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 CA070607011Fcu · malfunctioned(CAN) (FLAPS FAIL) MESSAGE DISPLAYED ON APPROACH. FLAPS FAILED WHEN SELECTING FROM FLAP 20 DEGREES TO FLAPS 30 DEGREES. FLAPS REMAINED AT 20 DEGREES AT A SPEED OF 170 KIAS. MAINTENANCE REPLACED FECU (FLAPS ELECTRONIC CONTROL UNIT) DUE TO UNABLE TO TEST AND Jun 6, 2007 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA070601004Wire · burned(CAN) FLAP FAIL MESSAGE COME ON DURING CRUISE AT ALT FL330 WITH NO FLAP SELECTION MADE. AIRCRAFT RETURN TO ORIGINATING STATION, MAINTENANCE REPLACED THE BPSU AND FECU BUT NO FIX. FURTHER INVESTIGATION REVEALED SOME BURNED WIRES AT LT BPSU CONNECTOR. TEMPORAMay 29, 2007 · Cndair CL6002B19 · Flight Control System WiringSDR CA070531002Engine · vibration(CAN) AIRCRAFT (FLT 4344) WAS ENROUTE WHEN CREW EXPERIENCED AN UNCONTROLLABLE VIBRATION FROM THE RT ENGINE. THE ENGINE WAS SHUTDOWN IN FLIGHT. THE AIRCRAFT WAS DIVERTED AND LANDED AT TRI. IT WAS REPORTED BY THE CREW (TO MAINT CONTROL) THAT THE RT THROTTLE WAMay 24, 2007 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA0670390Engine · overtempFLIGHT 4988 - DURING TAKEOFF ROLL THE RIGHT ENGINE ITT INDICATED 905C, ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED THE RIGHT ENGINE ASSEMBLY.May 21, 2007 · N965CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA070520001Landing Gear · collapsed(CAN) UPON ARRIVAL CREW HAD A SUSPECTED HARD LANDING, STAB TRIM AURAL WARNING CLACKER SOUNDED AND BOTH MAIN GEAR COLLAPSED. THERE WAS MAJOR STRUCTURAL DAMAGE AND PRELIMINARY REVIEW OF PICTURES SHOWS EXCESSIVE ENGINE BLADE DAMAGE DUE TO DEBIS INGESTION, FURTHERMay 20, 2007 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR CA070521001Landing Gear · collapsed(CAN) UPON ARRIVAL, CREW HAD A SUSPECTED HARD LANDING. STAB TRIM AURAL WARNING CLACKER SOUNDED AND BOTH MAIN GEAR COLLAPSED. THERE WAS MAJOR STRUCTURAL DAMAGE AND A PRELIMINARY REVIEW OF THE PICTURES SHOWS EXCESSIVE ENGINE BLADE DAMAGE DUE TO DEBRIS INGESTION.May 20, 2007 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR CA070518006Pseu · malfunctioned(CAN) IN CRUISE FLIGHT CREW RECEIVED PROX SYS CHAN FAULT CAUTION MESSAGE AS WELL AS (3) RED GEAR INDICATIONS, IAW AFM HAD TO PERFORM ALTERNATE EXTENSION, FLIGHT LANDED WITHOUT INCIDENT. AFTER MAINTENANCE TROUBLESHOOTING THE MDC IS POINTED TOWARDS THE PSEU ITSMay 16, 2007 · Cndair CL6002B19 · Landing Gear Position and WarningSDR CA070506002Nose Cowl · damaged(CAN) DURING A SCHEDULED MAINTENANCE CHECK, AFTER FAN COWL RT REMOVAL, STRUCTURAL DAMAGE WAS OBSERVED ON THE INLET COWL BY THE CAPPED 14TH STAGE BLEED AIR DUCT. DAMAGE WAS OBSERVED ON THE REMOVED FAN COWL, SAME AREA, AS WELL. MAINTENANCE PROCEED TO REPLACE THMay 5, 2007 · Cndair CL6002B19 · Engine Cowling SystemSDR