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 CA030312007Window · cracked(CAN) AIRCRAFT 7169 TAT = 13433.6 HOURS F/O SIDE WINDOW CRACKED AND ARCING ON DESCENT. OUTER PANE CRACKED.ROAD TRIP CREW DESPATCHED. REMOVED AND REPLACED RT SIDE WINDOW (ORIGINAL EQUIPMENT). RETURNED TO SERVICE.Mar 8, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA0360121EngineFLIGHT 5048 LEFT ENGINE N2 VIB INDICATION.COULD NOT DUPLICATE. NO VIB INDICATIONS DURING ENGINE RUNS.Feb 25, 2003 · N984CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA030221002Windshield · cracked(CAN) FLT 5030 FROM SLC TO HLN, CAPTAINS WINDSHIELD SHATTERED AT FL 260. REPLACED WINDSHIELD.Feb 18, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA030221005Windshield · broken(CAN) WHILE TAXIING, CAPTAINS WINDSHIELD SHATTERED. TEMP -26, THIS WAS THE ORIGINAL WINDSHIELD. WINDSHIELD TOTAL TIME 11,696Feb 17, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA030312008Control Cable · failed(CAN) AILERON CONTROL JAM. ACTION QRH ESTABLISHED THAT PILOT SIDE WAS OPERATING CHANNEL. CONTROL ON CO-PILOT AILERON, FULL CONTROL FOR AILERON UP. AILERON MOTION FROM APPROX NEUTRAL AND DOWN NON EXISTENT. CONTROL ON CAPTAIN SIDE WAS FULL AND FREE. FOUND RT AFeb 14, 2003 · Cndair CL6002B19 · Aileron Control SystemSDR COMA0360093EngineFLIGHT 5115 LEFT ENGINE N2 VIBE MESSAGE DURING T/O.COULD NOT DUPLICATE, INSPECTED ENGINE, FOUND NO DEFECTS.Feb 8, 2003 · N984CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA030221001Windshield · cracked(CAN) DURING CLIMBOUT CAPTAINS WINDSHIELD CRACKED. DECLARED AN EMERGENCY AND RETURNED TO BASE. REMOVED AND REPLACED WINDSHIELD.Feb 7, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA200311751Engine · flamed outRT ENGINE EXPERIENCED FLAME-OUT DURING LANDING ROLLOUT AT PNS. PERFORMED FULL ENGINE RUN WITH CREW. TAKEOFF POWER, THEN REDUCED TO IDLE AND REVERSE POWER UP. CHECKED NORMAL OK FOR CONTINUED SERVICE. PERFORMED INSPECTION AND RUN UP PER MM 76-10-00 AND 71-00Jan 29, 2003 · N591SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA030119002Windshield(CAN) RIGHT WINDSHIELD CRACKED DURING FLIGHT. DIVERTED FLIGHT TO HAMBURG.RIGHT WINDSHIELD REPLACED PER AMM.Jan 12, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA030114008Compressor · damaged(CAN) DURING CLIMB RIGHT ENGINE ITT ROSE TOWARDS 860 DEG. THROTTLES PULLED BACK AND ITT RISE RESTORED. UNABLE TO GET CRUISE POWER BELOW 860 DEG ITT FL 310 IN CRUISE 860 DEG AT 94 PERCENT CRUISE 93.2 PERCENT AT FL 330. MAINTENANCE BOROSCOPED ENGINE AND FOUND THJan 10, 2003 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR CA030116002Pump · failed(CAN) PRODUCTION FLIGHT TEST NR 4 DATED 8 JAN 03, HYDRAULIC NR 2 HI TEMP CAUTION POSTED JUST AFTER LEVELING ATF 410 TEMP MAXIMUM 104C, RT ENGINE SHUTDOWN, TEMP DECREASE TO NORMAL LIMIT. ENGINE