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 SWIA200311789Control Unit · malfunctionedBOTH STAB TRIM & MACH TRIM DISCONNECT IN FLIGHT, HARD TO RESET. ON LANDING, BOTH STAB AND MACH TRIM DISCONNECTED AGAIN. REMOVED AND REPLACED HSTCU IAW MM 27-41-01. OPS CHECK GOOD.Feb 14, 2003 · N403SW · Cndair CL6002B19 · Elevator Tab Control SystemSDR CA030212005Seal · leaking(CAN) EVIDENCE OF HYDRAULIC FLUID LEAKING FROM PCU SHAFT SEAL AREA.SUSPECT LEAKING IS WORSE AT ALTITUDE ORIN EXTREME COLD CONDITIONS.Jan 31, 2003 · Cndair CL604 · Aileron Control SystemSDR CA030419002Skin · cracked(CAN) CRACKS FOUND IN LT WING LEADING EDGE MID SECTION. CRACK IS APPROX. 10 - 15 CM VERTICAL AND IS CONNECTED TO THE RIVETS IN THE MIDDLE OF THE L.E. ASSY.IN ADDITION TO THIS CRACK, 2 SMALLER CRACKS WERE FOUND ON EACH SIDE OF THIS CRACK, BOTH OF THESE CRACKS Jan 30, 2003 · Cndair CL6002B19 · Leading Edge DevicesSDR CA030206001Window · cracked(CAN) RIGHT WINDOW CRACKED ALONG WITH MESSAGE R WINDOW HEAT (C).RIGHT WINDOW AND RIGHT WINDOW HEAT CONTROLLER REPLACED AND AIRCRAFT RETURNED TO SERVICE.Jan 29, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA030123003Window · cracked(CAN) DESCENDING THROUGH APPROXIMATLY 18000 FT, HEARD A THUD, LOOKING TO MY LT, NOTICED THAT THE LT SIDE WINDOW HAD NUMUROUS CRACKS. THERE WERE NO AIR SOUNDS AND THE CABIN PRESSURE WAS NORMAL. QRH PROCEDURE, ADVISE ATC OF THE SITUATION AND REQUESTED LOWER.Jan 24, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA030131006Feel Unit · rough(CAN) CREW STATED THAT ON TAKEOFF, EXCESSIVE FORCE ( AS COMPARED TO NORMAL TAKEOFF FORCE) WAS REQUIRED TO PULL THE YOKE BACK FOR TAKEOFF. CREW STATED THAT THE REQUIRED FORCE WAS SUCH THAT THEY CONSIDERED ABORTING TAKEOFF, BUT DID NOT. CREW ALSO NOTED THAT THE Jan 22, 2003 · Cndair CL604 · Elevator Control SystemSDR CA030130004Actuator · failed(CAN) ON DEPARTURE FLAPS FAILED AT 20 DEGREES. DURING TROUBLE SHOOTING IT WAS DISCOVERED THAT THE FOLLOWING ACTUATORS FAILED THE ACTUATOR TORQUE CHECK AS PER MM 27-53-00-750-002, AND WERE REPLACED.Jan 21, 2003 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CA030123001Window · cracked(CAN) RH SIDE WINDOW CRACKED ON LANDING. WINDOW ASSY REPLACED.Jan 17, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA030120001Wire · loose(CAN) DURING CLIMB, FLIGHT CREW RECEIVED EICAS MESSAGES THAT FOLLOW "LT WINDOW HEAT, LT STATIC HEAT, LT AOA HEAT, STBY PITOT HEAT, BASE PITOT HEAT" SINCE ICING CONDITION EXISTED AHEAD, IT WAS DECIDED TO RETURN TO DEPARTURE BASE IT WAS FOUND THAT TWO WIRESJan 16, 2003 · Cndair CL6002B19 · Electrical Power System WiringSDR CA030123002Window · cracked(CAN) SHORTLY BEFORE LANDING, THE RIGHT WINDOW CRACKED. CRACK FURTHER PROGRESS ON TOUCH DOWN. AIRPLANE FERRIED. RIGHT WINDOW REPLACED.Jan 16, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA030117004Pcu · leaking(CAN) WHILE IN THE HANGAR, HYDRAULIC FLUID WAS NOTICED ON THE WING UNDERSIDE LEAKING FROM