GE CF34-3A1

Service difficulty reports · 1,372

Newest first. General aviation reporting is voluntary.

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 CA031029001Line · leaking(CAN) DURING APPROACH TO EWR UNABLE TO LOWER LANDING GEAR. HAD HYD 3 LOW PRESSURE WARNING. HYD LEVEL 'O' MANUAL GEAR EXTENSION PERFORMED '3 GREEN' FOUND LEAK COMING FROM 3A PUMP PRESSURE HOSE. PUMP AND HOSE REPLACED, LEAK AND OPERATION NORMAL.Oct 26, 2003 · Cndair CL6002B19 · Hydraulic System, MainSDR CA031030007Engine · failed(CAN) LOUD BANG AT 3000 FT AND LT ENGINE SHUT DOWN. AIRCRAFT LANDED IN TLH WITHOUT FURTHER INCIDENT. LT ENGINE REPLACED, AIRCRAFT RETURNED TO SERVICE.Oct 25, 2003 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA031030006Window · cracked(CAN) FOS SIDE WINDOW CRACKED WHILE IN CRUISE. EMERGENCY DECLARED, AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT RETURNED TO SERVICE FOLLOWING THE WINDOW REPLACEMENT. (SEE ALSO: US NR 2003121000202)Oct 24, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA0360468Engine · failedFLIGHT 5308 LOUD BANG FOLLOWED BY LEFT ENGINE FAILURE. REPLACED LEFT ENGINE.Oct 23, 2003 · N956CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA031023001Circuit Card · malfunctioned(CAN) IN CRUISE THE RUDDER MOVED WITH NO INPUT CAUSING YAW. THE MOVEMENT WAS INTERMITTENT ALWAYS RETURNING TO NEUTRAL. REPLACED FCC CARD AND YAW DAMPER ACTUATOR, CHECKS SERVICABLE.Oct 22, 2003 · Cndair CL6002B19 · Autopilot ComputerSDR CA031024003Adc · malfunctioned(CAN) ON DEPARTURE AT 2000 FT THE SPEED BUG WENT FROM 200 KTS TO 40 KTS UN COMMANDED AT THE SAME TIME THE 'STALL FAIL MSG' ON FOR 30 SEC. PURGED NR 1 AND 2 PITOT LINES AND CHANGED ADC NR 1.Oct 22, 2003 · Cndair CL6002B19 · Air Data ComputerSDR CA031020003Sensor · malfunctioned(CAN) AFTER T/O UNABLE TO PRESSURIZE ABOVE 1.5 PSI. PASSENGER LATCH WARNING ON DOOR SYNOPTIC PAGE WITH ASSOCIATED (OB COOL) CAUTION EICAS MESSAGE AND (IB COOL) EICAS STATUS MESSAGE WITH PASS DOOR OPEN. REPLACED OUTER DOOR HANDLE LOCKED SENSOR. ALL CHECKS NOROct 19, 2003 · Cndair CL6002B19 · Door Warning SystemSDR COMA0360463Fuel Control · malfunctionedFLIGHT 5243 RT ENGINE HUNG AT 79 DEGREES N1 DURING T/O 3 INCHES POWER LEVER SPLIT. REPLACED THE RT FUEL CONTROL.Oct 18, 2003 · N779CA · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR CA031017003Switch · dirty(CAN) PAX DOOR WARNING AT FL200. DOOR RIGGING CARRIED OUT IAW AMM 52-11-02. NOTE: A/C HAD TWO PREVIOUS SNAGS. BIT CHECK FAULTED S47 AT WHICH TIME SWITCH WAS CLEANED AND LUBED.Oct 15, 2003 · Cndair CL6002B19 · Door Warning SystemSDR CA031015002Pump · failed(CAN) HYD NR 2 QUANTITY DROPPED STEADILY DURING FLT. AT LANDING HAD NR 2 QTY AT 25 