GE CF34-3B1

Service difficulty reports · 5,402

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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 = 'CF343B1'
  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 JBXA000236Engine · malfunctionedFLIGHT 863 RDU/EWR UPON POWER APPLICATION RIGHT ENGINE DID NOT SPOOL UP. N1, N2 AND FUEL FLOW WERE AT IDLE LEVELS TWO SECONDS AFTER INITIAL POWER APPLICATION. TAKEOFF WAS ABORTED. PERFORMED ACCEL-DECEL CHECK OF RIGHT HAND ENGINE IAW AMM 71-00-00. ALL PERIMJan 14, 2001 · N578ML · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA010213025Windshield · cracked(CAN) CREW RPORTED THAT PASSING FLT 160 AT A DIFFERENTIAL CABIN PRESSURE 6,4, R/H WINDSHIELD CRACKED. NO INFO IF EMERGENCY WAS DECLARED.AIRCRAFT RETURNED INTO SERVICE AFTER WINDSHIELD REPLACEMENT.Jan 13, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA010205006Windshield · cracked(CAN) THE CREW REPORTED THAT THE LT WINDSHIELD CORE PLY CRACKED DURING FLIGHT.THE MAINTENANCE REPLACED THE WINDSHIELD.Jan 11, 2001 · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR SWIA972260Warning System · activatedSTALL FAIL MESSAGE ON TAKEOFF ROLL. ABORTED TAKEOFF. PERFORMED STALL WARNING TEST AND CHECK STALL VANES. OPS CHECK GOOD. COULD NOT DUPLICATE.Jan 9, 2001 · N903SW · Cndair CL6002B19 · Stall Warning SystemSDR CA010202022Gearbox · failed(CAN) NR 2 ENGINE VIBRATION FLUCTUATION INDICATED .4 TO .7 MILS APPROXIMITELY 3 TO 5 MIN. LATER, NR 2 ENGINE SHUT DOWN UNCOMMANDED. PERFORMED QRH PROCEDURE & DIVERTED INTO NEXT AIRPORT (ISO), THE FLIGHT CREW DECLARED EMERGENCY (UNEVENTFUL).FOUND METAL IN CHIP Jan 7, 2001 · Cndair CL6002B19 · Turbine Engine Reduction GearSDR AU010005Handle · malfunctioned(AUS) CARGO DOOR MASTER CAUTION LIGHT ILLUMINATED. INVESTIGATION FOUNDTHE CARGO DOOR HANDLE PARTIALLY RELEASED. A FUNCTIONAL CHECK OF THE DOOR LATCHING SYSTEM COULD FIND NO FAULT. SUSPECT THAT THEHANDLE WAS INCORRECTLY STOWED.Jan 7, 2001 · Cndair CL6002B19 · Cargo/Baggage DoorsSDR CA010202013Fire Detector · failed(CAN) DURING DESCENT INTO MEMPHIS, THE CREW ON AIRCRAFT 7416 SHUT DOWN ENGINE NR 1 PER THE EMERGENCY PROCEDURES DUE TO THE POSTING OF AN INTERMITTENT LT ENGINE FIRE MESSAGE ON THE EICAS. DURING TROUBLESHOOTING THE MECHANICS FOUND THE FIRE DETECTION UNIT UNDER Jan 6, 2001 · Cndair CL6002B19 · Fire DetectionSDR SWIA972242Potentiometer · out of adjON TAXI OUT FLAPS WERE SET TO 20 DEGREES AND EICAS INDICATION IS 18 DEGREES. ADJUSTED LEFT AND RIGHT FLAP INDICATION POTENTIOMETERS PER CRJ MM 27-55-01. RAN FLAPS EICAS INDICATIONS NORMAL. FECU INDICATION OPS