THE AILERON PCU DRAIN HOLES. DURING SUBSEQUENT LEAK CHECKS WITH THE PCU INSPECTION PANEL REMOVED NO SIGNIFICANT LEAKAGE NOTICED. DURING SHORT TURN AROUND FLIGHTS NO EVIDJan 15, 2003 · Cndair CL604 · Aileron Control SystemSDR CA030116001Engine · failed(CAN) PRODUCTION FLIGHT TEST 1 (2002-12-21) UNABLE TO AIRSTART RT ENGINE EITHER WINDMILL OR WITH AIR TURBINE START. N2 REMAINED AT 0 PERCENT EVEN WITH ATS ENGAGED. RNC (RAPPORT DE NON CONFORMANCE) C302087572 RAISED. PILOTS TO CARRIED OUT DISPOSITION OF RNC AS Jan 13, 2003 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA030221003Windshield · cracked(CAN) CLIMBING OUT OF DENVER AT ABOUT 9600 MSL, WINDSHIELD SHATTERED. SMALL SMUDGE MARK BUT NO FEATHERS. VMC ABOUT 220 KTS.PERFORMED CHECKLIST LEVELED OFF AT 12,000.DECIDED TO RETURN TO DENVER.BURNE D OFF ROUGHLY 2000 LBS OF FUEL TO LAND BELOW 47,000 LBS.INNEJan 12, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA030120002Tube · chafed(CAN) A SUSPECTED BOOST PUMP INDICATION DEFECT WAS BEING WORKED WHEN IT WAS NOTICED THAT CENTRE FUEL TANK QUANTITY WAS INCREASING DURING PERIODS OF PUMP ACTIVITY. ON INSPECTION THE LT BOOST PUMP PRESSURE INDICATION LINE PT 601R6226135 WAS FOUND TO HAVE BEEN COJan 11, 2003 · Cndair CL6002B19 · Aircraft Fuel Distribution SystemSDR CA030119003Window · cracked(CAN) EN ROUTE, LEFT WINDOW CRACKED. FERRY FLIGHT PERFORMED.LEFT WINDOW REPLACED PER AMM.Jan 10, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA030119006Window · cracked(CAN) UPON LANDING IT WAS NOTICED THE CAPT'S SIDE WINDOW WAS CRACKED. CAPT'S SIDE WINDOW REPLACED AIRCRAFT RETURNED TO SERVICE.Jan 10, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA200340016Fuel Control · malfunctionedRIGHT ENGINE INFLIGHT FLAMED OUT WITH RIGHT ENGINE OIL PRESSURE CAS MESSAGE ON ED1. REMOVED AND REPLACED NR 2 FUEL CONTROL UNIT. NO DEFECTS NOTED. REPLACED FUEL FILTER, RIG CHECKED, TANKS SUMPED, NO DEFECTS. (M)Jan 9, 2003 · N431AW · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR CA030119004Fcu(CAN) 60 MILES FROM SAVANNAH, ON DESCENT FROM FL230 TO FL110, CREW REPORTED SLOW RH ENGINE. FLAMEOUT ON DESCENT AT 330 KTS AT 3200 FEET/MIN DESCENT. THE INFORMATION THAT FOLLOWS WAS TAKEN FROM AIRCRAFT DEFECT LOG BEGIN QUOTE:DEFECT: ON DESCENT RIGHT ENGINE FJan 9, 2003 · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR CA030119005Window · cracked(CAN) LT SIDE WINDOW CRACKED, WINDOW ASSY REPLACED.Jan 8, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA030119007Windshield · crackedPERFORMED TECH FERRY FLIGHT AC FERRY FLIGHT APPROVAL AND REPLACED WINDSHIELD ACC AMM 56-11-01.Jan 7, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA021228003Windshield · cracked(CAN) UPON LANDING IN BUDAPEST IT WAS NOTICED THE CAPT'S SIDE WINDOW WAS CRACKED.CAPT'S SIDE WINDOW REPLACED AIRCRAFT RETURNED TO SERVICE.Dec 23, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA200211596Wire · damagedSTARTED APU ON APPROACH AND RECEIVED