Canadair CL-601-3A
Service difficulty reports · 81
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 = 'CL6013A' 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 = 'CL6013A' 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 2023FA0000291Unknown · unknownDURING FLIGHT VNY - APC, CREW REPORTED EHSI WAS SHOWING APPROX 100 DEG OFF CORRECT READING. CREW DECLARED AN EMERGENCY AND DIVERTED TO BFL. MX C/W OPS CHECKS BUT COULD NOT DUPLICATE, NO DEFECTS WERE NOTED.SDR CA190530003Gcu · faulted(CAN) CREW DID RAM AIR TURBINE DROP TEST IN FLIGHT AND AFTER RAT DEPLOYED, A/C LOST ALL COCKPIT INDICATION (INCLUDING GEAR INDICATIONS) ONLY STANDBY INSTRUMENTS WERE FUNCTIONING, RAT HANDLE WAS STOWED IN THE ALLOTTED TIME, CREW TRIED TRANSFER OVERRIDE WITH SAMSDR CA190415007Door · malfunctioned(CAN) DURING TAKE OFF THE NOSE LANDING GEAR (NLG) DOORS DID NOT CLOSE. AIRCRAFT LANDED AT DEPARTURE AIRPORT WITHOUT FURTHER INCIDENT. NO RECTIFICATION OR PARTS ISSUES HAVE BEEN PROVIDED. BOMBARDIER TRYING TO CONTACT SUBMITTER FOR DETAILS. SDR REVIEWED (TC# 20SDR CA190416014Actuator · failed(CAN) AOG DUE TO HSTA FAILURE PREVIOUSLY INSTALLED HSTA HAS BEEN A NFF. (TC# 20190416014)SDR CA191203013Proximity Switch · out of rig(CAN) AFTER TAKE OFF, GEAR UP SELECTION, GEARS CAME UP BUT NO GREEN INDICATION FOR THE NLG. CREW DECIDED TO GO BACK AND HAD TO USE THE EMERGENCY HANDLE TO EXTEND THE NLG GEAR. BOTH NLG DOWN-LOCK PROXIMITY SWITCHES WERE FOUND OUT OF RIG. THE SWITCHES WERE READJSDR 2017FA0000108Tire · failedWHEN ACFT DEPARTED, THE NR 2 TIRE TREAD SEPARATION, SIDEWALL OF THE TIRE. THE CREW DID NOT FEEL OR HEAR ANYTHING. TIRE DAMAGE FOUND ON POST FLIGHT INSPECTION.SDR RU3A20170210003Connector · dirtyRIGHT ENGINE COWL ANTI-ICE FAIL LIGHT ILLUMINATED DURING FLIGHT, PROBLEM WAS CORRECTED AFTER CLEANING OF ELECTRICAL CONNECTORS.SDR RU3A20160114003Panel · defectiveACRID ELEC ODOR EMANATING FROM PILOT'S ALTITUDE AWARENESS PANEL. REPLACEMENT OF THE PILOTS ALTITUDE AWARENESS PANEL RESOLVED THE ISSUE.SDR CA151111001Bolt · failed(CAN) DURING PRE-FLIGHT, FOUND ONE BOLT SHEARED ON NUMBER 3 MAIN WHEEL. AFTER INVESTIGATION IT WAS FOUND THAT THE WHEEL HAD LAST BEEN OVERHAULED AND NO BOLT WERE REPLACED. NDT HAD NOT REVEALED ANY PROBLEMS WITH THE WHEEL BOLTS. NO HEAVY LANDING OR OTHER STRESSSDR CA151002001Line · leaking(CAN) IN FLIGHT, LH HYDRAULIC ENGINE PUMP FAIL LIGHT CAME ON - PRESSURE 0 PSI AT NR 1 HYDRAULIC SYSTEM, AS REPORTED BY CREW. ON GROUND, FOUND EVIDENCE OF HYDRAULIC FLUID COMING FROM LH PYLON AND INSIDE AFT COMPARTMENT. FURTHER INVESTIGATION SHOWED LH HYDRAULICSDR