Bombardier CL-604
Service difficulty reports · 220
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 = 'CL604' 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 = 'CL604' 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 CA101101006Smoke Detector · shorted(CAN) PLEASE BE ADVISED WE HAD AN INCIDENT ABOARD THE ABOVE AIRCRAFT ON APPROACH TO AIRPORT ON THE 1ST OCTOBER 2010. THE FOLLOWING IS THE COMMANDERS REPORT. FL 400 APPROACHING TOD P2 HANDLING, NIGHT, 3 PAX, 2 PILOTS, 1 CABIN ATTENDANT. BAGGAGE BAY SMOKE WASDR 2010FA0000534Sensor · unsecure((JGVR)) RECEIVED UNIT, AS A REPAIRED UNIT. SENSOR HSG FOUND, NOT SECURED. SENSOR COULD BE ROTATED (RECLOCKED) GIVING IMPROPER READINGS. DISCOVERED WHEN TECH ATTACHED MOUNTING BRACKETS, TEMPORARILY INSTALLED SENSOR IN ACFT, ROTATED SENSOR TO CLOCK POSITION SDR CA110224003Pitot System · contaminated(CAN) ON DESCENT, RECEIVED AN EFIS COMP MON CAUTION ON ED 1 WITH A YELLOW IAS FLAG ON BOTH PFD`S. NOTICED LT IAS MATCHED THE STANDBY IAS, RT IAS INDICATING 15 KNOTS HIGHER. ON APPROACH, FLAPS AT 20 DEGREES & 190 KNOTS ON LT IAS, STANDBY IAS INDICATING 170 KNSDR CWQA04142010Duct · contaminatedREJECTED TAKEOFF DUE ANTI-ICE FLUID IN APU DUCTS CAUSING SMOKE IN PLANE. RAN ENGINES AT N1 FOR THE DAY TO CLEAR ANY ANTI-ICE FLUID. OPS CHECK GOOD. AIRCRAFT WAS DE-ICED PRIOR AND EMERGENCY EQUIP WAS REQUESTED AFTER EVENT.SDR CA100216009Rod · unserviceable(CAN) BOTH THROTTLE ACTUATOR RODS WERE FOUND WITH CHAFING DAMAGE RESULTING FROM CONTACT WITH THE ELEVATOR TORQUE TUBE ASSY PN 600-90410-803. THE CONTACT WAS WHEN THE THROTTLES WERE IN OR BETWEEN IDLE AND CUTOFF. LOCATION DAMAGE ON THE RODS IS AT THE FIRST BESDR CA100119002Deice System · failed(CAN) UPON RETURN FROM FLIGHT, HEATED DRAIN MAST WAS COVERED OVER WITH ICE INDICATING THAT IT WAS NOT FUNCTIONING IN FLIGHT. WHEN THE ACFT WAS PLACED IN THE HANGAR, ELECTRICAL POWER APPLIED AND THE SKIN REMAINED BELOW 45 DEG AND ALLOWED ELECTRICAL CURRENT TO SDR CA091218003Power Lever · stiff(CAN) CAPTAIN REPORTED THE NR 1 THRUST LEVER WAS STIFF TO OPERATE AND GETTING WORSE AS FLIGHT CONTINUED. A RETURN TO THE FIELD OF DEPARTURE WAS CARRIED OUT. (TC NR 20091218003)SDR CA091201001Oil System · low pressure(CAN) DURING THE TAKEOFF ROLL, THE RT ENG LOW OIL PRESS INDICATION CAME ON THE CREW REDUCED ENGINE POWER TO IDLE AND THE ENGINE SHUT DOWN UNCOMMANDED AIRCRAFT RETURNED TO PARKING POSITION. INVESTIGATION ON GOING, FIRST CHECK OF OIL LEVEL SHOWED SUFFICIENT OILSDR CA091202015Solenoid · open(CAN) MLG FAILED TO DEPLOY. QRH PROCEDURES FOLLOWED, ALT EXTENSION CARRIED OUT. T/S DISCOVERED OPEN CIRCUIT ON EXTEND SOLENIOD OF MLG SELECTOR VALVE. VALVE CHANGED AND GEAR SWINGS COMPLETED PER AMM. A/C RETURNED TO SERVICE. (TC NR 20091202015)SDR CA091201004Transmitter · malfunctioned(CAN) CADOR 2009C3326 ON TAKEOFF WHEN THE PILOT