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 CA090624004Thermal Switch · failed(CAN) OPS CHECK OF WING DEICE STANDBY THERMAL SWITCHES WAS CALLED UP DURING A SCHEDULED "C" CHECK INSP. MOST OF THERMAL SWITCHES FAILED THE OPS CHECK. NEW SWITCHES WERE DRAWN FROM STOCK AND RETESTED PRIOR TO INSTALLATION. MOST OF THESE NEW SWITCHES TESTED Jun 24, 2009 · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR CA090624001Apu · inoperative(CAN) AT COMPLETION OF SECOND ENG START, GROUND CREW REPORTED A "POPPING" SOUND AND SMOKE COMING FROM APU EXHAUST. FLIGHT CREW OBSERVED APU SHUTTING DOWN AND APU DOOR CLOSING. NO SMOKE OR UNUSUAL ODORS WERE DETECTED IN CABIN OR COCKPIT. UPON FURTHER INVESTIGJun 19, 2009 · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) SystemSDR CA090616001Line · corroded(CAN) APU FEED LINE FAILED LEAK TEST & SHROUD REMOVED . FEED LINE FOUND HEAVILY CORRODED & LINE BROKEN DUE TO CORROSION . INSP AT FIRST REVEALED A DEPOSIT AT BOTTOM OF SHROUD. SHROUD ALSO CORRODED IN VARIOUS AREAS. PARTS HAVE BEEN REPLACED. SHROUD AND FUELJun 15, 2009 · Cndair CL6002B19 · APU Engine Fuel and ControlSDR CHQA200900145Generator · failedFLIGHT 5596, AMA TO IAH. DURING CRUISE THE FLIGHT CREW RECEIVED A GENERATOR 2 FAIL MESSAGE ON EICAS. THE AIRCRAFT DIVERTED TO DFW AND LANDED WITHOUT INCIDENT. THE GENERATOR WAS PLACED ON MEL AND THE AIRCRAFT WAS RELEASED FOR SERVICE. THE GENERATOR MEL WAS Jun 14, 2009 · N647BR · Cndair CL6002B19 · AC Generator-AlternatorSDR REXA200900071Blades · damagedON TAKEOFF, AIRCRAFT SUFFERED A BIRDSTRIKE TO THE LT ENGINE WHICH PRODUCED INCREASED N1 VIBRATION. THE FLIGHT CREW ELECTED TO RETURN AND NOTIFIED ATC. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE. MAINTENANCE INSPECTED THE ENGINE AND FOUND TWO DAMAGED Jun 14, 2009 · N8969A · Cndair CL6002B19 · Turbine Engine Air Inlet SectionSDR CHQA200900141Duct · dirtyFLIGHT 5512, SDF TO CLE. AT FL220 THE CREW RECEIVED A DISPLAY COOL MESSAGE ON EICAS. THE QRH WAS FOLLOWED AND IT WAS DECIDED TO DIVERT TO IND, WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE SYSTEM ON MEL AND THE AIRCRAFT CONTINUED ON THEJun 11, 2009 · N702BR · Cndair CL6002B19 · Air Distribution SystemSDR CHQA200900142Oil Filter · cloggedFLIGHT 5993, YQB TO IAH. AT FL360 THE FLIGHT CREW RECEIVED AN E2 OIL PRESSURE WARNING MESSAGE ACCOMPANIED BY THE OIL PRESSURE VARYING BETWEEN 22-40 PSI AND OIL TEMPERATURES AS HIGH AS 160 DEGREES. THE CREW DIVERTED TO CLE WHERE THE AIRCRAFT LANDED WITHOUT INJun 11, 2009 · N647BR · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA200940302Pressure Switch · malfunctioned204552/2 - ON CLIMBOUT, LT ENG OIL PRESS CAS WARNING MULTIPLE TIMES. ACCOMPANIED BY OIL PRESS OF 22-24 PSI UP TO 44 