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 CA020925001Pdu · failed(CAN) FLAP FAIL MESSAGE FOUND ON EICAS INTEROGATION CHECK ( FOUND ON ACCOMPLISHMENT OF SERVICE CHECK.)DURING TEST FOUND PDU2 C/B POPPING AND FLAPS HALF SPEED . PDU REPLACED AS PER AMMSep 22, 2002 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CA020923003Control Unit · failed(CAN) 'FLAP FAIL ' MESSAGE ON EICAS IN CRUISE FECU CHANGED AND TESTED AS PER AMMSep 20, 2002 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA020923002Engine · failed(CAN) AIRCRAFT 7134 TAT, 15090.5HRS.FLIGHT 5895 FROM CVG TO ROA 'AT APPROX 1500-2000 FT IN CLIMB THERE WAS A LOUD BOOM & YAW FROM THE LT SIDE OF AIRCRAFT. NR 1 ENG ITT WAS 980+. THOUGHT THE ENGINE HAD BEEN DAMAGED & SHUT IT DOWN AFTER 30 SECS. EVERYTHING ELSSep 19, 2002 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA0260539Engine · blownFLIGHT 5895 - LOUD BOOM AND YAW LEFT - LEFT ENGINE ITT 980+. IFSD.REPLACED THE LEFT ENGINE.Sep 18, 2002 · N967CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA020918002Handle · corroded(CAN) UPON INSPECTION MECHANIC FOUND OUTER HANDLE OF CREW ESCAPE HATCH STUCK IN THE DOWN POSITION. REMOVED AND REPLACED CORRODED HANDLE.Sep 17, 2002 · Cndair CL6002B19 · Emergency ExitsSDR CA020920002Actuator · malfunctioned(CAN) WHEN FLAPS 450 SELECTED A/C ROLLS LT HALFWAY OF RT, AILERON TRIM NEEDED TO LEVEL WINGS, LT FLAPINDICATION JUMPS 400 TO 450 REPLACED RT NR 1 ACTUATOR , FLEXSHAFT ON INBD FLAP AND LT POS TRANSMITTER, PERFORMED RIGGING OF AILERON SYS AND FLAP SYSTEM, OPS NOSep 17, 2002 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA020917008Handle · corroded(CAN) ON INSPECTION, MECHANIC FOUND OUTER HANDLE OF CREW ESCAPE HATCH STUCK IN THE DOWN POSITION. WOULD NOT POP UP WHEN BUTTON IS DEPRESSED. UNABLE TO RELEASE HANDLE EVEN WHEN FORCED. REMOVED HANDLE ASSEMBLY AND INSTALLED NEW ASSEMBLY.Sep 15, 2002 · Cndair CL6002B19 · Emergency ExitsSDR CA020916001Hydraulic System · contaminated(CAN) DURING APPROACH, NLG DID NOT EXTEND. ALT EXTENSION ATTEMPTED APPROX SIX TIMES WITHOUT SUCCESS. AN EMERGENCY WAS DECLARED AND LANDING PERFORMED WITH THE NLG RETRACTED. NO INJURIES REPORTED. NLG WAS EXTENDED WHERE THE A/C STOPPED AND WAS TOWED TO A HANGASep 14, 2002 · Cndair CL6002B19 · Nose/Tail Landing GearSDR CA020918001Fan · failed(CAN) SMOKE ODOR IN COCKPIT, REPORTED BY FLIGHT CREW. DISPLAY FAN NR 2 FOUND UNSERVICEABLE. CIRCUIT BREAKER PULLED AND AIRCRAFT RETURNED TO BASE UNDER MEL. DISPLAY FAN NR 2 REPLACED IN ACCORDANCE WITH AMM.Sep 12, 2002 · Cndair CL6002B19 · Central ComputersSDR CA020910002Window · cracked(CAN) LT SIDE WINDOW CRACKED. DIVERTED FLIGHT, LT WINDOW REPLACED AS PER AMM.Sep 8, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020912005Window · cracked(CAN) DURING APPROACH, LT SIDE WINDOW CRACKED. LT SIDE WINDOW REPLACED IN ACCORDANCE WITH AMMSep 6, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020910001Window · cracked(CAN) DURING FLIGHT, LT SIDE WINDOW CRACKED. DIVERTED FLIGHT. LT SIDE WINDOW REPLACED IN ACCORDANCE WITH AMM.Sep 5, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020903008Selector Valve · failed(CAN) GEAR DISAGREE UPON SELECTION OF GEAR HANDLE DOWN NOSE GEAR DID NOT DROP, NOSE DOOR DID NOT OPEN, RECYCLED HANDLE WITH NO SUCCESS AS PER QRH, MANUAL EXTENSION CARRIED OUT WITH NO FURTHER INCIDENT.Aug 29, 2002 · Cndair CL6002B19 · Landing Gear SelectorSDR CA020821005Handle · out of adjust(CAN) PASSENGER DOOR WOULD NOT OPEN. ( SECOND OCCURANCE IN TWO WEEKS). DOOR HANDLE LOADS FOUND HIGH. INNER HANDLE TENSION ADJUSTED. UPPER PIVOTS FOUND GOING SLIGHTLY OVER CENTER. UPPER STOP BOLT ADJUSTED. LATCH CAM TORQUE TUBE ROD SHORTENED TO ACHIEVE ALIGNAug 19, 2002 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA020826005Window · failed(CAN) 1ST OFFICER`S SIDE WINDOW SHATTERED AT FL 330 PRIOR TO DECENT, LATER HEAT AND CAUTION MESSAGE ILLUMINATED. CABIN PRESS/ALT NORMAL AND QRH PROCEDURES CARRIED OUT. F/O'S SIDE WINDOW REPLACED AND LEAK CHECKED AS PER AMM.Aug 19, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA0260472Carbon Seal · wornFLIGHT 5542 LEFT ENGINE LOW OIL PRESSURE WARNING.REPLACED THE #6 BEARING CARBON SEAL.Aug 5, 2002 · N963CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA020806006Bpsu · failed(CAN) FLAP FAILED AT 8 DEGREES. LT AND RT BPSU REPLACED AND ADJUSTED AS PER AMM 27-51-10Aug 5, 2002 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA020820001Mixer Box · contaminated(CAN) WHILE EN-ROUTE AT 29,000 FT, THE FLIGHT CREW EXPERIENCED AILERON CONTROL LOCKUP. A/P TRIM CAUTION MSG. AIRCRAFT DESCENDED TO 15,000 FT FOR 5 MIN. CONTROL RETURNED. AIRCRAFT CONTINUED TO DESTINATION WITHOUT INCIDENT. AIRCRAFT TOOK OFF IN HEAVY RAIN ANDAug 5, 2002 · Cndair CL6002B19 · Aileron Control SystemSDR CA020827005Mixer Box · stiff(CAN) WHILE EN-ROUTE THE FLIGHT CREW EXPERIENCED AILERON CONTROL STIFFNESS & JAM. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT TOOK OFF IN HEAVY RAIN AND STANDING WATER ON THE RUNWAY. LT AILERON CABLE SYSTEM WAS INSPECTEAug 5, 2002 · Cndair CL6002B19 · Aileron Control SystemSDR CA020806005Fan · failed(CAN) AFTER T/O STRONG ACRID SMELL ON THE FLIGHT DECK, SIMILAR TO ELECTRICAL BURNING. SOURCE OF ODOR WAS NOT LOCATED BUT LIMITED TO THE FLIGHT DECK. ODOR WAS SUSTAINED. GALLEY EXHAUST FAN CHANGED, AIRCRAFT GROUND. RUN AND PNEUMATICS CHECKED SERVICEABLE.Aug 2, 2002 · Cndair CL6002B19 · Air Distribution FanSDR CA020802004Acm · seized(CAN) COCKPIT PACK TEMP