GE CF34-3B1

Service difficulty reports · 5,402

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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 = 'CF343B1'
  ORDER BY difficulty_date DESC"

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SDR CA091019002Fitting · cracked(CAN) DURING AN INTERNAL WINTER PREVENTIVE MX CHECK, AN ENGINEER OBSERVED BY COINCIDENCE A CRACK ON THE MAIN CABIN DOOR AFT COUNTERBALANCE ANCHOR FITTING. THE CRACK LENGTH WAS EXCEEDING REPAIR EO 601R-52-11-272, THE FITTING WAS REPLACED AND THE ACFT RETURNED IOct 15, 2009 · Cndair CL6002B19 · Fuselage, Door HingeSDR CHQA200900221Fan Blade · out of balanceDURING OVERNIGHT MAINTENANCE ON 10/13/2009, THE FAN DISK ON E1 WAS REPLACED BY CONTRACT MAINTENANCE. DURING POST MAINTENANCE GROUND POWER ASSURANCE RUN THE E1 FAN VIBES WERE AT 2.2MILS. MAINTENANCE REPLACED THE EVM SENSOR AND DURING THE SECOND POWER RUN THE Oct 14, 2009 · N702BR · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR VNAA2009102100008Panel · damagedCREW REPORTED A BIRD STRIKE ABOVE THE RT WING LANDING LIGHT LENS AT MOB. EVIDENCE OF BIRD STRIKE DEBRIS ENTERING THE COWLING ON THE RT ENGINE WAS ALSO REPORTED. MAINTENANCE INSPECTED AND REWORKED THE DENTED RT WING LEADING EDGE PANEL IAW REO 601R-57-41-629. Oct 14, 2009 · N250PS · Cndair CL6002B19 · Wing, Plate/SkinSDR CA091029001Engine · overtemp(CAN) DISCREPANCY: "RT ENG LOW OIL PRESSURE INDICATED, RT ENG ITT TEMP EXCEEDED, ON APPROACH INTO. CREW FOLLOWED EMERGENCY PROCEDURES AND SHUT THE RT ENG DOWN". ENGINE WAS REPLACED.Oct 7, 2009 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA200922770Fuel Control · malfunctionedFLT 6175, RIGHT ENGINE OVERTEMPED AND LOST OIL PRESSURE IN CRUISE. FUEL CONTROL REPLACED, ALL INSPECTIONS AND BOROSCOPE FOUND NORMAL CONDITIONS, ENGINE RETURNED TO SERVICE.Oct 5, 2009 · N907SW · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR ASOA200901103Oil System · overtempDURING CLIMB OUT OF ATL NR 1 ENG OIL TEMP INCREASED AMBER AT 150+ F/O PULLED OUT QRH & IT ALREADY WAS RED 163 & RAN QRH. AFTER IDLING FOR ALMOST 2 MIN FINALLY STARTED DECREASING. LOWERED TO IDLE & STILL SHOWING 131' (RT SHOWING 99) ALSO NR 1 OIL PRESS WAS 5 TOct 3, 2009 · N930EV · Cndair CL6002B19 · Turbine Engine Oil SystemSDR REXA200900114Throttle Cable · brokenFLIGHT 4107 MOT/MSP ATC REQUESTED A DESCENT TO BEGIN APPROACH INTO MSP, WHEN THROTTLES RETARDED THE LEFT WAS FOUND TO BE INOPERATIVE, NO ENGINE CHANGE WITH THROTTLE MOVEMENT. QRH FOLLOWED FOR "STUCK THROTTLE" AND ENGINE SHUTDOWN. EMERGENCY DECLARED AND LANDEOct 3, 2009 · N8506C · Cndair CL6002B19 · Power LeverSDR VNAA2009100700001Carbon Seal · unknownCREW REPORTED AT 35,000 A LOW OIL PRESSURE MESSAGE. AIRCRAFT RETURNED TO CLT LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT USING AIRCRAFT MAINTENANCE MANUAL, REMOVED AND REPLACED CARBON SEALS ON ACCESSORY GEARBOX. CHECKS WERE MADE PER THE AIRCRAFOct 