Canadair CL-600-2A12

Service difficulty reports · 78

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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 aircraft_model_key = 'CL6002A12'
  ORDER BY difficulty_date DESC"

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SDR 2021FA0000132Flap Track · bindingFAILURE OF THE FLAPS AT 10 DEGREES. CORRECTIVE ACTION WAS LUBRICATION OF THE FLAP ACTUATORS IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUALS FOLLOWED BY AN OPERATIONAL CHECKFeb 19, 2021 · N601RC · Cndair CL6002A12 · Trailing Edge FlapsSDR MXIA201902084Switch · crackedDURING APPROACH, GEAR WAS SELECTED DOWN. NOSE GEAR GREEN LIGHT DID NOT COME ON & NOSE DOOR REMAINED OPEN. AS PER THE CHECKLIST THE GEAR WAS SELECTED UP, THE MAINS RETRACTED BUT THE NOSE DOOR REMAINED OPEN. GEAR WAS RE-SELECTED DOWN AND NORMAL GEAR DOWN INDICATFeb 7, 2019 · N824DH · Cndair CL6002A12 · Landing Gear Position and WarningSDR 2017FA0000234Tire · bulgedPRE-FLIGHT WALK AROUND REVEALED A SMALL BULGE IN THE NR 2 MAIN TIRE. THE BULGE WAS ONLY EVIDENT WHEN THAT SPECIFIC AREA OF THE TIRE WAS ON THE BOTTOM. THE BULGE WENT AWAY WHEN THE AIRCRAFT WAS ROLLED FORWARD.May 25, 2017 · N601RC · Cndair CL6002A12 · TireSDR 4DUA20170101Flap System · failedDURING THE FINAL APPROACH, A FLAPS FAIL LIGHT WHEN THE FLAPS WERE PLACED IN THE 45 DEGREE POSITION. CONTINUED TO AVIATE AND GET THE AIRCRAFT ON THE GROUND. REPORTED A LOSS OF 15-20 KTS DURING THE SHORT FINAL FLARE STAGE. THE LANDING PHASE BECAME UNSTABLE ANJan 26, 2017 · N947KK · Cndair CL6002A12 · Trailing Edge Flap Control SystemSDR 2016FA0000582Dimmer · meltedFLIGHT CREW REPORTED A PORTION OF THE PILOTS INSTRUMENTATION BACK LIGHTING INOPERATIVE, TECHNICIAN REPLACED FAULTY INCANDESCENT LAMP DIMMER, VISUALLY INSPECTING FAULTY INCANDESCENT LAMP DIMMER REVEALED OUT PUT 7 1/2 AMP CIRCUIT BREAKER LV2 MELTED AND CIRCUIT BNov 28, 2016 · N601RC · Cndair CL6002A12 · Flight Compartment LightingSDR 2016FA0000247Tire · failedRIGHT MAIN INBD TIRE HAS A PORTION OF THE TREAD THAT SEPARATED ON LANDING. NEW TIRE WAS INSTALLED AT WHEEL ASSY O/H.May 17, 2016 · N601RC · Cndair CL6002A12 · TireSDR 1KSA2015FA0000513Skin · corrodedDURING ROUTINE MAINTENANCE FOUND CORROSION UNDER VHF ANTENNA AT FS 360, BL0 AND UNDER TRANSPONDER ANTENNA, FS 386, LBL4.Oct 19, 2015 · N97SG · Cndair CL6002A12 · Fuselage Main, Plate/SkinSDR LOMA2015FA0000280Warning Light · illuminatedRIGHT FUSELAGE BLEED WARNING CAME ON.Jun 13, 2015 · N807MM · Cndair CL6002A12 · Pneumatic SystemSDR 3BOR20150605001Wire · meltedELECTRICAL POWER WAS LOST DURING CRUISE FLIGHT. ACFT MADE AN UNSCHEDULED LANDING. VISUAL INSPECTION FOUND SEVERAL WIRES TO BE MELTED, SINGED AND/OR HEAT STRESSED, AND CIRCUIT BREAKERS TO BE SINGED AND/OR HEAT STRESSED IN CIRCUIT BREAKER PANEL CBP-A. ROOT CAJun 5, 2015 · N601PR · Cndair CL6002A12 · Electrical Power System WiringSDR LOMA2014FA0000687Loop · defectiveRIGHT 10TH STAGE BLEED WARNING LIGHT CAME ON DURING DECENT. LANDED FOR REPAIR. REPLACED RT 10TH STAGE BLEED AIR WARNING LOOP A ELEMENT.Dec 4, 2014 · N807MM · Cndair CL6002A12 · Fire Protection SystemSDR LOMA2014FA0000688Valve · leakingRIGHT 10TH STAGE WARNING LIGHT CAM ON DURING DECENT.Nov 25, 2014 · N807MM · Cndair CL6002A12 · Pneumatic Distribution SystemSDR LOMA2015F00009Shutoff Valve · leakingRIGHT 10TH STAGE BLEED AIR WARNING ILLUMINATED. DIVERTED FOR REPAIR. REPLACED 10TH AND 14TH STAGE BLEED AIR SHUTOFF VALVES.Nov 18, 2014 · N807MM · Cndair CL6002A12 · Compressor Bleed ValveSDR CA140606002Control Cable · failed(CAN) DURING AN 60 MONTH INSPECTION. THE TECH FOUND BY VISUAL CHECK UP, WHEN HE OPEN THE PANEL IN THE VERTICAL STABILIZER RT SIDE.Jun 5, 2014 · Cndair CL6002A12 · Elevator Tab Control SystemSDR LOMA2014042500279Detection Sys · false activationRIGHT 10TH STAGE DUCT FAIL LIGHT ILLUMINATED DURING FLIGHT. TROUBLESHOT AND FOUND NO BLEED AIR LEAKS FROM RT 10TH STAGE MANIFOLD. FALSE INDICATION. REPLACED ALL OVERHEAT DETECTOR LOOPS FOR RT 10TH STAGE BLEED AIR LEAK DETECTION SYSTEM.Apr 22, 2014 · N807MM · Cndair CL6002A12 · Overheat DetectionSDR BQVA20130507001Support Angle · corrodedCABIN DOOR WAS REMOVED AND SENT TO REPAIR FACILITY FOR COMPLIANCE OF BOMBARDIER SERVICE BULLETIN 601-0613 R1. THE FOLLOWING ITEMS WERE FOUND WITH CORROSION DURING SERVICE BULLETIN COMPLIANCE: AFT SUPPORT ANGLE P/N 600-31902-65 LOWER END, ATTACH CLIP P/N 600-May 3, 2013 · N57MH · Cndair CL6002A12 · Passenger/Crew DoorsSDR 2012F00197Water Heater · shortedENROUTE, CABIN ATTENDANT DETECTED AND SAW SMOKE COMING FROM THE GALLEY AREA. CONFIRMED LOCATION OF SMOKE AND PULLED ALL CIRCUIT BREAKERS TO GALLEY AND CAPTAIN SHUTOFF ALL GALLEY AND CABIN POWER. DECLARED AN EMERGENCY AND LANDED. TROUBLESHOT AND INSPECTED, FSep 21, 2012 · N125PS · Cndair CL6002A12 · Potable Water SystemSDR WWQA201209240001Water Heater · shortedWHILE ENROUTE, THE CABIN ATTENDANT DETECTED AND SAW SMOKE COMING FROM THE GALLEY AREA. CAPTAIN HAD THE F/O GO BACK TO VERIFY & HELP LOCATE WHERE THE SMOKE WAS COMING FROM. ONCE CONFIRMED LOCATION OF SMOKE, HAD THE CABIN