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"

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 COMA0860396Sensing Element · failedFLIGHT NR 6264 ON CLIMBOUT FROM GSO TO CVG RECEIVED RT ENGINE 14TH STAGE DUCT MSG. PERFORMED QRH, EMERGENCY DECLARED. A/C DIVERTED TO ROA AND LANDED SAFELY. R&R RT PYLON SENSING ELEMENT A58WK.Sep 28, 2008 · N523CA · Cndair CL6002B19 · Overheat DetectionSDR CA081003001Window · cracked(CAN) CAPTAINS SIDE WINDOW CENTER PANE SHATTERED ENROUTE. MX CHANGED THE WINDOW.Sep 26, 2008 · Cndair CL6002B19 · Flight Compartment WindowsSDR CHQA200800188Inverter · inoperativeTHE EMERGENCY LIGHT TRACK IN FRONT OF THE EMERGENCY EXIT WOULD NOT ILLUMINATE. MX TROUBLESHOT THE FAULT AND FOUND THE EMERGENCY LIGHT INVERTER OVER THE EMERGENCY EXIT TO BE BAD. THE INVERTER WAS REPLACED AND THE EMERGENCY LIGHTS OPERATED NORMALLY.Sep 24, 2008 · N470SM · Cndair CL6002B19 · Emergency LightingSDR CHQA200800185Control Panel · faultedFLIGHT 5601 IAH TO JAX. DURING FLIGHT THE CREW RECEIVED AN E2 REV ICON INTERMITTENTLY. THE REVERSER DID NOT DEPLOY. THE FLIGHT LANDED WITHOUT INCIDENT. THE REVERSER WAS PLACED ON MEL AND THE ACFT WAS RELEASED BACK TO SERVICE. THE MEL WAS CLEARED ON THE 22Sep 21, 2008 · N701BR · Cndair CL6002B19 · Engine Thrust ReverserSDR VNAA0809007Radome · delaminatedCREW REPORTED DURING LANDING A BIRD STRIKE TO THE NOSE OF THE ACFT. MX FOUND DELAMINATION ON THE RADOME. THE RADOME WAS R&R. NO OTHER DEFECTS WERE NOTED AND ACFT WAS RELEASED FOR SERVICE.Sep 15, 2008 · N258PS · Cndair CL6002B19 · Aerodynamic FairingsSDR VNAA0809005Selector Valve · failedCREW REPORTED A NOSE GEAR DISAGREE INDICATION FOR 1.5 MINUTES ON TAKE OFF. THE ACFT LANDED IN RIC WITHOUT INCIDENT. MX INSPECTED AND R&R THE NOSE LANDING GEAR SELECTOR VALVE ASSEMBLY. NO OTHER DEFECTS WERE NOTED. THE ACFT WAS RELEASED FOR SERVICE.Sep 13, 2008 · N207PS · Cndair CL6002B19 · Landing Gear SelectorSDR VNAA0809006Inverter · failedDURING SCHEDULED MX, FORWARD EMERGENCY TRACK LIGHTING AND EXIT OVER LT WING FAILED. MX R&R THE NR 2 INVERTER. NO OTHER DEFECTS WERE NOTED AND ACFT WAS RELEASED FOR SERVICE.Sep 13, 2008 · N206PS · Cndair CL6002B19 · Emergency LightingSDR VNAA0809004Handle · failedCREW REPORTED LANDING GEAR WOULD NOT RETRACT AFTER TAKE OFF. ANTI-SKID INBD AMBER AND PARKING BRAKE SOV AMBER MSG DISPLAYED. AFTER 3 MINUTES, MSG WENT AWAY AND LANDING GEAR RETRACTED. THE ACFT LANDED IN CLT WITHOUT INCIDENT. MX INSPECTED THE ACFT, PERFORMESep 12, 2008 · N244PS · Cndair CL6002B19 · Landing Gear SelectorSDR VNAA0809003Module · failedCREW REPORTED ON TAKE OFF ACFT PULLED HARD LT NEEDED FULL RT RUDDER AND TILLER TO MAINTAIN RUNWAY HEADING. TAKE OFF ABORTED AT UNKNOWN SPEED. ACFT