AND OUTBOARD WHEEL ASSEMBLY CHANGED.Aug 8, 1997 · Cndair CL6002B19 · TireSDR CA970722037Duct · adrift(CAN) AIRCRAFT RETURNED FROM FLIGHT BECAUSE THE LEFT HAND THRUST REVERSER UNLOCK LIGHT WAS ON. INSPECTION FOUND THE PNEUMATIC INTERMEDIATE PRESSURE DUCT ADRIFT. DUCT REINSTALLED. ALSO THE LEFT ENGINE THROTTLE LOCKOUT AND STOW SWITCHES WERE REPLACED AND THE DAMJul 5, 1997 · Cndair CL6002B19 · Engine Thrust ReverserSDR CA970710014Spcu · failed(CAN) FLIGHT SPOILER FAULT, A CONFIGURATION SPOILER AURAL AND EICAS MESSAGE ON TAKEOFF. CIRCUIT BREAKER RESET DID NOT FIX. RIGHT HAND FLIGHT SPOILER POWER CONTROL UNIT REPLACED.Jun 29, 1997 · Cndair CL6002B19 · Drag Control SystemSDR CA970529007Duct · cracked(CAN) AFTER TAKEOFF THE WING ANTI-ICE DUCT OVERHEAT MESSAGE CAME ON SHORTLY AFTER SELECTING WING ANTI-ICE ON. AIRCRAFT RETURNED TO BASE. LEFT HAND LEADING EDGE ANTI-ICE DUCT REPLACED.Apr 20, 1997 · Cndair CL6002B19 · Air Intake Anti/De-Ice SystemSDR CA970505017Actuator · failed(CAN) ECAM MESSAGES, STABILIZER TRIM AND MACH TRIM APPEARED ON TAKEOFF ROLL AT 110 KNOTS. TAKEOFF REJECTED. HORIZONTAL STABILIZER TRIM ACTUATOR FOUND AT FAULT.Apr 5, 1997 · Cndair CL6002B19 · Stabilizer ActuatorSDR CA970428004Selector Valve · failed(CAN) #3 HYDRAULIC SYSTEM LOST IN FLIGHT. DECLARED EMERGENCY. GEAR EXTENDED MANUALLY. ON LANDING NO NOSE WHEEL STEERING. NOSE GEAR SELECTOR VALVE CHANGED.Apr 4, 1997 · Cndair CL6002B19 · Landing Gear SelectorSDR CA970407022Seal · out of position(CAN) AFTER CLIMB LOUD SQUEALING COMING FROM MAIN PASSENGER DOOR. PASSENGER DOOR SEAL REPOSITIONED.Mar 31, 1997 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA970407018Control Unit · required reset(CAN) HORIZONTAL STABILIZER TRIM CHANNEL #2 FAULT. PILOT COULD NOT SELECT NOSE DOWN TRIM. RESET HORIZONTAL STABILIZER TRIM CONTROL UNIT BY EXERCISING THE TWO HORIZONTAL STABILIZER TRIM SWITCHES. BITE TEST SHOWED NO FAILURE.Mar 16, 1997 · Cndair CL6002B19 · Stabilizer Control SystemSDR CA970407019Pseu · failed(CAN) LANDING GEAR FAILED TO EXTEND. ALTERNATE GEAR EXTENSION CARRIED OUT. PROXIMITY SENSOR ELECTRONIC UNIT REPLACED.Mar 16, 1997 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR CA970318012Pseu · failed(CAN) LANDING GEAR WOULD NOT EXTEND. PSEU (PROXIMITY SENSOR ELECTRONIC UNIT) REPLACED.Feb 23, 1997 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR CA970318013Pseu · failed(CAN) LANDING GEAR FAILED TO EXTEND. MANUAL EXTENSION CARRIED OUT. GEAR FOUND ICED UP AND PSEU (PROXIMITY SENSOR ELECTRONIC UNIT) ALSO FOUND WITH INTERNAL FAULT.Feb 22, 1997 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR CA970204003Blades · bent(CAN) AFTER TAKEOFF AT APPROX 8,000 FEET AND 250 KNOTS, A