ATTENDANT PULL ALL CIRCUIT BREAKERSSep 21, 2012 · N125PS · Cndair CL6002A12 · Water/Waste System WiringSDR 2012FA0000203Controller · failedAIRCRAFT ON RAMP, APU WAS SHUTDOWN AFTER RUNS AND ADG AUTOMATICALLY DEPLOYED. THIS OPERATION SHOULD NOT HAVE HAPPENED UNLESS ACFT IS IN THE AIR. TROUBLESHOOTING FOUND THE CONTROLLER FAILED. RECOMMENDED REPLACEMENT TO CUSTOMER AND THIS WAS ACCOMPLISHED. UNKFeb 14, 2012 · N275MT · Cndair CL6002A12 · Electrical Power SystemSDR CA111102004Seal · bent(CAN) HARD CHAFING CONDITION AND DAMAGED MOVING PART HAVE BEEN FOUND BY MX PERSONNEL WHILE PERFORMING POST FLIGHT CHECK FOLLOWING ACFT FIRST FLIGHT. RT AILERON OTBD LOWER L/E PANEL HAD SEVERELY COME INTO CONTACT WITH RT AILERON OTBD LOWER GAP SEAL. INTERFERENov 1, 2011 · Cndair CL6002A12 · AileronsSDR 2011FA0000384Selector · failedLANDING GEAR DID NOT EXTEND NORMALLY. ALTERNATE EXTENSION USED SUCCESSFULLY FOR DOWN AND LOCKED.Jun 17, 2011 · N601VH · Cndair CL6002A12 · Landing Gear SelectorSDR CA110615007Gps · malfunctionedAPPROXIMATELY ONE HOUR AFTER TAKEOFF AND ENROUTE, CREW REPORTED BACK TO MX THAT BOTH GPS RECEIVERS HAD LOST THE SATELITE FIX AND HAD STARTED TO REACQUIRE. CREW ALTERED THEIR FLIGHT PATH TO RETURN AND APPROX 10 MINUTES LATER BOTH GPS HAD REACQUIRED THE SATELITJun 11, 2011 · Cndair CL6002A12 · Global Positioning SystemSDR CA110418006Tube · chafed(CAN) MOTIVE FLOW SENSE LINE, RT, T/O MAIN EJECTOR PRESSURE SWITCH CHAFED THROUGH UNDER AND BY CLAMP, PN 417-4. THE ANTI-CHAFE MATERIAL WAS IN PLACE ON THE CLAMP BUT IT WAS ALSO WORN THROUGH EXSPOSING THE METAL PORTION OF THE CLAMP TO THE TUBE. THIS CAUSEDApr 18, 2011 · Cndair CL6002A12 · Aircraft Fuel Distribution SystemSDR CA120426011Pin · misinstalled(CAN) THROUGH AN SRPSA, 58446, REPORTED DAMAGE TO THE ANTI-ROTATION TAB OF SIDE STAY FITTING 601-10374-1/-2. AFTER INVESTIGATION, SHAFT, 600-10237-5 WAS FOUND INSTALLED ON SIDE STAY FITTING 601-10374-1/-2 ON AC 3010 BY ERROR.Jan 12, 2011 · Cndair CL6002A12 · Nose/Tail Landing GearSDR 2011F00005Tire · failedDURING LANDING, THE NR 2 TIRE TREAD SEPARATED FROM THE TIRE. THE TIRE STAYED INFLATED. WHEN THE TREAD SEPARATED, IT CUT THE NR 2 ANTI-SKID HARNESS IN HALF AND DAMAGED THE LT INBD FLAP BEYOND LIMITS. NO PROBLEMS EXISTED FROM THE HARNESS BEING CUT AS THE CREWS ODec 23, 2010 · N39CD · Cndair CL6002A12 · TireSDR 2010FA0000201Frame · crackedFWD FUSELAGE FRAME AT FS235 ABOVE FLOOR, PILOTS AND COPILOTS SIDE, FOUND CRACKED. DURING 240 MONTH INSP.Feb 5, 2010 · N500PG · Cndair CL6002A12 · Fuselage