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 SWIA971324Wire · failedAT 10,000 FEET ENCOUNTERED ICE. TURNED ON ANTI-ICE AND GOT ON ANTI-ICE DUCT MESSAGE. FOLLOWED QRH AND RETURNED TO SLC IN STANDBY POSITION. ANTI-ICE DUCT MSG WOULD CYCLE ON AND OFF. REPLACED NR S27WK LX WIRING LEADING EDGE THERMAL SWITCH.Nov 28, 1998 · N409SW · Cndair CL6002B19 · Ice/Rain Protection System WiringSDR SWIA971323Switch · failedWITH WING ANTI-ICE SELECTED ON ANTI-ICE DUCT MESSAGE CAME ON SHOWING LEFT WING RED, SAME IN BOTH NORMAL, STANDBY MODES. RETURNED TO SLC. REPLACED 3 THERMAL SWITCHES IN LEFT WING MID SECTION AND HEAT SHRINK INSTALLED ON LEFT WIRE ENDS. RAN AIRCRAFT AND TAXIENov 27, 1998 · N409SW · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR COMA9860361Fuel Control · malfunctionUNABLE TO REDUCE POWER BELOW 60 PERCENT N1. RIGHT HAND ENGINE (IFSD). REPLACED THE FUEL CONTROL.Nov 19, 1998 · N971CA · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR VTZA98350Seal · failedFLT 6700 - IAD-BNA - DURING TAKEOFF, EXPERIENCED A SMELL OF SMOKE IN THE CABIN ALONG WITH THE ACTIVATION OF THE LAVATORY SMOKE DETECTOR. A/C DECLARED AN EMERGENCY AND RETURNED TO IAD WHERE IT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE CONTROL WAS NOTIFIED Nov 18, 1998 · N629BR · Cndair CL6002B19 · Turbine Engine Reduction GearSDR VTZA98376Seal · failedIAD/BNA - FLT 6700 - DURING TAKEOFF ON 11-18-98 AT 0820 HOURS, EXPERIENCED A SMELL OF SMOKE IN THE CABIN ALONG WITH THE ACTIVATION OF THE LAVATORY SMOKE DETECTOR. AIRCRAFT DECLARED AN EMERGENCY AND RETURNED TO IAD WHERE IT LANDED WITH NO FURTHER INCIDENT. MANov 18, 1998 · N629BR · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR SWIA971315Indication · malfunctionedFLAP FAIL MESSAGE COMES ON IN CRUISE WHILE LEVEL AT 35,000. FLAPS REMAINED AT 0, NO CONTROL PROBLEMS. RETURNED TO SLC. RESET CB1-F4 AND CB2-F4, IAW A/D 98-20-01 PAR B. FLAP SYSTEM RESET TO NORMAL AND NO EVIDENCE OF TWISTING, SKEWING OR ABNORMAL DEFORMATIONNov 15, 1998 · N407SW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR CA981130011Power Pack · odor(CAN) OILY SMELL IN COCKPIT, FROM NR 1 POWER PACK, ABOVE 30 DEGREE CELSIUS OUTLET TEMPERATURE. NR 1 ENGINE REPLACED.Nov 13, 1998 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA9860339Connector · dirtyUNCOMMANDED ACCELERATION RIGHT HAND ENGINE DURING CRUISE FLIGHT. CLEANED WIRING CONNECTOR AT ENGINE ECU.Nov 6, 1998 · N991CA · Cndair CL6002B19 · Fuel Controlling SystemSDR CA981207017Nose Cone · damaged(CAN) ON APPROACH, AIRCRAFT ENCOUNTERED BIRD STRIKES. FIVE STRIKES ON AIRCRAFT WERE NOTED, BOTH LANDING LIGHT LENSES BROKEN, RIGHT ENGINE NOSE COWL DENTED, BOTH LANDING GEARS NO DAMAGE, AND RIGHT FLAP TRAILING EDGE DENT. NOSE COWL REPLACED, LIGHT LENSES REPLNov 5, 1998 · Cndair CL6002B19 · Aerodynamic FairingsSDR SWIA971301Stall Unit · failedDURING CLIMBOUT, THE EICAS CAUTION MESSAGE STALL FAIL DISPLAYED. CONSULTED MAINTENANCE CONTROL, ADVISED RETURN TO SLC AFTER COMPLETING QRH. REMOVED AND REPLACED STALL PROTECTION UNIT, OPS CHECK GOOD ON GROUND.Oct 30, 1998 · N411SW · Cndair CL6002B19 · Stall Warning SystemSDR COMA9860328Engine · flamed outLEFT ENGINE FLAMED OUT AND WOULD NOT RELIGHT. REPLACED LEFT ENGINE.Oct 25, 1998 · N967CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA9860324Engine · vibrationNR 1 ENGINE N1 FAN VIB PEAKED AT 4.0 DURING CRUISE IN ICING CONDITIONS. ALL INDICATIONS IS NORMAL RANGE UPON LANDING. INSPECTED FAN INLET AND TURBINE, NO DAMAGE WAS NOTED. OPERATED LEFT ENGINE AT VARIOUS POWER SETTINGS FOR 25 MINUTES. LEFT ENGINE N1 VIBS WEOct 21, 1998 · N969CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA971293Control Unit · malfunctionedTHE L 14TH DUCT WARNING MESSAGE ON IN FLIGHT. LEFT ENGINE PRECAUTIONARY SHUT DOWN ACCOMPLISHED. REMOVED AND REPLACED LEFT BLEED AIR CONTROL UNIT, IAW CRJ MM 36-21-10.Oct 20, 1998 · N403SW · Cndair CL6002B19 · Compressor Bleed ControlSDR CA981030010Fecu · malfunctioned(CAN) AFTER TAKEOFF, FLAP FAIL MESSAGE. AIRCRAFT RETURNED AND LANDED WITH ZERO FLAP POSITION. FOUND FLAP ELECTRONIC CONTROL UNIT POTENTIOMETER OUT OF LIMITS.. PART TC: 5,059.Oct 19, 1998 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA981030014Lighting Panel · shorted(CAN) IN TAXI, THE FIRST OFFICER'S LIGHTING PANEL SHORTED AND THERE WAS AN ELECTRICAL SMELL IN THE COCKPIT. WATER FOUND LEAKING THROUGH THE BOTTOM BOLTS ON THE RIGHT SIDE WINDOW. WATER FOUND BEHIND THE CIRCUIT BREAKER PANEL.. PART TC: 5,683.Oct 10, 1998 · Cndair CL6002B19 · Flight Compartment LightingSDR SWIA971282Tire · failedRIGHT MAIN TIRE BLEW RIGHT AT ROTATION ON TAKEOFF NR 3 MAIN. RETURNED TO SLC. REPLACED NR 3 AND NR 4 MAIN WHEEL ASSEMBLIES.Oct 8, 1998 · N411SW · Cndair CL6002B19 · TireSDR CA981019019Bpsu · malfunctioned(CAN) FLAPS FAIL ON EICAS ON INITIAL SELECTION. FLAPLESS LANDING CARRIED OUT. LEFT HAND BRAKE AND POSITION SENSOR UNIT FAILED.. PART TC: 4,991.Oct 4, 1998 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA971275Uplock Actuator · failedGEAR DISAGREE ON TAKEOFF RETRACTION. RETURNED TO SLC. REMOVED AND REPLACED UPLOCK ACTUATOR IAW MM 32-33-01 AND 32-33-05. OPS CHECK AND LEAK CHECK GOOD. REMOVED AND REPLACED NLG RETRACTION ACTUATOR.Oct 4, 1998 · N405SW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR CA981019020Fecu · failed(CAN) AFTER SELECTING FLAPS 8, A FLAP FAIL MESSAGE APPEARED AND FLAPS REMAINED AT ZERO. FLAPLESS LANDING CARRIED OUT. FLAP ELECTRONIC CONTROL UNIT RESET.. PART TC: 4,991.Oct 2, 1998 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA981019016Acm · malfunctioned(CAN) CREW REPORTED WHITE SMOKE COMING OUT OF LEFT SIDE OF AFT ACCESSORY COMPARTMENT. LEFT AIR CYCLE MACHINE USING OIL. REPLACED.. PART TC: 6,154.Sep 30, 1998 · Cndair CL6002B19 · Cabin Cooling SystemSDR CA981006023Uplock · out of adjust(CAN) DURING TAKEOFF, UNSCHEDULED LANDING CARRIED OUT BECAUSE OF GEAR DISAGREE MESSAGE. UPLOCK TARGET ON LEFT MAIN LANDING GEAR HAD TO BE ADJUSTED.Sep 24, 1998 · Cndair CL6002B19 · Landing Gear Position and WarningSDR COMA9860263Amplifier · malfunctionedRT ENGINE N1 AND ITT FLUCTUATIONS WHICH EXCEED LIMITS. COULD NOT DUPLICATE FLUCTUATIONS DURING GROUND RUN. REPLACED CONTROL AMPLIFIER FOR TROUBLESHOOTING.Sep 13, 1998 · N989CA · Cndair CL6002B19 · Engine RPM Indicating SystemSDR SWIA971256Light · illuminatedAFTER TAKEOFF, CARGO DOOR LIGHT ILLUMINATED. RETURNED TO GATE. OPERATIONAL CHECK OF CARGO DOOR CHECKS GOOD.Sep 10, 1998 · N403SW · Cndair CL6002B19 · Door Warning SystemSDR SWIA971254Seal · failedDURING CRUISE FLIGHT, LT ENGINE OIL PRESS MSG ILLUMINATED ON EICAS. ALSO, LT ENGINE OIL PRESS WAS FLUCTUATING BETWEEN 20 AND 40 PERCENT. PERFORMED ALL ITEMS ON ALL PERTINENT CHECK LIST AND SHUT DOWN ENGINE. PERFORMED SINGLE ENGINE LANDING. FOUND LT ENGINE Sep 9, 1998 · N407SW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR VTZA98285Valve · failedFLT 6700 - IAD-BNA - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO 10 TH STAGE BLEED AIR SHOWS PSI WITH VALVE CLOSE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND GROUND RAN AIRCRAFT AND COULD NOT DUPLICATE PROBLESep 7, 1998 · N621BR · Cndair CL6002B16 · Compressor Bleed ValveSDR SWIA971269Sensor · failedFLAPS FAILS MESSAGE AT LEVEL OFF EN ROUTE SLC/BOI. RETURNED TO SLC. REPLACED LEFT FLAP BRAKE POSITION SENSOR.Sep 4, 1998 · N403SW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR SWIA971268Retract Mech · malfunctionedWHILE DESCENDING INTO TUC FLAPS FAIL MESSAGE CAME ON. COMPLIED WITH CHECKLIST AND LANDED IN TUC WITH 0 FLAPS. POWERED DOWN AIRCRAFT FLAPS SYSTEM AND RESET SYSTEM. CHECKS NORMAL.Sep 3, 1998 · N403SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA9860251Compressor · dirtyDURING TAKEOFF, RT ENGINE ITT REACHED 900 DEGREES. TAKEOFF ABORTED. COMPRESSOR WASH ENGINE AND FOUND ITT WITHIN LIMITS.Sep 1, 1998 · N917CA · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR CA980909013Apu · malfunctioned(CAN) ON DEPARTURE CLIMB OUT, WHEN AIR CONDITIONING PACKS TURNED ON, SMOKE PRESENT IN CABIN AND FLIGHT DECK. PACKS TURNED OFF AND SMOKE DISSIPATED. AUXILIARY POWER UNIT CHANGED. PACKS OPERATED NORMALLY.Aug 21, 1998 · Cndair CL6002B19 · APU Core EngineSDR CA980909018Latch Spring · contaminated(CAN) PASSENGER DOOR MESSAGE IN CLIMB, NO DELTA PRESSURE IN CABIN. OUT HANDLE STOW KNOB MESSAGE CHANGED TO PASSENGER DOOR STOW THEN BACK TO HANDLE OUT. LATCH SPRINGS AND PIN CLEANED.. PART TC: 4,823.Aug 18, 1998 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA980928030Engine · malfunctioned(CAN) SHORTLY AFTER TAKEOFF, THE NR 1 ENGINE LOW OIL PRESSURE WARNING MESSAGE CAME ON. ALL ENGINE PARAMETERS WERE NORMAL. PILOT ELECTED TO DO A PRECAUTIONARY ENGINE SHUT DOWN. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE. PART TC: 1,790.Aug 17, 1998 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA980827021Seal · dirty(CAN) IN CRUISE, RIGHT EMERGENCY DOOR MESSAGE ON EICAS. QUICK REF. CARRIED OUT. RIGHT OVERWING EXIT DOOR REMOVED AND DOOR SEAL AND SURFACE MATES CLEANED.. PART TC: 4,768.Aug 12, 1998 · Cndair CL6002B19 · Emergency ExitsSDR CA980827025Computer · failed(CAN) AILERON MISTRIM DURING DESCENT. AMBER POSTED ON BOTH PRIMARY FLIGHT DISPLAYS. AUTOPILOT TRANSFERRED TO COPILOT SIDE, AIRCRAFT ROLLED VIOLENTLY TO RIGHT. A/P DISCONNECTED. CONTROL REGAINED MANUALLY. A/P RE-ENGAGED ON PILOT'S SIDE. REPLACED NR 1 FLIGAug 9, 1998 · Cndair CL6002B19 · Flight ControllerSDR COMA9860218Wire · chafedLEFT ENGINE THRUST REVERSER UNLOCKED MESSAGE AFTER TAKEOFF. REPAIRED CHAFED WIRE AT CONNECTOR P28EZ.Aug 9, 1998 · N935CA · Cndair CL6002B19 · Engine Exhaust System WiringSDR SWIA971242Sill · corrodedCORROSION AROUND SERVICE DOOR SILL AREA ON ANGLES. REMOVED AND REPLACED SERVICE DOOR SILL AREA ANGLE IAW CJR SRM 51-00-00.Aug 9, 1998 · N412SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA971243Sill · corrodedCORROSION AROUND PASSENGER DOOR SILL AREA ON ANGLES. REMOVED AND REPLACED PASSENGER DOOR SILL AREA ANGLE IAW EMB SRM 51-00-00.Aug 9, 1998 · N412SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA980909012Te Flap · failed(CAN) FLAPS FAIL MESSAGE ON FLAP SELECTION FROM 30 TO 45 DEGREES. RESET CIRCUIT BREAKERS ON BOTH CHANNELS, TWIST CHECK CARRIED OUT AND SYSTEM CHECKED SERVICEABLE.Aug 8, 1998 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA9860217Connector · failedDURING CRUISE FLIGHT, THE LEFT COWL ANTI-ICE CAUTION MESSAGE CAME ON. THE BLEED AIR CONNECTION AT THE THRUST REVERSER MOTOR CAME OFF CAUSING EXTENSIVE HEAT DAMAGE TO ENGINE AND COWLING. REPLACED ENGINE AND COWLING.Aug 8, 1998 · N935CA · Cndair CL6002B19 · Air Intake Anti/De-Ice SystemSDR SWIA971244Strap · corrodedTHERE IS CORROSION IN A NUMBER OF PLACES IN BUTT STRAPS RBL 9, RBL 27, LBL 27 FROM STATION 280, STATION 400. REMOVED AND REPLACED BUTT STRAP, REMOVED CORROSION ON OTHER AREAS, IAW SRM 51-10-00.Aug 4, 1998 · N408SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA980909015Fecu · failed(CAN) ON FLAP SELECTION FROM 8 DEGREES TO ZERO, FLAP FAIL MESSAGE ON EICAS. QUICK REF. CARRIED OUT. LEFT HAND FLAP ELECTRONIC CONTROL UNIT FAILED. LEFT HAND