STARTED CLIMBING UNCONTROLLABLY IN AUTOMATIC AND MANUAL MODE. PACK PSI NORMAL. FAULT TRACED TO SEIZED AIR CYCLE MACHINE. ACM REPLACED.Jul 31, 2002 · Cndair CL6002B19 · Cabin Cooling SystemSDR CA020809001Control Cable · frozen(CAN) PILOT REPORTED THAT THE AILERON TRIM MESSAGE WAS DISPLAYED ON EICAS WHILE IN CRUISE AND THAT AILERONS WERE VERY STIFF. AIRCRAFT DECENDED TO A LOWER ALTITUDE AND PROBLEM CLEARED. CREW REPORTED THAT THERE WAS HEAVY RAIN ON TAKE OFF. AIRCRAFT LANDED WITHOJul 25, 2002 · Cndair CL6002B19 · Aileron Control SystemSDR CA020725005Plunger · unserviceable(CAN) DURING THE VALIDATION OF AMM TASK 24-23-01-720-803 IAW BOMBARDIER ENGINEERING TDS 601R-0566, WE DAMAGE THE ADG BACK PLATE AND BLADE LOCK PLUNGER OCCURRED. THE DAMAGE OF THE ADG WAS CAUSED BY AN IMPROPERLY CRIMPED LOCK TABFROM THE FACTORYLOCATED BETWEEN TJul 19, 2002 · Cndair CL6002B19 · AC Generation SystemSDR CA020820008Windshield · cracked(CAN) RT WINDSHIELD OUTER PLY CRACKED DURING TAXI. A/C RETURNED TO BLOCKS. WINDSHIELD REPLACED. WINDSHIELD HAD BEEN INSTALLED SINCE NEW.Jul 17, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020718002Handle · corroded(CAN) DURING A C CHECK INSPECTION WHILE PERFORMING THE CREW ESCAPE HATCH FUNCTIONAL CHECK, THE HANDLE WAS HARD TO UNLATCH.THE ASSEMBLY WAS REMOVED AND LIGHT CORROSION WAS FOUND ON THE SHAFT.THE LIGHT CORROSION ON THE SHAFT WAS REMOVED, THE HANDLE WAS REINSTALLJul 12, 2002 · Cndair CL6002B19 · Emergency ExitsSDR CA020715011Handle · corroded(CAN) DURING A C CHECK INSPECTION WHILE PERFORMING THE CREW ESCAPE HATCH FUNCTIONAL CHECK, MAINTENANCE WERE UNABLE TO OPEN THE HATCH USING THE EXTERNAL HANDLE. THE HANDLE WOULD NOT UNLATCH WHEN THE EXTERNAL TRIGGER WAS PUSHED.FURTHER VERIFICATION ON THE BENCH Jul 6, 2002 · Cndair CL6002B19 · Emergency ExitsSDR CA020819001Shutoff Valve · failed(CAN) RIGHT 14TH STAGE DUCT WARNING MESSAGE APPEARED DURING FLIGHT. QRH PROCEDURE APPLIED AND RETURNED TO DEPARTURE AIRPORT. RIGHT 14TH STAGE SOV REPLACED.Jul 6, 2002 · Cndair CL6002B19 · Engine Bleed Air SystemSDR CA030417006Bushing · loose(CAN) MIGRATING BUSHINGS ON WING ATTACHMENT FITTINGS.Jun 25, 2002 · Cndair CL6002B19 · Wing, Fuselage Attach FittingsSDR COMA0260381Pump · leakingFLIGHT 5322 IFSD LEFT ENGINE DUE TO LOW OIL PRESSURE.REPLACED THE LUBE SCAVANGE OIL PUMP.Jun 18, 2002 · N916CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA020709001Check Valve · failed(CAN) RT ENGINE STAGNED AT APPROX. 