CA070505001Window · cracked(CAN) THE CAPTAIN`S SIDE WINDSCREEN OUTER PANE CRACKED. THE FLIGHT WAS AT 34000FT, WHEN THE INCIDENT OCCURRED, THEN THEY DESCENDED AND DAWNED THEIR OXYGEN MASKS AS A PRECAUTION. THERE WAS NO PRESSURE LOSS AND NO EMERGENCY DECLARED. MAINTENANCE INSPECTED THE AIMay 1, 2007 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA070423004Wire Harness · chafed(CAN) SHORTLY AFTER T/O, THE RT ENGINE VIBRATION INDICATOR FLUCTUATED ERRATICALLY THE WENT TO DASHES MOMENTARILY THEN RETURNED TO NORMAL OPERATION. FLIGHT RETURNED FOR MAINTENANCE TROUBLESHOOTING. AFTER CHANGING THE ENGINE ACCELEROMETER AND SIGNAL CONDITIONEApr 21, 2007 · Cndair CL6002B19 · Turbine Engine System WiringSDR COMA0760318Warning Message · illuminatedDURING CLIMB RECEIVED AN A/ICE DUCT WARNING MSG, FLIGHT RETURNED TO JFK. PERFORMED ENGINE RUNS WITH A/ICE SYSTEM ON, DISCREPANCY COULD NOT BE DUPLICATED.Apr 14, 2007 · N917CA · Cndair CL6002B19 · Central WarningSDR COMA0760316Warning Message · illuminatedFLAPS FAIL CAUTION MESSAGE DURING TAXI IN. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE (FIRST EVENT) MAINTENANCE ACTION, PARAGRAPH (G) 1,2,3, (A,B,C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.Apr 13, 2007 · N916CA · Cndair CL6002B19 · Central WarningSDR CA070416005Connector · contaminated(CAN) ON APPROACH NOSE LANDING GEAR DID NOT EXTEND. CREW CARRIED OUT A GO-AROUND AND COMPLETED A MANUAL EXTENSION. THE GEAR LOWERED AND LOCKED-CREW RECEIVED 3 GREENS IN THE COCKPIT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO TROUBLApr 13, 2007 · Cndair CL6002B19 · Landing Gear System WiringSDR CA070412002Wheel · cracked(CAN) DURING ROUTINE NDT HFEC INSP OF MAIN WHEELS, ACCORDING TO ABSC NDT MANUAL PART 1, CH. 32-42-03, CRACKS WERE FOUND IN THE LOCKING RING GROOVE. THE DEPTH OF 3 CRACKS IS GREATER THAN .040 INCH AND THE LENGTH OF THE CRACKS ARE 30MM, 20MM AND 5MM. ONE CRACK HApr 11, 2007 · Cndair CL6002B19 · Wheel/Ski/FloatSDR CA070412003Wheel · cracked(CAN) DURING ROUTINE NDT HFEC INSP OF RJ MAIN WHEELS, ACCORDING TO NDT MANUAL PART 1, CH. 32-42-03, CRACKS WERE FOUND IN THE LOCKING RING GROOVE. THE DEPTH OF 3 CRACKS IS GREATER THAN .040 INCH AND THE LENGTH OF THE CRACKS ARE 30MM, 20MM AND 5MM. ONE CRACK HASApr 11, 2007 · Cndair CL6002B19 · Wheel/Ski/FloatSDR COMA0760299Engine · damagedFLIGHT 5226 - PRONOUNCED VIBE DURING TAKEOFF. ABORTED TAKEOFF. MDC SHOWS VIBE AND ITT EXCEEDANCES. FAN CANNOT BE TURNED BY HAND. REPLACED LEFT ENGINE ASSEMBLY.Apr 4, 2007 · N810CA · Cndair CL6002B19 · Turbine SectionSDR CA070405009Relay · burned(CAN) DURING CRUISE IB, FLIGHT CREW NOTICED AN AC ESSENTIAL BUS MESSAGE FOLLOWED BY A POPPING SOUND AND A BURNED ODOR ON THE FLT DECK. LOOKED AT AC ELECTRICAL SYNOPTIC PAGE AND EVERYTHINGS WAS NORMAL BUT THE F/A NOTICED