CHECKS GOOD.Jan 3, 2001 · N423SW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR CA010202008Windshield · failed(CAN) THE CREW REPORTED THAT THE CAPTS FRONT WINDSHIELD SHATTERED IN CRUISE. THE LANDING WAS UNEVENTFUL.THE MAINTENANCE REPLACED THE WINDSHIELD.Jan 3, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA010205008Windshield · cracked(CAN) THE CREW REPORTED THAT THE RT WINDSHIELD CARACKED IN FLIGHT. THE MAINTENANCE REPLACED THE RT WINDSHIELD.Jan 1, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA010202006A/C Pack · overheated(CAN) AFTER TAKEOFF, THE CREW REPORTED SMOKE IN THE COCKPIT AND DECLARED AN EMERGENCY. THE LANDING WAS UNEVENTFUL.THE MAINTENANCE CREW REPORTED THAT ONE OR BOTH PACKS OVERHEATED AND CAUSED THE SMOKE. THE MAINTENANCE INSPECTED THE ECS SYSTEM AND NOTED NO DEFECTDec 24, 2000 · Cndair CL6002B19 · Cabin Cooling SystemSDR SWIA972219Warning Light · illuminatedRIGHT EMERGENCY DOOR CAUTION ILLUMINATED IN FLIGHT. CYCLED RIGHT EMERGENCY EXIT. OPS CHECK GOOD.Dec 21, 2000 · N423SW · Cndair CL6002B19 · Door Warning SystemSDR SWIA972249Aileron · malfunctionedAILERON, RUDDER TRIM SHOW FULL SCALE DEFLECTIONS AND NO INDICATION OF FLAP EXTENSION SWAPPED BOTH FCC CARDS NO HELP PUT CARDS BACK IN ORIGINAL POSITION AC IS NOW DOWN GRADED TO CAT I DUE TO NON QUALIFIED MECHANIC WORKDec 20, 2000 · N423SW · Cndair CL6002B19 · Aileron Control SystemSDR MASA00172Engine · overservicedFLT 6915 - EWR-CMH - DECLARED AN EMERGENCY AND RETURNED TO EWR DUE TO THE OIL TEMP RISING UP TO 173-174 WITH THE OIL PRESSURE DROPPING TO 48 PSI. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE IAW THE FIM DISCOVERED THAT THE ENGINE HAD BEEN OVER SERVICED.Dec 17, 2000 · N27191 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR SWIA972175Stall Warning · malfunctionedON TAKEOFF ROLL, STALL FAIL CAUTION MESSAGE ON EICAS. ABORTED TAKEOFF. REMOVED AND REPLACED STALL PROTECTION UNIT. OPS CHECKS GOOD IAW MM 27-35-01. P/N ON: 3995100208, S/N ON: 249, S/N OFF: 608.Dec 15, 2000 · N418SW · Cndair CL6002B19 · Stall Warning SystemSDR SWIA972172Actuator · failedSTAB TRIM CH 1 INOP STATUS MESSAGE DURING FLIGHT. WOULD NOT ENGAGE. REMOVED AND REPLACED STAB TRIM ACTUATOR AND CONTROL BOX IAW CANADAIR RJ MM 27-41-00. OPS CHECK GOOD.Dec 13, 2000 · N905SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR CA001229023Stator · failed(CAN) CAPTAIN REPORTED A LEFT ENGINE N2 FLUCTUATION AT CRUISE BETWEEN 88.2 AND 97.6.FOLLOWING SEVERAL PROCEDURES AND PART CHANGES (ADJUSTMENT OF IDLE SPEED, VG FEEDBACK, REPLACEMENT OF FCU & OF T2C SENSOR), THE AIRCRAFT WAS FERRY TO