Canadair CL600-1A11

Service difficulty reports · 69

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'CL6001A11'
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SDR CA190402017Lanyard · wrong part(CAN) FOLLOWING AN ISSUE ON THE CL605 (CL6-CA-35-7), TCCA HAS REQUESTED BOMBARDIER TO CONFIRM THAT CL600/601 WAS NOT IMPACTED BY THIS ISSUE. BOMBARDIER CONDUCTED A SAMPLING IN SERVICE AND DISCOVERED THAT A SIMILAR ISSUE WAS POTENTIALLY PRESENT ON THE FLEET.Nov 12, 2018 · Cndair CL6001A11 · Crew Oxygen SystemSDR CA140106008Thrust Reverser · failed(CAN) RIGHT THRUST REVERSER DEPLOYMENT JAN 3. 2014. ACFT DEPARTED YOW. TAKEOFF WENT WITHOUT INCIDENT. CLIMBING THROUGH 5000 FT. WE HEARD A BANG, ACFT YAWED AND BUFFETED. REVERSER UNLOCK LIGHT CAME ON & AUTO THROTTLE RETARD SNAPPED RT THROTTLE TO IDLE. WE Jan 3, 2014 · Cndair CL6001A11 · Engine Thrust ReverserSDR 2012FA0000169Carbon Seal · defectiveAFTER PERFORMING SEVERAL PREFLIGHTS, IT WAS NOTED THAT THE NR 2 INTEGRATED DRIVE GENERATOR HAD AN INCREASE IN THE FREQUENCY AND QUANITY OF OIL SERVICING. AFTER INVESTAGATING THE CAUSE, IT WAS DETERMINED THAT THE DRIVE END CARBON SEAL WAS LEAKING, ALLOWING PREMar 12, 2012 · N396KM · Cndair CL6001A11 · AC Generator-AlternatorSDR 2008FA0000537Skin · corrodedSURFACE CORROSION (PITTING) DISCOVERED ON BOTH WINGS LOWER SURFACES ADJACENT TO AND OB OF WHEEL WELLS, CORROSION DEEMED UNUSUALLY SEVERE. (K)Jul 24, 2008 · N100QR · Cndair CL6001A11 · Wing, Plate/SkinSDR ZLJ2008F00000Skin · corrodedSURFACE CORROSION DISCOVERED ON FUSELAGE SKIN ADJACENT TO PRE-COOLER EXHAUSTS ON LT AND RT SIDES OF FUSELAGE. DISCREPANCY DISCOVERED WHILE PERFORMING PROCEDURE C53-00-814. CORROSION DEEMED TO BE UNUSUALLY SEVERE. (K)Jul 24, 2008 · N100QR · Cndair CL6001A11 · Fuselage Main, Plate/SkinSDR 2007F00069Windshield · crackedEN ROUTE AT FL330, THE CAPTAIN NOTICED A CRACK IN THE EXTERIOR PANEL OF THE LT FWD WINDSHIELD. THE APPROPRIATE CHECKLIST WAS COMPLETED AND A SPEED REDUCTION AND DECENT REQUESTED. WHILE DESCENDING A LOUD (POP) AND SUBSEQUENT WHISTLING WAS HEARD. A FURTHER SPEEDDec 13, 2007 · N900LG · Cndair CL6001A11 · Flight Compartment WindowsSDR WAI2007F00001Fire Loop · shortedFLIGHT CREW REPORTED LT ENGINE FIRE DETECTION FAIL LIGHT CAME ON JUST PRIOR TO ROTATION, THEN FIRE LIGHT CAME ON JUST PRIOR TO ROTATION, THEN FIRE WARNING CAME ON AT 1,500 FT DURING CLIMB. STAYED ON AFTER DISCHARGING BOTH FIRE BOTTLES. RETURNED TO BASE AFTER Mar 6, 2007 · N403WY · Cndair CL6001A11 · Fire DetectionSDR 2007F00023Fire Loop · shortedFLIGHT CREW REPORTED LT ENGINE FIRE DETECTION