THAT THE EMERGENCY LIGHTS WERE ON. FLIGHApr 3, 2007 · Cndair CL6002B19 · AC Power Distribution SystemSDR COMA0760274Pump · malfunctionedFLIGHT 5428 - LEFT ENGINE FLAMED OUT ON APPROACH, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED LEFT FUEL PUMP. NO FURTHER DEFECTS.Mar 21, 2007 · N810CA · Cndair CL6002B19 · Engine Fuel PumpSDR COMA0760275Fuel Control · malfunctionedFLIGHT 5428 - LEFT ENGINE FLAMED OUT ON APPROACH, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE FUEL CONTROL. NO FURTHER DEFECTS.Mar 21, 2007 · N810CA · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR CA070315002Socket · burned(CAN) REF LOG PAGE NR 593976. F/A REPORTS ELECTRICAL SMELL IN FORWARD CABIN, AROUND ROW 2 AND 3. 4FD SIDEWALL LIGHT HOLDER FOUND AT FAULT, CBP2 C/B S5 OPENED AND SECURED. SIDEWALL LIGHT INOP, DEFERRED IAW MEL 33-21-01 CAT (C). SOCKET ASSY P/N BB1-0020-02-58 (Mar 13, 2007 · Cndair CL6002B19 · Passenger Compartment LightingSDR COMA0760241Compressor · contaminatedFLIGHT 5307 - DURING CLIMBOUT OF TUL EVIDENCE OF SMOKE IN CABIN AND COCKPIT, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. PERFORMED ENGINE RUNS TO REMOVE RESIDUAL COMPRESSOR WASH FLUID.Mar 9, 2007 · N927CA · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR CA070301002Fitting · cracked(CAN) BOTH MAIN LANDING GEAR FITTING FOUND CRACKED ON NDT INSPECTION IAW ADCF-1999-32R3. MAIN LANDING GEAR WILL BE REPLACED. LT P/N 5321103 S/N PO-422V5Q, RT P/N 3521104 S/N PO-BBBB10. (TC NR 20070301002)Feb 28, 2007 · Cndair CL6002B19 · Fuselage, Landing Gear Attach FittingsSDR CA070302001Wire · damaged(CAN) AFTER A NORMAL LANDING AND WHILE TAXING TO THE GATE, THE FLT CREW REPORTED INTERMITTENT ARCING AND SMOKE COMING FROM BEHIND THE CAPTAINS SIDE CB PANEL. AIRCRAFT DEPLANED NORMALLY. ELECTRICAL POWER WAS SHUT DOWN AND FIRE CREW WERE CALLED TO CHECK OF FIRFeb 28, 2007 · Cndair CL6002B19 · Electrical Power System WiringSDR CA070321005Wire · burned(CAN) AFTER LANDING ELECTRICAL SHORT/ARCING BEHIND CAPTAINS SEAT IN CIRCUIT BREAKER PANEL. SOME SMOKE OBSERVED. AC TAXIED CLEAR OF ACTIVE RUNWAY. SMOKE AND SPARKS STOPPED, AIRCRAFT TAXIED TO RAMP, PRIOR TO ARRIVAL AT GATE SPARKS RE-OCCURRED. AIRCRAFT STOPPED AFeb 28, 2007 · Cndair CL6002B19 · Electrical Power System WiringSDR COMA0760200Engine · power lossFLIGHT 5103 - DURING ADDITION OF POWER FOR TAKEOFF NR 2 ENGINE WILL NOT SPOOL ABOVE 30 PERCENT. ABORTED TAKEOFF AT 15 KTS. INSPECTED ENGINE, NO DEFECTS NOTED. PERFORMED LOW AND HIGH POWER RUNS, NO DEFECTS NOTED (CND).Feb 19, 2007 · N784CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA070219001Fan Blade · bent(CAN) FEB 16/07, AIR TURN BACK. THE CREW REPORTED THAT AFTER TAKEOFF A LOUD RUMBLING NOISE WAS HEARD. CREW BELIEVED THAT ICE MAY HAVE BEEN INGESTED INTO THE RT ENGINE DURING LANDING