GE CF34-3A1

Service difficulty reports · 1,372

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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"

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SDR CA080403002Bpsu · malfunctionedTHE POST MAINTENANCE TEST FLIGHT WAS UNSUCCESSFUL. THE CREW RECEIVED A FLAP FAIL CAUTION MESSAGE ON APPROACH WHEN THE FLAPS WERE SELECTED FROM 0 TO 8 DEGREES. THE FLAP ELECTRONIC CONTROL UNIT (FECU) CODES WERE RETRIEVED. THE RT BRAKE AND POSITION SENSOR UNIT Mar 31, 2008 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA080331006Flap System · failed(CAN) FLAP FAILED ON APPROACH , LT FLAP INDICATING 3 DEG , RT INDICATING 4 DEG PARTIAL FLAP LANDING CARRIED OUT. MAINT ACTIONS : ALL 8 FLAP ACTUATORS REPLACED IAW COMPANY FLAP FAIL POLICY. (TC NR 20080331006)Mar 28, 2008 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA080328010Flap System · failed(CAN) ON APPROACH WHEN MAKING INITIAL FLAP SELECTION CREW RECEIVED FLAP FAULT MESSAGE, FLAPS FAILED TO OPERATE. CREW PERFORMED FLAP (0) LANDING. CREW ADVISE OAT WAS -57 TO -59 FOR ABOUT AN HOUR AT FLIGHT LEVEL 260 PRIOR TO COMMENCING DESCENT. ON GROUND FLAPS PMar 27, 2008 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0860158Connector · looseFLIGHT 5451 - WITH BLEED AIR SOURCE FOR PACKS ON, APU LT 10TH STAGE BLEED VALVES CLOSED RT 10TH OPEN AND LOAD CONTROL VALVE CLOSED. OPENED ISO SWITCH AND LOAD CONTROL OPENED, SAME, REPEATED SEVERAL TIMES. FOUND CONNECTORS LOOSE ON THE ISOLATION AND 10TH STAGMar 5, 2008 · N927CA · Cndair CL6002B19 · Engine Bleed Air System WiringSDR COMA0860115Engine · vibrationFLIGHT 5024 - DURING CRUISE, RIGHT ENGINE N1 VIBE SHOWED AMBER DASHES AT IDLE AND RIGHT ENGINE VIBE INDICATION SHOWED 3.0. DECLARED EMERGENCY, DIVERTED TO STL, LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE. NO FURTHER DEFECTS.Feb 8, 2008 · N427CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA080128002Flap System · failed(CAN) WHEN EXERCISING FLAPS DURING MAINTENANCE COLD WEATHER CHECKS, FLAP FAIL MESSAGE SHOWED AS SOON AS FLAPS SELECTED. A/C FERRIED, MFG FSR CALLED TO ATTEND HANGAR FOR TEARDOWN AND INSPECTION. MORE TO FOLLOW. (TC NR 20080128002)Jan 27, 2008 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA080126004Bushing · migrated(CAN) CREW REPORTED THAT AT 12000 FT PAX DOOR WARNING MSG POSTED. FOLLOWED QRH AND RETURNED TO FIELD. FOUND BUSHING IN FWD LATCH CAM FITTING MIGRATED. REINSTALLED BUSHING IN UPPER FWD CAM LEVER REF AMM 52-11-23. NOTE: AC WAS PRE SB 601R-52-110 CONFIGURATION.Jan 24, 2008 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA080121002Fcu · defective(CAN) FLAPS FAILED ON INITIAL SELECTION FROM 0 TO 8 DEGREES JUST AFTER PUSHBACK FOR HEADSTART FLIGHT. OAT WAS -29 C OVERNIGHT. MAINTENANCE GOT CODES FROM FECU, CLEARED FAULT AND RESET FLAPS. FLAPS FUNCTION CHECKED SERVICEABLE, BUT DUE TO