PSI. OIL TEMP WAS 10 DEGREES HIGHER THAN RT. WARNING WENT AWAY WITH POWER REDUCTION. REMOVED AND REPLACED LT LOW OIL PRESSURE SWITCH IAW AMMJun 9, 2009 · N467AW · Cndair CL6002B19 · Engine Oil PressureSDR MASA2009060300176Gearbox · faultyASH FLT 7346 EWR TO IAD - ABORTED TAKEOFF AND RETURNED TO GATE DUE TO NLG STRUT BOTTOMING OUT. WHEN FLIGHT CREW ABORTED TAKEOFF, BOTH ENGINES SHUT-DOWN. REPLACED NR 1 TGB, OP CHECK GOOD AND RT ENG OP CHECK GOOD.Jun 3, 2009 · N592ML · Cndair CL6002B19 · Turbine Engine Accessory DriveSDR CA090527004Window · failed(CAN) THE MSN 7190 IN ROUTE, EXPERIENCED THE RT WINDOW SHATTERING IN CRUISE. CREW COMPLIED WITH QRH AND MADE AN UNSCHEDULED LANDING.May 26, 2009 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA090616002Apu · smoke(CAN) FLT NR 2455, DURING TAXI OUT, FLT CREW REPORTED SMOKE IN THE CABIN WHEN THE APU BLEED WAS SELECTED. ACFT RETURNED TO GATE. MX REMOVED AND REPLACED APU ASSY IAW AMM.May 19, 2009 · Cndair CL6002B19 · APU Bleed Air SystemSDR CHQA200900126Oil Cooler · cloggedFLIGHT 5650, ELP TO IAH, DURING CRUISE WITH THE NR 2 IDG ON DEFERRAL, REQUIRING THE APU TO BE RUN THE ENTIRE FLIGHT, THE CREW RECEIVED AN APU HIGH OIL TEMPERATURE MESSAGE. THE QRH WAS FOLLOWED AND THE AIRCRAFT DIVERTED TO KMAF WERE IT LANDED WITHOUT INCIDENT.May 18, 2009 · N667BR · Cndair CL6002B19 · APU Oil SystemSDR SWIA200921630Engine · overtempFLT 6605 - NR 2 ENGINE OVERTEMP. REPLACED ENGINE.May 17, 2009 · N912SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA090521004Line · chafed(CAN) CREW REPORTED THAT THEY HAD AN OIL SMELL WHEN AIR CONDITIONING SYS WAS ON. APU AIR SUPPLY.TRAX DEFECT NR 846559 COMPLETED ON WO NR 191597 NR-001, APU FUEL LINE PN 3883449-1(FCU TO NOZZLES) WAS FOUND CHAFED THRU DUE TO THE MIGRATION OF THE APU INLET BELLOMay 15, 2009 · Cndair CL6002B19 · APU Engine Fuel and ControlSDR CA090514005Bearing · seized(CAN) DURING FUNCTION CHECKS AFTER A PCU REPLACEMENT, A BINDING NOISE WAS HEARD COMING FROM THE RT AILERON. THE RT AILERON PCU OUTPUT LINKS (PN 27295-5 IPC 27-14-01, FIG. 1-175A) WERE TAKEN APART. THE OTBD PCU OUTPUT LINK BRG WAS SEIZED SO THAT THE BOLT WAS ROMay 13, 2009 · Cndair CL6002B19 · Aileron Control SystemSDR SWIA190021555Engine · overtempFLT 6618 - RIGHT ENGINE VIBRATION INDICATION ENTERED RED ZONE AND TURBINE TEMPERATURE INDICATION SHOWED HIGH TEMPERATURE. ENGINE CHANGE IN PROGRESS.May 7, 2009 · N952SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA200921555Engine · overtempFLT 6618 - RIGHT ENGINE VIBRATION INDICATION ENTERED RED ZONE AND TURBINE TEMPERATURE INDICATION SHOWED HIGH TEMPERATURE. ENGINE CHANGE COMPLETED.May 7, 2009 · N952SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA090506010Fcu · failed(CAN) ON