CA150820012Transceiver · failed(CAN) WEATHER RADAR TRANSCEIVER FAILED DURING CRUISE. WEATHER RADAR WAS INOPERATIVE.SDR CA150608003Wire · burned(CAN) THE OPERATOR`S MAINTENANCE PROVIDER RECENTLY REPORTED TO BOMBARDIER THAT THE FLIGHT CREW REPORTED BOTH ENGINE GENERATORS DROPPED OFF LINE DURING CRUISE FLIGHT. THE AIR DRIVEN GENERATOR (ADG) SUCCESSFULLY DEPLOYED AND THE FLIGHT CREW DIVERTED FROM THEIR FSDR CA150327002Screw · broken(CAN) LT ACME SCREW ADJUSTING FOUND BROKEN FOLLOWING PILOT REPORT.SDR CA150108002Engine · shutdown(CAN) CUSTOMER REPORTS THE LEFT ENGINE SHUT DOWN UN-COMMANDED. THE AIRCRAFT WAS ON DESCENT. THE PILOTS THINK THEY HAD A COMPRESSOR STALL. THE LEFT ENGINE SHUTDOWN. THE PILOTS DIVERTED TO HOME BASE AND LANDED UNEVENTFULLY.SDR CA141114001Landing Gear · failed(CAN) AT APPROX. 5 MILES FINAL RUNWAY 16, AN EXECAIRE CANADAIR CL600-2B16 REPORTED A POSSIBLE NOSE GEAR PROBLEM. DID A FLY BY AND NOSE GEAR WAS NOT OBSERVED TO BE DOWN. DID A VFR CIRCUIT AND RECYCLED THE GEAR WHICH RESULTED IN A "THREE GREEN" INDICATION. AIRCRSDR CA131121013Tire · damaged(CAN) ON CREW WALK AROUND, FOUND TIRE WITH PARTIAL TREAD LOSS.SDR CA130916007Fitting · leaking(CAN) FITTING, PN MS 21926-6D IN MLG RUN AROUND AND DUMP VALVE STARTED TO LEAK DURING GEAR SWINGS DUE TO GEAR REPLACEMENT. FITTING WAS REMOVED AND INSPECTED. A CRACK WAS FOUND RUNNING PERPENDICULAR TO THE THREADS STARTING AT THE BASE OF THE FITTING. THE CRACKSDR DBCA2013041700003Outflow Valve · failedAIRCRAFT DEPARTED MKE - ON CLIMBOUT CREW NOTED AIRCRAFT WASN'T PRESSURIZING. CREW RETURNED TO MKE. LANDING WAS UNEVENTFUL. PRESSURIZATION SYSTEM TROUBLESHOT BY STERLING MTN. STERLING MTN FOUND SECONDARY OUTFLOW VALVE STICKING. REPLACED SECONDARY OUTFLOW SDR DBCA2013022700002Pressure Switch · failedAT START OF TAKEOFF ROLL THE RIGHT ENGINE NACELLE ANTI-ICE FAIL ANNUNCIATOR ILLUMINATED. CREW ABORTED TAKEOFF ROLL AND RETURNED TO BASE. MX TROUBLESHOT TO FAULTY NACELLE ANTI-ICE PRESSURE SWITCH. MX REPLACED FAULTY PRESSURE SWITCH WITH NEW. OPS CHECK GOOD.SDR CA130214019Wire · chafed(CAN) ACFT ESSENTIAL FEED 1 CIRCUIT BREAKER TRIPPED ON TOUCHDOWN. WIRE XD103B10WHT WAS FOUND WITH INSULATION CHAFED AND SHORTED TO AN AIRFRAME BONDING STUD BEHIND THE PILOT SIDE FORWARD CONSOLE CIRCUIT BREAKER PANEL AT BS 228.0. THE WIRE WAS REPLACED WITH NESDR CA130114012Tie Bolt · sheared(CAN) DURING WALK AROUND INSPECTION, NOTICED NR 3 MAIN WHEEL ASSY MISSING TIE BOLT. REMOVED WHEEL AND FOUND THE BOLT HAD SHEARED LEAVING THE HEAD AND WASHER BETWEEN THE WHEEL ASSY AND BRAKE ASSY. NO DAMAGE TO BRAKE ASSY, WHEEL ASSY SENT FOR