RELIT PRIOR TO LANDING. EDP REMOVED AND INSTALLED. GROUND RUN CARRIJan 8, 2003 · Cndair CL604 · Hydraulic Pump (Electric/Engine), MainSDR CA030114002Fuel Control · leaking(CAN) PILOTS REPORTED THAT IN FLIGHT THEY HAD A STRONG FUEL ODOR FROM THE BLEEDS WITH THE APU AIR ON. UPON LANDING, APU ACCESS PANEL WAS OPENED AND STRONG FUEL ODOR AND EVIDENCE OF SPRAY WAS NOTED. MAINTENANCE COMFIRMED MAJOR FUEL LEAKAGE FROM APU COMBUSTOR CJan 6, 2003 · Cndair CL6002B19 · APU Engine Fuel and ControlSDR COMA0360011EngineFLIGHT 5848 LEFT ENG FAN VIB WARNING, ITT IN RED. IFSDREPLACED THE LEFT ENGINE.Dec 31, 2002 · N712CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA030106001Compressor Wheel · vibration(CAN) FLT 5848, TPA-CVG, CLIMBING THROUGH 11,500FT, LT ENGINE FAN VIBRATION WARNING AND ITT INDICATED RED. N1 DECREASED RAPIDLY WITH NOISE. QRH AND MEMORY ITEMS FOLLOWED. OVERWEIGHT SINGLE ENGINE LANDING PER FORMED AT 48,950 LBS. VSI AT LANDING WAS LESS THDec 31, 2002 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR CA030108014Computer · malfunctioned(CAN) IN FLIGHT SHUTDOWN OF RT ENGINE DUE TO REOCCURANCE OF UNCONTROLLED FUEL IMBALANCE. CREW RECEIVED 'XFLOW/APU PUMP EICAS AMBER MESSAGE AFTER TAKEOFF, AFTER APU WAS SHUTDOWN'. ALSO HAD 'RT XFLOW SOV FAIL MESSAGE. REPLACEMENT OF : RT COMPENSATOR PROBE. RT Dec 30, 2002 · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR COMA0260737EngineFLIGHT 5511 LEFT ENGINE VIB MESSAGE.COULD NOT DUPLICATE. NO VIB LOGGED IN MDC.Dec 25, 2002 · N984CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA0260733Seal · leakingFLIGHT 5954 LEFT ENGINE OIL PRESSURE WARNING I.F.S.D.REPLACED THE BB AXIS DRIVE SEAL ON ACCESSORY GEAR BOX.Dec 22, 2002 · N924CA · Cndair CL6002B19 · Turbine Engine Accessory DriveSDR CA021227001Windshield · failed(CAN) CAPTAIN WINDSHIELD OUTER PAN SHATTERED ON DESCENT. REPLACED WINDSHIELD, HEAT CONTROLLER ALSO REPLACED.Dec 22, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA021228002Idg · leaking(CAN) FLT 5954, GRF-CVG, LT ENG OIL WARNING MSG POSTED WHILE IN CRUISE. QRH FOLLOWED AND MSG PERSISTED. OIL TEMP DECREASED, LT ENGINE SHUT DOWN AND AIRCRAFT LANDED IN CRW WITHOUT FURTHER INCIDENT. 16 DEC,02: OIL CONSUMPTION MONITORING DETECTS OIL CONSUMPTIONDec 22, 2002 · Cndair CL6002B19 · Alternator-Generator DriveSDR CA030106006Connector · damaged(CAN) UPON LANDING ONE OF THE RT SPOILERS DEPLOYED ON THE TAXI IN FOR NO APPARENT REASON. RT O/B SPOILERON PCU FOUND TO HAVE A NUMBER OF PINS IN THE CONNECTOR PLUG PUSHED BACK IN. THE SPOILER ELECTRONIC CONTROL UNIT PN 4916405, SN 0599 WAS ALSO REPLACED DUE TDec 20, 2002 · Cndair CL6002B19 · Flight Control System WiringSDR CA021220012Pressure Switch · failed(CAN) RT ENGINE SHUT DOWN IN FLGHT DUE TO LOW OIL PRESS INDICATION & FLUCTUATION. HAD RT ENGINE OIL PRESS EICAS MSG, HIGH