30 PERCENT DUE TO THE LT ENGINE 10 STAGE CHECK VALVE FLAPPER BROKEN. THE LT VALVE WAS REPLACED, INSPECTION WAS PERFORMED ON THE DUCTS, STARTER VALVES AND ENGINE RUNJun 18, 2002 · Cndair CL6002B19 · Engine Start Valves/ControlsSDR CA020726010Actuator · failed(CAN) MACH AND STAB TRIM MESSAGE ON CLIMB, PROCEDED WITH STAB TRIM 1 INOPERATIVE, FAULT DISAPEARED, AUTOPILOT ENGAGED, FLT CREW DISENGAGED A/P AT 10,000 FT, FOR MANUAL LANDING, EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. REPLACED HORIZONTAL STAB TRIM ACJun 17, 2002 · Cndair CL6002B19 · Stabilizer ActuatorSDR CA020726002Line · punctured(CAN) IN FLIGHT, LOST NUMBER ONE HYDRAULIC PRESSUE AND QUANTITY. FOUND NUMBER ONE PUMP PRESSURE LINE PUNCTURED. LINE REPLACED AND PUMP MPN 887055,OPERATION CHECKED NORMALJun 15, 2002 · Cndair CL6002B19 · Hydraulic System, MainSDR CA020610006Control Unit · lack of lube(CAN) AUTOPILOT TRIM RWD/LWD AFTER T/O AUTO PILOT DISCONNECTED AND FOUND DIFFICULT TO MOVE AILERONS.(L1255080) BOTH LT AND RT AILERON QUADRANTS LUBRICATED WITH BRAYCO NR 300 TO DISPLACE MOISTURE AND AILERON INSPECTION CHECK CARRIED OUT. OPS CHKS NORMAL SERVICEJun 7, 2002 · Cndair CL6002B19 · Aileron Control SystemSDR CA020606001Window · cracked(CAN) LT (CAPTAINS) FRONT WINSHIELD CRACKED DURING DESCENT (L1261423)LT WINSHIELD REPLACED AS PER AMM 56-10-01-400Jun 6, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA0260356Seal · leakingFLIGHT 5570 R/H ENGINE LOW OIL PRESSURE WARNING.REPLACED THE ACCESSORY GEAR BOX DRIVE SEALS AT AXIS D,F,&BB.Jun 5, 2002 · N958CA · Cndair CL6002B19 · Engine Oil Indicating SystemSDR CA020725007Windshield · cracked(CAN) CAPTAIN,S WINDSHIELD CRACKED ON DESCENT. WINDSHIELD REPLACEDJun 4, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA0260351Thermocouple · faultyFLIGHT 5640 LT ENG ITT HOT WARNING - ITT FLUCTUATED FROM NORMAL TO OVER 900 DEGREES.REPLACED THE LOW PRESSURE TURBINE ASSY DUE TO DEFECTIVE THERMOCOUPLE ASSY.Jun 2, 2002 · N964CA · Cndair CL6002B19 · Engine Temperature Indicating SystemSDR COMA0260344Engine · failedFLIGHT 5376 R/H ENGINE OIL PRESSURE WARNING - FAILED BY ENGINE FAILURE.REPLACED R/H ENGINE.May 30, 2002 · N713CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA020610001Engine · malfunctioned(CAN) AT FL270 RECEIVED A RT ENGINE OIL PRESSURE MESSAGE. ENGINE ROLLED BACK. PER QRH - ENGINE UNABLE TO START. SECURED ENGINE AND ACCOMPLISHED A SINGLE ENGINE LANDING. ON POST FLIGHT INSPECTION OBSERVED RT ENGINE CHIP DETECTOR LIGHT ON. VERBALLY REPORTEDMay 30, 2002 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA020822007Actuator · failed(CAN) FLAP FAIL MSG DURING EXTENSION ON DESCENT. FLAPS SHOWED 20 DEG. NO EMERGENCY DECLARED AND LANDED AT GRR. RT NR 3 ACTUATOR FAILED AND FLAP SURFACE TWISTED BADLY. ROAD TRIP SET UP AND MECHANICS DESPATCHED WITH PARTS. PARTS REPLACED IAW AMM. A/C RETURNMay 30, 2002 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CA020604004Line · failed(CAN) HYDRAULIC NR 1 LOW PRESSURE AND QUANTITY "0". HYDRAULIC PUMP RAN DRY FOR 3 