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 CA020502008Control Cable · failed(CAN) FLAPS FAIL MESSAGE ON EICAS AFTER TAKEOFF WITH FLAPS SELECTED AT 8, AIR TURN BACK. REPLACED FLEX CABLE ACTUATOR BETWEEN NR 1 AND 2 ACTUATORS ON THE LT SIDE.Apr 13, 2002 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA020502007Apu · failed(CAN) AIR TURN BACK, AIRCRAFT CABIN FILLED WITH SMOKE, RETURN TO ST-LOUIS. AIRCRAFT DEPARTED WITH THE APU UNDER MEL DUE TO LOW OIL QUANTITY & APU SHUTDOWN (APU FAILURE) OIL FROM THE APU WENT IN THE LT PACK CAUSING THE SMOKE. REPLACED THE APU AND THE PACK.Apr 11, 2002 · Cndair CL6002B19 · APU Oil SystemSDR COMA0260245Igniter · inoperativeFLIGHT 5877 LEFT ENGINE IGNITION STATUS MESSAGE.REPALCED THE ENGINE IGNITERS.Apr 10, 2002 · N952CA · Cndair CL6002B19 · Spark Plug/IgniterSDR CA020502009Computer · failed(CAN) STALL FAIL CAUTION MESSAGE SHORTLY AFTER TAKEOFF, QRH PROCEDURE APPLIED WITHOUT SUCCESS - MESSAGE DID NOT CLEAR. FOUND TO BE THE STALL PROTECT COMPUTER AT FAULT. REPLACED COMPUTER, SYSTEM CHECK SERVICEABLE.Apr 3, 2002 · Cndair CL6002B19 · Stall Warning SystemSDR CA020528001O-Ring · damaged(CAN) DURING APPROACH, MESSAGE RT ENG OIL PRESS (W) ALONG WITH RED PRESSURE INDICATION ON EICAS. RT ENGINE WAS SHUT DOWN AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE NOTICE AN HYDRAULIC LEAK COMING FROM THE ENGINE OIL AND SCAVENGE PUMP FLANGE. THE PUMP O'RINGMar 30, 2002 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA020502006Spring · failed(CAN) CARGO DOOR OPEN INDICATION ON EICAS DURING CLIMB, NO PRESSURIZATION FAULTS. FLIGHT CREW ELECTED TO TURN BACK. FOUND TO BE THE DOOR LATCH MECHANISM AT FAULT. REPLACED ON SPRING SPACER AND PIN AFFECTED. SPRING MPN 601-35082-1SPACER P/N NAS43DD4-18PIN P/Mar 29, 2002 · Cndair CL6002B19 · Cargo/Baggage DoorsSDR CA020328007Switch · failed(CAN) STABILIZER TRIM AND MACH TRIM TRIPPED OFF IN FLIGHT, WOULD NOT RE-ENGAGE. REPLACED CAPTAINS STAB TRIM DISCONNECT SWITCH, FUNCTIONAL TEST CARRIED OUT. AIRCRAFT FOUND SERVICEABLE.Mar 16, 2002 · Cndair CL6002B19 · Stabilizer ActuatorSDR CA020328006Bpsu · failed(CAN) AT 180 KIAS AND HAVING BEEN AT FLAP 8 FOR 2-3 MINUTES. CREW SELECTED FLAP 20 AND IMMEDIATELY "FLAP FAIL" CAUTION MESSAGE ILLUMINATED. FLIGHT CONTROL PAGE SHOWED LEFT FLAP 8 AND RIGHT FLAP 10. TOUCH DOWN SPEED APPROXIMATELY 175 IAS. LEFT BPSU AND LEFT NR Mar 11, 2002 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA020315003Selector Valve · failed(CAN) GEAR DISAGREE LIGHT ON AFTER TAKEOFF FROM LAGUARDIA. NOSE GEAR AND DOOR REMAINED DOWN AND LOCKED. AIRCRAFT CONTINUE TO OTTAWA WITH GEAR DOWN. NOSE GEAR DOOR SELECTOR VALVE REPLACED. MAIN AND NOSE GEARS RETRACTION AND EXTENSION CARRIED OUT SEVERAL TIMES. Mar 6, 2002 · Cndair CL6002B19 · Landing Gear SelectorSDR CA020301002Windshield · cracked(CAN) LEFT WINDSHIELD CRACKED