2, 2009 · N220PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA200940637Connector · looseON CLIMB-OUT, RECEIVED RT ENG OIL PRESS WARNING MSG WITH AURAL WARNING. C/W QRH. REDUCED POWER AND MSG WENT OUT. MSG CAME ON AT 90 PERCENT N1, APPROX 70 PSI. NO OTHER CAS MSGS. FOUND OIL PRESSURE TRANSDUCER CONNECTOR PLUG TO BE VERY LOOSE AT BACKSHELL ANDSep 29, 2009 · N415AW · Cndair CL6002B19 · Engine Oil System WiringSDR ASOA200901053Engine · overtempLT ENGINE OIL TEMP ROSE TO 169 DEGREES C CLIMBING OUT OF FL180, COMPLIED WITH QRH PULLED POWER TO IDLE, TEMP RETURNED TO GREEN RANGE. KEPT ENG AT IDLE UNTIL LANDING. SHUTDOWN AFTER LANDING [EMERGENCY DECLARED -- ACFT RETURNED TO DEPARTURE AFTER T/O].Sep 25, 2009 · N930EV · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA2009092300006Fan Blade · damagedCREW REPORTED, INGESTED SMALL BIRD(S) IN LEFT ENGINE. AIRCRAFT RETURNED TO DAY WITHOUT INCIDENT. MAINTENANCE INSPECTED LT ENGINE PER THE MANUFACTURER MAINTENANCE MANUAL AND REPLACE FAN BLADES. CHECKS WERE MADE PER THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFSep 20, 2009 · N260JS · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR CA090918003Valve · missing(CAN) ON AUGUST 23, 2009 CREW REPORTED A "X FLOW/APU PUMP" MESSAGE IN FLIGHT. CREW DEFERRED APU PUMP IAW MEL 28-24-01-2. ON AUGUST 24TH MX REPLACED APU PRESSURE SWITCH PN 601R62291-7 BUT NO FIX. APU PUMP REMAINED ON MEL. FURTHER TROUBLESHOOTING ON AUGUST 27TH Sep 17, 2009 · Cndair CL6002B19 · APU Engine Fuel and ControlSDR A6WA200940546Fcu · malfunctionedENG NR 1 W/N GO ABOVE 71.3 PERCENT N1 ON TAKEOFF POWER. ABORTED TAKEOFF BELOW 80 KTS, BRAKE TEMPS 2-2-2-2. SELECTED ENG SPEED CONTROL SYS OFF. C/W ENG RUNS WITH CREW ASSISTANCE BOTH ENGINES ENG RUNS WITH CREW ASSISTANCE BOTH ENGINES MADE AND SUSTAINED POWERSep 14, 2009 · N423AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR REXA200900109Engine · malfunctionedON TAKEOFF ROLL ON 22L AT KDTW, THE FLIGHT CREW NOTICED THE RIGHT ENGINE ITT AT THE TOP OF THE SCALE. THIS WAS FOLLOWED BY AN N2 VIBRATION ALERT. THE TAKEOFF WAS ABORTED AT 100 KNOTS AND THE AIRCRAFT EXITED THE RUNWAY. THE FLIGHT CREW ALERTED MAINTENANCE ANSep 7, 2009 · N8921B · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA090905001Engine · malfunctioned(CAN) FLT 5918 "CREW REPORTED THAT ON DEPARTURE FROM IND, HEARD A GROWLING SOUND, THEN FELT A SHUDDER FROM THE LT ENGINE. NOSE OF THE A/C YAWED, THE LT ENGINE ITT SPIKE INTO THE RED, AND THE ENGINE SHUT ITSELF DOWN. CREW DECLARED AN EMERGENCY, AND GOT BACK ON Sep 1, 2009 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CHQA200900186Warning System · malfunctionedDURING THE TAKEOFF ROLL THE CREW RECEIVED A CONFIG SPOILERS WARNING MESSAGE. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. ON ARRIVAL AT THE GATE, MAINTENANCE PERFORMED A BITE AND OPERATIONAL CHECK OF THE SECU AND PSEU SYSTEM. Aug 30, 2009 · N648BR · Cndair CL6002B19 · Drag Control SystemSDR CHQA200900187Bushing · missingON TAKEOFF FROM SDF, THE CREW RECEIVED A CONFIG SPOILER WARNING MESSAGE. THE TAKEOFF WAS ABORTED BEFORE 80 KIAS AND THE AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE PERFORMED A DETAILED INSPECTION OF THE SPOILER SYSTEM AND FOUND 2 BUSHINGS MISAug 30, 2009 · N648BR · Cndair CL6002B19 · SpoilersSDR VNAA2009090200011Carbon Seal · leakingCREW REPORTED A LOW OIL PRESS IN FLIGHT. ENGINE WAS SHUTDOWN. AIRCRAFT DIVERTED TO RIC LANDING WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOT PER THE OEM MAINTENANCE MANUAL AND REMOVED AND REPLACED THE IDG ATS & HYD PUMP AGB CARBON SEAL ASSEMBLY. OPERATIONAL Aug 30, 2009 · N220PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR SWIA200922479Engine · failedRIGHT ENGINE FAILURE ON CLIMB. (FLT 6724) REPLACED NR 2 ENGINE.Aug 28, 2009 · N969SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA200940511Panel · malfunctionedLOST ADC NR 1 INFORMATION DURING CLIMBOUT, SWITCHED TO ADC NR 2 INDICATIONS NORMAL. C/W QRH, PERFORMED AIR RETURN TO DEPARTURE. LANDED AT 47.200 LBS, 300 FT/MIN. BRAKE TEMPS READ 5-5-5-6. FOUND AIR DATA REF PANEL NR 2 TO HAVE NO OUTPUT TO AIR DATA COMPUTEAug 24, 2009 · N451AW · Cndair CL6002B19 · Air Data ComputerSDR CA090823001Contactor · damagedDURING FLIGHT PREP, WITH NO PAX ON BOARD, AFTER CONNECTING GPU, FLIGHT CREW HEARD A STRONG CLUNK NOISE FOLLOWED BY A PWR FLICKERING. FLIGHT CREW DECIDED TO SHUT THE POWER DOWN AND RIGHT AFTER, A STRONG ELECTRICAL SMELL AND SMOKE WERE NOTICED IN THE COCKPIT. BAug 18, 2009 · Cndair CL6002B19 · DC Power Distribution SystemSDR REXA200900104Transducer · malfunctionedON TAKEOFF ROLL THE FLIGHT CREW WAS ALERTED TO A HIGH OIL PRESSURE WARNING FOR THE LEFT ENGINE. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE OIL PRESSURE TRANSDUCER ON THE LEFT ENGINE. GROUND RUN WAS SATISFACTORY AAug 17, 2009 · N8659B · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA200940474Coalescer Bag · contaminatedAFTER BLEED TRANSFERE RECEIVED A STRONG BURNING RUBBER ODOR, APPEARED TO BE MORE IN COCKPIT THAN CABIN. REF WO 142295 W/C 1-5 FOR WORK COMPLETED. ODOR CAUSED BY COMP WASH FLUID THAT WAS NOT PROPERLY BURNED OFF. ALSO CHANGED COALESCER SOCKS. OPS CHECK GOOD.Aug 15, 2009 · N455AW · Cndair CL6002B19 · Humidity Control SystemSDR CA090826017Wire · burnedWHILE TROUBLESHOOTING, AN AIR DRIVEN GENERATOR FAULT MX FOUND THE ORANGE MAIN FEED WIRE BURNED THOUGH AFT OF THE CONNECTOR P1XC. WIRE ALSO EXHIBITED EVIDENCE OF PITTING CORROSION. INSULATION WAS ALSO FOUND DEGRADED ON ONE OF THE WHITE LEADS. ALL 3 MAIN FEEDAug 9, 2009 · Cndair CL6002B19 · Electrical Power System WiringSDR MASA2009080700251Engine · malfunctionedASH FLT 7256 SPI-ORD. ENGINE VIBRATION AND POPPING ON APPROACH. ON APPROACH CREW REPORTED SEVERE ENGINE VIBRATION AS THROTTLES WERE ADVANCED FROM THE DESCENT REDUCTION. CREW REDUCED THROTTLES