RETURNED TO GATE WITHOUT INCIDENT. MX INSPECTED ACFT AND R&R THE HAND CONTROL MODULE. NO OTHER DEFECTS WERE NSep 10, 2008 · N249PS · Cndair CL6002B19 · Landing Gear Steering SystemSDR CA080911002Windshield · cracked(CAN) ON DESCENT THE LT WINDSHIELD CRACKED AT FL370 AND THE LT WINDSCREEN HEAT CAUTION CAME ON. AN EMERGENCY WAS DECLARED, BUT THE A/C LANDED WITHOUT INCIDENT. THIS WINDSHIELD HAD OVER 18,000 HRS AND WAS WELL ABOVE THE AVERAGE FOR NORMAL FAILURE RATES.Sep 9, 2008 · Cndair CL6002B19 · Flight Compartment WindowsSDR VNA2008F00006None · noneCREW REPORTED A NR 2 ICE DETECTION MESSAGE. CIRCUIT BREAKERS FOR ICE DETECTOR SYSTEM WERE RESET. NO OTHER DEFECTS WERE NOTED AND ACFT WAS RELEASED FOR SERVICE. (K)Sep 6, 2008 · N215PS · Cndair CL6002B19 · Central WarningSDR CA080905002Wire Harness · broken(CAN) FOLLOWING THE COMPLETION OF AD CF2008-09, WHILE PERFORMING A FUNCTION CHECK OF THE AIR DRIVEN GENERATOR, 2 OF THE 3 MAIN FEED WIRES WERE FOUND BROKEN AFT OF THE CONNECTOR P1XC. CLOSER INSPECTION OF THE WIRES REVEALED PITTING CORROSION AND BREAK IN SEVESep 2, 2008 · Cndair CL6002B19 · Electrical Power System WiringSDR VNAA0808016Flap · malfunctionedCREW REPORTED A FLAPS FAIL AT 20 DEG MESSAGE. CREW ELECTED TO RETURN TO JAN AND LANDED WITHOUT INCIDENT. MX INSPECTED ACFT AND NO DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.Aug 29, 2008 · N250PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0808014Structure · damagedCREW REPORTED A POSSIBLE LIGHTNING STRIKE AFTER LANDING AT XNA. MX INSPECTED AND REPAIRED DAMAGE TO THE ELEVATOR. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.Aug 26, 2008 · N249PS · Cndair CL6002B19 · Elevator StructureSDR VNAA0808012Gearbox · failedCREW REPORTED THE LT ENGINE FAILED ON CLIMBOUT. CREW ELECTED TO DIVERT TO IAD LANDING WITHOUT INCIDENT. MX INSPECTED ENGINE AND FOUND THE LT GEARBOX FAILED. GEARBOX WAS R&R. CHECKS WERE COMPLETED AND NO DEFECTS NOTED. ACFT WAS RELEASED FOR SERVICE.Aug 23, 2008 · N237PS · Cndair CL6002B19 · Turbine Engine Accessory DriveSDR VNAA0808011Valve · malfunctionedCREW REPORTED ACFT WOULD NOT MAINTAIN PRESSURE. CREW ELECTED TO RETURN TO DTW AND LANDED WITHOUT INCIDENT. MX INSPECTED ACFT AND SECURED CLOSED GROUND VALVE. NO OTHER DEFECTS WERE NOTED AND ACFT WAS RELEASED FOR SERVICE.Aug 23, 2008 · N723PS · Cndair CL6002C10 · Cabin Pressure Control SystemSDR VNAA0808013Actuator · failedCREW REPORTED A FLAPS FAIL AT 45 DEG. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MX INSPECTED ACFT AND R&R LT OUTBOARD ACTUATOR. CHECKS WERE MADE AND NO OTHER DEFECTS WERE NOTED. ACFT WAS RELEASED FOR SERVICE.Aug 23, 2008 · N249PS · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CHQA20080165Control Unit · faultedFLIGHT 5338, IAH TO VPS. AFTER TAKEOFF THE CREW RECEIVED A STAB TRIM CHANNEL 1 FAIL MESSAGE AND RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND FAULT CODES POINTING TO THE MOTOR CONTROL UNIT. THE MOTOR CONTROL UNIT WAS REPLACEAug 18, 2008 · N652BR · Cndair CL6002B19 · Stabilizer Position IndicatingSDR VNAA0808010Switch · out of positionCREW REPORTED A GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF. CREW ELECTED TO RETURN TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE NOSE GEAR DOOR SWITCH NOT IN FLT/NORMAL POSITION. SWITCH WAS REPOSITIONED AND SYSTEM TESTED. NO OTHEAug 17, 2008 · N246PS · Cndair CL6002B19 · Landing Gear SystemSDR VNAA0808009Window · failedCREW REPORTED A WINDOW HEAT CAS MESSAGE AND ELECTED TO DIVERT TO CLT. ACFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ACFT AND CHANGED RT WINDSHIELD. NO DEFECTS WERE NOTED AND ACFT RETURNED TO SERVICE. (S)Aug 16, 2008 · N251PS · Cndair CL6002B19 · Flight Compartment WindowsSDR VNAA0808008Radome · damagedCREW REPORTED LIGHTNING STRIKE. MAINTENANCE INSPECTED ACFT AND REPAIRED DAMAGE ON RADOME AND LT WINGLET. NO OTHER DEFECTS NOTED. ACFT WAS RELEASED FOR SERVICE. (S)Aug 15, 2008 · N257PS · Cndair CL6002B19 · Aerodynamic FairingsSDR CA080814006Transducer · unserviceable(CAN) ON THE TAKE-OFF ROLL AT APRX 60KTS, THE FLIGHT CREW REJECTED TAKE-OFF DUE TO AN N2 ENGINE VIBRATION CAUTION MESSAGE. VIBE ICON ON LT ENG APPROX 87 PERCENT. SECOND RUN REVEALED NO VIBE RISE ON INDICATOR BUT GETTING VIBE AMBER MESSAGE. CREW DID NOT FEEL Aug 12, 2008 · Cndair CL6002B19 · Engine Vibration AnalyzerSDR REX2008F00030Unknown · unknownAT LEVEL CRUISE FROM KTYS TO KMSP, THE RT THRUST REVERSER DEPLOYED MASTER CAUTION ILLUMINATED. THERE WERE NO UNUSUAL ACFT FLIGHT CHARACTERISTICS NOTED. FLIGHT CREW PERFORMED THE QRH WHICH REQUIRED LANDING AT NEAREST SUITABLE AIRPORT. THE FLIGHT CREW DECLAREAug 11, 2008 · N841AY · Cndair CL6002B19 · Engine Thrust ReverserSDR VNAA0808007Warning System · false indicationAFTER TAKEOFF CREW RECEIVED A STALL FAIL CAS MESSAGE. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED SYSTEM AND FOUND NO DEFECTS. ACFT WAS RELEASED FOR SERVICE. (S)Aug 10, 2008 · N218PS · Cndair CL6002B19 · Stall Warning SystemSDR A6WA200840562Shaft · shearedSTARTER ON ENGINE NR 1 WILL NOT STAY ENGAGED. NO ROTATION N1 OR N2. STARTER SHAFT SHEARED. R&R NR 1 ENG ATS PER MM 80-11-01. OPS CHECK GOOD.Aug 10, 2008 · N461AW · Cndair CL6002B19 · Engine CrankingSDR VNAA0808005None · noneCREW REPORTED A BIRD STRIKE ABOVE THE WINDSHIELD ON TAKEOFF ROLL. CREW ELECTED TO ABORT THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NO DEFECTS OR DAMAGE. ACFT WAS RELEASED FOR SERVICE. (S)Aug 8, 