GE CF34-3A1

Service difficulty reports · 1,372

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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 = '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 CA980706026Coalescer Bags · failed(CAN) AT TAKEOFF, AIR CONDITIONING SMOKE AND FOG IN COCKPIT AND CABIN. BOTH COALESCER BAGS REPLACED, RIGHT HAND PACK CLEANED. PART TC: 6,718.Jun 18, 1998 · Cndair CL6002B19 · Humidity Control SystemSDR SWIA971210Switch · out of adjustSERVICE DOOR CAUTION MESSAGE IN FLIGHT. RETURNED TO FIELD. FOUND DOOR CLOSED, MICROSWITCH SLIGHTLY OUT OF ADJUSTMENT AND DOOR SEAL FLANGE BENT. CONFIRM DOOR CLOSED, MEL 52-70-5.Jun 8, 1998 · N406SW · Cndair CL6002B19 · Door Warning SystemSDR SWIA971211Valve · failedNOSE GEAR DISAGREE AND WOULD NOT EXTEND. USED EMERGENCY GEAR EXTENSION. UPON LANDING, NO NOSE WHEEL STEERING. SYSTEM NR 3 HYDRAULIC PRESSURE 2400 PSI MAXIMUM. REPLACED NOSE LANDING GEAR SELECTOR VALVE IAW MM 32-31-00. CYCLED GEAR AND TAXIED AIRCRAFT. OPSJun 8, 1998 · N408SW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR CA980629015Flaps · failed(CAN) ON APPROACH, FLAPS FAILED AT 45 DEGREES. ON GROUND, FLAPS SET AT ZERO DEGREES WITH HYD SYSTEM ON, CIRCUIT BREAKER PULLED AND FAULT CLEARED. PART TC: 5,682.May 31, 1998 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA980629016Flap · failed(CAN) ON FINAL, FLAPS TO HALF-SPEED AND THEN FLAPS FAILED. AFTER FLAPS SET AND INDICATING 45 DEGREES, FOUND FLAP CONTROL ELECTRONIC UNIT POTENTIOMETERS POSITION 5-8 OUT OF RIG. PART TC: 15,682.May 31, 1998 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA980608020Ballast · failed(CAN) ELECTRICAL BURNING SMELL IN CABIN. BALLAST OF OVERHEAD LIGHTING AT ROW 5/6F FOUND BURNED. PART TC: 6,154.May 22, 1998 · Cndair CL6002B19 · Passenger Compartment LightingSDR COMA9860101Switch · malfunctionOIL PRESSURE WARNING DURING TAKEOFF. REPLACED OIL PRESSURE SWITCH.May 12, 1998 · N917CA · Cndair CL6002B19 · Engine Oil PressureSDR COMA9860102Vg Actuator · leakingFUEL DRIPPING FROM LEFT HAND ENGINE DRAIN. REPLACED THE INBOARD VG ACTUATOR.May 12, 1998 · N977CA · Cndair CL6002B19 · Fuel Controlling SystemSDR COMA9860095Engine · bird strikeBIRD STRIKE AFTER TAKEOFF. LEFT ENGINE VIB INDICATED 2.8. COMPLIED WITH BIRD STRIKE INSPECTION. REPLACED THE LEFT ENGINE DUE TO BIRD INJESTION.May 4, 1998 · N916CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA980608028Bpsu · failed(CAN) FLAPS FAILED ON LANDING. REPLACED BRAKE POSITION SENSOR UNIT AND FLAP ELECTRONIC CONTROL UNIT (P/N 860D10018ABC). PART TC: 4,662.May 3, 1998 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR MASA98098Eec · failedSTL/PHL - FLT 5764 - AFTER TAKEOFF, LEFT N1 GAUGE BEGAN FLUCTUATING MINUS 20 PERCENT, CLIMB THRUST AND