TEMP, FUEL OIL EXCHANGER TEMP INCREASE. RT ENGINE CHIP DETECTOR TESTED OK. OIL LEVEL CHECKED AND ONE HALF LITER REMOVED. OIL PRESS TRANSDDec 14, 2002 · Cndair CL6002B19 · Engine Oil PressureSDR COMA0260709Fcu · malfunctionedFLIGHT 5639 LEFT ENGINE LAGGED SIGNIFICANTLY DURING POWER APPLICATION ON T/O ROLL.REPLACED THE LEFT ENIGNE FUEL CONTROL.Dec 11, 2002 · N798CA · Cndair CL6002B19 · Fuel Controlling SystemSDR CA021220005Controller · failed(CAN) WHILE AIRCRAFT WAS SITTING AT GATE CREW NOTICED THAT RT WINDSCREEN OUTER PLY WAS CRACKED. WINDSCREEN REPLACED. CREW ALSO NOTED THAT WINDOW HEAT CAME ON 2 TIMES (2 SEPERATE FLIGHTS) BUT CLEARED WHEN SWITCHED TO RESET/ON. RT WINDSHIELD TEMP CONTROLLER WASDec 6, 2002 · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR CA021210007Computer · malfunctioned(CAN) INTERMITTENT UNCOMMANDED RUDDER MOVEMENT RESULTING IN CONSTANT OSCILLATION OF A/C. ON FLIGHT CONT. SYN PG RT AIL+2 UNITS/ RT ELEVATOR SHOWS CONSTANT MOTION/RUDDER SHOWS CONSTANT MOVEMENT ALSO A/C UNCOMMANDED BANK TO LT WHEN A/P DISCONNECTED. FCC CHANGED,Dec 3, 2002 · Cndair CL6002B19 · Integrated Flight SystemSDR CA021217009Pdu · failed(CAN) DURING FLIGHT AT FL350 RECEIVED A RT REVERSER UNLOCK WARNING MESSAGE. FOLLOWED MEMORY ITEMS AND THEN QRH. ENGINE SHUTDOWN PER QRH. NORMAL SINGLE ENGINE LANDING WAS MADED. REMOVED AND REPLACED PDU IAW MM78-32-03 AND RIGGED LOWER INBOARD BALLSCREW ACTUANov 30, 2002 · Cndair CL6002B19 · Engine Thrust ReverserSDR CA021201001Shaft · broken(CAN) A ' RT ENG OIL PRESS' CAUTION MESSAGE INDICATED DURING CLIMB. THE OIL PUMP DRIVE SHAFT WAS FOUND BROKEN. THE ENGINE WAS REMOVED AND REPLACED.Nov 25, 2002 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA021129004Computer · inaccurate(CAN) AIRCRAFT OPERATING UNDER MEL 28-24-01-2 (XFLOW /APU FUEL PUMP INOP). ON TAKEOFF CREW NOTICED 600LB FUEL IMBALANCE. UNABLE TO TRANSFER FUEL FROM LT TO RT TANK USING GRAVITY FLOW. IMBALANCE INCREASED TO 2000LB IN STRAIGHT AND LEVEL DESPITE ALL EFFORTS. FUENov 17, 2002 · Cndair CL6002B19 · Fuel Quantity IndicatorSDR CA021221001Windshield · cracked(CAN) CAPTAIN'S WINDSHIELD CRACKED IN FLIGHT AT FL410. THE WINDSHIELD WAS REPLACED IAW AMM 56-11-01THE WINDSHILED INSTALLED WAS A POST SERVICE BULLETIN WINDSHIELD.Nov 16, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA021115007Hose · deteriorated(CAN) NR 3 HYDRAULIC SYSTEM LEAK AND QUANTITY DEPLETED TO ZEROAIRCRAFT WAS DIVERTED TO YUL FOR REPAIRS AND GEAR WAS VERY SLOW TO EXTEND. HYDRAULIC HOSE ASSY ON ACMP 3B FOUND LEAKING. HOSE ASSY, 3B HYD PUMP AND CASE DRAIN FILTERS REPLACED. LANDING GEAR RETRACTNov 13, 2002 · Cndair CL6002B19 · Hydraulic System, MainSDR CA021114001Shaft · sheared(CAN) ON APPROACH, FLAP FAIL MSG AT 0 DEG. LOCAL MECHANIC TRIED TO MECHANICALLY REPOSITION FLAPS TO 8 DEG FOR FERRY FLT RT OUTBOARD