FLAP SELECTION FROM 20 TO 8 RECEIVED FLAP FAIL MESSAGE ON EICAS. CARRIED OUT UNSCHEDULED LANDING WITH 20 FLAP WITH NO FURTHER INCIDENT. FOUND FECU POWER LEDS AND RT PANEL LEDS ILLUMINATED ON SKEW DETECTION UNIT. RESET SDU AND FECU, CARRIED OUT OPS CK May 5, 2009 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CHQA200900116Oil System · lowFLIGHT 5607, CMH TO IAH - AT FL310 THE CREW RECEIVED AN APU OIL PRESSURE MESSAGE ON EICAS. THE CREW FOLLOWED THE QRH AND DIVERTED TO SDF WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE APU OIL LEVEL LOW. THE APU WAS SERVICED WITH 1QT OF BP2380 OIL IApr 28, 2009 · N701BR · Cndair CL6002B19 · APU Oil SystemSDR CHQA200900117Pressure Switch · faultyFLIGHT 5607, SDF TO IAH - AT FL280 THE CREW RECEIVED AN APU OIL PRESS MESSAGE ON EICAS. THE QRH WAS FOLLOWED AND THE AIRCRAFT DIVERTED TO AEX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE APU OIL LEVEL LOW. THE APU WAS SERVICED WITH 1QT OF BP2380 Apr 28, 2009 · N701BR · Cndair CL6002B19 · APU Oil SystemSDR CA090502003Apu · smoke(CAN) DURING TAXI OUT, COCKPIT BEGAN TO FILL WITH SMOKE SHORTLY AFTER, FLT CREW REPORTED APU OIL (C) MSG AND APU AUTO SHUTDOWN. COMPLIED WITH QRH AND RETURNED TO GATE. MX INSPECTED AND FOUND APU FAILED ALONG WITH CONTAMINATED COALESCER SOCKS. REMOVED AND REPApr 26, 2009 · Cndair CL6002B19 · APU Core EngineSDR CA090502004Engine · seized(CAN) ON CLIMB OUT, FLT CREW REPORTED TOILET SMOKE (W) MSG POSTED. COPLIED WITH QRH AND RETURNED TO DEPARTURE. TOILET SMOKE MSG EXTINGUISHED AFTER COMPLETION OF QRH CHECK. APU ASSY REPLACED AND OPS CHECKED. NO FUTHER DEFECTS NOTED. APU ASSY 3800488-3 P-1012 Apr 26, 2009 · Cndair CL6002B19 · APU Core EngineSDR CA090502002Actuator · disconnected(CAN) THE LT OTBD FLAP SHOWS T/E DISTORTION. CONTACTED ACFT SERVICE TO INSPECT. AFTER INSP, LOCAL MX REPORTS LT FLAP LOOKS TWISTED. CAUSE IS PROBABLE ACTUATOR BROKEN. SLC MX INSPECTED FLAP. LOOKS LIKE NR3 OTBD ACTUATOR HAD FAILED AND TWISTED FLAP. SLC MX REPLAApr 25, 2009 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CA090423002Window · cracked(CAN) F/O SIDE WINDOW CRACKED ON APPROACH AT ABOUT 4542 FT. THE F/OS SIDE WINDOW WAS REMOVED AND REPLACED IAW AMM 56-12-01 AND RII 56-220-1000. SIDE WINDOW- (RT) NP-139322-2 01101H5335.Apr 17, 2009 · Cndair CL6002B19 · Flight Compartment WindowsSDR CHQA200900108Power Cable · defectiveDURING INSPECTION THE FLOOR EMERGENCY LIGHTS NEAR ROW NR 1 WERE INOPERATIVE WHEN TESTED. THE LIGHT STRIP WAS SWAPPED WITH THE AFT STRIP AND THE FAULT FOLLOWED. THE LIGHT STRIP WAS LEFT IN THE AFT POSITION AND DEFERRED. THE FINAL CORRECTIVE ACTION WILL BE SApr 14, 2009 · N652BR · Cndair CL6002B19 · Light System WiringSDR CHQA200900105Warning Light · false activationFLIGHT 5503, SDF TO IAH - CREW RECEIVED A STEERING INOP MESSAGE ON EICAS, CREW ATTEMPTED RESET BUT MESSAGE WOULD NOT CLEAR. THE QRH WAS FOLLOWED AND THE NOSE STEERING WAS DEACTIVATED FOR LANDING. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED AApr 12, 2009 · N667BR · Cndair CL6002B19 · Landing Gear Steering SystemSDR SWIA200922035Turbine Case · crackedLEFT ENGINE TURBINE CASE CRACKED. (C CHECK) REPLACED ENGINE.Apr 12, 2009 · N449SW · Cndair CL6002B19 · Turbine SectionSDR SWIA200922036Turbine Case · crackedRIGHT ENGINE TURBINE CASE CRACKED. (C CHECK) REPLACED ENGINE.Apr 12, 2009 · N449SW · Cndair CL6002B19 · Turbine SectionSDR CHQA200900104Bulb · burned outDURING INSPECTION THE NR 2, 5, AND 6 EXTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE WHEN TESTED. THE BULBS IN ALL THREE LIGHTS WERE REPLACED AND THE EMERGENCY LIGHT SYSTEM OPERATED NORMALLY WHEN TESTED.Apr 8, 2009 · N469SM · Cndair CL6002B19 · Emergency LightingSDR CA090407019Window · cracked(CAN) RT SIDE WINDOW CRACKED CLIMBING THROUGH 30,600 FT. THE FLIGHT CREW COMPLIED WITH THE QRH AND RETURNED TO DEPARTURE. REMOVED AND REPLACED F/O RT SIDE WINDOW IAW MM 56-12-01, PRE-SB.Apr 5, 2009 · Cndair CL6002B19 · Flight Compartment WindowsSDR VNAA2009040600003Wire Harness · failedCREW REPORTED AFTER ENGINE START THE LEFT ENGINE ITT STABILIZED LOWER THAN NORMAL. AIRCRAFT RETURNED TO GATE IN CLT. MAINTENANCE REMOVED AND REPLACED THE LEFT ITT HARNESS PER THE MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.Apr 2, 2009 · N237PS · Cndair CL6002B19 · Engine Exhaust System WiringSDR REXA200900038Carbon Seal · failedAT 500 AGL, DURING INITIAL CLIMBOUT, TOWER INFORMED FLIGHT CREW THAT THEY HAD SEEN EXCESSIVE SMOKE COMING FROM REAR OF THE ACFT. THE TOWER OPERATOR INFORMED THE CREW THAT THE AMOUNT OF SMOKE WAS GREATER THAN SHE WAS ACCUSTOMED TO SEEING. THE FLIGHT REQUESTEMar 30, 2009 · N8745B · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CHQA200900088Duct · leakingFLIGHT 5541, LIT TO IAH. ON CLIMBOUT OF LIT THE CREW RECEIVED A CARGO BTL LO CAUTION MESSAGE. THE QRH WAS FOLLOWED AND IT WAS DECIDED TO RETURN TO LIT WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A BROKEN DUCT COMING OFF THE LEFT PACK HEAT Mar 25, 2009 · N484CA · Cndair CL6002B19 · Air Distribution SystemSDR CHQA200900089Light · inoperativeDURING INSPECTION, THE EMERGENCY LIGHTS FOR THE RIGHT OVERWING FORWARD AND MIDDLE EXTERIOR LIGHTS, PASSENGER DOOR, AND CEILING LIGHTS 1, 2, 4 WERE FOUND INOPERATIVE. ALL LIGHTS WERE RE-LAMPED AND OPERATED NORMALLY.Mar 25, 2009 · N465SM · Cndair CL6002B19 · Emergency LightingSDR CA090405001Duct · leaking(CAN) ON CLIMB OUT, THE CREW REPORTED A CARGO BTL LO CAUTION MESSAGE. THE QRH WAS FOLLOWED AND