Main, FrameSDR 2010FA0000200Frame · crackedFWD FUSELAGE FRAME AT FS 235 ABOVE FLOOR, PILOTS AND COPILOTS SIDE, FOUND CRACKED DURING 240 MONTH INSP.Feb 4, 2010 · N500PG · Cndair CL6002A12 · Fuselage Main, FrameSDR WWQ2007F00001Wire Harness · shortedDURING APPROACH, THE CREW EXTENDED THE LANDING GEAR (NORMAL PROCEDURE). SEVERAL SECONDS AFTER THE GEAR EXTENSION THE NOSE LANDING GEAR DOWN AND LOCKED GREEN LIGHT EXTINGUISHED AND THE NOSE GEAR DOORS OPENED AND CLOSED. A FEW SECONDS LATER THE DOORS CYCLED AGAug 5, 2007 · N39CD · Cndair CL6002A12 · Landing Gear System WiringSDR 2007FA0000000Engine · failedRT ENGINE FAILURE AT T/O. ALL INDICATIONS WERE NORMAL ON ENGINE START AND TAXI. UPON THRUST ADVANCEMENT FOR TAKEOFF, AT APPROXIMATELY 60 PERCENT N1 WE HEARD AND FELT A COMPRESSOR STALL. THE THRUST LEVER WAS IMMEDIATELY RETARDED TO IDLE AND TEMPERATURES WERE NODec 1, 2006 · N388DB · Cndair CL6002A12 · Engine (Turbine/Turboprop)SDR 2006FA0000949Windshield · crackedLT WINDSHIELD (PILOTS) OUTER-PLY CRACKED DURING FLIGHT. NO KNOWN CAUSE AS TO THE EVENTS LEADING TO CRACK. KNOWN TO BE A COMMON FAILURE ON CHALLENGER ACRYLIC WINDSHIELD AND SIDE WINDOWS. WHETHER DUE TO IMPACT OF SOME SORTS OR WINDSHIELD NEAT FAILURE OR DELASep 7, 2006 · N150MH · Cndair CL6002A12 · Flight Compartment WindowsSDR DJFA2005103Relief Valve · leakingSHORTLY AFTER T/O, TOWER REPORTED FUEL SPRAYING FROM RT WING. CREW VISUALLY VERIFIED, RETURNED AND LANDED WITHOUT INCIDENT. INSP FOUND FUEL LEAKING FROM RT WING VENT. WING FUEL PRESSURE RELIEF VALVE FOUND TO BE OPEN. EXTENDED REFUELING TEST WAS PERFORMEDMay 30, 2005 · N633CW · Cndair CL6002A12 · Fuel StorageSDR DJFA2005086Bulb · burned outCREW REPORTED THAT UPON GEAR EXTENSION THEY DID NOT RECEIVE THE NOSE GEAR DOOR INDICATION. A FLY-BY PAST THE TOWER WAS PERFORMED TO VERIFY NOSE GEAR POSITION. DOOR INDICATION WOULD NOT TEST, AND A MANUAL GEAR EXTENSION WAS PERFORMED. GREEN NOSE GEAR DOOR LIApr 25, 2005 · N633CW · Cndair CL6002A12 · Landing Gear Position and WarningSDR 041251Clamp · brokenAPU HAD BEEN RUNNING ON THE GROUND FOR APPROXIMATELY ONE HOUR AND SHUT ITSELF DOWN DUE TO HIGH OIL TEMP AS INDICATED BY (BYTE) LIGHT. VISUAL INSPECTION SHOWED THAT BLEED AIR ELBOW HAD BROKEN OFF OF EXHAUST STACK CLAMP AT THE WELD. RECOMMEND REGULAR VISUAL INApr 12, 2005 · N601RC · Cndair CL6002A12 · APU Bleed Air SystemSDR N382005F00003Gcu · burnedUPON AIRCRAFT TEST FLIGHT FOR COMPLETION OF TAWS INSTALLATION. AIRCRAFT EXPERIENCED SMOKE IN THE CABIN AND COCKPIT. CREW DECLARED AND EMERGENCY LANDING