ITT WENT TO MOMENTARY RED LINE. CREW DID NOT DECLARE AN EMERGENCY, BUT THE FIRE TRUCKS WERE DISPATCHED BY THE TOWER AS A PRECAUTIONARY MEASURE. THE AIRCRAFMay 2, 1998 · N37208 · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR CA980608037Prox Sensor · failed(CAN) ON APPROACH, THE FLAPS LOCKED AT 30 DEGREES. AIRCRAFT LANDED OK WITH FLAPS AT 30. REPLACED LEFT HAND BRAKE PROXIMITY SENSOR UNIT AND FLEX CABLE TO BRAKE PROXIMITY SENSOR UNIT. PART TC: 4,647.Apr 30, 1998 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA980608038Fecu · locked(CAN) FLAPS FAULT MESSAGE AND FLAPS LOCKED AT 30 DEGREES ON LANDING. FLAP ELECTRONIC CONTROL UNIT REPLACED. PART TC: 4,643.Apr 29, 1998 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA971164Smoke Detector · malfunctionedSMOKE CARGO WARNING CAME ON INFLIGHT. PERFORMED EMERGENCY PROCEDURE AND RETURNED TO SLC. BOTH FIRE BOTTLES WERE FIRED. REPLACED FAULTY SMOKE DETECTOR AND REPLACED CARGO BAY FIRE BOTTLE WITH SERVICEABLE UNIT .Apr 7, 1998 · N407SW · Cndair CL6002B19 · Smoke DetectionSDR CA980417009Lockwire · broken(CAN) UNABLE TO PRESSURIZE AFTER TAKEOFF. FLIGHT RETURNED. INSPECTION FOUND OUTBOARD COOLING VALVE LOCKWIRE BROKEN, RESECURED INBOARD AND OUTBOARD VALVE.Apr 5, 1998 · Cndair CL6002B19 · Cabin Cooling SystemSDR SWIA971157Structure · lightning strikeDURING DEPARTURE CLIMB, INCURRED A LIGHTNING STRIKE. RETURNED TO AIRPORT. COMPLIED WITH LIGHTING INSPECTION AT MAINTENANCE BASE.Apr 4, 1998 · N407SW · Cndair CL6002B19 · Aircraft StructuresSDR SWIA971161Pseu · malfunctionedAFTER DEPARTURE THE FOLLOWING CAUTION MESSAGES APPEARED: L AOA HEAT, L STATIC, L PITOT, PITOT BASE HEAT, FOLLOWED QRH ELECTED TO RETURN TO SLC AIRPORT. REMOVED AND REPLACED PSEU. OPS CHECKS GOOD IAW MM 33-00-00.Apr 3, 1998 · N408SW · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA971095Yaw Damper · failedYAW DAMPER 2 FAILS INFLIGHT, BUT WOULD RESET AFTER SEVERAL SECONDS. RETURNED TO SLC. REPLACED NR 2 FCC 4000 IAW MM 22. OPS CHECKS GOOD FOR CATII.Mar 9, 1998 · N408SW · Cndair CL6002B19 · Autopilot SystemSDR SWIA971097Clamp · failedRIGHT 14TH STAGE BLEED AIR DUCT LEAK MSG OUT OF 18000 FT ON CLIMBOUT. SYNOPTIC PAGE SHOWED RED INSIDE OF VALVE. FOLLOWED QRH CLOSING 14TH STAGE VALVE, MSG WENT OUT. RETURNED TO SLC. SECURED AND SEALED RIGHT 14TH STAGE SHUT OFF VALVE THERMAL BLANKET. SECURMar 9, 1998 · N406SW · Cndair CL6002B19 · Pneumatic Distribution SystemSDR SWIA971110Pitot Syst · noiseIMMEDIATELY AFTER TAKEOFF FROM SLC, LEFT AND RIGHT IAS MESSAGES APPEARED FOLLOWED BY STALL FAIL, MACH TRIM ALSO HIGH PITCH NOISE FOLLOWED BY VERY UNRELIABLE AIRSPEED INDICATION FROM CO-PILOTS AIRSPEED INDICATOR. AS AIRCRAFT SLOWED DOWN, LOUD NOISE WENT AWAY. Mar 9, 1998 · N405SW · Cndair CL6002B19 · Pitot/Static