PERCENT DECLARED EMERGENCY AND LANDED NORMALLY IN ALBANY. PUMP CHANGED, SYSTEM FLUSHED AND FILTERS CHANGED ALL NOW NORMALOct 13, 2003 · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR CA031017002Window · failed(CAN) LT SIDE WINDOW SHATTERED IN FLIGHT. (EXTERNAL) NO CHANGE TO PRESSURIZATION. LT WINDOW CHANGED AND NO FURTHER FAULTS.Oct 13, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA0360446Engine · failedFLIGHT 5685 LEFT ENGINE VIBRATION FOLLOWED BY ENGINE FAILURE. REPLACED ENGINE.Oct 2, 2003 · N805CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA030930013Tube · burned(CAN) DURING AMJOR INSPECTION (C-CHECK AND 96 MTH INSP.) A FUEL TUBE ASSEMBLY IN CENTER TANK WAS DISCOVERED WITH EVIDENCE OF ARCING. FURTHER INSPECTION REVEALED ADJACENT PART (STIFFENER PN 60010011193) HAD ALSO SIMILAR EVIDENCE OF ARCING. TUBE ASSEMBLY WAS RESep 30, 2003 · Cndair CL6002B19 · Aircraft Fuel Distribution SystemSDR CA031006005Transmitter · failed(CAN) FLAPS FAILED AT 42 DEGREES ON LEFT FLAP (HAD 45 DEG ON RT FLAP) FOUND TO BE THE FLAP POSITION TRANSMITTER AT FAULT.Sep 25, 2003 · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR COMA0360426Powerplant · failedFLIGHT 5014 AT APPROXIMATELY 80 KTS DURING T/O ROLL THE RT ENGINE SPIKED TO 998 DEGREES C, WITH RAPID RPM DECREASE, ABORTED T/O AND RETURNED TO THE GATE. REPLAED THE RT ENGINE ASSEMBLY.Sep 21, 2003 · N937CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA030922003Control Panel · malfunctioned(CAN) UPON AUTOPILOT DISCONNECT ON APPROACH ELEVATORS WERE STUCK AND HAD TO OVERPOWER TO REGAIN CONTROL.FLT DID NOT ENTER ANY VISIBLE MOISTURE DURING FLT. A/C LANDED NORMALLY. PANEL REPLACED (FCP)AS PER AMM 22-11-07-400-801 AND ALL OPERATES NORMALLY.Sep 18, 2003 · Cndair CL6002B19 · Autopilot SystemSDR COMA0360412Oil System · lowRT ENGINE LOW OIL PRESSURE WARNING 3 TIMES. FOUND ENGINE OIL SYSTEM 5 QUARTS LOW. SERVICED OIL SYSTEM.Sep 15, 2003 · N914CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA030921001Windshield · cracked(CAN) AIRCRAFT HAS RECEIVED A REPORT WHICH WE FEEL IS A REPORTABLE EVENT. RT WINDSHIELD INNER PLY CRACKED WHILE EN-ROUTE FROM ORD TO AUS. THE AIRCRAFT WAS FERRIED TO ORD FOR THE WINDSHIELD REPLACEMENT.Sep 12, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA0360407Engine · failedFLIGHT 9486 RT ENGINE OVER TEMP AND AUTO SHUT DOWN. REPLACED RT ENGINE.Sep 5, 2003 · N739CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA030910002Pin · failed(CAN) DURING CLIMB THROUGH 15,000 FT CARGO DOOR CAUTION MESSAGE CAME ON. PRESSURIZATION NORMAL. PIN FOUND SHEARED ON LATCH TO STOW DOOR HANDLE. PIN REPLACED CHECKS SERVICABLE.Sep 5, 2003 · Cndair CL6002B19 · Cargo/Baggage DoorsSDR