MIN. HYDRAULIC RETURN LINE FOR PRESSURE MANIFOLD FOUND LEAKING. NR 1 ENGINE HYDRAULIC PUMP CHANGED AS PER 29-11-01-400-801, HYDRAULIC LINE REPLACED PER STANDARD PRACTICES 20-22-0May 29, 2002 · Cndair CL6002B19 · Hydraulic System, MainSDR CA020725002Line · failed(CAN) LOSS OF SYS 1 HYDRAULIC FLUID DURING FLIGHT. PIN HOLE FOUND ON PUMP RETURN LINE. RETURN LINE REPLACEDMay 29, 2002 · Cndair CL6002B19 · Hydraulic System, MainSDR CA030505001Window · failed(CAN) LT SIDE WINDOW SHATTERED IN FLIGHT. AIRCRAFT LANDED IN CINCINNATI WITHOUT FURTHER INCIDENT.WINDOW REPLACED, AIRCRAFT RETURNED TO SERVICE.May 29, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020530013Bearing · failed(CAN) SEVERE NOSE SHIMMY ON TAKE-OFF. (VIBRATION) (L1159330) LT AND RT NOSE WHEEL ASSY'S REPLACED AND WHILE REPLACING RT WHEEL DAMAGE FOUND ON AXLE DUE TO BEARING FAILURE. NOSE LANDING GEAR ASSY. REPLACED AS PER MM 32-21-01-000-400, PG. 401.May 25, 2002 · Cndair CL6002B19 · TireSDR CA020529002Pressure Panel · cracked(CAN) DURING THE FLEET LEADER STRUCTURAL INSPECTION, THE INSPECTION REVEALED FOUR CRACKS TO THE PRESSURE FLOOR AT FS 460.00, RBL 9.00 TO CENTER LINE AND LBL 9.00 TO CENTER LINE. AIRCARFT IS REPAIR PER REO 601R-53-41-090May 24, 2002 · Cndair CL6002B19 · Fuselage Floor PanelSDR COMA0260320EngineFLIGHT 5740 DURING LANDING APPROACH INTO AZO THE AIRCRAFT ENCOUNTERED A LIGHTNING STRIKE RESULTING IN FLAMING OUT THE #1 ENGINE.PERFORMED A LIGHTNING STRIKE INSPECTION, REPAIRED MINOR AIRFRAME SKIN BURN MARKS AND PERFORMED SUCCESSFUL ENGINE RUNS.May 19, 2002 · N451CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA020523003Control Cable · dirty(CAN) CLIMBING THROUGH 23000 FT THE AILERONS BECAME STIFF AT -22C . AUTOPILOT MANUALLY DISCONNECTED . AILERON TRIM MOVED BUT YOKE DID NOT. CONTROL RETURNED AT 20000 FT AND +4C . AIRCRAFT LANDED WITHOUT INCIDENT. LT & RT TENSION REGULATORS INSPECTED FOR MOISTURMay 18, 2002 · Cndair CL6002B19 · Aileron Control SystemSDR CA020524005Window · cracked(CAN) LT WINDOW CRACKED DURING FLIGHT. DIVERTED FLIGHT. LEFT SIDE WINDOW REPLACED.May 17, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020516002Windshield · cracked(CAN) RIGHT WINDSCREEN CRACKED WHILE ON THE GROUND. REPLACED FIRST OFFICERS WINDSHIELD IAW 56-11-01. OPS CHECK GOOD.May 15, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020502020Mfc · failed(CAN) IN CRUISE AT FL340, A LOUD SOUND WAS HEARD FOLLOWED BY THE RT ENGINE SHUTTING DOWN. NO INFLIGHT IGNITION ATTEMPTED. AIRCRAFT PERFORMED A SINGLE ENGINE LANDING. SENSOR TEMPERATURE INLET COMPRESSOR P/N 4071T72P01 S/N WYG86492 REPLACED. ENGINE RUN PERFOMEDApr 15, 2002 · Cndair CL6002B19 · Fuel Control/Turbine Engines
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