2008 · N215PS · Cndair CL6002B19 · Standard Practices/StructuresSDR VNAA0808004Skin · damagedCREW REPORTED A LIGHTNING STRIKE TO THE RT WING. MAINTENANCE PERFORMED AN EN ROUTE AND A DETAILED LIGHTNING STRIKE INSPECTION. MAINTENANCE INSPECTED AND FOUND DAMAGE TO LT FUSELAGE AND RT WINGTIP. MAINTENANCE REPAIRED ALL DAMAGE PER REO 601R-53-00-115 AND IAug 7, 2008 · N246PS · Cndair CL6002B19 · Wing, Plate/SkinSDR CHQA200800161Line · chafedFLIGHT 5723, SDF TO IAH. DURING CRUISE THE CREW RECEIVED A NR1 HYDRAULIC SYSTEM LOW PRESSURE MSG AND THE HYDRAULIC SYNOPTIC PAGE INDICATED ZERO QUANTITY. THE FLIGHT CREW FOLLOWED THE QRH CHECKLISTS AND THEN LANDED AT LIT WITHOUT INCIDENT. MAINTENANCE INSPECAug 6, 2008 · N486CA · Cndair CL6002B19 · Hydraulic System, MainSDR CHQA200800159Flap System · malfunctionedFLIGHT 5608, IAH TO CVG. WHILE ON APPROACH TO CVG, WHEN THE CREW SELECTED THE FLAPS FROM 29 TO 30, RECEIVED A FLAPS FAIL MESSAGE. THE ACFT PERFORMED A GO-AROUND TO RUN THROUGH THE QRH CHECKLISTS. THE ACFT THEN LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMEAug 5, 2008 · N473CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840557O-Ring · missingAT CRUISE SPEED RECEIVED LT ENG OPERATION WARNING MESSAGE AND OIL PRESSURE INDICATED 25-36 PSI. MESSAGE RECURRED AND PRESSURE DROPPED TO 25 PSI SEVERAL TIMES IN FLIGHT. INSPECTED NR 1 ENG AND FOUND OIL LEAKING FROM SCAVENGE FILTER. UPON REMOVING FILTER FOUNAug 4, 2008 · N419AW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA080806006Cowling · departed(CAN) AS INDICATED BY MAINT CONTROL, ACFT DEPARTED. MISSING COWLING FROM NR2 ENGINE WAS DISCOVERED DURING WALKAROUND INSP BY GROUND MAINT. IT WAS ALSO APPARENT THAT PORTIONS OF THE COWLING THAT DEPARTED ENGINE, STRUCK THE LEADING EDGES OF THE LT AND RT HORIZONAug 4, 2008 · Cndair CL6002B19 · Engine Cowling SystemSDR A6WA200840555Carbon Seal · leakingIN FLIGHT RT ENG OIL PRESSURE FLUCTUATED BETWEEN 30-45 PSI. ON SHORT FINAL RECEIVED "RT ENG OIL PRESSURE" WARNING MESSAGE, PRESSURE FLUCTUATED BETWEEN 23-33 PSI. ALSO, RECEIVED AURAL "ENG OIL" WARNING. REMOVED AND REPLACED RT ENG INTEGRATED DRIVE GENERATOR Aug 3, 2008 · N432AW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR VNAA0807017Flap · malfunctionedCREW REPORTED THE FLAPS FAILED AT 20 DEGREES. CREW ELECTED TO DIVERT TO RDU AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ACFT AND FOUND NO DEFECTS. ACFT WAS RELEASED FOR SERVICE. (S)Jul 25, 2008 · N250PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0807014A/C Pack · failedCREW REPORTED, THE LT PACK TEMP TO BE 113 DEG C AND UNCONTROLLABLE IN AUTO OR MANUAL. CREW ELECTED TO RETURN TO DTW LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LT AIR CYCLE MACHINE. CHECKS WERE ACCOMPLISHED WITHJul 24, 2008 · N237PS · Cndair CL6002B19 · Cabin Cooling SystemSDR VNAA0807012Warning Light · multiple failCREW REJECTED TAKEOFF AT 85 KNOTS DUE TO MASTER CAUTION LIGHT 900 DEG AND FLASHING ITT ON LT ENGINE. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED ENGINE AND FOUND ALL PARAMETERS WITHIN LIMITS AND NO DEFECTS. AIRCRAFT WAS RELEASED FOR SERVICE. (A)Jul 22, 2008 · N215PS · Cndair CL6002B19 · Central WarningSDR CHQA200800153Line · leakingFLIGHT 5581, IND TO IAH. DURING CRUISE THE FLIGHT CREW RECEIVED A HYD 2 SYS LOW PRESS MESSAGE. THE HYDRAULIC PAGE WAS BROUGHT UP IT WAS CONFIRMED THAT THE SYSTEM WAS INDICATING 0% QUANTITY AND VERY LOW PRESSURE. THE QRH PROCEDURES WERE FOLLOWED, AND THE FLIJul 22, 2008 · N466CA · Cndair CL6002B19 · Hydraulic System, MainSDR VNAA0807011None · noneCREW REPORTED A BIRD STRIKE ON NOSE OF AIRCRAFT. CREW ELECTED TO RETURN TO TYS AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AND INSPECTED AIRCRAFT. NO DAMAGE WAS NOTED AND AIRCRAFT WAS RELEASED TO SERVICE. (A) [NOT AN SDR]Jul 21, 2008 · N248PS · Cndair CL6002B19 · Standard Practices/StructuresSDR VNAA0807010Computer · failedCREW REPORTED A FUEL IMBALANCE AMBER MSG INFLIGHT. THE RT FUEL AND TOTAL FUEL QUANTITY INDICATORS SHOWED "DASHED". CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND CHANGED THE FUEL QUANTITY COMPUTER. MAINTENANCEJul 20, 2008 · N220PS · Cndair CL6002B19 · Fuel Indicating SystemSDR CHQA200800152Cabin Pressure · malfunctionedFLIGHT 5588, MCI TO IAH. DURING IDLE DESCENT WHILE DESCENDING AT APPROXIMATELY 2,500 FPM, THE CABIN ALTITUDE WAS OBSERVED TO CLIMB AT 900 FPM ON BOTH CPAM`S. THE FLIGHT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE PERFORMED PRESSURIZATION CHECKS AND COULD NOJul 19, 2008 · N639BR · Cndair CL6002B19 · Cabin Pressure Control SystemSDR VNAA0807009None · noneCREW REPORTED THE PDF SHOWED FLAPS EXTENDED TO 2 DEG UNCOMMANDED AT 30,000FT WITH NO AURAL WARNING AT CRUISE. THE CREW DIVERTED TO TYS AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO DEFECTS. AIRCRAFT WAS RETURNED TO SERVICE. (Jul 17, 2008 · N260JS · Cndair CL6002B19 · Standard Practices/StructuresSDR CHQA200800146Pump · low pressureFLIGHT 5701, AEX TO IAH. AFTER TAKEOFF WHILE THE LANDING GEAR WAS IN TRANSIT THE FLIGHT CREW RECEIVED A NOSE DOOR OPEN AND GEAR DISAGREE EICAS WARNING MESSAGE. THE CREW FOLLOWED THE QRH AND RETURNED TO AEX AND LANDED WITHOUT INCIDENT. THE ACFT WAS FERRIED BJul 16, 2008 · N653BR · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR CHQA200800147Uplock Sensor · out of adjustFLIGHT 5596, IAH TO BRO. AFTER TAKEOFF THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT WHEN THE GEAR