FAIL LIGHT CAME ON JUST PRIOR TO ROTATION, THEN FIRE WARNING CAME ON AT 1,500 FEET DURING CLIMB. STAYED ON AFTER DISCHARGING BOTH FIRE BOTTLES. RETURNED TO BASE, AFTER LANDING, APPEARED TO BE NO FIRE. FOUND LT ENGIMar 6, 2007 · N403WY · Cndair CL6001A11 · Fire DetectionSDR 2006FA0000563Adg · deployedAIR DRIVEN GENERATOR (ADG) UNEXPECTED DEPLOYED ON POST TAKEOFF CLIMB OUT. PRECAUTIONARY LANDING ACCOMPLISHED. ADG MECHANICALLY RETRACTED/ SAFED; AIRCRAFT FERRIED TO MAINTENANCE DEPOT. ALL WORK ACCOMPLISHED IAW MM. (K)Apr 24, 2006 · N777GD · Cndair CL6001A11 · AC Generation SystemSDR 2006FA0000589Battery · leakingA STRONG ACIDIC ODOR WAS PRESENT AFTER REMOVING ELT BATTERY FROM ELT INSPECTION FOUND A THICK WHITE LIQUID ON THE NEGATIVE SIDE OF ONE BATTERY CELL. THE EXPIRATION DATE OF THE ELT BATTERY IS APRIL 2010 (4 MORE YEARS). THE ELT BATTERY OUTPUT IS 13.2 VOLTS. (Apr 12, 2006 · N673TS · Cndair CL6001A11 · Emergency Locator BeaconSDR 2005FA0000845Floor Support · crackedFLOOR SUPPORT LOCATED AT RBL 9.0 FS 460 CRACKED AT FLANGE. DURING FLOORBEAM REPLACEMENT A VISUAL INSPECTION REVEALED CRACK AT FLANGE. INSPECTED 3 OTHER FLOOR SUPPORTS IN AIRCRAFT, NO OTHER CRACKS FOUND. THE FLOOR SUPPORT IS CURRENTLY INCLUDED IN THE 60 MONTMay 24, 2005 · N40HJ · Cndair CL6001A11 · Fuselage Miscellaneous StructureSDR DJFA2006372Fuel Control · unknownAT FLIGHT LEVEL 390 FT NR 2 ENGINE SHUTDOWN ON IT'S OWN. PILOTS DESCENDED AND AT FLIGHT LEVEL 100 FT THEY WERE ABLE TO GET THE ENGINE STARTED. LANDED WITH NO FURTHER PROBLEMS.Oct 18, 2003 · N602CW · Cndair CL6001A11 · Fuel Control/Turbine EnginesSDR DJFA200300003Fuel Control · malfunctionedAT FLIGHT LEVEL 390 FT NR 2 ENGINE SHUTDOWN ON IT'S OWN. PILOTS DESENDED AND AT FLIGHT LEVEL 100 FT, WAS ABLE TO GET THE ENGINE STARTED. LANDED WITH NO FURTHER PROBLEMS.Oct 18, 2003 · N602CW · Cndair CL6001A11 · Fuel Controlling SystemSDR 103901Duct · disconnectedDETECTED A RISE IN CABIN ALTITUDE THAT WAS NOT CONSIDERED NORMAL. MADE A PRECAUTIONARY DESCENT AND PERFORMED THE CABIN PRESSURE LOW CHECKLIST. LANDED AIRCRAFT AT INTENDED DESTINATION WITHOUT INCIDENT. FOUND A/C DISTRIBUTION DUCT FORWARD OF APU DISCONNECTED.Sep 4, 2003 · N895CC · Cndair CL6001A11 · Air Distribution SystemSDR EXO2003F00001Mount · crackedDURING INSPECTION OF THE RT THRUST REVERSER TRANSLATING SLEEVE. THE TOP JACKSCREW MOUNTING WAS FOUND CRACKED AROUND THE O-RING.Jan 21, 2003 · N678CG · Cndair CL6001A11 · Engine Thrust ReverserSDR EXO2003F00000Thrust Reverser · damagedDURING CLIMB THROUGH FL130 A LOUD BANG FOLLOWED BY RT THRUST REVERSER UNLOCK LIGHT, RETURNED