SystemSDR SWIA971111Oil Cap · leakingLEFT ENGINE SHUT DOWN DUE TO LOW OIL PRESSURE. DIVERTED TO CPR. ENGINE SHUT DOWN IAW QRH PROCEDURES. AFTER ARRIVAL IN CPR OIL LEVEL WAS CHECKED IN SHOW REFILL. ON SHUT DOWN THE PREVIOUS NIGHT IN CPR OIL LEVEL CHECKED NORMAL. RAN ENGINE FOUND LEFT ENGINE OMar 9, 1998 · N407SW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA980309010Flap · stuck(CAN) FLAPS FAIL CAUTION MESSAGE AND FLAPS STUCK AT 20 DEGREES, QUICK REFERENCE HANDBOOK PROCEDURE CARRIED OUT AND LANDED OUT WITH FLAPS AT 20. FLAPS RESET, NIL FOUND.Mar 2, 1998 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA971099Switch · dirtyDEPARTING SLC AND OUT OF ABOUT 1500 AGL, THE AMBER CARGO DOOR MESSAGE CAME ON. RETURNED TO SLC. CLEANED AND LUBED THE CARGO DOOR HANDLE MICROSWITCH, OPS CHECKS GOOD.Mar 1, 1998 · N403SW · Cndair CL6002B19 · Door Warning SystemSDR CA980305007Ram Air Turb · failed(CAN) THE AIR DRIVEN GENERATOR (ADG) MANUALLY DEPLOYED FOR TEST. AFTER 10 MINUTES OF NORMAL OPERATION THE RPM DROPPED AND ADG WENT OFF LINE.Feb 25, 1998 · Cndair CL6002B19 · AC Generation SystemSDR SWIA971091Fecu · failedFLAP FAIL MSESSAGE DURING FLAP RETRACTION ON CLIMB-OUT. RETURNED FOR LANDING. REMOVED FLAP PDU AND FECU AND REPLACED WITH SERVICEABLE UNITS IAW MM 27-52-01. ALL CHECKS GOOD.Feb 24, 1998 · N410SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA971086Adc · failedON APPROACH TO EUG PFD NR 1 LOST ALL AIR DATA (AIRSPEED, ALTITUDE, ATTITUDE, VSI) ALSO MACH TRIM. REMOVED AND REPLACED IDC 4000 CONVERTER. ALL SYSTEMS CHECKS NORMAL.Feb 22, 1998 · N410SW · Cndair CL6002B19 · Air Data ComputerSDR COMA9860042Tube · looseRIGHT ENGINE OIL PRESSURE DROPPED TO 25 PSI. ENGINE WAS SHUT-DOWN DURING FLIGHT. TIGHTENED LOOSE OIL LINE AT ENGINE LUBE PUMP. REPLENISHED 6 QUARTS OF OIL AND AIRCRAFT RETURNED TO SERVICE.Feb 10, 1998 · N976CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR SWIA971080Fail Message · illuminatedWHEN BRINGING FLAPS FROM 5 DEGREES TO 0 DEGREES, FLAP FAIL MESSAGE APPEARED. RETURNED TO AIRPORT. POWERED DOWN AIRCRAFT AND FAULT CLEARED. COULDN'T DUPLICATE PROBLEM. CLEARED FAULTS ON COMPUTER AND COMPUTER TESTED GOOD. RAN FLAPS UP AND DOWN NUMEROUS TIMEFeb 9, 1998 · N407SW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR SWIA971068Oil Syst · reqd serviceAT 57 MIN TO GO TO EUG, WE RECEIVED AND APU OIL TEMPERATURE MESSAGE. QRH CALLED FOR A DIVERSION TO NEAREST SUITABLE AIRPORT. SINCE EUG WAS IFR, THE SHUT DOWN OF APU WAS NOT AN OPTION. DIVERTED TO BOI. SERVICED APU OIL QUANTITY TO FULL, OPS CHECKS APU NORMAJan 7, 1998 · N408SW · Cndair CL6002B19 · APU Oil SystemSDR COMA9760253Engine · failedUNCOMMANDED ACCELERATION OF RIGHT ENGINE ALL ENGINE PARAMETERS WERE EXCEEDED. REPLACED ENGINE.Dec 22, 