Canadair CL600-1A11
Service difficulty reports · 69
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = 'CL6001A11' 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.
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 = 'CL6001A11' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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.SDR 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 SDR 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 PRESDR 2008FA0000537Skin · corrodedSURFACE CORROSION (PITTING) DISCOVERED ON BOTH WINGS LOWER SURFACES ADJACENT TO AND OB OF WHEEL WELLS, CORROSION DEEMED UNUSUALLY SEVERE. (K)SDR 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)SDR 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 SPEEDSDR 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 SDR 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 ENGISDR 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)SDR 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. (SDR 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 MONTSDR 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.SDR 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.SDR 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.SDR EXO2003F00001Mount · crackedDURING INSPECTION OF THE RT THRUST REVERSER TRANSLATING SLEEVE. THE TOP JACKSCREW MOUNTING WAS FOUND CRACKED AROUND THE O-RING.SDR 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 TOSDR 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 RIVSDR 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 CONFIRMSDR 20010612CW007Windshield · delaminatedOUTER FACE PLY DELAMINATION OF LEFT HAND PILOTS WINDSHIELD. PLY SEPARATION WAS BEYOND LIMITS OF MANUFACTURES STRUCTURAL REPAIR MANUAL TO CONTINUE OPERATION.SDR 20010612CW006Window · debondedPILOTS LEFT SIDE WINDOW WAS DISBONDED AT FORWARD VERTICAL EDGE.SDR 20010427CW001Windshield · crackedDURING CRUISE FLIGHT, LEFT WINDSHIELD CRACKED. CREW CALLED MAINTENANCE. MAINTENANCE ADVISED TO TURN HEAT OFF. DELAMINATION STOPPED, CONTINUED TO DESTINATION.SDR 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 9SDR 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 PLATSDR 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 INSPECTSDR 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 INDICASDR 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.SDR 20000424SH010Heater · inoperativePILOT'S RIGHT FRONT WINDSHIELD HEATER INOPERABLE. (X)SDR 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.SDR 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.SDR CA991230028Actuator · failed(CAN) DURING POST INSTALLATION TESTING,CHANNEL 2 FOUND HARD FAILED. UNIT WAS RECEIVED IN THIS CONDITION FROM SUPPLIER. 0.0 HOURSSDR 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.SDR 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 SDR 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)SDR 99ZZZX3568Windshield · crackedPILOT'S WINDSHIELD CRACKED (OUTER LAYER ONLY) IN CRUISE FLIGHT.SDR CA990119007Valve · failed(CAN) NOSE GEAR DOORS FAILED TO OPEN WHEN GEAR SELECTED DOWN. PROBLEM INTERMITTENT AFTER COLD SOAK AT ALTITUDE.SDR 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). SUBMITSDR 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.SDR 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.SDR 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 VIBRASDR 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.SDR 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 THESDR 97ZZZX4716Heater Element · explodedTHE HEATER ELEMENT FAILED WITH AN EXPLOSIVE LIKE CHARGE THAT SENT THE FAILED ELEMENT AND WIRES INTO THE HONEYCOMB GALLEY TOP.SDR 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.SDR 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.SDR 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 ANSDR 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 ANSDR 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 ANSDR 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.SDR 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 PRIORSDR 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.
Back to Canadair CL600-1A11