AND PERFORMED AN UNEVENTFUL LANDING, USING NORMAL PUBLISHED EMERGENCY PROCEDURE. TROUBLESHOOTING FOUND THFeb 16, 2005 · N163WG · Cndair CL6002A12 · Airborne Auxiliary Power Unit (APU) SystemSDR 2004F00032Windshield · crackedLEFT WINDSHIELD FAILED IN FLIGHT, OUTER PANE CRACKED AND SEPARATED. CREW FOLLOWED CHECKLIST PROCEDRUES AND LANDED AT A SUITABLE AIRFIELD. (M)Nov 25, 2003 · N163WG · Cndair CL6002A12 · Flight Compartment WindowsSDR N382003F00001Fuel Control · failedAT APPROXIMATELY 0650 PACIFIC TIME, WHILE ON CLIMB OUT AND CLIMBING THROUGH 5500 FT MSL THE AIRCRAFT EXPERIENCED AN UNCOMMANDED SHUTDOWN OF THE LEFT ENGINE. ALL CHECKLISTS AND PROCEDURES WERE FOLLOWED. AN EMERGENCY WAS DECLARED, AND AN UNEVENTFUL LANDING WASAug 1, 2003 · N163WG · Cndair CL6002A12 · Fuel Control/Turbine EnginesSDR SH52003F00000Fuel Control · inoperativeAIRCRAFT WAS HOLDING ON TAXIWAY WITH WINDS OVER 40 KNOTS AND BLOWING SNOW. A/C WAS BEHIND A/C WHICH WAS KICKING UP ADDITIONAL SNOW. PILOT PUT ON THE COWL ANTI-ICE. APPROXIMATELY ONE MINUTE LATER THE RIGHT ENGINE SHUTDOWN UNCOMMANDED, AIRCRAFT RETURNED TO HAFeb 14, 2003 · N500PG · Cndair CL6002A12 · Fuel Control/Turbine EnginesSDR SH52002F00000Sill · crackedDURING SCHEDULED INSPECTION FOUND LOWER WINDSHIELD SILL CRACKED (PRIMARY STRUCTURE) ON LEFT AND RIGHT SIDE OF COCKPIT. BOTH CRACKS ARE AT FS 235.0 WL 110.5 AND RUN ALONG THE BASE OF A WEB LEFT CRACK IS 1.5 INCHES LONG, RIGHT IS 1.0 INCH LONG. CRACKS IN THIS Jan 9, 2002 · N711SX · Cndair CL6002A12 · Fuselage Main, StructureSDR QXEA0101591Seal · dentedPDX - MAIN CABIN DOOR SEAL MATING SURFACE IS DENTED MIDWAY ALONG THE FORWARD LENGTH OF DOOR APERATURE. REPAIRED IAW EA R-53-03.Sep 25, 2001 · N606QX · Cndair CL6002A12 · Passenger/Crew DoorsSDR CA010912014Handle · broken(CAN) THE RAMP PERSONNEL BROKE THE OUTER HANDLE OF THE SERVICE DOOR DURING NORMAL OPERATION. THE PERSON WORKING REPORTED THAT HE DID NOT USED ANY EXCESSIVE FORCE TO OPEN THE DOOR. THE MAINTENANCE REPLACED THE OUTER HANDLE ON THE SERVICE DOOR.Sep 9, 2001 · Cndair CL6002A12 · Service DoorsSDR CA010501008Windshield · cracked(CAN) R/H WINDSHIELD CRACKED WHILE ON APPROACH. MAINTENANCE REMOVED AND REPLACED RT WINDSHIELD WITH NEW UNIT. AIRCRFT BACK IN SERVICE.Apr 16, 2001 · Cndair CL6002A12 · Flight Compartment WindowsSDR CA000720014Battery · wrong part(CAN) UPON ELT RECERTIFICATION, A NON TC APPROVED BATTERY WAS FOUND IN THE UNIT.ONLY THE DM U158-1 IS APPROVED BY TC (REF AWN BO14, EDITION 4) FOR USE IN THIS ELT. CORRECT BATTERY WAS INSTALLED AND