BPSU WIRING CHANGED AND FECU ADJUSTED.. PART TC: 4,726.Aug 3, 1998 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA971245Floorbeam · corrodedAREA AROUND NUT PLATE LBL 27, FS 330 INBOARD SIDE HAS CORROSION OUT OF LIMITS. REPLACED AREA AROUND NUT PLATE IAW MM.Aug 2, 1998 · N409SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA971246Floorbeam · corrodedAREA NEXT TO INSERTS CENTER OF LBL 9, FS 335 AND 345 HAS LIGHT CORROSION. CUT OUT DAMAGED AREA, FABRICATED A L-ANGLE AND FILLERS AND INSTALLED ON LBL 9, FS 335 AND 345 IAW MM .Aug 2, 1998 · N409SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR COMA9860197Engine · failedRIGHT HAND ENGINE OIL PRESSURE GRADUALLY DECREASED WITH FLUCTUATIONS DURING FLIGHT, AT TIME OF OIL PRESSURE WARNING, ENGINE WAS SHUT DOWN. REPLACED ENGINE.Jul 24, 1998 · N951CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA9860198Pad · failedA WEAR PAD P/N 5010880-1 OF THE NUMBER ONE STATIONARY DISK SEPARATED FROM THE BRAKE. THE ANTI-ROTATION TAB OF THE PAD MAY HAVE FAILED. INSPECTION OF THE REST OF THE BRAKE FOUND NO OTHER DEFECTS. REMAINING PIECES OF THE WEAR PAD WERE SENT TO AIRCRAFT BRAKINGJul 21, 1998 · N936CA · Cndair CL6002B19 · BrakeSDR CA980814017Shaft · sheared(CAN) ON APPROACH AFTER SELECTING FLAPS 45 DEGREES, A FLAP FAIL AMBER CAUTION MESSAGE AND FLAPS STOPPED AT 39 DEGREES. QUICK REF. PROCEDURE CARRIED OUT. RIGHT HAND OUTBOARD FLAP CENTER SHAFT HAD SHEARED.. PART TC: 6,520.Jul 17, 1998 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA9860177Compressor Blade · missingRIGHT HAND N2 VIBRATION WARNING. PERFORMED BORESCOPE INSPECTION AND FOUND STAGE 8 COMPRESSOR MISSING ONE BLADE. REPLACED ENGINE.Jul 14, 1998 · N924CA · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR SWIA971218Radome · bird strikeHIT A BIRD ON CLIMBOUT AND RETURNED FOR LANDING. PERFORMED BIRD STRIKE INSPECTION, FOUND NOSE RADOME RIGHT LOWER CORNER DAMAGED. REPLACED RADOME.Jul 9, 1998 · N409SW · Cndair CL6002B19 · Aerodynamic FairingsSDR SWIA971223Tire · failedHEARD LOUD BANG AT ROTATION ON TAKEOFF ON RUNWAY 34L. HAD TOWER CHECK FOR DEBRIS ON RUNWAY AND TOWER CONFIRMED TIRE DEBRIS ON RUNWAY SURFACE. RETURNED FOR LANDING WHICH WAS UNEVENTFUL. POST FLIGHT SHOWED A THROWN CAP ON RIGHT NOSE GEAR. INSPECTED AIRCRAFT Jul 8, 1998 · N403SW · Cndair CL6002B19 · TireSDR COMA9860167Fcu · failedTHE NR 2 ENGINE HAD ROLL BACK DURING LANDING APPROACH. REPLACED THE FUEL CONTROL UNIT.Jul 7, 1998 · N989CA · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR SWIA971226Computer · failedSTALL FAIL MESSAGE CAME ON DURING INITIAL CLIMB OUT. RETURNED TO SLC. REPLACED STALL WARNING COMPUTOR. OPS CHECKS GOOD.Jul 6, 1998 · N408SW · Cndair CL6002B19 · Stall Warning System
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