THE MAIN BASE. THE MAINTENADec 11, 2000 · Cndair CL6002B19 · Alternator-Generator DriveSDR CA010205028Pump · leaking(CAN) FUEL FOUND IN BOTH STANDBY AND APU FUEL BOOST PUMPS UNDER PLUG (REF CMM 28-20-78 PAGE 1010, ITEM 100).FUEL WAS FOUND ON BOTH SIDE OF PLUG AND ALSO FOUND IN CONDUIT WHERE WIRING FOR PUMP RUNS TO FRONT SPAR. LOCATION OF LEAK UNKNOWN AT THIS TIME.SEE ATTACHDec 11, 2000 · Cndair CL604 · Fuel Boost PumpSDR SWIA972159Bpsu · failedFLAP FAIL MESSAGE ON APPROACH AT 42 DEGREES. REMOVED AND REPLACED RIGHT BPSU IAW MM 27-51-00. PN 855D100-9 SN ON 301B SN OFF 1150A. REMOVED AND REPLACED OUTBOARD FLAP INBOARD ACTUATOR IAW MM 27-53-05 PN 853D106-17 SN ON 332 SNOFF 0964. OPS CHECKS GOOD. COMDec 8, 2000 · N417SW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR CA001229014O-Ring · leaking(CAN) FUEL WAS FOUND POOLED IN LEFT HAND ENGINE COWLING DURING POST FLIGHT INSPECTION. ENGINE RUN CARRIED OUT FOR LEAK CHECK PURPOSES AND FOUND FUEL STREAMING FROM MFC. MFC REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2001-01-03TC: MANUFACTURE OF AIRCRAFT AND EDec 7, 2000 · Cndair CL604 · Fuel Control/Turbine EnginesSDR CA010102009O-Ring · leaking(CAN) THE MAINTENANCE WAS DOING AN ENGINE RUN WHEN THEY NOTICED A FUEL LEAK THROUGH THE LT CORE COWL DRAIN.THE MAINTENANCE OPENED THE LOWER CORE COWL AND THEY FOUND THAT THE FUEL WAS LEAKING THROUGH THE LT MFC THROTTLE SHAFT BODY WITH THE STANDBY FUEL PUMPS ONDec 7, 2000 · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR CA010102007Gearbox · failed(CAN) THE CREW REPORTED THAT DURING CLIMB, THE RT ENGINE WAS LOST. THE CREW DECLARED EMERGENCY PROCEDURES, THEY LANDED WITHOUT FURTHER INCIDENT. THE MAINTENANCE REPORTED GEARBOX FAILURE. RT ENGINE WAS REPLACED.Dec 6, 2000 · Cndair CL6002B19 · Turbine Engine Reduction GearSDR CA010102010Harness · arced(CAN) AFTER TAKEOFF, THE CREW REPORTED HIGH RT N1 VIBRATION, THE FLIGHT CREW DECIDED TO RETURN TO THE BASE.THE MAINTENANCE FOUND THE RED ENGINE HARNESS, THE IDG CABLES, THE THERMOCOUPLE HARNESS AND THE RT LOWER CORE COWL WITH BURNT MARKS. THEY FOUND THE IDG CADec 4, 2000 · Cndair CL6002B19 · Ignition Harness (Distribution)SDR SWIA972140Computer · malfunctionedON TAKEOFF ROLL, RECEIVED A STALL FAIL CAUTION MESSAGE AND CONFIG SPOILERS WARNING. EXACTLY SAME THING OCCURRED ON SECOND TAKEOFF ATTEMPT. RESET SECUS AND POWERED DOWN AIRCRAFT. OPS CHECKED SPOILERS, ALL SYSTEMS CHECK GOOD.AFTER SECOND ATTEMPT, CLEARED MEMONov 30, 2000 · N903SW · Cndair CL6002B19 · Stall Warning SystemSDR SWIA972121Actuator · failedON AFTER LANDING CHECK, RUDDER TRIM FAILED TO