WAS SELECTED UP. THE GEAR LEVER WAS MOVED BACK TO THE DOWN POSITION AND THE LT MAIN LANDING GEAR INDICATED A RED UNSAFE CONDITION. THE GEAR FINALLJul 16, 2008 · N638BR · Cndair CL6002B19 · Landing Gear Position and WarningSDR CHQA200800148Computer · failedFLIGHT 5577, IAH TO CRP. DURING CLIMB THE CREW REPORTED THAT THE FIRST OFFICER`S ATTITUDE AND HEADING REFERENCE DATA DISAPPEARED WHEN THE AUTO-PILOT WAS ENGAGED. THE ACFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FAULT CODES FOR BOTH THJul 16, 2008 · N647BR · Cndair CL6002B19 · Integrated Flight SystemSDR CHQA200800149Access Panel · departedFLIGHT 5590, SDF TO CLE. THE FLIGHT CREW DISCOVERED ON THE POST FLIGHT INSPECTION THAT THE E2 LOWER NOSE ACCESS COWL WAS NOT ON THE ACFT. MAINTENANCE INSPECTED E2 AND INSTALLED A NEW LOWER ACCESS COWLING. (S)Jul 16, 2008 · N648BR · Cndair CL6002B19 · DoorsSDR A6WA200840544Wire Harness · damagedENG NR 1 SHUTDOWN IN FLIGHT, NO ASSOCIATED EICAS MESSAGES ILLUMINATED BEFORE SHUTDOWN. THRUST LEVERS WERE ABOVE IDLE AT APPROXIMATELY 80%. RAN QRH, TRIED TO RELIGHT. ENG RELIT FOR 15-20 SECONDS THEN GOT LOW OIL PRESSURE RED WARNING. DID PRECAUTIONARY SHUTDJul 15, 2008 · N445AW · Cndair CL6002B19 · Turbine Engine System WiringSDR CA080819002Window · failed(CAN) "F/O SIDE WINDOW SHATTERED JUST AFTER TAKE OFF (RETURNED), DETERMINED TO BE CENTER PANE". REMOVED AND REPLACED THE F/O`S SIDE WINDSHIELD.Jul 15, 2008 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA080819003Window · failed(CAN) "F/O WINDSHIELD SHATTERED ENROUTE, DIVERTED ". REMOVED AND REPLACED THE F/O`S WINDSHIELD.Jul 15, 2008 · Cndair CL6002B19 · Flight Compartment WindowsSDR VNAA0807006None · noneCREW REPORTED A LOUD NOISE ON RT SIDE OF AIRCRAFT AND ELECTED TO RETURN TO CLT LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE OXYGEN SERVICE DOOR LEFT OPEN. MAINTENANCE SECURED THE DOOR CLOSED. AIRCRAFT WAS RELEASED FOR SERVICE. (A)Jul 14, 2008 · N215PS · Cndair CL6002B19 · Standard Practices/StructuresSDR VNAA0807007Warning Message · false activationCREW RECEIVED A LT HAND STATIC HEAT CAS MSG AND ELECTED TO RETURN TO CLT LANDING WITHOUT INCIDENT. MAINTENANCE RE-SET THE SYSTEM AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. (A)Jul 14, 2008 · N262PS · Cndair CL6002B19 · Central WarningSDR CHQA200800142Sensor · faultyFLIGHT 5994, RDU TO SDF. DURING CLIMB AT 3,000 FT THE FLAPS WERE SELECTED FROM 3 DEGREES TO ZERO AND THE CREW RECEIVED A FLAP FAIL MESSAGE. THE CREW REPORTED THAT THE LEFT FLAP STOPPED AT 3 DEGREES AND THE RIGHT FLAP STOPPED AT ZERO. MAINTENANCE RIGGED THE Jul 13, 2008 · N701BR · Cndair CL6002B19 · Trailing Edge Flap Control System
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