ADVANCED THE THRUST LEVERS HE GOT A CONFIGURATION SPOILER WARNING MESSAGE. THE TAKEOFF WAS REJECTED AND THE AIRCRAFT RETURNED TO BASE. UPON INVESTIGATION IT WAS FOUND THAT MAINTENANCE WAS PERFORMED ON THE RT FLIGSDR CA091105001Fcu · obstructed(CAN) ON DESCENT LT ENG PWR LEVER COULD NOT BE RETRACTED. AN IN FLIGHT SHUTDOWN WAS CARRIED OUT. ACFT LANDED AT DESTINATION WITHOUT FURTHER INCIDENT. SUBSEQUENT INVESTIGATION FOUND THE LT ENG UPPER CORE COWL STAY OUT OF PLACE AND INTERFERING WITH THE FCU. THESDR CA091120002Rod · loose(CAN) DURING FLIGHT THE CREW COULD NOT RETARD THE LT THROTTLE. ENG WAS SHUTDOWN AND AN UNEVENTFUL LANDING MADE. IT WAS SUBSEQUENTLY FOUND THE UPPER COWL SUPPORT ROD HAD COME OUT OF ITS STORAGE CLIP AND FALLEN ONTO THE THROTTLE LINKAGE.SDR CA091020004Case · cracked(CAN) CRACKS TO THE AFT FAN CASE PN 6052T01G08 WERE DISCOVERED PRIOR TO SCHEDULED ACFT ENG WATER WASH. 2 CRACKS ALONG THE HORIZONTAL AXIS OF THE FAN CASE CONTINUING DOWNWARD ALONG THE FLANGE. ENG HASE BEEN REMOVED FOR FAN CASE REPAIR.SDR CA090924008Case · cracked(CAN) UPON CLEANING OF FAN ASSY. DURING MX EVENT, IT WAS NOTICED THAT A 3 INCH CRACK AFT OF THE FAN STATOR RING WAS PRESENT. FURTHER INVESTIGATION REVEALED A CRACK PROPOGATING ALONG 2 BOLT HOLES THAT ATTACH THE FAN CASE TO THE THRUST REVERSER DEFLECTOR RING.SDR CA090901004Cowling · departedDURING TAKE-OFF PHASE, ACFT LOST THE LT FWD ENG COWLING.SDR CA090731005Sensing Element · chafedCREW REPORT AT 14,000 FT GOT RT ENGINE FIRE WARNING. WARNING WENT OUT WHEN PWR LEVER WAS PULLED TO IDLE. SECURED ACFT VIA CHECKLIST. DID NOT USE ENG FIRE EXTINGUISHERS. RT ENG COMBUSTION SECTION FIRE DETECTION SENSE ELEMENT, PN:244-10457 SN:9724 REMOVED DSDR CA090728002Heater · overheated(CAN) OPERATOR REPORTED AFTER A 4 HR FLIGHT THAT SUITCASES STORED IN BAGGAGE COMPARTMENT ON THE FLOOR JUST INSIDE CARGO NET (RT SIDE) ARE TOO HOT TO TOUCH. ONE SUITCASE HAS SUFFERED HEAT DAMAGE (DAMAGE TO THE CREW SUITCASE HANDLE). MX WIRING VERIFICATION DONSDR CA090716001Bearing · failed(CAN) THE APU WAS STARTED IN FLIGHT AND ACFT LANDED. WHEN IT GOT TO FBO SMOKE STARTED TO COME INTO CABIN. IT WAS NOT BAD ENOUGH TO WARRANT AN EMERGENCY EVACUATION AND AS APU SHUT ITSELF DOWN IT DID NOT GET ANY WORSE. IT WAS OBSERVED BY FBO THAT AT THE SAME SDR CA090629006Apu · failed(CAN) WHILE THE ACFT WAS TAXIING TO FBO RAMP, SMOKE AND FLAMES WERE COMING OUT OF THE APU INLET. APU WAS SHUTDOWN. APU ENCLOSER AND INTAKE WAS INSPECTED, CHECKED OIL LEVEL AND CHIP DETECTOR. FOUND TO BE OK. TRIED TO START THE APU, IT WOULD ACCELERATE TO 14SDR CA090401011Holder · melted(CAN) NEON LIGHT, PLASTIC HOLDING CLAMP MELTED DOWN. THIS NEON IS LOCATED IN THE CABIN GALLEY. IT HAS BEEN DETECTED BY THE ODOR (SMELL IN THE CABIN). MFG HAS BEEN ADVISED AND THEY WILL WRITE A CONDITION REPORT. AT THE TIME OF THE SNAG, ACFT