AND ADVANCED THEM BACK SLOWLY AND GOT A SERIES OF POPPING SOUNDS Aug 7, 2009 · N27185 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA200940496Pressure Blkhd · crackedFS 202.75 AT LBL 23.71 PRESSURE BULKHEAD CRACKED AT PARKING BRAKE LOCATION, 3 CRACKS, 1.00 INCH, 1.00 INCH, .500 INCH. REPAIR IAW REO 601R-53-11-1738 AND 601R-53-11-563. (K)Aug 6, 2009 · N424AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR MASA2009080300244Oil System · overservicedFLT 7225, CAE-ORD. CREW RETURNED TO THE FIELD AND EMERGENCY DECLARED FOR LT ENGINE HIGH OIL TEMP ABOVE 166 FOR MORE THAN 2 MINUTES. MX FOUND ENG OVERSERVICED, DESERVICED TO PROPER LEVELS, ENGINE RUNS GOOD.Aug 3, 2009 · N27314 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR SWIA200922266Case · crackedLEFT ENGINE LOW PRESSURE TURBINE CASE CRACKED BEYOND LIMITS. (C-CHECK) REPLACED ENGINE.Aug 3, 2009 · N946SW · Cndair CL6002B19 · Turbine SectionSDR CHQA200900168Flex Drive · shearedFLIGHT 5512, SDF TO CLE. ON FINAL APPROACH INTO CLE THE CREW CONFIGURED THE FLAPS FROM 20 DEGREES TO 30 DEGREES. UPON SELECTION THE CREW RECEIVED A FLAP FAIL MSG. THE FLIGHT CONTROL STATUS PAGE INDICATED 28 DEGREES ON THE LEFT FLAP AND 27 DEGREES ON THE RIGJul 28, 2009 · N645BR · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR VNAA2009080300006Connector · contaminatedCREW REPORTED AFTER T/O ABOVE 1000 FT LEFT ENG OIL PRESSURE WAS READING ZERO. AIRCRAFT RETURNED TO CLT LANDING WITHOUT INCIDENT. MAINTENANCE FOUND CB M1 CBP1 POPPED. MAINTENANCE RESET CB AND INSPECTED LT ENG OIL PRESS TRANSDUCER. FOUND TRANSDUCER CONNECTORJul 28, 2009 · N247JS · Cndair CL6002B19 · Engine Oil System WiringSDR A6WA200940458Floor Support · crackedFLOOR EDGE MEMBER CRACKED AT FS 605, LBL 45, WHERE RIVET ATTACHED TO FLOORBEAM. (CRACK LENGTH .250 INCH) FLOOR EDGE MEMBER REPAIR AT FS 605, LBL 45 IAW REO 601R-53-61-433. (K)Jul 28, 2009 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CHQA200900165Pseu · faultyFLIGHT 5559, CLE TO ORD. ON LIFT-OFF RECEIVED AN EICAS CAUTION MESSAGE FOR ANTI-SKID, PROX SYS, AND STEERING INOP, AND NOSE GEAR DOOR OPEN. THE CREW PERFORMED QRH CHECKLISTS AND RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE PSEU AND Jul 26, 2009 · N653BR · Cndair CL6002B19 · Landing Gear Position and WarningSDR MASA2009072600230Fitting · looseAIR SHUTTLE 7299 FROM DAY TO ORD. DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY DUE THE NR 1 ENGINE FLAMING OUT 20 MILES FROM LANDING. THE CREW DID NOT HAVE ANYTHING TO ADD OTHER THAN THEY DID NOT HEAR SEE OR FEEL ANYTHING ABNORMAL PRIOR TO SHUTDOWN. MX SECJul 26, 2009 · N570ML · Cndair CL6002B19 · Engine Fuel DistributionSDR CA090728005Lock · loose(CAN) PILOTS REPORTED LT ENG JET PIPE OVERHEAT WARNING ACTIVATED DURING CRUISE FOR APPROX 20 SECONDS THEN WENT AWAY BY ITSELF. ACFT RETURNED TO BASE. MX INVESTIGATED AND FOUND A PLUG/PLATE AT APPROX 11 0`CLOCK WITH 1 NUT FOUND IN BOTTOM