COMA0360395Thrust Plate · brokenRIGHT THRUST REVERSER SPRING BOX ASSEMBLY AT 4 O'CLOCK POSITION WAS FOUND BROKEN. REMOVED BROKEN SPRING BOX ASSEMBLY AND INSTALLED A SERVICEABLE ONE.Aug 30, 2003 · N716CA · Cndair CL6002B19 · Engine Thrust ReverserSDR COMA0360396Blocker Door · brokenFLIGHT 5675 RT THRUST REVERSER BLOCKER DOOR AT 4 O'CLOCK POSITON FOUND BROKEN IN HALF. REMOVED BROKEN BLOCKER DOOR AND INSTALLED A SERVICEABLE ONE.Aug 30, 2003 · N716CA · Cndair CL6002B19 · Engine Thrust ReverserSDR CA031001001Windshield · cracked(CAN) RT WINDSHIELD INNER LAYER CRACKED DURING FLIGHT. AIRPLANE FERRIED. RT WINDSHIELD REPLACED.Aug 13, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA030807002Controller · malfunctioned(CAN) A/C HAD MULTIPLE WARNINGS ON APPROACH. APU FIRE INDICATOR. (APU RUNNING DUE ONE ENG GEN ON MEL) APU AUTO SHUTDOWN. RT & LT JET OVERHEAT MSG, LT & RT FIRE FAIL CAUTION MSG. LT WINDSHIELD HEAT IN FLT. CHGED FIRE DET CONTROLLER ALL CKS SERV. CONTROLLER INAug 5, 2003 · Cndair CL6002B19 · Fire DetectionSDR A6WA200340114Transducer · failedDURING TAKE-OFF POWER APPLICATION RECEIVED VIBE INDICATION NR 1 ENGINE AT 88.1 PERCENT N1 IN PROGRESS. REPLACED VIBRATION TRANSDUCER WIRE HARNESS ON LEFT ENGINE, OPS CHECK GOOD. RAN LT ENGINE TO 90 PERCENT N1 NO N2 VIBRATION INDICATION NOTED. (M)Jul 28, 2003 · N422AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA0360342Pump · cloggedFLIGHT 5655 LT ENGINE OIL PRESSURE WARNING. SCAVANGE LUBE PUMP INLET SCREENS CLOGGED. REPLACED LUBE PUMP.Jul 25, 2003 · N807CA · Cndair CL6002B19 · Engine Oil Storage (Airframe Furnished)SDR COMA0360339Engine · failedFLIGHT 5284 LEFT ENGINE OIL PRESSURE WARNING AND SMALL VIBRATION, ENGINE THEN FAILED. REPLACED ENGINE.Jul 24, 2003 · N807CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA030729003Engine · shutdown(CAN) LT ENGINE SHUT ITSELF DOWN WITH SMALL VIB AND OIL PRESSURE WARNING. MTCE REPORTED CHIP DETECTOR WAS CONTAMINATED AND SOME DEBRIS WAS IN THE TAILPIPE. FOLLOWING LT ENGINE REPLACEMENT, THE AIRCRAFT RETURNED TO SERVICE.Jul 24, 2003 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA030806002Line · leaking(CAN) ON ARRIVAL FOUND NR 1 HYD SYSTEM QTY AT 0 PERCENT. LARGE HYD LEAK NOTICED IN AFT SERVICE COMPARTMENT. FOUND LINE LEAKING IN AFT COMPARTMENT. NEW LINE FABRICATED AND INSTALLED.SYSTEM FLUSHED. NR 1 EDP REPLACED DUE DISENTIGRATION. ALL FOUR HYD FILTERS REPLJul 17, 2003 · Cndair CL6002B19 · Hydraulic System, MainSDR SWIA200312198Engine · malfunctionedLEFT ENGINE FAILED ON DESCENT. JUST PRIOR TO FAILURE, ''L MAIN EJECTOR'' AND ''L SCAV EJECTOR'' MSG DISPLAYED ON EICAS. REMOVED AND REPLACED LEFT POWER PLANT IAW CRJ MM 72-00-00. OPS AND LEAK