A DOOR INHIBIT MESSAGE, BUT APU STILL STARTED. SHUTDOWN APU AND RECEIVED APU FIRE MESSAGE. FIRED THE FIRE BOTTLE. FOUND TB202 BLOCK 9 INTERMITTANT. REPLACED TB 202 BLOCK 9. REINSTALLED WIRES INTO BLOCK IAW WM 49-60-00.Dec 16, 2002 · N413SW · Cndair CL6002B19 · APU System WiringSDR CA021217011Pump · failed(CAN) AFTER TAKEOFF AT ABOUT 200 FT AGL ' HYD 1 HIGH TEMP ' MSG. CAME ON EICAS. WHEN CHECKED, HYD TEMP IT WAS 116-117OC PRESSURE WAS AT 3600 PSI DURING FURTHER CLIMB THE TEMP WENT UP TO 133OC ON LEVEL FLIGHT TEMP WAS STABILIZED AT 124-126OC. FOR REST OF THE FLDec 16, 2002 · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR CA021211008Engine · malfunctioned(CAN) ON TAKE-OFF, CREW REPORTED AN HIGH VIBRATION AND A LOUD NOISE, FOLLOWED BY AN ITT INCREASE. ENGINE SHUT DOWN, AND RETURNED TO DEPARTURE AIRPORT. ENGINE REPLACEDDec 9, 2002 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA200211537Priority Valve · malfunctionedUPON GEAR RETRACTION AFTER TAKEOFF, ''GEAR DISAGREEMENT'' AND ''NOSE DOOR'' WARNINGS ILLUMINATED. RETURNED TO FAT. ALSO ''WOW INPUT'' , ''NOSE WHEEL STEERING'' CAUTIONS ILLUMINATED AND ''WOW OUTPUT FAIL'' STATUS ILLUMINATED. ''NWS'' CAUTION EXTINGUISHED UPODec 3, 2002 · N587SW · Cndair CL6002B19 · Landing Gear ActuatorSDR SWIA200211538Detector · malfunctionedCAPTAIN'S HEADING 5-10 DEGREES OFF FROM COMPASS AND FIRST OFFICER'S. RECEIVED SEVERAL EFIS COMP MON CAUTION MESSAGES. PERFORMED QRH PROCEDURE AND RETURNED TO SLC. REMOVED AND REPLACED LT FLUX DETECTOR UNIT IAW MM 34-21-04. DEGAUSSED WINGS AND LANDING GEAR.Dec 2, 2002 · N405SW · Cndair CL6002B19 · Directional Gyro and Indicating SystemSDR CA021217008Gate · out of rig(CAN) CABIN CLIMBED UNCONTROLLABLY IN AUTO AND MANUAL MODES. REPAIRED AND RIGGED THE PASSENGER DOOR GATE IAW CRJ MM TASK 52-11-15-820-801.OPERATIONAL CHECK OF PRESSURE SYSTEM IAW 21-31-00-710-801 GOODNov 28, 2002 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA030417007Bushing · loose(CAN) MIGRATING BUSHINGS ON WING ATTACHMENT FITTINGS.Nov 22, 2002 · Cndair CL6002B19 · Wing, Fuselage Attach FittingsSDR CA030329001Carbon Seal · leaking(CAN) 15 MINUTES INTO THE FLT, THE RT ENGINE OIL PRESSURE BEGAN TO FLUCTUATE BETWEEN 25 & 33 PSI FOR FIVE MINUTES (STABLE OIL TEMPERATURE WAS NOTED). THE OIL PRESSURE SLOWLY BEGAN TO DECREASE BELOW 25 PSI, WHEREBY THE FLIGHT CREW INITIATED AN IN-FLIGHT SHUT DONov 16, 2002 · Cndair CL6002B19 · Turbine Engine Accessory DriveSDR CA021114003Windshield · cracked(CAN) RT WINDSHIELD CRACKED DURING CRUISE. A/C DIVERTED WHERE THE WINDSHIELD WAS REPLACED REPLACEMENT WINDSHIELD.Nov 12, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA200211437Windshield · failedRT WINDSHIELD FAILED (OUTER PANEL SHATTERED) DURING CLIMBOUT. REMOVED AND REPLACED RT SIDE WINDSHIELD IAW RJ MM 56-11-01.Nov 6, 2002 · N440SW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA200211512Support Angle · crackedFS 621 LEFT FLOOR SUPPORT ANGLE CRACKED. FOUND