OF COWL AND THE OTHER Jul 22, 2009 · Cndair CL6002B19 · Engine Bleed Air SystemSDR CA090724001Actuator · failed(CAN) INBOUND OF LANDING DESTINATION, CREW RECEIVED A "MACH TRIM" AND "STAB TRIM" CAUTION MESSAGE. ABNORMAL PROCEDURES, DESCRIBED IN THE QUICK REFERENCE HANDBOOK (QRH), WERE EXECUTED AND THE ACFT LANDED WITHOUT FURTHER INCIDENT. BOTH STAB CHANNELS COULD BE ENJul 21, 2009 · Cndair CL6002B19 · Stabilizer Control SystemSDR CHQA200900159Oil System · lowFLIGHT 5531, SDF TO IAH. DURING CRUISE AT FL360, THE FLIGHT CREW RECEIVED A TRIPLE CHIME AND ENG OIL PRESS MESSAGE ON EICAS FOR E2. THE OIL PRESSURE WAS FLUCTUATING BETWEEN 20 AND 35 PSI. THE QRH WAS FOLLOWED AND THE ENGINE POWER WAS PULLED BACK TO IDLE. WJul 20, 2009 · N647BR · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA090722001Actuator · faulted(CAN) ON CLIMB, THE CREW RECEIVED A "MACH TRIM" AND "STAB TRIM" CAUTION MESSAGE. ABNORMAL PROCEDURE DESCRIBED IN (QRH) WAS COMPLETED AND DECISION WAS MADE TO TURN BACK. ACFT LANDED WITHOUT FURTHER INCIDENT. NEITHER OF HORIZ STAB TRIM CHANNEL 1 OR 2 COULD BE Jul 20, 2009 · Cndair CL6002B19 · Stabilizer Position IndicatingSDR CA090722010Cable · frayed(CAN) WHILE COMPLETING TASK RJ252-11-21-OP-801-FCD "PAX DOOR INNER HANDLE UNLOCK FORCE CHECK" DISCOVERED DOOR ICE BREAKER CABLE PN 601R318127-3 (IPC 52-11-15, FIG 01A, ITEM 085) BADLY FRAYED/ALMOST SEVERED. MX HAD FOUND A BROKEN CABLE ON ANOTHER ACFT A FEW DAJul 20, 2009 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA090722009Cable · broken(CAN) MX WHILE COMPLETING TASK RJ252-11-21-OP-801-FCD, "PAX DOOR INNER HANDLE UNLOCK FORCE CHECK" DISCOVERED DOOR COULD NOT BE OPENED FROM INSIDE. TROUBLSHOOTING DISCOVERED ICE BREAKER CABLE PN 601R318127-3 (IPC 52-11-15, FIG 01A, ITEM 085) BROKEN/SEVERED. CAJul 18, 2009 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CHQA200900156Element · intermittentFLIGHT 5516, IAH TO ATL. THE FLIGHT CREW REPORTED AN ANTI-ICE DUCT FAIL MESSAGE ON EICAS, WITH WING ANTI-ICE DUCT FAIL ILLUMINATED ON THE PUSH BUTTON. THE SYNOPTIC PAGE ON EICAS SHOWS THE LEFT-HAND FUSELAGE DUCT IN RED. THE AIRCRAFT WAS NEVER IN ICING CONDIJul 16, 2009 · N652BR · Cndair CL6002B19 · Overheat DetectionSDR CA090723003Element · damaged(CAN) FLT CREW REPORTED AN ANTI ICE DUCT FAIL MSG ON EICAS ALONG WITH ANTI-ICE DUCT FAIL SWITCH LIGHT. THE SYNOPTIC PAGE ON EICAS SHOWS LT FUSELAGE DUCT IN RED. ACFT WAS NEVER IN ICING CONDITIONS AND RETURNED TO AND LANDED WITHOUT FURTHER INCIDENT. MX FOUND Jul 16, 2009 · Cndair CL6002B19 · Overheat DetectionSDR CHQA200900155Clamp · looseFLIGHT 5531, SDF TO IAH. ON CLIMB OUT FROM SDF THE CREW RECEIVED L 10TH DUCT, ANTI ICE DUCT, AND L 14TH DUCT MESSAGES ON EICAS. THE QRH WAS FOLLOWED AND THE AIRCRAFT RETURNED TO SDF AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A LOOSE CLAMP ON THE 14TH STJul 15, 2009 · N652BR · Cndair CL6002B19 · Pneumatic Indicating