ON THE PREVIOUS LEG INBOUND TO DESTINATION. MAINTENANCE CONFIRMED SEVERAL FANFeb 16, 2007 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR CA070222001Wire Harness · chafed(CAN) DURING ROUTINE MAINTENANCE INSPECTION , FOUND WIRING HARNESS ON NR1 ENGINE FOR THRUST REVERSER STOW SWITCH WIRING CHAFING ON EDGE OF LIGHTENING HOLE OF MOUNTING BRACKET. DAMAGED WIRING CUT OFF AND END RE-TERMINATED. MFG ILLUSTRATED PARTS CATALOG (CSP A-0Feb 12, 2007 · Cndair CL6002B19 · Engine Exhaust System WiringSDR CA070222002Skin · dented(CAN) CREW REPORTED BIRDSTRIKE ON APPROACH, MAINTENANCE INSPECTION FOUND DENT IN LT WING LEADING EDGE APPROX 6 FT OB FROM FUSELAGE. DENT ALLOWABLE IAW SRM LIMITS. (TC NR 20070222002)Feb 12, 2007 · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA0760152Loop · faultyFLIGHT 5204 - LT AND RT ANTI-ICE DUCT MESSAGE ON TAKEOFF ROLL. LT AND RT ANTI-ICE BLEED LOOPS SHORTED TO GROUND. REPLACED LT FUSELAGE BLEED LOOP. NO FURTHER DEFECTS.Feb 4, 2007 · N983CA · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR CA070201004Wire · broken(CAN) APPROX 1 MILE OUTSIDE THE OUTER MARKER AT 3000 AGL, THE AMBER FLAP CAUTION LIGHT ILLUMINATED. THE CREW SELECTED FLAP 20 AND THE FLAPS WENT TO 20. WHEN THE LIGHT ILLUMINATED THE CREW WENT THROUGH THEIR EMERGENCY CHECKLIST AND CARRIED OUT AN UNEVENTFUL LAFeb 1, 2007 · Cndair CL6002B19 · Flight Control System WiringSDR CA070207002Striker · damaged(CAN) DURING A TYPE III REPAIR (MFG REO 601R-53-22-033) DUE TO A CRACK FOUND ON THE OUTER FLANGE OF THE PASSENGER DOOR FWD SEAL STRIKER, THE FORWARD SEAL STRIKER FLANGE WAS FOUND CRACKED IN THE RADIUS (OVER 3INCHES IN LENGTH) UNDER AN EXISTING REPAIR (REPAIR Jan 31, 2007 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA070131002Flap System · malfunctioned(CAN) THE CREW REPORTED THAT ON APPROACH THAT THEY RECEIVED AN INITIAL FLAP HALFSPEED MESSAGE FOLLOWED BY A (FLAP FAIL) MESSAGE WHEN FLAPS SELECTED ON APPROACH. ZERO FLAP LANDING WAS COMPLETED. THE AIRCRAFT IS CURRENTLY WITH LINE MAINTENANCE TROUBELSHOOTING TJan 31, 2007 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA070131003Flap System · failed(CAN) THE CREW REPORTED THAT UPON APPROACH FLAPS 8 DEGREES WERE SELECTED OKAY. UPON FLAP 20 DEGREE SELECTION, THE FLAPS DID NOT MOVE AND THE FLAP FAIL CAUTION LIGHT ILLUMINATED. THE FLAPS LOCKED AT 8 DEGREES. THE AIRCRAFT IS CURRENTLY IN LINE, MAINTENANCE IS TJan 30, 2007 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA070128002Apu · contaminated(CAN) SHORTLY AFTER DEPARTURE, THE CREW NOTICED A LAV SMOKE WARNING AND SMOKE WAS VISIBLE IN THE CABIN FOR 3-4 MINUTES THEN IT DISSIPATED. SMOKE WAS BLUISH IN COLOR AND OILY SMELLING. (2) MAINTENANCE PERSONNEL WERE ON BOARD, INITIALLY THEY THOUGHT SINCE THE AJan 26, 2007 · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) SystemSDR CA070202002Line · chafed(CAN) JANUARY 296/2007 DEFECT 591259, THERE WAS A FUEL SMELL COMING FROM THE APU BLEED. THE APU WAS DEFERRED AND INHIBITED IAW MEL 49-10-01-1. JANUARY 29/2007 MAINTENANCE REPLACED THE ECU FOR TROUBLESHOOTING, BUT THERE WAS NO FIX. FEBRUARY 01/2007 FURTHER TRJan 26, 2007 · Cndair CL6002B19 · APU Engine Fuel and ControlSDR CA070123008Fairlead · worn(CAN) DURING MAINTENANCE INSPECTION , FOUND AFT FUSELAGE EQUIPMENT BAY HYDRAULIC LINE CLAMPS (FAIRLEAD), WITH CENTER (PRESSURE LINE) HOLES WORN THROUGH RUBBER/SILICON COMPOUND AND ALLOWING TUBING TO CHAFE ON METAL PORTION OF BLOCK. BLOCK PN TA3050024-03 CONSIJan 23, 2007 · Cndair CL6002B19 · Nacelle/Pylon, Attach FittingsSDR CA070123002Flap System · jammed(CAN) AIRCRAFT HAD A FLAPLESS LANDING, AFTER FLAP SELECTION 8, LT FLAP INDICATED ZERO, RT UNKNOWN, CREW THEN SELECTED TO 20 AND FLAPS TRAVELED TO APROX 5 DEGREES INDICATION WAS GREEN TRAVELED TO 5 DEGREES AND THEN TURNED WHITE. CREW THEN RETRACTED FLAPS BACK TJan 22, 2007 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA070124001Computer · malfunctioned(CAN) JUST PRIOR TO TOP OF CLIMB, LEFT FUEL QUANTITY AND TOTAL FUEL QUANTITY STARTED TO REDUCE, FOLLOWED BY FUEL IMBALANCE MESSAGE. CREW ELECTED TO RETURN TO DEPARTURE AIRPORT. ON FINAL APPROACH FUEL INDICATIONS RETURNED TO NORMAL. FUEL SYSTEM INSPECTED, WITH Jan 22, 2007 · Cndair CL6002B19 · Fuel Indicating SystemSDR CA070123005Actuator · worn(CAN) ON FINAL APPROACH CREW SELECTED FLAPS 20 DEGREES. FLAPS STUCK AT 8 DEGREES AND CREW RECEIVED A FLAP FAIL MESSAGE. CREW BROKE OFF APPROACH AND CONTACTED DISPATCH. AIRCRAFT SUBSEQUENTLY LANDED WITHOUT INCIDENT WITH FLAPS AT 8 DEGREES. MAINTENANCE TROUBLESHJan 18, 2007 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CA070118008Actuator · contaminated(CAN) ON APPROACH CREW REPORTED A FLAPS FAIL MESSAGE AFTER SELECTION TO 8 DEGREES. FLIGHT COMPLETED A FLAPLESS LANDING WITHOUT INCIDENT. AIRCRAFT THEN COMPLETED A FERRY FLIGHT. TROUBLESHOOTING OF FAULT CODES AND REPAIRS CURRENTLY ONGOING BY MAINTENANCE. THE RTJan 17, 2007 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CA070123013Hose · leaking(CAN) ON FINAL APPROACH WITH GEAR DOWN AND AT 2000FT THE MESSAGE HYD NR3 LOW PRESS CAME ON EICAS WITH THE HYDRAULIC NR3 RESERVOIR LEVEL AT 0 PERCENT. CREW COMPLIED WITH QRH. THE AIRCRAFT LANDED NORMALLY AND DEPLOYED THE THRUST REVERSER , THE GROUND SPOILERSJan 17, 2007 · Cndair CL6002B19 · Hydraulic System, MainSDR CA070118009Line · loose(CAN) ENROUTE CREW ADVISED THAT THEY HAD LOST NR 2 HYDRAULIC SYSTEM AND WERE DIVERTING. CREW DECLARED AN EMERGENCY AND ADVISED PASSENGERS OF REASON. WHEN THE INCIDENT HAPPENED THE CREW HAD A HYD 2 LOW PRESSURE MESSAGE, WHEN THEY TURNED ON NR 2 PUMP (HYD PUMJan 