DURING DESCENT. REMOVED AND REPLACED WINDSHIELD.Mar 1, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020301001Engine · failed(CAN) A/C 7216, FLT 5266 FROM ATW TO CVG. PRELIM INFO.AT 3000 FEET IN CLIMB RIGHT ENGINE SHUTDOWN DUE TO VIBRATION. RETURNED TO ATW. AFT END (LPTM) OF NR 2 ENGINE MISSING. RIGHT HORIZ STAB L/E DAMAGED. VERTICAL STAB APPARENTLY HAS A SMALL HOLE. NO CONFIRMATIONFeb 28, 2002 · Cndair CL6002B19 · Turbine SectionSDR COMA0260127Engine · failedFLIGHT 5266 - DURING CLIMBOUT OF ATW RECEIVED ABNORMAL VIBRATION FROM THE RIGHT ENGINE. CREW DECLARED AN EMERGENCY AND PERFORMED AN IFSD. REPLACED THE RIGHT ENGINE ASSY.Feb 27, 2002 · N991CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA020222002Switch · failed(CAN) AFTER TAKEOFF STAB TRIM CAUTION MESSAGE POSTED. RE-ENGAGEMENT NOT POSSIBLE. RETURNED TO BASE. LT STAB TRIM DISCONNECT SWITCH SUSPECTED, CONFIRMED BY MDC. SWITCH REPLACED.Feb 22, 2002 · Cndair CL6002B19 · Elevator Tab Control SystemSDR CA020308011Rod · broken(CAN) AIRCRAFT NOT PRESSURIZING ON CLIMB OUT. FLIGHT DIVERTED WITH OVERWEIGHT LANDING. FOUND MAIN PASSENGER DOOR PRESSURE VALVE PUSHROD BROKEN. PUSHROD REPLACED AND RIGGED. PRESSURIZATION CHECK AND OVERWEIGHT LANDING CHECK CARRIED OUT AS PER AMM 05-51-01.NO FAFeb 22, 2002 · Cndair CL6002B19 · Pressure Regulator/Outflow ValveSDR CA020221015Access Panel · cracked(CAN) WHILE PERFORMING SCHEDULED MAINTENANCE, TASK CARD 002-57-510/610-603, A CRACK WAS FOUND ON ONE OF THE FUEL BOOST PUMP ACCESS SCREW HOLES.Feb 20, 2002 · Cndair CL6002B19 · Wing, Plate/SkinSDR CA020221010Aileron · frozen(CAN) "AT 24,000 FEET DURING CLIMB LEFT AILERON CONTROL FROZE - LIGHT PRESS UNSTUCK CONTROL". VERBAL REPORT FROM PILOT STATES: "PUDDLES OF WATER ON TAXI/RWY WHEN LEAVING MEMPHIS. DID NOT HAVE CONTROL OF AILERON AT 24,000 FEET & MINUS 20 DEG C. DISCONNECTED AILFeb 19, 2002 · Cndair CL6002B19 · Aileron Control SystemSDR CA020221007Gearbox · failed(CAN) RT REV ICON ON N1 GUAGE AND REV UNSAFE CAUTION MESSAGE APPEARED AFTER TAKEOFF. RT ENGINE THROTTLE GEARBOX ASSEMBLY REMOVED AND REPLACED. AIRCRAFT BACK IN SERVICE.Feb 14, 2002 · Cndair CL6002B19 · Power LeverSDR CA020228008Window · cracked(CAN) DURING FLIGHT L-2 WINDOW DEVELOPED A CRACK. CAPTAINS SIDE WINDOW REPLACED AS PER AIRCRAFT MAINTENANCE MANUAL 56-12-01.Feb 14, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA030417005Bushing · loose(CAN) MIGRATING BUSHINGS ON WING ATTACHMENT FITTINGS.Feb 8, 2002 · Cndair CL6002B19 · Wing, Fuselage Attach FittingsSDR CA020228010Pcu · failed(CAN) FLIGHT SPOILER CAUTION MESSAGE CAME ON DURING APPROACH. WENT OUT AFTER LANDING. INTERMITTENT PROBLEM THAT OCCURRED SEVERAL TIME IN RECENT PAST. SECU (SPOILER ELECTRONIC CONTROL UNIT) NR 1 FAULT CODES 02,51,E8 DISPLAYED. SECU NR 2 FAULT CODES EC,52,EA DIFeb 5, 2002 · Cndair CL6002B19 · Drag Control SystemSDR