REPAIR/TIRE CHANGESDR DBCA2012112900006Unknown · malfunctionedON AIRCRAFT POWER UP CREW NOTED ALTITUDE COMPENSATOR ANNUNCIATOR WAS ILLUMINATED. CREW POWERED DOWN AIRCRAFT AND CONTACTED MAINTENANCE. BOMBARDIER COMPLETED ALL ALTITUDE COMPENSATOR TESTS AND STALL PROTECTION SYSTEM CHECKS PER A/M/M. COULD NOT DUPLICATE DISSDR CA121005006Wire · arced(CAN) THE CBP-A AND CBP-B WERE OPENED TO ACCESS THE POWER DISTRIBUTION BUSSES. WE WERE ATTACHING A METER TO THE BUSSES USING AN ALLIGATOR CLIPPED LEAD TO MEASURE THE VOLTAGE ON THE BUS. AT THE TIME OF THE FIRE, NOTHING WAS ATTACHED TO THE CB PANEL BUSSES. NO SDR CA120405004Fuel Control · malfunctioned(CAN) DURING DESCENT, BOTH THRUST LEVERS WERE RETARDED TO IDLE. THE RT ENGINE FLAMEDOUT. THE CREW ELECTED TO CONTINUE WITH THE APPROACH SINGLE ENGINE. THE CUSTOMER IS REQUESTING TROUBLESHOOTING GUIDE LINES. ACFT WAS 5.5 HRS INTO FLIGHT LEG, STARTING DESCENTSDR DBCA2011113000007Hydraulic Line · failedON APPROACH TO RDU CREW NOTED HYDRAULIC SYSTEM 3 QUANTITY LOW. CREW FOLLOWED AFM CHECKLIST PROCEDURES AND LANDED UNEVENTFULLY AT RDU. STERLING MX CONTACTED LOCAL MX TO EVALUATE. LOCAL MX FOUND PRESSURE LINE OF HYDRAULIC PUMP 3A HAD FAILED. REPLACED FAILED SDR CA110908001Engine · malfunctioned(CAN) AFTER DEPARTURE, THE ACFT WAS CLIMBING THROUGH, APPROX 20,000- 21,000 FEET, WHEN THE CREW NOTICED THE RT ENGINE, "RED LOW OIL PRESSURE LIGHT", ON, AS WELL AS THE CORRESPONDING OIL PRESSURE GAGE READING ZERO. ALL OTHER ENGINE PARAMETERS WERE INDICATING NSDR CA110822013Engine · shutdown(CAN) LT ENGINE EXCEEDANCES AND COMMANDED SHUTDOWN AFTER ENCOUNTERING TURBULENCE. WHILE CRUISING AT FL410 WITH 4 PASSENGERS AND NO F/A THE CREW WAS NAVIGATING AROUND A THUNDERSTORM WHEN THEY ENCOUNTERED EXTREME TURBULENCE. THE LT JETPIPE OVERHEAT LIGHT ILLUMSDR CA110803015Engine · inoperative(CAN) THEY WERE AT CRUISE ALTITUDE WHEN THE CAPTAIN NOTICED THE LT ENGINE OIL PRESSURE WAS ON THE RISE AND REACHING THE YELLOW BAND. HE PULLED THE POWER BACK A BIT AND NOTICED THE PRESSURE CAME DOWN. HE CONTINUED TO PULL THE POWER BACK AND STILL REMAIN ABOVESDR CA110721011Unknown · unknownDURING A TRAINING FLT, AFTER LANDING WHILE SLOWING BELOW 100 KNOTS, AS THRUST REVERSERS DEPLOYED, THE ACFT PITCHED UP AND BECAME AIRBORNE. AFTER TOUCHING DOWN AGAIN, THE ACFT BOUNCED AND ROLLED TO THE RT. THE RT WING TIP THEN CONTACTED THE RUNWAY. THERE WERSDR CA110106010Actuator · wornDURING AN APPROACH AT QB, THE CAPTAIN DURING THE DESCENT TRIED TO SET THE FLAPS DOWN AND HE HAD FLAP FAIL AT 15 DEGREES (JAM), CALLED THE TOWER FOR EMERGENCY LANDING AND LANDED SAFELY THE