CHECKS GOOD.Jul 16, 2003 · N592SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA030825016Gearbox · failed(CAN) LT FUEL PUMP AND LT SCAV EJECTOR CAUTION MESSAGES WERE POSTED AND LT ENGINE FUEL PRESSURE WENT TO ZERO CAUSING THE LT ENGINE TO SHUT DOWN. NO N2 ROTATION WHEN STARTER MOTORED. REPLACED ENGINE QEC ASSEMBLY.Jul 16, 2003 · Cndair CL6002B19 · Accessory GearboxesSDR CA030718005Window · cracked(CAN) FLIGHT AT FL220, THE EXTERNAL PLY OF THE RT WINDOW CRACKED. THE FLIGHT CREW DID AN EMERGENCY DESCENT AND DEPLOYED THE OXYGEN MASK IN THE CABIN.Jul 14, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA030730006Pcu · erratic(CAN) AIRCRAFT OUT OF ROLL TRIM ON T/O, FLAP 8, IMMEDIATELY REQUIRED RIGHT CONTROL INPUT. AUTOPILOT ALSO SHOWED RIGHT CONTROL INPUT. ON APP. HAND FLOWN, FLAP 45, REQD. RWD TRIM TO ALMOST FIRST HASH MARK. REPLACED LT WING OB FLIGHT SPOILER PCU DUE FLOATING/Jul 9, 2003 · Cndair CL6002B19 · Drag Control ActuatorSDR CA030729002Windshield · cracked(CAN) DURING CLIMB, RT WINDSHIELD CRACKED. RETURNED TO DEPARTURE AIRPORT. FOLLOWING THE WINDSHIELD REPLACEMENT, THE AIRCRAFT RETURNED TO SERVICE.Jul 8, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA030624001Bolt · corroded(CAN) ROLLER BEARING WITH NLG DOORS FULLY CLOSED SHOULD FALL WITHIN ITS MECHANICAL CAM-LOCK WHEN FUNCTIONING NORMALLY. WHEN HYDS ARE REMOVED, RETRACT ACTUATOR WILL RELAX AND CAM-LOCKED ROLLER BEARING WILL KEEP NLG DOOR FULLY CLOSED, PREVENTING FROM FALLING 'Jun 18, 2003 · Cndair CL6002B19 · Landing Gear Door ActuatorSDR CA030619004Pseu · failed(CAN) ON GEAR DOWN SELECTION, GEAR DISAGREE MESSAGE DISPLAYED. POSITION SENSOR ELECTRONICS UNIT REPLACED AND CHECKED SERVICABLE.Jun 16, 2003 · Cndair CL6002B19 · Landing Gear Position and WarningSDR COMA0360271Engine · overtempFLIGHT 5879 RIGHT ENGINE OVER TEMPERATURE, INDICATED 901 DEGREES CELSIUS. REPLACED ENGINE.Jun 11, 2003 · N984CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA030612009Pcu · failed(CAN) NOTICED AN UNCOMMANDED MOMENTARY ROLL IN CRUISE. THIS WAS FOLLOWED BY A SPOILERON FAULT STATUS MSG, WHICH REMAINED ON. LANDING PERFORMED UNEVENTFULLY. MAINTENANCE FOUND RIGHT SPOILERON INBOARD PCU FAILED. FOLLOWING THE PCU REPLACEMENT, THE AIRCRAFT RJun 10, 2003 · Cndair CL6002B19 · Drag Control ActuatorSDR CA030603001Shutoff Valve · failed(CAN) ON TAKE OFF ROLL, THE FLIGHT CREW REPORTED THAT THEY COULD NOT MAINTAIN RUNWAY CENTERLINE. HAD TO USE FULL LT RUDDER DEFLECTION. AIRCRAFT PULLED TO RT.ABORTED TAKE OFF AT 60 KTS (WIND WAS STRAIGHT DOWN THE RUNWAY). AFTER REPLACING THE NOSE WHEEL STEERIMay 31, 2003 · Cndair CL6002B19 · Landing Gear Steering SystemSDR COMA0360247Frame · crackedFLIGHT 5016 RT ENGINE