CA020228009Spoiler · failed(CAN) SPOILER FAULT EICAS INDICATES LEFT OUTBOARD SPOILER PROBLEM (WHITE BOX).SEVERAL PREVIOUS SNAGS OCCURRED WITH SYSTEM CHECKED OUT AND NO FAULTS FOUND (INTERMITTENT FAULT). WIRING CHECKED OUT NO FAULT FOUND.FLIGHT SPOILER CONTROL LEVER HANDLE REPLACED.Feb 4, 2002 · Cndair CL6002B19 · Drag Control SystemSDR CA020211002Windshield · cracked(CAN) RT WINDSHIELD CRACKED DURING GROUND HANDLING. REMOVED AND REPLACED WINDSHIELD.Feb 1, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020211005Windshield · cracked(CAN) DURING FLIGHT, IN CRUISE AT FL350, THE MIDDLE PLY OF THE LT WINDSHIELD CRACKED. PILOTS APPLIED QRH EMERGENCY PROCEDURE AND THE FLIGHT WAS DIVERTED. AIRCRAFT LANDED SAFELY.Feb 1, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020211003Carbon Seal · damaged(CAN) AIRCRAFT TAT:4900.3 FLIGHT 5589 FROM CVG TO MKE.R. ENGINE LOW OIL PRESSURE WARNING IN FLIGHT. PERFORMED QRH. R. ENGINE TO IDLE, MSG WOULD NOT CLEAR. SHUT ENGINE DOWN. ENGINE OIL PSI FLUCTUATES BETWEEN 21 TO 30 PSI.DIVERTED TO GRR, DECLARED AN EMERGENCY AJan 30, 2002 · Cndair CL6002B19 · Turbine Engine Accessory DriveSDR CA020123001Wire Harness · chafed(CAN) WHILE IN FLIGHT, CREW REPORTED THAT THE LEFT FUEL QTY INDICATION AND TOTAL FUEL QTY INDICATION WENT TO DASHES. FUEL QTY INDICATION WAS DEFERRED PER MEL AND MLIS WRE USED TO CHECK FUEL QUANTITY BEFORE EACH FLIGHT. UPON FURTHER INVESTIGATION, MAINTENJan 23, 2002 · Cndair CL6002B19 · Fuel System WiringSDR CA020201018Door Latch · lack of lube(CAN) DURING FLIGHT, AIRCRAFT WAS DIVERTED DUE TO PASSENGER DOOR FAULT. FOUND PASSENGER DOOR LATCH RED HANDLE STICKING. CLEANED AND LUBED, OPERATED DOOR SEVERAL TIMES, DOOR OPERATION AND INDICATION OK.Jan 20, 2002 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA020201017Sensor · contaminated(CAN) ON DEPARTURE THROUGH 4000 FT PAX OR LATCH. CAUTION MSG ILLUMINATED. CHECKLIST CARRIED OUT WITH PRESSURIZATION NORMAL. DECIDED ATO CONTINUE THROUGH 10000 FT, PASSENGER DOOR WARNING MSG WITH NORMAL PRESSURIZATION.AIRCRAFT RETURNED TO TORONTO. ON ARRIVAL FJan 19, 2002 · Cndair CL6002B19 · Door Warning SystemSDR CA020201022Proximity Switch · failed(CAN) OVERBOARD COOL MESSAGE ACCOMPANIED BY PASSENGER DOOR LATCH MESSAGE DURING CLIMB. FAULT ISOLATION GUIDE PROCEDURE PERFORMED BY FLIGHT CREW, OVERBOARD MESSAGE DISAPPEARED. PROXIMITY SWITCH PS2MB (DI 17) REPLACED. OPERATIONAL TEST OF DOOR WARNING SYSTEMJan 17, 2002 · Cndair CL6002B19 · Door Warning SystemSDR CA020117005Windshield · cracked(CAN) LEFT WINDSHIELD CRACKED DURING FLIGHT AT FL270. LEFT WINDSHIELD REPLACED PER AMM.Jan 16, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020215006Element · failed(CAN) LEFT 14TH DUCT WARNING ON AT TAKEOFF ROLL ABOVE V, ON EICAS, RED BY ENGINE. AIRCRAFT RETURNED TO TORONTO. RIGHT BLEED LEAK DETECTION CONTROL UNIT AND LOOP SENSING