TO AIRPORT. FOUND 12 O'CLOCK BALL SCREW ACTUATOR AFT ATTACH POINT FAILED CAUSING TRANSLATING STRUCTURE TO MOVE DOWN AND AFT ENOUGH TO CAUSE OTHER TWO ATTACH POINTS TONov 21, 2002 · N63HJ · Cndair CL6001A11 · Engine Thrust ReverserSDR CA020517008Crossbeam · cracked(CAN) DURING INTERNAL STRUCTURAL INSPECTION OF THE TAIL AREA, A 5/8 INCH CRACK WAS FOUND ON THE RUDDER CONTROL CROSS BEAM SUPPORT (EMPENNAGE).THE PROBABLE CAUSE MAY BE THAT ON THE LOWER LT OUTBOARD RIVETS WITH BELLOW MINIMUM EDGE DISTANCE. IN ADDITION, THE RIVApr 4, 2002 · Cndair CL6001A11 · Vertical StabilizerSDR J8G2001F00000Bearing · defectiveFLIGHT CREW NOTICED SMOKE IN THE CABIN AFTER TAKE-OFF FROM AIRPORT. THE AIRCRAFT RETURNED TO THE AIRPORT WITH NO FURTHER INCIDENT. INITIAL TROUBLESHOOTING INDICATED EXCESSIVE OIL PRESENCE AT NR 2 BEARING ON THE RIGHT ENGINE. DEFECT WITH NR 2 BEARING CONFIRMJun 29, 2001 · N710HL · Cndair CL6001A11 · Turbine SectionSDR 20010612CW007Windshield · delaminatedOUTER FACE PLY DELAMINATION OF LEFT HAND PILOTS WINDSHIELD. PLY SEPARATION WAS BEYOND LIMITS OF MANUFACTURES STRUCTURAL REPAIR MANUAL TO CONTINUE OPERATION.Jun 4, 2001 · N103HB · Cndair CL6001A11 · Flight Compartment WindowsSDR 20010612CW006Window · debondedPILOTS LEFT SIDE WINDOW WAS DISBONDED AT FORWARD VERTICAL EDGE.Jun 4, 2001 · N103HB · Cndair CL6001A11 · Flight Compartment WindowsSDR 20010427CW001Windshield · crackedDURING CRUISE FLIGHT, LEFT WINDSHIELD CRACKED. CREW CALLED MAINTENANCE. MAINTENANCE ADVISED TO TURN HEAT OFF. DELAMINATION STOPPED, CONTINUED TO DESTINATION.Apr 5, 2001 · N63HJ · Cndair CL6001A11 · Flight Compartment WindowsSDR 20001019SH026Compressor · crackedCUSTOMER REPORTED HIGH OIL CONSUMPTION AND OIL SMELL IN CABIN. APU DISASSEMBLED FOR COMPRESSOR REPAIR. DURING MAINTENANCE, FOUND COMPRESSOR ROTOR CRACKED AT SEVERAL VANE PLATFORM AREAS, NO FRACTURE NOTED, APU DID NOT FAIL. COMPRESSOR ROTOR PN 3822014-2 SN 9Aug 31, 2000 · N602AS · Cndair CL6001A11 · APU Core EngineSDR 20001019SH025Compressor · fracturedCUSTOMER REPORTED APU FAILURE, SUDDEN STOPPAGE, AND GEARBOX FAILURE. ACFT WAS ON GROUND AND APU IDLE, NOT LOADED. APU SUSTAINED A POWER GROUP CONTAINED SEPARATION FAILURE AND UNCONTAINED GEARBOX FAILURE. TEARDOWN REVEALED COMPRESSOR ROTOR FAILURE, VANE PLATAug 9, 2000 · N920DS · Cndair CL6001A11 · APU Core EngineSDR CA000724013Turbine · seized(CAN) AFTER LANDING, DURING ROLLOUT, THE CREW DEPLOYED THE THRUST REVERSER AND THE RT ENGINE SHUTDOWN. THE AIRCRAFT CONTINUED TO THE HANGAR AND AN INITIAL EVALUATION OF THE ENGINE REVEALED THAT THE TURBINE WHEEL