IT WAS DECIDED TO RETURN TO WHERE THE ACFT LANDED WITHOUT INCIDENT. MX FOUND A BROKEN DUCT COMING OFF THE LT PACK HEAT EXCHANGER THAT HAD CAUSED THE BOTTLE TO DISCHMar 25, 2009 · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA200940143Fan Blade · damagedON CLIMB, BIRD STRIKE IN RT ENGINE IMMEDIATELY AFTER SMOKE ODOR IN CABIN, RETURNED TO DEPARTURE. LANDED OVERWEIGHT 47,500 IN., RATE OF DESCENT, 300 FT PER MINUTE. REMOVED AND REPLACED 10 FAN BLADES. DAMAGED ONES AND BLADES 180 DEGREE OUT IAW AMM 72-20.Mar 21, 2009 · N422AW · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR CA090326016Coalescer Bag · odor(CAN) AT FL230, FLT CREW REPORTED THAT WHEN TURNING UP TEMP ON LT PACK, THEY GOT A STRONG BURNED OIL ODOR IN THE COCKPIT. THEY DESCENDED AND TURNED LT PACK OFF AND ODOR WENT AWAY. THE ACFT CONTINUED ON AND LANDED WITHOUT ANY FURTHER INCIDENTS. MX INSPECTED ACMar 19, 2009 · Cndair CL6002B19 · Humidity Control SystemSDR CA090326017Windshield · failed(CAN) FLT 2428, AFTER DEPARTURE FROM DAY, THE FLT CREW REPORTED A L WINDSHIELD HEAT (C) MSG JUST BEFORE THE CAPTAINS WINDSHIELD SHATTERED (AT FL250). THE ACFT RETURNED TO DAY AND LANDED WITHOUT FURTHER INCIDENT. MX REMOVED AND REPLACED THE LT WINDSHIELD AND LMar 16, 2009 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA090405002Actuator · malfunctioned(CAN) FLAP FAIL MSG POSTED AT 41 DEG WHEN FLAPS SELECTED TO 45 DEG ON APPROACH. ACFT LANDED WITHOUT FURTHER INCIDENT. BRAKE TEMP 4,3,4,4. MX REMOVED AND REPLACED RT INBD OUTER FLAP ACTUATOR AND OPS CHECKED FLAP SYS. NO FURTHER DEFECTS NOTED. ACFT RETURNED TO Mar 15, 2009 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CHQA200900079Battery Pack · dischargedDURING INSPECTION THE NR 3 EMERGENCY LIGHT BATTERY PACK WAS FOUND TO INOP. THE NR 3 EMERGENCY LIGHT BATTERY PACK WAS REPLACED AND THE EMERGENCY LIGHT SYSTEM OPERATED NORMALLY.Mar 13, 2009 · N470SM · Cndair CL6002B19 · Emergency LightingSDR CHQA200900078Light · inoperativeDURING INSPECTION THE RIGHT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOP. THE LIGHT WAS RE-LAMPED AND OPERATED NORMALLY.Mar 12, 2009 · N701BR · Cndair CL6002B19 · Emergency LightingSDR VNAA2009031600008Pump · failedCREW REPORTED IN CRUISE THE RT ENGINE OIL PRESSURE AND OIL TEMPERATURE HIGH. AIRCRAFT DIVERTED TO CAK AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND CARBON PIECES IN SCREEN LUBE AND SCAVENGE OIL PUMP. MAINTENANCE REMOVED AND REPLACED THE RT ENMar 12, 2009 · N218PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA090319005Scavenge Pump · contaminated(CAN) FLT CREW REPORTED IN CRUISE THE RT ENGINE OIL PRESSURE AND OIL TEMPERATURE HIGH. ACFT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MX INVESTIGATION