OPERATE. REPLACED RUDDER TRIM ACTUATOR PER MM 27-22-01 P/N AL00101, S/N ON 9862, S/N OFF 4411, OPS CHECK GOOD.Nov 19, 2000 · N418SW · Cndair CL6002B19 · Rudder Tab Control SystemSDR SWIA972129Windshield · crackedFIRST OFFICERS FRONT WINDSHIELD HAS SEVERAL LARGE CRACKS. REMOVED AND REPLACED RIGHT FRONT WINDSHIELD IAW 56-11-01, P/N 601R33033-2, S/N ON 97154H7754, S/N OFF 00224H5235.Nov 18, 2000 · N905SW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA972108Controller · failedON CLIMBOUT, RIGHT AOA HEAT CAME ON. REMOVED AND REPLACED RIGHT AIR DATA SENSOR CONTROLLER IAW CRJ MM 30-31-15. OPS CHECKS GOOD. P/N ON: 785-806-2, S/N ON: 1377, S/N OFF: 218.Nov 13, 2000 · N417SW · Cndair CL6002B19 · Air Data ComputerSDR SWIA972085Computer · failedSTALL FAIL CAUTION MESSAGE CAME ON AFTER ROTATION. RETURNED TO FIELD. INTERROGATED FAULT HISTORY AND LRU DIAGNOSTICS. NO FAULTS LOGGED. REPLACED STALL COMPUTER IAW MM 27-35-01. STALL TEST CHECKS GOOD, FAIL MESSAGE CLEARED. P/N: 39-951-002-08, S/N ON: 1Nov 5, 2000 · N417SW · Cndair CL6002B19 · Stall Warning SystemSDR CA001110031Amplifier · failed(CAN) FLT 4627, AFTER SETTING CLIMB THRUST THE LT ENGINE ACCELERATED TO OVER 101 PERCENT. THE POWER LEVER WAS RETARDED AND THE ENGINE (N1) THEN LATER DROPPED BY 6 PERCENT UNCOMMANDED. REMOVE AND REPLACE NR 1 ENGINE N1 CONTROL AMPLIFIER. PERFORMED FUNCTIONAL CNov 2, 2000 · Cndair CL6002B19 · Engine ControlsSDR CA001129036Pin · failed(CAN) DURING DISASSEMBLY OF THROTTLE QUADRANT TO COMPLY WITH BOMBARDIER SB 604-76-001/RATHER FIGEAL SB FE210-76-01 IT WAS FOUND THAT PIN 160 HAD MIGRATED OUT OF LATCH ASSEMBLY. THIS PIN IS A PRESS FIT AND WE FOUND IT COULD BE REMOVED BY HAND. IF THIS PIN IS RENov 2, 2000 · Cndair CL604 · Power LeverSDR JBXA000212Housing · damagedNR 2 ENGINE N2 GAUGE FLUCTUATES. UPON FURTHER INSPECTION FOUND N2 GENERATOR SHAFT NICKED AND FOUND N2 GENERATOR HOUSING AND STATOR DAMAGED. REMOVED AND REPLACED NR 2 ENGINE WITH SERVICABLE PART IAW CRJ AMM 71-00-00 AND ENGINE CHANGE PACKAGE. PERFORMED ENGINOct 24, 2000 · N572ML · Cndair CL6002B19 · AC Generation SystemSDR CA001024029Torque Box · damaged(CAN) DURING FLIGHT, AN UNUSUAL RUMBLING NOISE AND SOME VIBRATION WAS OBSERVED. ALL ENGINE PARAMETERS WERE NORMAL. CREW ELECTED TO DECLARE AN EMERGENCY LANDING AS A PRECAUTIONARY MEASURE. FOUND THE LT THRUST REVERSERS TORQUE BOX DAMAGED, ALONG WITH THE UPPER SOct 6, 2000 · Cndair CL6002B19 · Engine Thrust ReverserSDR SWIA972003Controller · failedSTAB TRIM CHANNEL 2 WILL NOT ENGAGE. FAILED TRIM TEST ON GROUND DURING PREFLIGHT. ON TWO STAB TRIM TESTS CHANNEL 2 FAILURE INDICATED