RECENT HISTORY IT WASJan 20, 2008 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA080126002Throttle Control · malfunctioned(CAN) CREW REPORTED LT ENG REMAINED AT HIGH POWER SETTING WHEN AC BROUGHT TO IDLE. N1 REMAINED BETWEEN 82 AND 91 PERCENT. IFSD PILOT COMMANDED IN FLIGHT SHUTDOWN: CONFIRMED, AFTER (ABORTED APPROACH) PILOT SHUTDOWN THE LT ENG USING FIRE PUSH DURING (GO AROUND)Jan 17, 2008 · Cndair CL6002B19 · Power LeverSDR COMA0860071Engine · failedFLIGHT 5341 - EN ROUTE FROM MKE TO CVG SEVERE ENGINE NOISE AND SHUDDER ON LEFT ENGINE. PERFORMED IFSD. EMERGENCY DECLARED AND AIRCRAFT DIVERTED TO ORD AND LANDED SAFELY. REMOVED AND REPLACED LEFT ENGINE.Jan 16, 2008 · N964CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA080121001Windshield · cracked(CAN) ON CLIMB OUT THROUGH 6000 FT CREW SELECTED WINDSHIELD HEAT. THE (L WSHLD HEAT) EICAS MESSAGE ILLUMINATED. ABOUT 15 SECONDS LATER CAPTAIN’S FRONT WINDSHIELD OUTER PLY BEGAN CRACKING. SPIDER WEB LIKE CRACKING CONTINUED UNTIL WHOLE OUTER PANE APPEARED SHATTJan 16, 2008 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA080206004Engine · vibration(CAN) CREW REPORTED SEVERE NOISE AND VIBRATION FELT ON LT ENGINE. SHUT ENGINE DOWN AS PRECAUTION AND RETURNED TO FIELD. ENGINE/QEC REMOVED AND REPLACED. SIGNIFICANT DAMAGE TO TURBINE.Jan 16, 2008 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA080109009Converter · faulty(CAN) DURING ENGINE START, AT ABOUT 40 TO 50 PERCENT, N2, ALL LIGHTS ON THE ITT TAPE INSTANTLY LIGHTED UP. WE IMMEDIATELY SHUTDOWN ENGINE. RESIDUAL ITT WAS ONLY 56 AND NR9702, AFTER MOTORING. VISUALLY INSPECTED THE ENGINE FOR SIGNS OF HEAT OR DAMAGE AND FOUND Jan 7, 2008 · Cndair CL6002B16 · Engine Integrated Instrument SystemSDR CA080102001Fcu · unserviceable(CAN) ON APPROACH, GOING THROUGH 6500FT AT 200KTS, FLAP FAIL MESSAGE ILUMINATED WHEN SELECTED FROM 0 TO 8 DEGREES. FLAPS DID NOT MOVE, REMAINED AT 0 DEGREES. FLAPLESS LANDING CARRIED OUT WITHOUT FURTHER INCIDENT. NOTE: NO SKEW DETECTION LIGHTS WERE ILLUMINATEDJan 1, 2008 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA071228002Idg · damaged(CAN) AT ALTITUDE CREW RECEIVED AN IDG CAUTION MESSAGE. THE NR 2 IDG WAS DEFERRED UNTIL MAINT COULD BE ACCOMPLISHED. AC WAS BROUGHT TO THE HANGER TO HAVE REPAIRS C/O, REMOVAL OF THE IDG REVEALED THAT THE INTERNAL SHAFT OF THE IDG PUNCHED THROUGH THE OUTER CASIDec 27, 2007 · Cndair CL6002B19 · AC Generator-AlternatorSDR CA080105001Relay · failed(CAN) UPON ARRIVAL, GROUND PWR APPLIED TO AC BUT SHUTOFF IMMEDIATELY. GROUND PWR RESTARTED AND AFTER ABOUT A MINUTE CREW NOTED NUMEROUS CIRCUIT BREAKERS POPPED, HEARD A LOUD BANG FROM THE NOSE SECTION AND A LIGHT SMELL OF SMOKE IN THE COCKPIT. CIRCUIT BREAKERSDec 24, 2007 · Cndair CL6002B19 · Electrical Power System WiringSDR CA071219006Skin · cracked(CAN) BOTH THE LT AND RT REPAIR DOUBLERS THAT ARE IDENTIFIED