AME FOUND THE RT INBD FLAP ACTUATOR LOOSE AND REPLACED. NOTE HAD FLAP FASDR CA101222013Powerplant · shutdown(CAN) BOTH ENGINES SHUTDOWN DURING LANDING ROLLOUT. PILOTS HAD APU RUNNING FOR BLEED, BUT APU GEN WAS NOT ON LINE. ADG ALSO AUTO DEPLOYED. NO WATER IN FUEL. THROTTLES WERE PULLED TO IDLE AT 50` AGL. THRUST REVERSERS WERE NOT USED ON LANDING ROLL OUT ASSDR CA101022003Converter · failedDURING CRUISE THE PILOT NOTICE THE AUXILIARY WARNING LIGHT WAS ON, ON THE ENG CONTROL PANEL, AN INDICATION OF POWER LOSS ON 1 CHANNEL, IN A DUAL CHANNEL SIGNAL DATA CONVERTER. ALL ENG INSTRUMENTS N1,N2, FF, ITT, FP, OP, & FUEL TOTALIZER GO THROUGH BOTH CHANNSDR CA100928015Flex Hose · burstBURST IN FLEX NEAR QUICK DISSCONNECT FITTING END, LOSS OF HYD PRESSURE AND FLUID.SDR CA100825002Inverter · failed(CAN) DEFECT ON 1 OF THE 3 CIRCUITS IN THE INVERTER, MADE AN OVERVOLTAGE AND BURNED 1 OF THE 2 FLUORESCENT TUBE PN: 6845-375 IN LT GLARESHIELD FLOOD LIGHT PN: 10-701T-2LR16-00 MAKING ODOR AND DUST IN LT COCKPIT FOR 15 SECONDS THEN STOPPED.SDR CA090529001Cable · worn(CAN) DURING APPROACH THE CREW EXPERIENCED MULTIPLE COMPRESSOR STALLS ON THE LT ENG. THEY CARRIED OUT THE APPROACH WITH THAT ENGINE AT IDLE. AT ONE POINT, THE ITT STARTED RISING AND THE CREW ELECTED TO SHUTDOWN THE ENGINE FOR THE REMAINING OF THE APPROACH. THESDR CA081009001Water Heater · damaged(CAN) ON CLIMB OUT SMOKE WAS OBSERVED COMING OUT OF THE FUEL CONTROL PANEL IN THE FORWARD GALLEY. THE WATER HEATER INSULATION BLANKET IN THE FORWARD GALLEY HAD EVIDENCE OF HEAT DAMAGE. INSTALLATION OF THIS PART IN THE FORWARD GALLEY OF THE ACFT IS A PART OF SDR CA080813003Hydraulic Line · burst(CAN) IN FLIGHT NR 2 HYDR "LO PRESS" CAME ON, FWD BY "LO LEVEL". NR 2 HYDR FLUID COMPLETLY LOST THROUGH A BURST HYDR PRESSURE HOSE IN RT NACELLE.SDR CA071022001Tube · cracked(CAN) DURING POWER PLANT BUILD UP, FOUND LINE P/N 228-52402-115 FOR PYLON STATIC PRESSURE TO FCU CRACKED AT MIDDLE. THE CRACK WAS HIDDEN BY A LINE IDENTIFICATION DECAL. LINE WAS REMOVED AND REPLACED AIRCRAFT WILL BE RETURNED TO SERVICE. (TC NR 20071022001)SDR CA070917005Unknown · multiple fail(CAN) AIRCRAFT EXPERIENCED FLAP FAILURE ON PREPARATION FOR LANDING, THEN FLEW APPROXIMATELY A FURTHER 10 MINUTES ATTEMPTING,UNSUCCESSFULLY, TO DEPLOY THE FLAPS. ON TOUCHDOWN THE THRUST REVERSERS (TR) DID NOT DEPLOY WHEREUPON THE CREW RECYCLED THE TR ARM SWITCHSDR CA070403005Water Heater · odor(CAN) WHILE EN ROUTE, A BURNING ODOR WAS NOTICED BY THE CREW AND PASSENGERS. NO SMOKE WAS APPARENT IN THE CABIN OR COCKPIT. THEN SEARCHED THE LAVATORY AND BAGGAGE