HAD SEIZED.FURTHER DETAILS OF THE ENGINE INSPECTJul 8, 2000 · Cndair CL6001A11 · Turbine SectionSDR CA000724012Engine · failed(CAN) DURING CRUISE AT 41,000 FT THE FLIGHT CREW NOTICED A SMALL SURGE IN POWER ON THE RT ENGINE FOLLOWED ABOUT 10 SECONDS LATER BY A DECREASE IN RPM AND INCREASE IN ITT. THE ENGINE AND AIRCRAFT IMMEDIATELY BEGAN VIBRATING, WITH THE RT ENGINE VIBE METER INDICAJul 5, 2000 · Cndair CL6001A11 · Engine (Turbine/Turboprop)SDR CA000516033Fan · failed(CAN) FOLLOWING A/C ROTATIONAT 100AGL THE NUMBER 2 ENGINE AUTOMATICALLY SHUTDOWN WITH AN OVERSPEED INDICATION. N1 FAN WOULD NOT ROTATE. ENGINE REPLACED.Apr 11, 2000 · Cndair CL6001A11 · Turbine Engine Bypass SectionSDR 20000424SH010Heater · inoperativePILOT'S RIGHT FRONT WINDSHIELD HEATER INOPERABLE. (X)Mar 12, 2000 · N750GT · Cndair CL6001A11 · Windshield/Door Rain/Ice RemovalSDR 2000ZZZX836Fitting · crackedIN THE LAST 2 MONTHS HAVE FOUND 3 T-FITTINGS CRACKED AND LEAKING. (TWO ON 600 CHALLENGER, ONE ON 601). ONE DID CAUSE AN INTERRUPTION OF A FLIGHT. ALL THREE ARE ALUMINUM FITTINGS THAT HAD NOT BEEN DISTURBED SINCE MANUFACTURE.Mar 2, 2000 · N751DB · Cndair CL6001A11 · Fuselage Miscellaneous StructureSDR CA991230029Actuator · intermittent(CAN) DURING POST INSTALLATION TEST, CHANNEL 2 FOUND OPERATING INTERMITTENTLY. DURING TRIM COMMAND MOTOR WOULD OPERATE BUT SCREW JACK WOULD NOT ALWAYS TURN. COMPONENT RECIEVED IN THIS CONDITION FROM SUPPLIER.Dec 20, 1999 · Cndair CL6001A11 · Stabilizer ActuatorSDR CA991230028Actuator · failed(CAN) DURING POST INSTALLATION TESTING,CHANNEL 2 FOUND HARD FAILED. UNIT WAS RECEIVED IN THIS CONDITION FROM SUPPLIER. 0.0 HOURSDec 20, 1999 · Cndair CL6001A11 · Stabilizer ActuatorSDR 99ZZZX4400Bracket · crackedINSPECTION OF THE ADG BAY REVEALED THE ATTACH BRACKET, IN TWO PLACES, TO BE CRACKED. REMOVED AND REPLACED WITH A NEW BRACKET. LANDINGS: 4,672.Sep 23, 1999 · N491DB · Cndair CL6001A11 · Fuselage Miscellaneous StructureSDR 99ZZZX3566Duct · chafedDURING SCHEDULED INSPECTION, THE BLEED AIR DUCT, PN 215-0809-501, WAS FOUND CHAFING ON NR 2 BEARING OIL TUBE, PN 2-263-060-01. BOTH PARTS WERE CHAFED BEYOND LIMITS AND REQUIRED REPLACEMENT. OIL TUBE CHAFED 50 PERCENT WALL THICKNESS AND BLEED AIR DUCT CHAFED Aug 30, 1999 · N601SA · Cndair CL6001A11 · Engine Bleed Air SystemSDR 20001212AP012Windshield · crackedTAKEOFF FROM PUEBLO, COLORADO WAS NORMAL. AFTER 1:45 OF FLIGHT, A CRACK APPEARED ON THE LEFT WINDSHIELD. THE LEFT WINDSHIELD HEAT C/B WAS MANUALLY SWITCHED OFF; WEATHER WAS CAVU TO FXE. (M)Aug 16, 1999 · N63HJ · Cndair CL6001A11 · Fuselage