ELT RECERTIFIED.SUPJun 20, 2000 · Cndair CL6002A12 · Emergency Locator BeaconSDR 20000620SH027Potentiometer · failedA DIMMER POT (R3LM) WAS FOUND BURNT AND MELTED AFTER IT WAS REPORTED THE NR 1 F/D WAS TRIPPING THE CIRCUIT BREAKER ON THE DC ESSENTIAL BUSS. THE POT IS PART OF THE PILOTS LIGHTING CONTROL PANEL. (X)May 25, 2000 · N601AA · Cndair CL6002A12 · Flight Compartment LightingSDR CA000519016Actuator · failed(CAN) WHILE TAXING TO RAMP PILOT MOVED STAB TRIM TO NOSE DOWN POSITION. CHANNEL 1 NOSE DOWN FAIL LIGHT CAME ON AND ACT WOULD NOT MOVE. MAINT CHANGED PITCH TRIM ACTUATOR AND RETURNED A/C TO SERVICE.May 15, 2000 · Cndair CL6002A12 · Stabilizer ActuatorSDR 20000503SH050Window Post · crackedDURING THE ACCOMPLISHMENT OF THE AIRCRAFT MANUFACTURER''S REQUIRED 6,600 HOUR CHECKS, A CRACK WAS NOTED ON THE UPPER SURFACE OF THE WINDSCREEN LOWER SILL FRAME AT BS 235 LEFT. THE CRACK WAS NOTED DURING INSPECTION WHICH WAS ACCOMPLISHED AT TT: 6,552.2 HOURS.Apr 13, 2000 · N608CW · Cndair CL6002A12 · Passenger Compartment WindowsSDR 20000424SH011Heater · inoperativePILOT''S LEFT FRONT WINDSHIELD HEAT ELEMENT INOPERATIVE. (X)Mar 15, 2000 · N651CW · Cndair CL6002A12 · Windshield/Door Rain/Ice RemovalSDR 2000ZZZX109Cover · crackedTHE LEFT NOSE COWL AIRLINE COVER (POCKET) FOR THE 14TH STAGE T/R PDU LINE SHOWS SIGNS OF HEAT DAMAGE AND IS BUCKLED AND CRACKED.Dec 10, 1999 · N998JR · Cndair CL6002A12 · Engine Cowling SystemSDR CA991209046Actuator · failed(CAN) OCCASIONALLY FLAPS FAILED IN COLD WEATHER. NR 3 ACTUATOR REPLACED AND PROBLEM WENT AWAY.Nov 13, 1999 · Cndair CL6002A12 · Trailing Edge Flap ActuatorSDR CA991028064Brake · failed(CAN) TECHNICIAN NOTICED THE RIGHT OUTBOARD MAIN WHEEL WAS FLAT. THE FUSE PLUG WAS FOUND MELTED AS WELL AS A LOCALIZED WEAR (FLAT SPOT) ON THE TIRE. IT WAS NOTICED THAT THE WHEEL HAD OVERHEATED AND SUFFERED PREMATURE WEAR CAUSED BY THE BRAKE WHICH WAS STUCK OOct 7, 1999 · Cndair CL6002A12 · BrakeSDR CA990521046Engine · making metal(CAN) AT 7,000 FEET, A SHEARING NOISE WAS HEARD FROM NR 2 ENGINE. THE ENGINE WAS SHUT DOWN. POST-FLIGHT INSPECTION FOUND METAL IN THE MAIN OIL FILTER AND CHIP DETECTOR. THE ENGINE WAS REMOVED AND SENT FOR INVESTIGAITON.May 13, 1999 · Cndair CL6002A12 · Engine (Turbine/Turboprop)SDR CA990226006Pump · malfunctioned(CAN) NR 2 ENGINE LOW OIL PRESSURE LIGHT IN-FLIGHT. POST-FLIGHT INSPECTION FOUND THE NR 2 ENGINE OIL PUMP WAS INOPERATIVE.Feb 2, 1999 · Cndair CL6002A12 · Turbine Engine Oil System
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