LOW OIL PRESSURE WARNING. REPLACED CRACKED EXHAUST FRAME.May 26, 2003 · N420CA · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR CA030516001Controller · jammed(CAN) SHORTHLY AFTER TAKE OFF THRU FL250 THE AILERON SYSTEM JAMMED, FLIGHT CREW SUSPECTED ICE AS THERE WASHEAVY RAIN WHILE DEPARTING, THE FIRST OFFICER SIDE WAS AFFECTED, PILOTS SIDE WAS OK (AFTER CONTROL COLUMN DISCONNECT INVESTIGATION UNDERWAY,May 15, 2003 · Cndair CL6002B19 · Aileron Control SystemSDR COMA0360229Oil System · lowFLIGHT 5533 RT ENGINE OIL PRESSURE WARNING. SERVICED RT ENGINE WITH 4.75 QTS OF OIL.May 4, 2003 · N719CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR COMA0360226Carbon Seal · leakingFLIGHT 5854 RT ENGINE LOW OIL PRESSURE WARNING. REPLACED THE ACCESSORY GEAR BOX DRIVE CARBON SEALS.May 3, 2003 · N408CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA030501005Selector Valve · failed(CAN) AFTER TAKE OFF GOT A STEERING INOP MESSAGE FOLLOWED BY GEAR DISAGREE , WITH NOSE GEAR NOT IND IN THE UP POSITION, AIRCRAFT RETURNED WITH NO INCIDENT TOTAL TIME 10992 HRS.May 1, 2003 · Cndair CL6002B19 · Steering UnitSDR CA030514018Switch · out of adjust(CAN) (L REV UNLOCK) WARNING MESSAGE POSTED WHILE IN CRUISE. AIRCRAFT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. FOLLOWING READJUSTMENT OF THE THRUST REVERSER STOW SWITCH, THE AIRCRAFT RETURNED TO SERVICE.Apr 25, 2003 · Cndair CL6002B19 · Engine Thrust ReverserSDR CA030421006Selector Valve · defective(CAN) GEAR DISAGREE MESSAGE ON APPROACH, NOSE GEAR SHOWED DOWN & GREEN, MAIN SHOWED UP & WHITE, GEAR HANDLE CYLCLED TWICE WITH SAME INDICATION, HYD INDICATION OK. MANUAL EXTENSION COMPLETED AS PER QRH. THIS WAS THE ORIGINAL PART FROM THE MANUFACTURER.Apr 18, 2003 · Cndair CL6002B19 · Landing Gear SelectorSDR COMA0360162FanFLIGHT 5490 VIB WARNING WHEN T/O THRUST APPLIED.COULD NOT DUPLICATE - INSPECTED ENGINE AND FOUND NO DISCREPANCIES, C/W A FAN TRIM BALANCE AND REDUCED VIB FROM .9 TO .4Mar 21, 2003 · N984CA · Cndair CL6002B19 · Turbine Engine Bypass SectionSDR CA030321012Window · failed(CAN) SIDE WINDOW SHATTERED OUTER PANE IN FLIGHT TSN 3205HRSMar 18, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA0360142Pump · leakingFOUND SMALL PIN HOLE IN RT ENG FUEL PUMP HOUSING, FOUND DURING A LEAK CHECK FOR A NON RELATED ITEM. REPLACED FUEL PUMP.Mar 9, 2003 · N721CA · Cndair CL6002B19 · Engine Fuel PumpSDR CA030312009Window · cracked(CAN) AIRCRAFT TAT = 15823.8 HOURS.FLIGHT 5788. CAPTAIN'S SIDE WINDOW CRACKED IN CRUISE FLIGHT. DECLARED AN EMERGENCY AND LANDED. REMOVED AND REPLACED SIDE WINDOW.Mar 9, 2003 · Cndair CL6002B19 · Flight Compartment Windows
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