ELEMENT (A58WK) REPLACED.OPERATIONAL TEST OF 14TH STAGE BLEED PERFORMED AND OPERATION TEST Jan 16, 2002 · Cndair CL6002B19 · Overheat DetectionSDR CA020124005Control Handle · failed(CAN) GEAR DISAGREE LIGHT ON APPROACH INTO WASHINGTON. CREW CONDUCTED A GO AROUND THEN CARRIED OUT A MANUAL EXTENSION. AFTER LANDING THE NOSE STEERING WAS INOPERATIVE. FOUND TO BE THE LANDING CONTROL LEVER AT FAULT. REPLACED LANDNG CONTROL LEVER, OPERATIONAL CJan 14, 2002 · Cndair CL6002B19 · Landing Gear SelectorSDR CA020201020Landing Gear · failed(CAN) GEAR DISAGREE WARNING AFTER LANDING GEAR SELECTED UP ON TAKEOFF (NOSE GEAR UNSAFE). AIRCRAFT RETURNED TO BASE.AFTER EXTENSIVE TROUBLE SHOOTING, NEW NOSE LANDING GEAR ASSEMBLY INSTALLED.Jan 10, 2002 · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR CA020110007Window · cracked(CAN) DURING CLIMB OUT, THE CO-PILOT'S WINDOW CRACKED. RIGHT SIDE WINDOW REPLACED AS PER AMM.Jan 9, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020110009B-Nut · loose(CAN) LEFT ENGINE OIL TEMP PEAKED AT 175 DEG FOLLOWED BY LOW OIL PRESSURE AT 22-25 PSI. PERFORMED IN-FLIGHT SHUTDOWN. ENGINE HAD JUST BEEN INSTALLED DIRECTLY FROM GE OVERHAUL. FOUND OIL 3-4 QTS LOW. SENT MECHS TO ALB. MECHS FOUND OIL ALL OVER THE ENGINE AJan 9, 2002 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA020110010Engine · failed(CAN) NR 1 ENGINE LOST OIL PRESSURE AT 31,000 FT. PERFORMED IN-FLT SHUT-DOWN. DECLARED EMERGENCY AND LANDED. INSPECTED ENGINE FOR LEAKS, SERVICING AND GROUND RUNS, NOTHING UNUSUAL FOUND. FERRIED TO CVG FOR FUTHER INVEST. NO ABNORMALITIES NOTED DURING Jan 9, 2002 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA020201019Apu · failed(CAN) AT 10,000 FT TRIED TO START THE APU, NO LIGHT OFF. APU SELECTED OFF. 2 MINUTES LATER, ATTEMPTED ANOTHER START, START COMPLETED, FUEL TRANSFERRED WITH STRONG SMELL OF FUEL, EGT HIGHER THAN NORMAL WITH ONE FIRE DETECTOR LOOP INOP. APU SHUTDOWN AND FJan 6, 2002 · Cndair CL6002B19 · APU Start/Ignition SystemSDR COMA0260018Pump · malfunctionedFLIGHT 5958 LEFT ENGINE LOST OIL PRESSURE I.F.S.D.COULD NOT DUPLICATE DISCREPANCY - REPLACED THE ENGINE OIL PUMP FOR TROUBLE SHOOTING.Jan 1, 2002 · N912CA · Cndair CL6002B19 · Engine Oil PressureSDR CA020121007Harness · faulty(CAN) EICAS CAUTION MESSAGE FOR PASSENGER DOOR UNSAFE IN FLIGHT. AFTER TROUBLESHOOTING, NO FAULT FOUND, FLEET MANAGEMENT REQUESTED TO REPLACE THE DOOR WIRE HARNESS. WIRE HARNESS REPLACED.Jan 1, 2002 · Cndair CL6002B19 · Door Warning SystemSDR COMA0260010Engine · lack of lubeFLIGHT 5383 LEFT ENGINE OIL TEMP MESSAGE. SERVICED ENGINE OIL TO PROPER LEVEL.Dec 30, 2001 · N912CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR COMA0260016Engine · faultyFLIGHT 5959 L/H ENGINE HIGH OIL TEMP AND LOW OIL PRESSURE I.F.S.D.REPLACED L/H ENGINEDec 26, 2001 · N912CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA020110004Acm · failed(CAN) LT PACK FAULT WITH SMOKE IN COCKPIT, NO OVERHEAT OBSERVED. PACK WAS IN AUTO MODE. PACK SELECTED OFF AND SMOKE CLEARED. LT AIR CYCLE MACHINE AND COALESCER BAG REPLACED AS PER AMM. SYSTEM SERVICEABLE.Dec 24, 2001 · Cndair CL6002B19 · Cabin Cooling SystemSDR CA011217008Selector Valve · failed(CAN) MLG DID NOT EXTEND WHEN GEAR SELECTED DOWN ON APPROACH. MLG SELECTOR VALVE REPLACED AND TESTED SERICABLE IAW AMM.Dec 7, 2001 · Cndair CL6002B19 · Landing Gear SelectorSDR CA020104014Control Unit · failed(CAN) STAB TRIM FAILED BOTH CHANNELS ON APPROACH INTO BOSTON. EMERGENCY LANDING DECLARED BY FLIGHT CREW. HORIZONTAL STAB CONTROL UNIT (HSTCU, MOTORS CONTROL UNIT (MCU) AND HORIZONTAL STAB ACTUATOR (HSTA)REPLACED. SYSTEM TESTED AS PER AMM. CONSIDERED SERVICEABLDec 6, 2001 · Cndair CL6002B19 · Stabilizer ActuatorSDR CA011217012Outflow Valve · contaminated(CAN) A/C EXCEEDED 10,000 FT CABIN ALTITUDE DESCENDING THROUGH FL. 240. OXYGEN MASKS DEPLOYED AUTOMATICALLY. PRECEEDED BY CABIN ALT CAUTION. TRIED ALT CONTROLLER & MANUAL W/O SUCCESS IN PREVEN TING CABIN CLIMBING. DECLARED EMERG&MADE UNSCHEDULED LANDING AT SDec 5, 2001 · Cndair CL6002B19 · Pressure Regulator/Outflow ValveSDR COMA0160939Seal · leakingFLIGHT #5639. LEFT ENGINE OIL PRESSURE WARNING.REPLACED THE IDG AND STARTER DRIVE, CARBON SEALS.Dec 1, 2001 · N798CA · Cndair CL6002B19 · Turbine Engine Accessory DriveSDR COMA0160938Insert · looseFLIGHT #5639 - LEFT ENGINE OIL PRESSURE WARNING. IFSD FOUND ENGINE OIL FILTER INSERT LOOSE, TIGHTENED FILTER INSERT AND ACFT RETURNED TO SERVICE.Nov 29, 2001 · N798CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR COMA0160940EecFLIGHT #5553 LEFT ENGINE ROLLED BACK TO IDLE THRUST DURING CRUSIE FLIGHT - 7 MINUTES LATER POWER RETURNED TO NORMAL.DEFERRED THE LEFT ENIGNE A.P.R. SYSTEM PER MEL. AIRCRAFT CONTINUED SERVICE.Nov 29, 2001 · N926CA · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR CA011218010O-Ring · nicked(CAN) LEFT ENGINE OIL PRESS WARNING, REQD SHUTDOWN OF ENGINE. DIVERTED & MADE EMERG LDG. SENT MECHS AND FOUND LUBE PUMP INSERT SLEEVE BACKED OFF. TIGHTENED LUBE PUMP INSERT SLEEVE PER GEMM. CHIP DETECTOR CHECKED GOOD. REPLENISHED OIL TANK WITH 5.5 QTS OF OIL. Nov 29, 2001 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA020104007Smoke Detector · false activation(CAN) "SMOKE CARGO" WARNING MESSAGE ON SHORT FINAL TO TORONTO. DRILL CARRIED OUT. BOTH BOTTLES DISCHARGED. BOTH CARGO FIRE EXTINGUISHER BOTTLES, FWD & AFT SMOKE DECTECTORS, BOTH COALESCOR BAGS REPLACED. CARGO COMPT. SMOKE AND FIRE DETECTION SYSTEM TEST CARRIEDNov 28, 2001 · Cndair CL6002B19 · Smoke DetectionSDR CA011128006Support · cracked(CAN) CRACK ON THE ENGINE SUPPORT BEAM. REPAIRED.Nov 23, 2001 · Cndair CL6002B19 · Engine Mount Section
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