AS ITEM -1 ON THE ATTACHED REO601R-53-61-358, REVISION A, WERE FOUND CRACKED DURING AN INSPECTION OF THE ENGINE SUPPORT BEAMS AT A HEAVY CHECK VISIT. THIS AC CAME INTO OUR AIRLINE OPERATION AT APPRODec 17, 2007 · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR CA080115011Line · ruptured(CAN) PRESSURE LINE ON NR 3A PUMP RUPTURED AND SYS FLUID WAS LOST. GEAR WAS ALTERNATELY EXTENDED AND LANDED WITHOUT INCIDENT. THE HOSE WAS REPLACED AND THE AC WAS FERRIED. THE GEAR WAS SWUNG AND THE HYDRAULICS BLED, TESTED SERVICEABLE. THERE ARE CURRENTLY NO LDec 17, 2007 · Cndair CL6002B16 · Hydraulic System, MainSDR COMA0760727Pump · faultyFLIGHT 9658 - DURING CRUISE FLIGHT RECEIVED A RIGHT ENGINE OIL PRESSURE WARNING MESSAGE, CREW DECLARED AN EMERGENCY, PERFORMED AN I.F.S.D. AND DIVERTED TO MDT. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT ENGINE LUBRICATION AND SCAVENGE PUMP.Dec 14, 2007 · N713CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR COMA0760728Transducer · faultyFLIGHT 9658 - DURING CRUISE FLIGHT RECEIVED A RIGHT ENGINE OIL PRESSURE WARNING MESSAGE, CREW DECLARED AN EMERGENCY, PERFORMED AN I.F.S.D. AND DIVERTED TO MDT. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT ENGINE OIL PRESSURE TRANSDUCER.Dec 14, 2007 · N713CA · Cndair CL6002B19 · Engine Oil PressureSDR CA071217005Actuator · frozen(CAN) FLAP FAIL DURING DESCENT. FLAPS WOULD NOT EXTEND WHEN SELECTED, FLAP 0 APPROACH AND LANDING CONDUCTED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. FAULT CODES SENT TO TECH OPS, AIRCRAFT WILL BE FERRIED WHEN CREW AVAILABLE. FAULT CODES ARE AS FOLLOWS: EVENDec 14, 2007 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CA071218007Shroud · chafed(CAN) DURING HEAVY CHECK INSP, THE FUEL DISTRIBUTION PRESSURE BOX ASSY, P/N 601R62676-5 WAS FOUND CRACKED AND BOTH THE FUEL SHROUD AND FUEL LINES HAVE CHAFFING DAMAGE BEYOND LIMITS. THESE COMPONENTS ARE LOCATED AT FUSELAGE STATION FS559. PARTS ARE ON ORDER ANDec 14, 2007 · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA071214004Actuator · unserviceable(CAN) FLAP FAIL ON DESCENT, WHEN FLAP SELECTED FROM 0 DEG TO 8 DEG. FLAPLESS LANDING CARRIED OUT WITHOUT FURTHER INCIDENT. TROUBLESHOOTING IN PROGRESS. WILL UPDATE WHEN MORE INFORMATION IS AVAILABLE (TC NR 20071214004)Dec 13, 2007 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CA071213001Scavenge Pump · failed(CAN) DURING CRUISE FLIGHT, THE CREW RECEIVED RED NR 2 ENG LOW OIL PRESS MESSAGE AND GAUGE INDICATION FOR NR 2 ENGINE SHOWED (0) PSI, CREW ELECTED TO SHUTDOWN ENGINE AND RETURN TO DEPARTURE AIRPORT, NORMAL LANDING. MAINTENANCE FOUND NR 2 ENGINE, OIL LUBE/SCAVEDec 12, 2007 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA071217001Fan Blade · damaged(CAN) CREW REPORTED N2 VIB ICON (RT ENG) POSTED DURING CRUISE AT FL320. CREW FOLLOWED QRH AND COULD NOT CONTROL VIB IFSD AND DIVERTED. MAINTENANCE