ON HSTCU TEST PANEL. REPLACED HSTCU IAW CL600 MM 27-42-05. STAB CHANNELS AND MACH TRIM TEST GOOD ON GROUND. AIRCRAFT OK FOSep 30, 2000 · N417SW · Cndair CL6002B19 · Stabilizer Control SystemSDR CA001024013Carbon Seal · failed(CAN) DURING CLIMB FLIGHT CREW NOTICED LEFT ENGINE OIL PRESSURE FLUCTUATION. AIRCRAFT RETURNED TO DEPARTING AIRPORT. LT ENGINE CARBON SEAL REPLACED. AIRCRAFT BACK IN SERVICE.Sep 29, 2000 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA971998Transducer · failedJUST AFTER LIFT OFF ''''''''STALL FAIL'''''''' MESSAGE. RETURNED TO SLC. REPLACED STALL COMPUTER. FAILED TEST. (P/N 39-951-002-08) ON, (S/N 521) ON, (S/N 589) OFF. REMOVED AND REPLACED NUMBER ONE MACH TRANSDUCER IAW MM 27-35-25. OPS CHECKS GOOD AT THIS TSep 27, 2000 · N417SW · Cndair CL6002B19 · Speed-Attitude Correction SystemSDR CA001002010Probe · failed(CAN) ON CLIMBOUT, ENG OIL WENT RED ON LEFT ENGINE (>165 DEG C). QRH UTILIZED AND TEMP BROUGHT BACK INTO GREEN AT A VERY REDUCED POWER SETTING. ITT NORMAL THROUGHOUT EVOLUTION. PRESSURE WAS LOW BUT IN NORMAL RANGE. MAINTENANCE FOUND OIL REPLENISHMENT SYSTEM COSep 8, 2000 · Cndair CL6002B19 · Engine Oil QuantitySDR CA001002011Packing · cut(CAN) ABORTED TAKEOFF DUE TO THE IDG 2 CAUTION MESSAGE. MAINTENANCE FOUND AN OIL LEAK FROM THE IDG NR 2 OUT PORT CAUSED BY A CUT O-RING . O-RING REPLACED AND A/C RETURNED TO SERVICE.Sep 8, 2000 · Cndair CL6002B19 · Accessory GearboxesSDR AU000752Indicator · faulty(AUS) RT PYLON BLEED AIR LEAK DETECTOR LOOP HAD LOW RESISTANCE. FOUND DURING INSPECTION IAW SBA601R-36-104.Aug 21, 2000 · Cndair CL6002B19 · Bleed Air Indicating SystemSDR JBXA000198Engine · malfunctionedLEFT ENGINE UNABLE TO ACHIEVE TAKEOFF POWER, MAX OF 76.9 PERCENT N1 WITH THRUST LEVER AT STOP. ALL OTHER ENGINE PARAMETERS WERE NORMAL. TAKEOFF ABORTED AT +- 60 KNOTS WITH MIN BRAKING.POWERED DOWN NR 1 ECU. INSPECTED CANNON PLUGS AND RESEATED. PERFORMED EAug 17, 2000 · N576ML · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA000830019Engine · malfunctioned(CAN) AFTER TAKEOFF, WITH TAKEOFF POWER APPLIED, THE CREW HEARD A LOUD BANG. AFTER THE NOISE, THE LT ENGINE ITT & N2 WENT INTO THE RED. PILOT SET ENGINE TO IDLE AND OPERATION WAS NORMAL AT IDLE. PILOTS WERE THEN UNABLE TO INCREASE THRUST, ENGINE WOULD NOT RESPAug 15, 2000 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA971906Fan Blade · dirtyRIGHT ENGINE N1 VIBRATION 2.7 MLS AT 89 PECENT AT FL 180. RETURNED TO SLC. REMOVED AND CLEANED RIGHT ENGINE FAN BLADES. OPS CHECKS GOOD.Jul 31, 2000 · N417SW · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR CA000808023Fuel Control · failed(CAN) CAPTAIN BROUGHT THROTTLES BACK TO FLIGHT IDLE AND THE NR 1 ENGINE STAYED AT A CRUISE POWER SETTING. IN FLIGHT SHUTDOWN PERFORMED ON THE LT ENGINE. DECLARED EMERGENCY. MAINTENANCE REPLACED THE LT ENGINE FUEL CONTROL UNIT. ENGINE CHECKED SERVICEABLE AND AIJul 30, 2000 · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR MASA00087Fuel Control · failedCMH/BWI - FLT 5146 - WHILE STARTING THE DESCENT INTO BWI, THE PILOT WAS UNABLE TO GET THE NR 1 ENGINE TO SPOOL DOWN TO FLIGHT IDLE. UNABLE TO SET THE AIRCRAFT ON A STABILIZED APPROACH. THE DECISION WAS MADE TO SECURE THE NR 1 ENGINE. AFTER LANDING SAFELY, MJul 29, 2000 · N87353 · Cndair CL6002B19 · Fuel Controlling SystemSDR CA000802011Carbon Seal · leaking(CAN) PILOT REPORTED LT ENGINE OIL PRESSURE WARNING AND OIL PRESSURE FLUCTUATING BETWEEN 24 & 45 PSI. PILOT SHUT DOWN THE ENGINE. MAINTENANCE FOUND THAT THE ENGINE REQUIRED 5 LITERS OF OIL. NO EXTERNAL LEAK FOUND. ENGINE RUN CARRIED OUT AND LEAKAGE FOUND FROMJul 22, 2000 · Cndair CL6002B19 · Turbine Engine Accessory DriveSDR CA000724003Fire Loop · failed(CAN) IN CRUISE ON FLIGHT 5367 FROM CINCINNATI TO MINNEAPOLIS / ST PAUL LT 14TH STAGE DUCT WARN ILLUMINATED. CREW FOLLOWED THEIR QRH AND SHUT DOWN THE ENGINE. AFTER DECLARING AN EMERGENCY AND DIVERTING TO MADISON THEY COMPLETED AN UNEVENTFUL LANDING.Jul 14, 2000 · Cndair CL6002B19 · Bleed Air Indicating SystemSDR CA000714003Blade · failed(CAN) DURING SCHEDULE BORESCOPE INSPECTION SEVERAL STAGE ON COMPRESSOR BLADES ON NR 1 ENGINE, FOUND NICKS.Jun 24, 2000 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR CA000614062Carbon Seal · failed(CAN) DURING A FLIGHT, THE CREW NOTICED A FUEL/OIL ODOR IN THE COCKPIT. IT WAS ALSO NOTICED IN THE CABIN WHILE ON THE GROUND. THE NR 1 CARBON SEAL WAS REPLACED. THE FAN DISK ASSEMBLY P/N 6078T57G04, S/N GEE0893 WAS REPLACED (TSN: 10423.9, CNS: 9754).Jun 11, 2000 · Cndair CL6002B19 · Engine Oil System (Airframe Furnished)SDR CA000329030Engine · malfunctioned(CAN) IN CRUISE 32 ENGINE N1, ITT AND FF FLUCTUATED ABOVE AND BELOW 79 PERCENT. CREW DECLARED AN EMERGENCY. BROWN HARNESS REPLACED.Mar 28, 2000 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA000329033Packing · damaged(CAN) PILOT REPORTED RIGHT OIL PRESSURE WARNING MESSAGE. OIL TANK FILLER CAP SEAL DAMAGED. REPLACED.Mar 28, 2000 · Cndair CL6002B19 · Engine Oil PressureSDR CA000301040Computer · failed(CAN) DFDR DATA DOWNLOAD COMPLETED DATA AT GE FOR ANALYSIS.Mar 1, 2000 · Cndair CL6002B19 · Fuel Controlling System
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