16, 2007 · Cndair CL6002B19 · Hydraulic System, MainSDR CA070111006Flap · frozen(CAN) FLAP FAIL AT 20. ON APPROACH, ON FLAP EXTENSION, THEY FROZE AT 20 DEGREES. OAT WAS ABOUT -25 DEGREES C AT THE TIME, ALTHOUGH THEY WERE ABOUT 1 HOUR AND 10 MINUTES IN FLIGHT AT ABOUT -50 DEGREES FOR MOST OF THE FLIGHT. AIRSPEED WAS 170 KNOTS AT THE TIMEJan 10, 2007 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA070111011Flap · obstructed(CAN) FLAPS FAILED ON RETRACTION AFTER LANDING L 5 DEG, R 6 DEG. AFTER LANDING, FOUND SNOW COMPACTED, ALL SNOW REMOVED, FLAPS CYCLED. (TC NR 20070111011)Jan 10, 2007 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA070111003Flap System · jammed(CAN) FLAPS FAILED ON APPROACH WHEN SELECTED TO 8 DEGREES, FLAPS DID NOT MOVE AND FLAP FAIL EICAS MESSAGE, OAT WAS -30 DEGREES ON APPROACH, DURING CRUISE -58 DEGREES C, FAULTS CODES BEING RETRIEVED AND AIRCRAFT BEING PREPARED FOR FERRY FOR FOLLOW UP. (801573 1Jan 9, 2007 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA070105001Radome · bird strike(CAN) AFTER DEPARTURE CREW WITNESSED A BIRD STRIKE ON THE NOSE OF THE AIRCRAFT. CREW ELECTED TO RETURN TO DEPARTURE AIRPORT AND LAND OVERWEIGHT (ESTIMATED AT 49200 LBS). AIR TRAFFIC CONTROL WAS NOTIFIED BUT EMERGENCY EQUIPMENT WAS NOT REQUIRED. MAINTENANCE INDec 30, 2006 · Cndair CL6002B19 · Aerodynamic FairingsSDR CA061229002Receptacle · damaged(CAN) DURING CLIMB, PASSENGER ALERTED FA TO SMOKE SMELL IN REAR OF CABIN. SMOKE WAS THEN VISIBLY OBSERVED BY PASSENGERS AND FA. FLIGHT RETURNED TO DEPARTURE AIRPORT AND ERS WAS REQUESTED. AIRCRAFT WAS APPROX 2000 LBS OVERWEIGHT BUT LANDED AND TAXIED TO THE GATDec 27, 2006 · Cndair CL6002B19 · Passenger Compartment LightingSDR CA070104002Fcu · malfunctioned(CAN) (DIVERTED, WITH ENGINE PROBLEMS, CREW CALLED WHEN ON GROUND. ON APPROACH, THE LT ENGINE WOULD NOT IDLE BACK BELOW 79 PERCENT N1. IT WOULD RESPOND TO INPUTS ABOVE 79 PERCENT. CREW ELECTED TO SHUTDOWN THE ENGINE, AND DIVERT.) MX WAS UNABLE TO DUPLICATE Dec 24, 2006 · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR CA061214001Flap System · malfunctioned(CAN) ON APPROACH THE CREW SELECTED FLAP 40 AND THE FLAPS FAILED AT 20 DEGREES. THE AIRCRAFT LANDED WITHOUT INCIDENT AND WAS LATER FERRIED WHERE IT IS CURRENTLY UNDERGOING INSPECTION. (TC NR 20061214001)Dec 13, 2006 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0660700Strut · underservicedAFTER TAKE-OFF AT APPROXIMATELY 145 KTS, GEAR DISAGREE MESSAGE ILLUMINATED, NOSE GEAR HAD RED HASH MARKS AND AFTER 10 SECONDS NOSE GEAR RETRACTED. AIRCRAFT RETURNED AND LANDED SAFELY. INSPECTED AIRCRAFT AND FOUND NOSE STRUT DID NOT FULLY EXTEND DURING JACKINDec 8, 2006 · N933CA · Cndair CL6002B19 · Main Landing Gear Strut/Axle/Truck
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