SystemSDR MASA2009070700205Oil System · lowASH FLT 2930 PHX-TUS. CREW REPORTED DURING CLIMB LT ENG OIL TEMP REACHED 176*C AND CONTINUED TO CLIMB. CREW ELECTED TO SHUT DOWN THE ENGINE AND RETURN TO THE FIELD. AIRCRAFT DECLARED AND EMERGENCY, LANDED SAFELY AND TAXIED TO THE GATE WITHOUT FURTHER INCIDEJul 7, 2009 · N37178 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA090723001Stabilizer · stuck(CAN) STAB/MACH TRIM CAUTION MESSAGE. DISCONNECTED AUTOPILOT AFTER STAB MACH TRIM MESSAGE AND APPLIED QRH. CREW INDICATED THAT TRIM WAS STUCK AND WOULD NOT MOVE WITH QRH PROCEDURES. LANDED ACFT WITH FLAPS 20 NORMALLY.EMERGENCY SERVICES NOTIFED. NO ADDITIONJul 7, 2009 · Cndair CL6002B19 · Stabilizer Control SystemSDR CA090708008Indicator · malfunctioned(CAN) CREW SELECTED FLAP LEVER TO 8 DEGREES AND RECEIVED A FLAP FAIL CAUTION MESSAGE. MULTIFUNCTION DISPLAY (MFD) WAS INDICATING FLAP AT ZERO DEGREE. THERE WAS NO EMERGENCY DECLARED AND ACFT LANDED WITHOUT FURTHER INCIDENT. FLAP ELECTRONIC CONTROL UNIT (FECJul 6, 2009 · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR CA090703004Engine · inoperative(CAN) AT FL 250, LOSS OF PWR ON LT ENGINE. LT ENGINE THROTTLE RETARDED TO IDLE. UNABLE TO GET CLIMB THRUST ON LT ENGINE. LT ENGINE THROTTLE RETARDED TO IDLE. FLIGHT ABORTED AND RETURN TO ORIGIN AIRPORT. PROBLEM TO REACH TOP ON GROUND TESTINGS. REMOVED LT EJul 2, 2009 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR REXA200900072Thermocouple · defectiveON CLIMBOUT, RT ENGINE ITT BEGAN TO FLUCTUATE WILDLY. ALL OTHER ENGINE PARAMETERS WERE NORMAL. THE FLIGHT CREW PERFORMED THE QRH, DECLARED AN EMERGENCY AND REQUESTED TO RETURN TO DEPARTURE. AN OTHERWISE NORMAL APPROACH AND LANDING WERE MADE. CFR MET THE ACFJun 29, 2009 · N8505Q · Cndair CL6002B19 · Engine Temperature Indicating SystemSDR CA090629005Wheel · cracked(CAN) ON LANDING NR 1 MAIN WHEEL ASSY (PN 5010571-1, SN DEC98-0302), OUTER FLANGE (PN 5010581, IPC 32-41-00, FIG 5-40) DEPARTED WHEEL HUB ASSY FOLLOWED BY TIRE WHICH SHREDDED TO 2 LARGE PIECES. CREW DID NOT REALIZE THEY HAD LOST A TIRE UNTIL THE FOD WAS REPORJun 28, 2009 · Cndair CL6002B19 · Wheel/Ski/FloatSDR CA090703005Fcu · malfunctioned(CAN) "ENROUTE DECENT AT 300 KTS, FLAPS WERE DEPLOYING/RETRACTING BETWEEN 0-20 DEGREES ERRATICALLY WITH FLAP SELECTOR POSITION AT 0 DEGREES. RECEIVED INTERMITTENT "HYD PUMP 2B" CAUTION MESSAGE. RECEIVED "FLAPS DEGRADED" STATUS MESSAGE. SLOWING THROUGH 220 KTS Jun 28, 2009 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2009070100007Carbon Seal · defectiveCREW REPORTED RT ENGINE HAD LOW OIL PRESSURE. AIRCRAFT DIVERTED TO ATL LANDING WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED IDG CARBON SEALS ON RT ENGINE. CHECKS AND LEAK CHECKS WERE ACCOMPLISHED PER THE AIRCRAFT MAINTENANCE MANUAL. AJun 27, 2009 · N218PS · Cndair CL6002B19 · Turbine Engine Oil System
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