OBSERVED FOD DAMAGE TO FAN BLADES. ENGINE REMOVED AND REPLACED (TC NR 20071217001)Dec 5, 2007 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR COMA0760688Engine · flamed outFLIGHT 5672 - LEFT ENGINE FLAMED OUT DURING START. FOUND THAT THE PREVIOUS ENGINE START HAD A TAILWIND OF APPROXIMATELY 40 KTS. DRY MOTORED ENGINE AND PERFORMED 2 ENGINE STARTS WITH NO FAULTS.Dec 4, 2007 · N931CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA071126003Bpsu · unserviceable(CAN) FLAP FAIL CAUTION MESSAGE ILLUMINATED WHILE IN CRUISE AND FLAPS WERE AT 0 DEG. FLAPLESS LANDING C/O AND A/C LANDED SAFELY. MAINT RANG OUT WIRES AND COULD NOT FIND ANY FAULTS. THE FECU AND THE RT BPSU WERE REPLACED. A TEST FLIGHT WAS C/O TO COLD SOAK TEMPNov 23, 2007 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA071113006Camlock · worn(CAN) DURING AN OVERNIGHT MAINTENANCE INSPECTION IT WAS DISCOVERED THAT THE LT WING INSPECTION LIGHT LENS WAS MISSING TOGETHER WITH THE BULB HOLDER LEAVING THE WIRES EXPOSED. WHEN THE FAIRING WAS REMOVED TO REPLACE THE ASSEMBLY IT WAS NOTICED THAT A CAMLOC NUTNov 12, 2007 · Cndair CL6002B19 · Exterior LightingSDR CA071103001Ecu · faulty(CAN) FLIGHT RETURNED DUE TO APU OIL PRESSURE MESSAGE CAUSING THE APU TO FAIL. AIRCRAFT WAS ALREADY OPERATING WITH 1 IDG GENERATOR UNSERVICEABLE. MAINTENANCE CHECKED THE SYSTEM AND FOUND AN ECU FAULT MESSAGE. THE APU ECU WAS REPLACED AND THE A/C WAS CHECKED SENov 1, 2007 · Cndair CL6002B19 · APU Indicating SystemSDR CA071102009Actuator · fractured(CAN) DURING SHORT FINAL, THE FLAPS WERE SELECTED TO 45 DEGREES AND THE AIRCRAFT ROLLED TO THE RT. FULL AILERON TRIM AND A LITTLE BIT OF AILERON WAS REQUIRED TO KEEP THE AIRCRAFT LEVEL. THE EICAS FLIGHT CONTROL PAGE WAS REVIEWED AND THE RT SPOILERON WAS SHOWIOct 30, 2007 · Cndair CL6002B19 · Drag Control ActuatorSDR CA071102001Actuator · failed(CAN) DURING APPROACH, THE CREW RECEIVED A FLAP FAIL CAUTION MESSAGE WHEN THE FLAPS WERE SELECTED FROM 0 TO 8 DEGREES. THE EICAS FLIGHT CONTROL PAGE WAS INDICATING 0 DEGREE ON BOTH SIDES. THE CREW CONTINUED THE APPROACH AND COMPLETED A FLAPLESS LANDING WITHOUTOct 29, 2007 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CA071029010Housing · damaged(CAN) JUST BEFORE PUSHBACK, THE RAMP CREW OBSERVED A FUEL LEAK COMING FROM THE APU AREA. CAPTAIN PERFORMED RAPID PASSENGER DEPLANEMENT WITH EMERGENCY CREWS ON STAND-BY. MAINTENANCE FOUND THE FUEL LEAK COMING FROM THE NR 2 ENGINE- FUEL FILTER HOUSING, BY THE FOct 28, 2007 · Cndair CL6002B19 · Aircraft Fuel Filter/StrainerSDR 2007F00066Wire Harness · shortedON THE IB FLIGHT, THE NR 1 PITCH TRIM CIRCUIT BREAKER POPPED. THE AIRCRAFT WAS TAKEN TO MFG AND THE TECHNICIANS WERE UNABLE TO DUPLICATE THE PROBLEM. AT MAINTENANCE REQUEST,THE TAIL WIRE HARNESS (FROM THE PRESSURE BULKHEAD TO THE STABILIZER TRIM ACTUATOR) WAS Oct 17, 2007 · N28KA · Cndair