COMPARTMENT. A TRACE OF SMOKE WAS FOUND IN THE BAGGAGE COMPARTMENT. A QUICK VISUAL INSPECTIONSDR CA070209023Windshield · cracked(CAN) RT WINDSHIELD OUTER LAYER CRACKED DURING FLIGHT, A SINGLE CRACK LOCATED IN THE CENTER OF THE WINDSHIELD AND IS VERTICAL FROM TOP TO BOTTOM. AIRCRAFT PRESSURIZATION WAS NOT AFFECTED AND AIRCRAFT RETURNED TO BASE. (TC NR 20070209023)SDR CA061227006Windshield · broken(CAN) RT WINDSHIELD FACE PLY BROKEN IN FLIGHT. APPROX. 7000 INCH ON APPROACH. FOD INSPECTION CARRIED OUT ON ENGINE INTAKE AND WINDSHIELD REPLACED. A/C HOURS; 6836 A/C CYCLES; 7326 (TC NR 20061227006)SDR CA061218015Pump · damaged(CAN) LOST OF NR 3 SYSTEM HYDRAULIC FLUID IN FLIGHT. THE NR 3B PUMP HAS FAILED ON FLANGE GASKET. THE PUMP HAS BEEN REPLACED AND A\C RETURNED TO SERVICE. A/C HOURS: 6816:27 A/C CYCLES ; 7302 (TC NR 20061218015)SDR CA061208001Actuator · cracked(CAN) DURING SCHEDULE LUBRICATION OF THE FLAP ACTUATORS, THE TECHNICIAN NOTICED GREASE WAS OOZING OUT OF A CRACKED WELD ON THE HOUSING OF THE LT OB FLAP ACTUATOR JACK SCREW. (TC NR 20061208001)SDR CA060712003Feeder Cable · arced(CAN) RT GEN TRIPPED OFFLINE DURING APPROACH. GEN OFF ANNUNCIATOR CAME ON, PWR AUTO TRANSFERED FROM GEN 1. NO LOSS OF PWR ON ANY AC BUSES. AC FERRIED WITH GENERATOR 2 SELECTED OFF. ON 3RD ENGINE RUN, PROBLEM WAS DUPLICATED. PROBLEM WAS ISOLATED TO A WIRING PROSDR CA060704009Stall Warning · false activation(CAN) THE FOLLOWING WAS REPORTED BY THE PILOT; "THE STALL WARNING HORN SOUNDED, STICK SHAKER ACTIVATED FOLLOWED BY THE PUSHER AT FL320 DURING CLIMB. R AFCS WAS ENGAGED AND COUPLED TO CO-PILOT¿S FD AT THE TIME. WHEN THE PILOT GRABBED THE YOKE THE SHAKER ACTIVSDR 2006FA0000072Wire · shortedWHILE TROUBLESHOOTING INTERMITTENT UPPER BEACON CIRCUIT BREAKER FAULT, DISCOVERED LT ELEVATOR CONTROL CABLE HAD TORN THROUGH WIRING CONDUIT IN VERTICAL STABILIZER. THE CABLE WORE THROUGH THE CONDUIT AND SHORTED OUT THE WIRING FOR THE UPPER BEACON. REPAIRED WSDR CA041223003Engine · malfunctioned(CAN) UNCOMMANDDED ACCELERATION ON THE LT ENGINE ON TAKE OFF AROUND + 7 PERCENT ABOVE RETURN TO NORMAL 40 SECONDS LATER.SDR O2G2005F00000Windshield · crackedTHE OUTER PLY OF THE PILOTS WINDSHIED CRACKED AT APPROX 35,000 FT. CHANGED PILOTS NR 1 WINDSHIELD.SDR CA041115005Wire Harness · damaged(CAN) PILOT'S EFIS EADI WIRE BUNDLE CHAFING 12 INCHES FROM CONNECTOR 1P3FH. WIRE BUNDLE CONSISTS OF SEVERAL SHIELDED TWISTED PAIR. SOME WIRE FOUND TO HAVE ABRADED INTO CENTER CONDUCTOR. WIRES FH215D24, FH216D24, 1FH108A24, 1FH109A24, FH230D24, FH231D24, 1FH116
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