1997 · N959CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA971051Engine · malfunctionedABOUT 20 MINUTES OUT OF EUGENE, LEFT OIL PRESS LIGHT AND WARNING CAME ON. DID PRECAUTIONARY ENGINE SHUT DOWN PROCEDURES. DIVERTED TO PDX DUE TO WEATHER IN EUG. REPLACED ENGINE AS REQUIRED.Dec 21, 1997 · N411SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA971040Thermo Switch · failedBLEED AIR DUCT RED MESSAGE. RETURNED TO SLC. REMOVED AND REPLACED THERMO SWITCH AT 56 WK AND 58SF IAW MM 36-12-00, OPS CHECKS GOOD.Dec 7, 1997 · N408SW · Cndair CL6002B19 · Pneumatic Indicating SystemSDR CA971219032Cable · contaminated(CAN) LEFT HAND THROTTLE VERY STIFF, ALMOST FROZEN WHEN CLIMBING THROUGH 20,000 FEET. THIS IS A REPEAT SNAG. LEFT HAND THROTTLE CABLE AFT OF THROTTLE CONTROL BOX CHANGED. MOISTURE INGRESS RECTIFICTION SB A601R-76-013B COMPLETED.Nov 22, 1997 · Power LeverSDR CA971208007Cable · stiff(CAN) UNABLE TO MOVE LEFT HAND THROTTLE IN-FLIGHT. IT WAS VERY STIFF. THROTTLE CABLE, AFT OF THE THROTTLE CONTROL BOX, RE-ROUTED AND RIGGING CHECKED. PART TC: 3,734.Nov 21, 1997 · Power LeverSDR CA971219035Apu · leaking(CAN) LAVATORY SMOKE CAUTION MESSAGE AND MIST IN THE CABIN. AUXILIARY POWER UNIT (APU) SUSPECTED OF ALLOWING OIL INTO THE BLEED AIR SYSTEM. NO FAULTS FOUND.Nov 18, 1997 · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) SystemSDR CA971125015Detector · failed(CAN) ON APPROACH, A TOILET SMOKE MESSAGE ON ENGINE INDICATION AND CREW ALERT SYSTEM WITH LAVATORY SMOKE DETECTOR ALARM ON. SMOKE ODOR NOTICED, BUT NO SMOKE OR FIRE VISIBLE. EMERGENCY RESPONSE VEHICLES CALLED OUT. FLIGHT LANDED OK. NO EVIDENCE OF SMOKE OR Nov 16, 1997 · Cndair CL6002B19 · Smoke DetectionSDR SWIA971030Window · crackedCO-PILOTS SIDE WINDOW CRACKED ON DESCENT INTO PDX. REMOVED AND REPLACED RIGHT SIDE WINDOW IAW MM 56-12-01. OPS CHECKS GOOD.Nov 15, 1997 · N405SW · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA9760226Fuel Control · malfunctionedIN FLIGHT AT FLIGHT IDEL POWER SETTING THE N2 PERCENT IS SPLIT BETWEEN LEFT AND RIGHT ENGINES. REPLACED THE RIGHT HAND ENGINE FUEL CONTROL UNIT.Nov 11, 1997 · N964CA · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR CA971125010Tru · failed(CAN) ELECTRICAL SMELL IN FLIGHT DECK. CHANGED NR 4 TRANSFORMER RECTIFIER UNIT. PART TC: 4,439.Nov 8, 1997 · Cndair CL6002B19 · DC Rectifier/ConverterSDR CA971110013Power Drive Unit · failed(CAN) ON APPROACH, NIL INDICATION OF FLAPS. OVERSHOOT CARRIED OUT, AND FLAPLESS LANDING CARRIED OUT. FLAP POWER DRIVE UNIT REPLACED AND LEFT AND RIGHT FLEX DRIVE DISASSEMBLED, CLEANED AND LUBED. PART TOTAL CYCLES, 5,227.Oct 23, 1997 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA971008Hyd Line · failedAFTER DEPARTURE APPROXIMATELY 80 MILES OUT OF BIL, NR 2 