Main, StructureSDR 99ZZZX3568Windshield · crackedPILOT'S WINDSHIELD CRACKED (OUTER LAYER ONLY) IN CRUISE FLIGHT.Aug 16, 1999 · N63HJ · Cndair CL6001A11 · Flight Compartment WindowsSDR CA990119007Valve · failed(CAN) NOSE GEAR DOORS FAILED TO OPEN WHEN GEAR SELECTED DOWN. PROBLEM INTERMITTENT AFTER COLD SOAK AT ALTITUDE.Jan 7, 1999 · Cndair CL6001A11 · Landing Gear Door Retract SectionSDR 98ZZZX4312Idg · failedTHE NR 2 GENERATOR DROPPED OFF-LINE ON LANDING. MAINTENNACE FOUND THE INTEGRATED DRIVE GENERATOR (IDG) DIFFERENTIAL INDICATORS POPPED AND THE OIL BLACK. THE OIL-OUT LINE FILTER REVEALED CHUNKS OF METAL. SUSPECT THE CONSTANT SPEED DRIVE FAILED (CSD). SUBMITNov 6, 1998 · N90UC · Cndair CL6001A11 · AC Generator-AlternatorSDR 99ZZZX436Bulkhead · crackedCRACKED BULKHEAD WEB AT FS 409. REF: SB 600-679. DATE SEPT 10, 1997. AD 97-24-02 AMEND 39-10209 EFFECT DATE 12-3-97. FS 409 REPAIRED ERGINEERING ORDER 600-53-175.Oct 27, 1998 · N550CW · Cndair CL6001A11 · Fuselage Main, BulkheadSDR CA980608009Relay · failed(CAN) BATTERY CHARGER ANNUNCIATOR ILLUMINATED DURING GROUND OPERATION. RELAY KP7A FOUND FAULTY. WHEN RELAY IS LATCHED BY A DC SENSE CIRCUIT, IT, IN TURN, WILL ALLOW THE AC BUS TO OPERATE BATTERY CHARGER. PART TC: 4,348.May 30, 1998 · Cndair CL6001A11 · DC Generating SystemSDR 98ZZZX3215Spacer · misinstalledHPN - NORMAL TAKEOFF EN ROUTE BAHAMAS. APPROX 1 HR EN ROUTE AT FL 310, PILOT NOTED NR 1 ENG VIBRATION INCREASE FROM .3 M/S TO .6 M/S AND INCREASE IN ENG NOISE. ALL OTHER ENG INDICATIONS WITHIN NORMAL PARAMETERS. ENG NOISE SUBSIDED THEN INCREASE IN ENG VIBRAMar 29, 1998 · N818TH · Cndair CL6001A11 · Turbine SectionSDR 98ZZZX533Sensor · misinstalledLEFT AND RIGHT WING ANTI-ICE FAIL LIGHTS CAME ON INTERMITTENTLY ANY TIME WING ANTI-ICE SYSTEM SELECTED. FOUND THE LEFT AND RIGHT WING TEMP SENSORS INSTALLED BACKWARDS FROM THE FACTORY. INSTALLED NEW SENSORS PER MM. SYSTEM WORKED NORMALLY ON NEXT FLIGHT.Jan 22, 1998 · N19HF · Cndair CL6001A11 · Airfoil Anti/De-ice SystemSDR 97ZZZX5136Tire · defectiveDURING POST-FLIGHT INSPECTION, A BUBBLE WAS FOUND ON THE SIDEWALL OF TIRE. AFTER TIRE WAS REPLACED, THE S/N WAS CHECKED AGAINST ANOTHER TIRE THAT HAD BEEN REMOVED PREMATURELY FOR AIR LEAKING FROM WEEP HOLES IN SIDEWALL. THAT TIRE S/N WAS 7102030. SINCED THENov 25, 1997 · N90UC · Cndair CL6001A11 · TireSDR 97ZZZX4716Heater Element · explodedTHE HEATER ELEMENT FAILED WITH AN EXPLOSIVE LIKE CHARGE THAT SENT THE FAILED ELEMENT AND WIRES INTO THE HONEYCOMB GALLEY TOP.Nov 7, 1997 · N711SX · Cndair CL6001A11 · Buffet/GalleysSDR 97ZZZX3498Cell · shortedAIRCRAFT BATTERY CHARGER DROPPING OFF-LINE. REMOVED AND SHIPPED BATTERY TO INSPECTION AND SERVICE. FOUND SHORTED CELL, STRAPS HAD BURNED SMALL HOLE THROUGH SIDE OF CELL. BATTERY WILL BE SHIPPED BACK TO MANUFACTURER DUE TO LOW TSN.Jul 22, 1997 · N100LR · Cndair CL6001A11 · DC Generator-AlternatorSDR CA970314005Gen Control Unit · failed(CAN) DURING FLIGHT APU STARTED AND STABILIZED. THE #2 AC ESSENTIAL BUS WAS KNOCKED OFF LINE. APU GENERATOR CONTROL UNIT REPLACED AS WELL AS #2 GENERATOR CONTROL UNIT.Mar 7, 1997 · Cndair CL6001A11 · DC Generating SystemSDR 96ZZZX5475Tee Fitting · leaking50 HRS AFTER MAJOR INSP, DEVELOPED LEAK IN LT WHEELWELL. FOUND NR 6 ELBOW CRACKED AND LEAKING. NEXT DAY FOUND HYD FLUID LEAKING OUT OF LT WHEELWELL AGAIN. FOUND NR 6 TEE FITTING CRACKED AND LEAKING. REPLACED BOTH. PRE-FLIGHTED A/C ON THIRD DAY FOR TRIP ANOct 8, 1996 · N100LR · Cndair CL6001A11 · Hydraulic System, MainSDR 96ZZZX5474Tee Fitting · leaking50 HRS AFTER MAJOR INSP, DEVELOPED LEAK IN LT WHEELWELL. FOUND NR 6 ELBOW CRACKED AND LEAKING. NEXT DAY FOUND HYD FLUID LEAKING OUT OF LT WHEELWELL AGAIN. FOUND NR 6 TEE FITTING CRACKED AND LEAKING. REPLACED BOTH. PRE-FLIGHTED A/C ON THIRD DAY FOR TRIP ANOct 8, 1996 · N100LR · Cndair CL6001A11 · Hydraulic System, MainSDR 96ZZZX5473Elbow · leaking50 HRS AFTER MAJOR INSP, DEVELOPED LEAK IN LT WHEELWELL. FOUND NR 6 ELBOW CRACKED AND LEAKING. NEXT DAY FOUND HYD FLUID LEAKING OUT OF LT WHEELWELL AGAIN. FOUND NR 6 TEE FITTING CRACKED AND LEAKING. REPLACED BOTH. PRE-FLIGHTED A/C ON THIRD DAY FOR TRIP ANOct 8, 1996 · N100LR · Cndair CL6001A11 · Hydraulic System, MainSDR CA960703019Id Generator · defective(CAN) GENERATOR TRIPPPING OFF LINE. METAL IN SCAVENGE FILTER AND ON CHIP DETECTOR. COMPONENT CAUSING TROUBLE WILL HAVE TO BE DETERMINED ON TEARDOWN.Jul 17, 1996 · Cndair CL6001A11 · AC Generator-AlternatorSDR 96ZZZM1323Outflow Vlv · malfunctionedAPPROX TWO HOURS INTO FLIGHT, CABIN PRESSURIZATION BEGAN TO FLUCTUATE 300 FEET IN AUTO MODE. AIR RUSHING NOISE COULD BE HEARD IN BAGAGE AREA. THE ELECTRO/PNEUMATIC OUTFLOW VALVE WAS REPLACED DURING AT 1200 HOUR INSPECTION APPROXIMATELY (8) FLIGHT HOURS PRIORJun 24, 1996 · N601WW · Cndair CL6001A11 · Pressure Regulator/Outflow ValveSDR 96ZZZX3018Support · crackedDURING 300-HOUR ENGINE INSPECTION, A 6.5 INCH HORIZONTAL CRACK WAS FOUND IN THE FAN COWL SUPPORT AT 3 O'CLOCK POSITION. ALSO, VARIOUS BRACKETRY ATTACHED TO COWL ASSY FOUND TO HAVE SMALL CRACKS.May 9, 1996 · N68SD · Cndair CL6001A11 · Engine Cowling System
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