WAS ON EXTERNAL SDR CA090318002Balance Tube · blocked(CAN) FOLLOWING RECEPTION OF ADVISORY WIRE NR AW604-28-0082, BORESCOPE INSP HAS BEEN PERFORMED IN THE 1 AND 3 INCHES FUEL BALANCE TUBES OF BOTH WINGS. THE RESULT IS, ALL TUBES SEALED WITH PRC ARE PARTIALLY BLOCKED (ESTIMATED AVERAGE BLOCKAGE 10 TO 20 PERCENT, SDR CA090202007Duct · dented(CAN) WHILE IN SCOTTSDALE, ARIZONA, DURING THE PREFLIGHT CHECK THE CREW NOTICED THE APU INLET WAS DENTED AND APU INLET BELLOWS WAS RIPPED. NO OPERATIONAL ABNORMALITY WERE NOTICED BY THE CREW PRIOR TO THE DISCOVERY. MAINTENANCE TECHNICIAN WAS DISPATCHED AND BSDR CA090127005Butterfly Valve · brokenPILOT REPORTED LEFT AIR CONDITIONING PACK BLOWS HOT AIR REGARDLESS OF TEMPERATURE SELECTION. SYSTEM INTERROGATED AND DETERMINED THE LOW PRESSURE MODULATING AND SHUTOFF VALVE DEFECTIVE. CLOSE INSPECTION OF VALVE PLENUM DETERMINED BUTTERFLY VALVE HAD BEEN EJECSDR CA090102002Flap System · malfunctioned(CAN) ON APPROACH THE FLAP FAILED TO EXTEND AND THE AIRCRAFT DIVERTED WHERE THEY LANDED WITH THE FLAPS UP. UPON INSPECTION FOUND THE FLAPS WOULD NOT MOVE AND WERE IN ASYMMETRIC CONDITION. BOTH THE LT AND RT BDU WERE REPLACED AND THE FLAP SYSTEM TESTED SERVICSDR CA081218003Display · malfunctioned(CAN) IN CRUISE FL 380, 3.5 HOURS IN FLIGHT, THE MFD NR 2 LOWER WINDOW STARTED TO CYCLE BETWEEN THE DIFFERENT FORMATS (PPOS, PLAN, TCAS ECT) AT FEW SECONDS INTERVAL WITH UNDEFINED SYMBOLS/TEXT LINE (HIEROGLYPH). AT THAT TIME THE PFDS 1 AND 2, MFD 1 SHOWED NORSDR CA081205002Display · inoperative(CAN) 30 MINUTES PRIOR TO LANDING, THE PILOT PRIMARY FLIGHT DISPLAY(PFD 1) WENT BLANK. THEN IAW AFM (SECTION 05-15-1) THE CREW SELECTED THE REVERSION MODE TO HAVE THE MULTIFUNCTION DISPLAY (MFD 1) IN COMPRESSED MODE, AT THAT TIME THE MFD 1 ALSO WENT BLANK. THESDR CA081029001Tube · damaged(CAN) WHILE TROUBLESHOOTING A FUEL TRANSFER PROBLEM ON THE CHALLENGER 604, SERIAL NR 5320, WE FOUND 3 DAMAGED FUEL TUBES IN THE CENTER FUEL TANKS, 2 IN THE RT SIDE AND 1 IN THE LT SIDE. ALL 3 FUEL TUBES WERE REPLACED.SDR CA080923002Window · cracked(CAN) WHILE IN CRUISE, CREW EXPERIENCED THE FAILURE OF THE COCKPIT LT SIDE WINDOW OUTER MAIN PLY. A CRACK SPANNED FROM THE LOWER FWD FRAME, TO THE FWD SECTION OF THE UPPER FRAME OF THE WINDSHIELD. THE ACFT HAD DEPARTED AND WAS ENROUTE SOUTHBOUND WHEN THE FAISDR CA080903006O-Ring · deteriorated(CAN) DEPARTING, EN ROUTE, NR3 HYDR SYS LO PRESS. LIGHT CAME (ON) AND QTY READ 2 PERCENT. ACFT RETURNED TO BASE. INVESTIGATION SHOWED A (BLOWN) SEAL ON PRIORITY VALVE IN THE LANDING GEAR WHEEL WELL. O-RING FOUND DETERIORATED. REPLACED O-RING, FUNCTION TESTEDSDR CA080623006Heat Tape · burned(CAN) DURING THE 96 MONTH INSPECTION ON ACFT BURNED HEAT TAPE PART NR 3043-10 AND 3043-15 WAS DISCOVERED. THIS TAPE WAS INSTALLED UNDER A DRAWING NR 34-260W011 ON THE AFT WATER