FLAP SURFACE INCURRED SOME TWISTING (SKIN RIPPLING). FOUND NR 4 FLEX DRIVE UNRAVELLED WITH OUTBOARD DRIVE END BROKEN OFF (AT Nov 9, 2002 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA021115001Wire Harness · failed(CAN) AFTER TAKE OFF, WHEN FLAPS WERE RETRACTED, STALL FAIL CAUTION MESSAGE APPEARED ACCOMPANIED BY HYD CAUTION FOR HYD PUMP 1B & 3B. STALL TAPE ON CAPTAINS & F/O'S PFD APPEAR TO RUN FULL LENGTH OF AIR SPEED INDICATOR. AIRCRAFT FERRIED FOR TROUBLESHOOTING. Nov 7, 2002 · Cndair CL6002B19 · Flight Control System WiringSDR CA021114002Windshield · cracked(CAN) CAPTAIN'S WINDSHIELD CRACKED DESCENDING.APPEARED TO BE AN ELECTRICAL SHORT LOW IN THE WINDSHIELD AT THE CENTER PRIOR TO THE CRACK.REMOVED AND REPLACED LEFT WINDSHIELD WITH SERVICEABLE UNIT IAW MM 56-11-01. OPS AND LEAK CHECK GOOD.Nov 4, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA021108001Windshield · failed(CAN) CAPTAIN'S WINDSHIELD SHATTERED AT FL290. DIVERTED. WINDSHIELD REPLACED AND AIRCRAFT RETURNED IN SERVICE.Nov 2, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA0260625Engine · failedFLIGHT 5546 LEFT ENGINE OIL PRESSURE WARNING MESSAGE.REPLACED THE LEFT ENGINE.Oct 30, 2002 · N940CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA021104002Window · failed(CAN) CAPTAIN'S SIDE WINDOW SHATTERED AT 23,000 FT. LANDING UNEVENTFUL. FERRIED AIRCRAFT FOR WINDOW REPLACEMENT.Oct 29, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA021104003Windshield · failed(CAN) CAPTAIN'S WINDSHIELD SHATTERED AT 28,000FT ON DESCENT.CABIN AT 8 PSID. NO EMERGENCY DECLARED.SENT ROAD CREW TO R&R WINDSHIELD.Oct 28, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA021031001Seal · broken(CAN) IN CLIMB TO FL 240, A LOUD NOISE COMING FROM THE PAX DOOR WAS HEARD ALONG WITH A DEPRESSURIZATION OF THE AIRCRAFT OF APPROXIMATELY -4000 FT/MIN (ON EICAS). THE FLIGHT CREW DID AN EMERGENCY DESCENT PER THE QRH AND LANDED AT THE DESTINATION AIRPORT. ONCE AOct 27, 2002 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA030417003Bushing · loose(CAN) MIGRATING BUSHINGS ON WING ATTACHMENT FITTINGS.Oct 25, 2002 · Cndair CL6002B19 · Wing, Fuselage Attach FittingsSDR CA021029012Windshield · cracked(CAN) WHILE IN FLIGHT OUTER PANE OF L/H WINDSHIELD CRACKED. WINDSHIELD REPLACED.Oct 24, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA021025006Windshield · failed(CAN) AIRCRAFT 7046 TAT = 18805.9 HOURS.FLIGHT 5539 FROM CVG TO MKE.R. WINDSHIELD SHATTERED ON TAXI OUT. INSTALLED REPLACEMENT WINDSHIELDOct 21, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA021023008Fitting · cracked(CAN) DURING OVERNIGHT CHECK, MAINTENANCE FOUND AFT ANCHOR FITTING OF PASSENGER DOOR COUNTER BALANCE MECHANISM CRACKED IN MIDDLE OF BRACKET. BRACKET REPLACED. IPC REF 52-11-17 FIG.2 ITEM 395.Oct 19, 2002 · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0260592Engine · malfunctionedFLIGHT 5847 SMOKE IN CABIN. REPLACED THE RT ENGINE. EVIDENCE OF OIL AROUND VG ACTUATOR SPINDLE, SUSPECT NR 3 CARBON SEAL FAILURE.Oct 18, 2002 · N931CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA0260619Engine · smokeFLIGHT 5847 SMOKE IN CABIN.REPLACED THE R/H ENGINE, (EVIDENCE OF OIL AROUND VG ACTUATOR SPINDLE, SUSPECT #3 CARBON SEAL FAILURE.)Oct 18, 2002 · N931CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA021023007Control Unit · failed(CAN) SHORTLY AFTER AIRBORNE, STAB & MACH TRIM DISCONNECTED. RE-ENGAGED SUCCESSFULLY, BUT WOULD DICONNECT AGAIN SHORTLY AFTER.(30SEC) HORIZ STAB TRIM CONTROL UNIT DISPLAYED 'MOTOR 1''CHANNEL 1' FAILED MESSAGE. UNIT REPLACEDOct 18, 2002 · Cndair CL6002B19 · Elevator Control SystemSDR CA021017002Aileron · frozen(CAN) AILERONS BECAME VERY STIFF AND WOULD MOVE ONLY UNDER HIGH LOADING, SUSPECT FROZEN CONTROLS DESCENDING OUT OF 6000 FEET CONTROLS BECAME NORMAL. LT AND RT AILERON REAR QUADRANTS CLEANED AND SPRAY WITH WATER REPELLANT. OPERATIONAL TEST CARRIED OUT AS. UNOct 16, 2002 · Cndair CL6002B19 · Aileron Control SystemSDR SWIA200211327Carbon Seal · leakingRIGHT ENGINE OIL PRESSURE WENT TO 25-27 PSI AND ENGINE TEMPERATURE WAS GOING UP. FOLLOWED QRH AND SHUT DOWN THE RIGHT ENGINE. DIVERTED TO DEN. INSTALLED NEW CARBON SEALS IN HYD PUMP, AIR STARTER AND IDG POSITIONS, AND NEW 3 EA SEAL RINGS IN EACH POSITION. Oct 14, 2002 · N430SW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA021015005Line · unapproved part(CAN) AIRCRAFT HAS BEEN EXPERIENCING HIGH ITT INDICATION ON THE LT ENGINE SINCE ITS ACCEPTANCE CHECK.4 LEAKS AT DIFFERENT LOCATION FROM THE 10 STAGE WERE FOUND. ONE WAS AT THE RT 10TH STAGE MANIFOLD PRESSURE SENSING LINE. THE LINE WAS NOT SITTING PROPERLY AND Oct 12, 2002 · Cndair CL6002B19 · Engine Bleed Air SystemSDR CA021112002Servo · failed(CAN) AILERON STIFFNESS DURING LAST 3000 FT OF APPROACH IN RAIN AILERON STIFFNESS DURING LAST 3000 FT OF APPROACH IN RAIN. PERFORMED GROUND INSPECTION DE-ICING FLUID ON BOTH AILERON PCU PANEL AND ON LT LOWER AILERON SERVO MOUNT ADJUSTMENT TEST FOUND SLIP-CLUTCOct 8, 2002 · Cndair CL6002B19 · Autopilot Main ServoSDR CA021010001Windshield · cracked(CAN) WINDSHIELD FOUND CRACK AFTER FLIGHT. A/C HAD ACCUMULATED 18778 HOURS AND 14803 CYCLES. WINDHIELD WAS REMOVED AND REPLACED.Oct 7, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA021009003Thrust Reverser · sheared(CAN) RT REV UNLOCKED MESSAGE POSTED. THRUST REVERSER CYCLED SEVERAL TIMES BUT UNSUCCESSFULL. RETURNED TO GATE. AT GATE, SEVERE DAMAGE FOUND TO THRUST REVERSER TRANSLATING COWL. FOUND ACTUATOR AT 11 O'CLOCK POSITION SHEARED. ACTUATOR REPLACED IN ACCORDANCE WOct 5, 2002 · Cndair CL6002B19 · Engine Thrust Reverser
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