HYDRAULIC LOW PRESSURE ANNUNCIATOR LIGHT CAME ON. HYDRAUYLIC PAGE SHOWED NR 2 RESERVOIR AT 0 QUANTITY. RETURNED AND LANDED AT BIL. REMOVED AND REPLACED HYDRAULIC PRESSURE LINE ON RIGHT ENGINE PYLON. SOct 20, 1997 · N408SW · Cndair CL6002B19 · Hydraulic System, MainSDR SWIA971002De-Ice Syst · malfunctionedRIGHT AOA HEAT AND TAT PROBE HEAT CAME ON DURING FLIGHT. RETURNED TO SLC. RECYCLED AIRCRAFT POWER. EICAS MESSAGE NOT DISPLAYED ON TAT PROBE HEAT. OPS CHECKS NORMAL AT THIS TIME.Oct 8, 1997 · N408SW · Cndair CL6002B19 · Pitot/Static Anti-Ice SystemSDR SWIA971001Fire Loop · malfunctionedLEFT JET PIPE LOOP A FAILED. MEL 26-11-2, INSPECTED LEFT EXHAUST NOZZLE FAIRING FOUND LOOSE HARDWARE. REMOVED AND INSTALLED SERVICEABLE HARDWARE AND SECURED IAW MM 78-11-01. OPS CHECKS OF ENGINE FIRE/OVERHEAT DETECTION GOOD AT THIS TIME IAW MM 26-11-00-710.Oct 7, 1997 · N410SW · Cndair CL6002B19 · Fire DetectionSDR COMA9760183Fan Blade · damagedBIRD STRIKE DURING TAKEOFF. RIGHT HAND ENGINE INGESTED BIRDS AND SUSTAINED DAMAGE TO FAN BLADES. REPLACED 10 BLADES ON RIGHT HAND ENGINE FAN.Sep 25, 1997 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR CA971016013Oil System · failed(CAN) IN CRUISE AT FL 290 TRIPLE CHIME ENG OIL ENGINE LIGHT ON INSTRUMENT CREW ALERTING SYSTEM, LIGHT ON ENG OIL PRESSURE LOW AT 30-34 PSI, AND FLUCTUATING ENG MONITORED, QUICK REFERENCE HANDBOOK DRILL CARRIED OUT, AND FLIGHT DIVERTED. AFTER LANDING ENGINE SHSep 24, 1997 · Turbine Engine Oil SystemSDR COMA9760173Actuator · leakingRT ENGINE INBD GUIDE VANE ACTUATOR IS LEAKING. REPLACED ACTUATOR.Sep 16, 1997 · N938CA · Cndair CL6002B19 · Compressor Bleed ControlSDR SWIA97926Smoke Detector · failedSMOKE CARGO WARNING DURING CLIMB. PROCEEDED VIA QRH. RETURNED TO FIELD. REMOVED AND REPLACED BOTH LEFT AND RIGHT SMOKE DETECTORS.Sep 9, 1997 · N406SW · Cndair CL6002B19 · Smoke DetectionSDR SWIA97927Smoke Detector · failed5 MINUTES AFTER TAKEOFF RECEIVED CARGO SMOKE MESSAGE. PERFORMED EMERGENCY PROCEDURE AND RETURNED TO AIRPORT. INDICATION WAS NOT STEADY MESSAGE WOULD GO ON AND OFF. INSPECTED CARGO BAY AREA, NO SIGN OF SMOKE OR FIRE. REMOVED AND REPLACED SMOKE DETECTORS IAWSep 9, 1997 · N413SW · Cndair CL6002B19 · Smoke DetectionSDR SWIA97928Fire Bottle · failed testCARGO BTL LO MESSAGE ON EICAS. CARGO SQUIBB 1 AND 2 FAIL TEST. THIS OCCURRED ON THE GROUND DURING PREFLIGHT INSPECTION. REMOVED AND REPLACED BOTH FIRE BOTTLES, OPS CHECKS GOOD.Sep 9, 1997 · N413SW · Cndair CL6002B19 · Fire Bottle, FixedSDR COMA9760168Fuel Control · failedRIGHT HAND ENGINE ACCELERATED TO 101 DEGREES WITH NO POWER LEVER COMMAND. REPLACED THE FUEL CONTROL UNIT.Sep 4, 1997 · N940CA · Cndair CL6002B19 · Fuel Control/Turbine Engines
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