CL6002B16 · Flight Control System WiringSDR CA071005001Shroud · chafed(CAN) DURING A HEAVY CHECK THE FUEL SHROUD ASSY AND FUEL LINES AT FRAME 559 WERE REMOVED TO FACILITATE A SHEET METAL REPAIR. IT WAS DISCOVERED THAT BOTH SHROUD AND FUEL LINES HAVE CHAFING BEYOND LIMITS. THIS SAME REPAIR IS BEING C/O ON A/C C-FZSI(126) AND SIMIOct 4, 2007 · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA070928002Scavenge Pump · fluctuates(CAN) SHORTLY AFTER TAKEOFF THE NR ONE ENGINE OIL HIGH TEMPERATURE/LOW PRESSURE CAUTION LIGHT CAME ON. FLIGHT RETURNED TO DEPARTURE AIRPORT. FLIGHT LANDED APPROX 1000 POUNDS OVERWEIGHT. NO EMERGENCY DECLARED BUT EMERGENCY VEHICLES ON STANDBY. MAINTENANCE TROUBSep 27, 2007 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA070925003Priority Valve · failed(CAN) AFTER TAKEOFF THE FOLLOWING MESSAGES WERE DISPLAYED IN THE COCKPIT: STEERING INOP, GEAR DISAGREE, W.O.W. SENSOR FAILURE AND W.O.W. STATUS. NOSE GEAR REMAINED IN DOWN POSITION WITH MAIN GEAR RETRACTED. AIRCRAFT TURNED-BACK AND LANDED UNEVENTFULLY. MAINTENSep 23, 2007 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR CA070917007Flex Drive · worn(CAN) CREW REPORTED THAT THE FLAPS OPERATED NORMALLY ON APPROACH, WHEN SELECTED TO FLAPS 45. AFTER LANDING AND DURING TAXI, WHEN THE CREW SELECTED FLAPS 0, THEY RECEIVED A FLAP FAIL AND THE FLAPS REMAINED AT 45. CONTRACT MAINTENANCE RETRIEVED THE CODES FROM THSep 13, 2007 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA070905007Dcu · inoperative(CAN) DURING CLIMB OUT, CREW REPORTED A (L ENG MISCOMP) MESSAGE FOLLOWED BY A HIGH ITT. THE CREW ELECTED TO SHUTDOWN THE ENGINE. AFTER SHUTDOWN THE ITT REMAINED AT 998 DEGREES CELSIUS. AT TIME OF THE INCIDENT, THE AIRCRAFT WAS OPERATING UNDER MEL31-41-01 DUE TAug 31, 2007 · Cndair CL6002B19 · Automatic DataSDR COMA0760542Oil System · overservicedFLIGHT 5363 - RECEIVED HIGH OIL TEMPERATURE MESSAGE FOR NR 1 ENGINE. SHUTDOWN NR 1 ENGINE, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND ENGINE OVERSERVICED BY 2 QTS. REMOVED EXCESS OIL. RAN ENGINE, NO FURTHER DEFECTS.Aug 26, 2007 · N805CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA070827004Ballast · burned(CAN) CREW REPORTED WHEN THEY APPLIED EXT AC POWER TO THE AIRCRAFT AND TURNED ON THE SWITCH IN THE COCKPIT, THEY COULD SMELL SOMETHING BURNING AND SAW A BLUE HAZE IN THE AIR. THEY IMMEDIATELY TURNED POWER OFF AND CALLED MAINTENANCE CONTROL. MAINTENANCE INSPECAug 24, 2007 · Cndair CL6002B19 · Passenger Compartment LightingSDR CA070828002Line · chafed(CAN) DURING C-CHECK INSPECTION, CHAFING DAMAGE WAS NOTED ON THE HYDRAULIC PUMP 3B SUCTION LINE P/N 601R75239-463. THIS HYDRAULIC TUBE LINE WAS RUBBING AGAINST THE UPLOCK NR 3 HYDRAULIC TUBE LINE (P/N 601R75239-273) THAT FEEDS INTO THE EXTEND LINE FOR THE RHS Aug 24, 2007 · Cndair CL6002B19 · Hydraulic System, MainSDR CA070828003Line · chafed(CAN) DURING A C-CHECK INSPECTION IN THE RT MAIN LANDING GEAR WHEEL WELL, THE HDRAULIC SUCTION TUBE ASSY(P/N 601R75239-463) OF HYDRAULIC PUMP 3B WAS FOUND WITH CHAFING DAMAGE. THIS TUBE WAS RUBBING AGAINST THE HYDRAULIC LINE(P/N 601R75239-273),WHICH IS THE UPLAug 24, 2007 · Cndair CL6002B19 · Hydraulic System, MainSDR CA070902003Windshield · cracked(CAN) FL 330 LT, WINDSHIELD CRACKED. AIRCRAFT CONTINUED TO DESTINATION. NO FURTHER REPORTED DETAILS. (TC NR 20070902003)Aug 24, 2007 · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA0760529Engine · leakingFLIGHT 9432 - RECEIVED RIGHT ENGINE OIL PRESSURE WARNING MESSAGE. DIVERTED TO PIT, LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE. NO FURTHER DEFECTS.Aug 15, 2007 · N969CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA0760530Oil System · overservicedFLIGHT 5158 - DURING CLIMB NOTED HIGH OIL TEMP ON RIGHT ENGINE. DIVERTED TO JFK. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND ENGINE OIL OVERSERVICED. DRAINED EXCESS OIL. RAN ENGINE, NO FURTHER DEFECTS.Aug 15, 2007 · N779CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR COMA0760517Engine · unknownFLIGHT 5337 - EN ROUTE FROM BOS TO SAV, FLIGHT DIVERTED TO JFK AFTER CREW NOTICED WHAT APPEARED TO BE A LACK OF ENGINE POWER, AIRCRAFT LANDED SAFELY. PERFORMED ENGINE GROUND RUNS AND FOUND ENGINES TO OPERATE WITHIN LIMITS.Aug 4, 2007 · N735CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA0760509Oil System · lowFLIGHT 5387 - DURING CLIMBOUT RECEIVED LEFT ENGINE LOW OIL PRESS WARNING MESSAGE. AIRCRAFT RETURNED BACK TO CID AND LANDED SAFELY. INSPECTED LEFT ENGINE AND FOUND IT TO BE LOW ON OIL. SERVICED ENGINE AND PERFORMED GROUND RUNS.Aug 1, 2007 · N709CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA070729003Strut · damaged(CAN) ON ARRIVAL IT WAS DISCOVERED THAT THE PAX AIRSTAIR HAD BEEN DAMAGED WHEN CLOSED. MAINTENANCE FOUND A SMALL PUNCTURE IN THE MAIN CABIN DOOR INNER SKIN BESIDE UPPER STEP. MAINTENANCE DISCOVERED THE GAS STRUT ON THE MCD FAILED CAUSING THE SKIN PUCTURE BY Jul 28, 2007 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA070724004Wire · damaged(CAN) IN CRUISE GEAR/FLAPS/BTMS INDICATIONS APPEARED WITH FLAP INDICATION SHOWING BOTH SIDES. FLAPLESS LANDING WAS SAFELY PERFORMED. MAINTENANCE FOUND WIRE CF61A22WHT AT CONNECTOR P2CF OF RT FLAP POSITION TRANSDUCER WITH DAMAGED INSULATION AND TOUCHING THE SHIJul 21, 2007 · Cndair CL6002B19 · Flight Control System WiringSDR CA070713001Piccolo Tube · ruptured(CAN) THE FLIGHT CREW RECEIVED AN ANTI-ICE DUCT WARNING MESSAGE DURING FLIGHT. THE APPLICABLE SYNOPTIC PAGE SHOWED THE RT WING LEADING EDGE BEING AT FAULT. WING ANTI-ICE SWITCH WAS SELECTED FROM NORMAL TO STAND-BY WITHOUT SUCCESS. DURING TROUBLESHOOTING, MAINTJul 10, 2007 · Cndair CL6002B19 · Airfoil Anti/De-ice System
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