VIBRATION WAS FELT. LEFT N1 ENGINE VIBRATION HIGHER THAN RIGHT ENGINE. VIBRATION CHANGED WITH LEFT THROTTLE MANIPULATOR. N1 VIBRATION IN AMBER RANGE ON FINAL APPROACH. FOUND LEFT HAND ENGINE THREE IJan 28, 1997 · Turbine Engine Compressor SectionSDR CA970204004Sensor · out of adjust(CAN) NOSE LANDING GEAR FAILED TO RETRACT ON TAKEOFF. NOSE GEAR PROXIMITY SENSOR ADJUSTED.Jan 26, 1997 · Cndair CL6002B19 · Landing Gear Position and WarningSDR CA970131004Switch · bent(CAN) GEAR DISAGREEMENT ON TAKEOFF. GEAR CYCLED TWICE, SAME INDICATION. NOSE GEAR SHOWED DOWN DOOR OPEN. GEAR EXTENDED, 3 GREEN LIGHTS. FOUND NOSE GEAR EXTEND PROXIMITY SWITCH BENT AWAY FROM TARGET.Jan 23, 1997 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR CA970129003Bracket · out of adjust(CAN) AFTER TAKEOFF UNABLE TO RETRACT NOSE GEAR. TARGET BRACKET REMOVED AND REPAIRED.Jan 12, 1997 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR CA970115006Idg · failed(CAN) AIRCRAFT REJECTED TAKEOFF DUE TO #2 GENERATOR TRIPPING OFF LINE. INTEGRATED DRIVE GENERATOR REPLACED.Jan 8, 1997 · Cndair CL6002B19 · AC Generator-AlternatorSDR CA970114025Oil Tank · over serviced(CAN) LEFT ENGINE OIL TEMP 176 DEGREES AND RISING FOLLOWED BY PRESSURE DROP OF 30 PSI. ENGINE SHUT DOWN. FOUND LEFT OIL TANK OVER SERVICED. OIL LEVEL ADJUSTED. OIL FILTER REMOVED AND INSPECTED, NO FAULT FOUND. ENGINE RUN CARRIED OUT AND LEAK CHECKED OK.Jan 1, 1997 · Engine Oil Storage (Airframe Furnished)SDR CA970114029Bracket · damaged(CAN) AFTER NOSE GEAR RETRACTION, NOSE GEAR REMAINED DOWN. GEAR DISAGREE AND NOSE DOOR OPEN MESSAGES APPEARED. FOUND NOSE LANDING GEAR CENTERING PROXIMITY SWITCH BRACKET DAMAGED. BRACKET REPLACED AND SWITCH ADJUSTED.Jan 1, 1997 · Cndair CL6002B19 · Landing Gear Position and WarningSDR CA970114020Sensor · out of adjust(CAN) NOSE GEAR WOULD NOT RETRACT. NOSE GEAR SENSOR FOUND OUT OF ADJUSTMENT. RIGGED AS PER MAINTENANCE MANUAL.Dec 26, 1996 · Cndair CL6002B19 · Landing Gear Position and WarningSDR CA970109018Bearing · grinding(CAN) EXCESSIVE VIBRATION FELT ON TAKEOFF. TAKEOFF REJECTED. SUSPECTED NOSE GEAR TIRE. FOUND LEFT HAND NOSE WHEEL BEARING GRINDING.Dec 17, 1996 · Cndair CL6002B19 · Wheel/Ski/FloatSDR CA970109019Selector Panel · failed(CAN) AIRCRAFT WOULD NOT DEPRESSURIZE. PRESSURIZATION SELECTOR PANEL REPLACED.Dec 9, 1996 · Cndair CL6002B19 · Cabin Pressure ControllerSDR CA970129014Fecu · failed(CAN) FLAPS FAILED AFTER TAKEOFF. CIRCUIT BREAKER RESET - NO GOOD. FLAPS STUCK AT 8 DEGREES. REPLACED FLAP ELECTRONIC CONTROL UNIT AND ALSO BRAKE POSITION SENSING UNIT.Nov 25, 1996 · Cndair CL6002B19 · Trailing Edge Flap Control System
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