DURING C CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-117 REV. ''A''. ANGLE P/N: 601R53-61-117-1.Nov 5, 2002 · N427SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200211361Pdu · failedFLAPS FAILED MESSAGE IN FLIGHT. REMOVED AND REPLACED PDU FOR FLAPS. OPS CHECKS GOOD IAW 27-52-01.Oct 24, 2002 · N441SW · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CA021022002Engine · leaking(CAN) 'FLIGHT RETURN DUE TO SMOKE IN CABIN' PASSENGERS DISEMBARKED ON THE RUNWAY AND PARAMEDICS CALLED. FOUND RT DUCTS AND WATER SEPARATOR HOUSING STILL REQUIRED SOME CLEANING. REPLACED RIGHT WATER SEPARATOR SOCK AND CLEANED DUCTS BETWEEN ACM & SEPARATOR. INOct 18, 2002 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR MASA200200030Engine · failedAIRSHUTTLE 6017 FROM PHX TO FAT DECLARED AN EMERGENCY WHEN CREW RECEIVED RT ENGINE OIL PRESSURE WARNING IN FLIGHT. A/C RETURNED BACK TO PHX. MX WILL BE REPLACING THE ENGINE.Oct 17, 2002 · N87353 · Cndair CL6002B19 · Engine Oil PressureSDR CA021009001Windshield · failed(CAN) CREW REPORTED THE LEFT WINDSHIELD SHATTERED WHILE AIRCRAFT WAS ON GROUND, AT GATE.MAINTENANCE SENT TEAM TO ELP. REMOVED AND REPLACED THE LT WINDSHIELD. TSN/CSN/TSO AIRCRAFT HOURS: 11621.9 AIRCRAFT CYCLES: 10677 COMPONENT DATA THE SAME. DATA I HAVE INDICAOct 8, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA200211285Oil System · lowRECEIVED AN IDG MESSAGE ON TAKEOFF AND ABORTED. RESET CB 1NS, 2N8, 4A2, 4A3, MESSAGE CLEARED. GOT THE IDG MESSAGE AGAIN AND ABORTED TAKEOFF. FOUND THE NR 1 IDG HAD NO OIL. SERVICED OIL TO PROPER LEVEL AND RECONNECTED IDG. OPS CHECK AND LEAK CHECK GOOD.Oct 6, 2002 · N917SW · Cndair CL6002B19 · AC Generator-AlternatorSDR CA021125004Engine · failed(CAN) WHILE ADVANCING POWER LEVERS (APPROXIMATELY 50 PERCENT N1 ONLY) TO INITIATE T/O ROLL, FLIGHT CREW NOTICED A HOT ICON AND EXCESSIVE ITT READINGS ON THE RT ENGINE. CONTRACT MAINTENANCE LOOKED AT THE MDC EXCEEDENCE PAGE AND REPORTED THE RT ENGINE EXPERIENCEOct 6, 2002 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA200211305Trim Switch · inoperativeAILERON SWITCH INOP. REMOVED AND REPLACED AILERON TRIM SWITCH. OPERATED AILERON TRIM. OPS CHECK GOOD.Oct 4, 2002 · N431SW · Cndair CL6002B19 · Aileron Control SystemSDR REX02020O-Ring · cutENROUTE, IN CRUISE CONFIGURATION AT FL290, AT A POSITION 80 MILES NORTH, THE RT ENG OIL PRESSURE BEGAN TO FLUCTUATE BETWEEN 28 AND 42 PSI, FOLLOWED BY INTERMITTENT ILLUMINATION OF LOW OIL PRESSURE WARNING. FLIGHT CREW DECLARED EMERGENCY AND SHUT DOWN THE ENGISep 29, 2002 · N8506C · Cndair CL6002B19 · Engine Oil CoolerSDR CA021009002Carbon Seal · leaking(CAN) SMOKE IN COCKPIT IMMEDIATELY AFTER TAKEOFF. MOSTLY COMING FROM CAPTAIN'S VENT. DONNED O2 MASKS. SMOKE LAV MESSAGE FOLLOWED. PERFORMED EMERGENCY PROCEDURE. FA NOTICED SMOKE IN CABIN AS WELL.NO FIRE IN LAV. PERFORMED EVACUATION AT GATE.LANDED OVERWEISep 29, 2002 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR SWIA200211265Ecu · malfunctionedSPOILERON FAULT STATUS MESSAGE. REMOVED NR 1 & NR 2 SECU'S AND REPLACED WITH SERVICEABLE ONES IAW CL600 MM 27-61-05. REMOVED LEFT INBOARD FLIGHT SPOILER PCU & REPLACED WITH SERVICEABLE ONE IAW CL600 MM 27-62-01. OPS CHECKS GOOD.Sep 26, 2002 · N432SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200211260Bpsu · failedFLAPS FAIL MESSAGE DURING CLIMBOUT. RETURNED TO FIELD. RIGHT BPSU REMOVED DUE TO FLAPS FAIL MSG. INSTALLED A SERVICEABLE BPSU IAW CRJ MM 27-51-10.Sep 24, 2002 · N441SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200211255Amplifier · malfunctionedAFTER ESTABLISHING CLIMB POWER AFTER DEPARTURE FROM FAT, RIGHT SIDE N1 FLUCTUATIONS OF +/- 10 PERCENT AND FUEL FLOW OF +/- 500 PPH CAUSED A/C TO YAW UP TO 20K FT. REDUCED POWER AND RIGHT ENGINE STABILIZED. NO FURTHER FLUCTUATIONS WERE OBSERVED. RETURNED TO Sep 22, 2002 · N918SW · Cndair CL6002B19 · Fuel Controlling SystemSDR SWIA200211240Trim Switch · malfunctionedAFTER RUNNING A GOOD STAB & MACH TRIM TEST, STAB CH 1 DROPPED OFF LINE FOR NO APPARENT REASON AND WOULD NOT REENGAGE. POWERED DOWN A/C AND POWERED UP. NO DEFECTS NOTED AT THIS TIME. REPLACED CAPT'S TRIM SWITCH DUE TO PREVIOUS DISCREPANCIES. HSTC SYSTEM OPSep 20, 2002 · N910SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200211231Warning System · malfunctionedDURING TAKEOFF ROLL, CONFIG TRIM THEN CONFIG SPOILERS WARNING ILLUMINATED. ABORTED TAKEOFF. RESET SPOILER SYSTEM, VERIFIED AILERON TRIM AT NEUTRAL.Sep 15, 2002 · N426SW · Cndair CL6002B19 · Central WarningSDR CA021008001Tire · failed(CAN) AT APPROXIMATELY VR, HEARD AND FELT A LOUD BANG IN THE NOSE AREA. DURING CLIMB CALLED TOWER AND ASKED TO CHECK THE RUNWAY. SENT AN INSPECTION VEHICLE OUT AND FOUND TIRE REMENANTS. NOTIFIED THE F/A AND PAX. ASKED THE EMERGENCY EQUIMPMENT STANDING BYSep 15, 2002 · Cndair CL6002B19 · TireSDR CA030329002Brace · unsecure(CAN) FLT CREW REPORTED THAT THE NR 1 THRUST LEVER JAMMED AT 90 PERCENT THRUST AND WERE UNABLE TO REDUCE POWER. LT ENGINE HAD TO BE SHUT DOWN USING FIRE PUSH SWITCH. AIRCRAFT LANDED IN ORLANDO WITHOUT INCIDENTMAINTENANCE FOUND THAT THE UPPER CORE COWL HOLD OPSep 15, 2002 · Cndair CL6002B19 · Engine Thrust ReverserSDR SWIA200211364Frame · crackedFUSE FRAME AT FS 640.0 IS CRACKED AT STR 9 CUTOUT. FOUND DURING C CHECK INSPECTION, HFEC INSPECTION CARRIED OUT ON CUTOUT EDGE AND AREA AS REQUIRED IAW REO 601R-53-61-532. NO CRACKS FOUND. REPAIRED FRAME IAW CRJ REO 601R-53-61-532 REV NC.Sep 12, 2002 · N405SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA200211365Frame · crackedFUSE FRAME AT FS 718 CRACKED ON RIGHT SIDE AT STR 11. FOUND DURING C-CHECK INSPECTION, HFEC INSPECTION CARRIED OUT ON CUTOUT REPAIR EDGE AND AREA AS REQUESTED IAW RJ NDTM 51-20-01. NO CRACKS FOUND. REPAIRED FRAME IAW CRJ REO 601R-53-61-193 REV A ANGLE.Sep 12, 2002 · N405SW · Cndair CL6002B19 · Fuselage Main, Frame
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