REPORTED CARBON PIECES IN SCREEN LUBE AND SCAVENGE OIL PUMP. REMOVED AND REPLACED RT ENGINE OIL PUMP. Mar 12, 2009 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CHQA200900073Pressure Sensor · false indicationFLIGHT 5517, MCI TO IAH. THE CREW REPORTED THAT DURING CRUISE THE OIL PRESSURE DROPPED TO 2 PSI WITH 94% N1. THEY STARTED TO DESCEND AND PULLED THE THROTTLES BACK TO 86% AND THE OIL PRESSURE STABILIZED AT 80PSI. THE AIRCRAFT THEN DIVERTED TO TUL WHERE IT LANMar 8, 2009 · N648BR · Cndair CL6002B19 · Engine Oil Indicating SystemSDR CHQA200900071Warning System · malfunctionedFLIGHT 5994, HOT TO HOT (CHECK FLIGHT) - DURING DESCENT BACK INTO HOT DURING A MAINTENANCE FLIGHT THE CREW RECEIVED A LOW OIL PRESSURE WARNING. THE QRH WAS FOLLOWED AND E2 WAS SHUT DOWN. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED AN ENGINE Mar 6, 2009 · N648BR · Cndair CL6002B19 · Engine Oil PressureSDR CHQA200900069Trim Switch · faultyFLIGHT 5737 - IAH TO HRL. THE CREW RECEIVED A STAB TRIM DISCONNECT MESSAGE AFTER TAKEOFF AND RETURNED TO FIELD. THE FAULT WAS TRACED TO A FAULTY CO-PILOTS PITCH TRIM DISCONNECT SWITCH. THE SWITCH WAS REPLACED AND THE SYSTEM OPERATED NORMALLY.Mar 3, 2009 · N653BR · Cndair CL6002B19 · Stabilizer Control SystemSDR CA090312013Electrical Sys · fire(CAN) IT WAS REPORTED THAT AFTER STARTING THE APU THE CAPTAIN NOTED THE OVERHEAD COCKPIT AREA BEGAN TO FILL WITH HEAVY BLACK SMOKE. THE COCKPIT AREA CONTINUED TO BURN RESULTING IN AN OVAL SHAPED 18 INCH HOLE THAT HAD BURNED THROUGH THE UPPER COCKPIT CANOPY ARMar 1, 2009 · Cndair CL6002B19 · Electrical Power SystemSDR REXA2009F00028Engine · flamed outON APPROACH, ATC ISSUED DESCENT CLEARANCE TO 9000. BOTH THRUST LEVERS WERE REDUCED TO IDLE AT WHICH POINT THE FLIGHT CREW NOTICED A SEVERE YAW IN THE ACFT AND RT ENG OIL PRESSURE MASTER WARNING. ECIAS INDICATED A FLAMEOUT OF THE RT ENGINE. THE FLIGHT CREW DFeb 28, 2009 · N8665A · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA090225012Engine · flamed out(CAN) DUAL ENGINE FLAME OUT ON DESCENT. PRELIMINARY INFORMATION (VERBAL)- SUBJECT TO CHANGE: FLIGHT 8876, ON DESCENT, DUAL ENGINE FLAME OUT. ADG AUTO DEPLOYED. BOTH ENGINES RE-STARTED SUCCESSFULLY USING WIND MILLING PROCEDURE. ACFT LANDED AT DESTINATION. FDFeb 24, 2009 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA090223011Carbon Seal · leaking(CAN) ON CLIMB AT FL 180, VISIBLE SMOKE IN CABIN COMPARTMENT AND "SMOKE TOILET" MESSAGE ON ED1. FLIGHT ABORTED, ACFT LANDED AT ORIGIN AIRPORT. MX FOUND LT NR 1 CARBON SEAL LEAKING. LT NR 1 CARBON SEAL REPLACED IAW AMM 72-20-00-000/400-802. CARBON SEAL ELEMFeb 23, 2009 · Cndair CL6002B19 · Engine (Turbine/Turboprop)
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