SYSTEM LINES (AFT CABIN). THE SURROUNDING INSULATION AND AFFECTED PIPING WAS DEEPLYSDR CA080604013Engine · flamed out(CAN) ACFT TOOKOFF AND ENGINE FLAMED OUT AT 41000 FT, ENGINE RESTARTED AT 25 000 FT AND LANDED SAFELY. ENG MFG WAS CALLED AND OPERATOR INSTRUCTED TO DO POWER ASSURANCE. AT THE TIME ARCRAFT WAS AT IMC SOME 17NM OFF TRACK DIVERTING AROUND SOME MODERATE INTENSITSDR CA080604016Rod · out of rig(CAN) UPON GEAR RETRACTION DURING TAKEOFF A RHYTHMIC THUMPING SOUND WAS HEARD COMING FROM THE NOSE AREA. A RETURN TO FIELD WAS REQUESTED AND AN EMERGENCY DECLARED. NO EICAS MESSAGE WAS POSTED AND NOISE STOPPED WHEN GEAR SELECTED DOWN. LANDING DONE WITHOUT ANYSDR CA080225012Fitting · corrodedDURING LANDING GEAR 96 MONTH DETAIL INSPECTION HEAVY PITTING CAUSED BY CORROSION. FOUND ON MAIN LANDING GEAR MAIN FITTING TRAILING ARM ATTACHMENT INBOARD LUG BUSHING AREA AND BORE, RESULTING CONSIDEABLE AMOUNT OF MATERIAL FROM AFFECTED LOCATION, LEADING MAIN SDR CA080227003Oil System · low pressure(CAN) LOW OIL PRESS WARNING ON NR 2 ENGINE APPROX 3 MINS AFTER TAKEOFF AT 6000FT MSL ON DEPARTURE CLIMBOUT. AFTER IDENTIFICATION OF FAULT AND CONFIRMATION THAT THE FAULT WAS NOT AN INDICATION PROBLEM NR 2 ENGINE WAS SHUTDOWN AND SECURED. RETURNED SAFELY. THE SDR CA080116024Proximity Switch · misinstalled(CAN) DURING APPROACH, GEAR WAS SELECTED DOWN AND NLG INDICATED AMBER. NO GEAR DISAGREE MESSAGE POSTED. GEAR WAS RAISED NORMALLY AND MISSED APPROACH WAS EXECUTED. AT THAT MOMENT QRH ACTIONS WERE CARRIED OUT FOR GEAR MALFUNCTION. NOSE GEAR INDICATION BECAME RESDR CA070913001Adg · unwanted deploy(CAN) DURING TAKEOFF, AS SOON AS A/C LEFT GROUND ADG DEPLOYED. CREW DECIDED TO CONTINUE FLIGHT USING ADG DEPLOY FLIGHT PROCEDURES. A/C LANDED WITHOUT INCIDENT. ADG AUTODEPLOY UNIT WAS FOUND TO HAVE BEEN REPLACED A FEW HOURS BACK DUE TO FAILURE OF UNIT`S SELF SDR CA070816003Potentiometer · inoperative(CAN) ON TAKEOFF ROLL, AS THE AC WAS ACCELERATING AND PRIOR TO 80 KTS. FULL RUDDER INPUT WAS APPLIED TO MAINTAIN CENTERLINE. CENTERLINE WAS UNABLE TO BE MAINTAINED AND THE TAKEOFF WAS ABORTED. THE AIRCRAFT TAXIED WITHOUT INCIDENT BACK TO BASE. AIRCRAFT IS OPESDR 554304292007Flap System · malfunctionedFLAPS FAILED AT 13 DEGREES ON APPROACH. CREW DECLARED AN EMERGENCY AND PERFORMED AN UNEVENTFULL LANDING. MX DISPATCHED WITH BREAKOUT BOX. AFTER RESET, FLAPS OPERATIONAL CHECKS PERFORMED ON COMPLETE AND ISOLATED SYSTEMS. COULD NOT DUPLICATE ERROR. NO MX HISTOSDR CA070308003Gearbox · failed(CAN) DURING CLIMB, THE RT ENGINE WAS NOT ABLE TO ACHIEVE CLIMB POWER. THE AIRCRAFT DIVERTED TO ANOTHER AIRPORT AND LANDED UNEVENTFULLY. INVESTIGATION REVEALED THAT THE THROTTLE GEARBOX HAS AN AREA WHERE MOVEMENT OF THE THROTTLE HAS NO EFFECT ON THE MFC. THIS SDR CA061221005Hose · ruptured(CAN) UPON SHUTDOWN ON THE RAMP, CREW NOTICED A STRONG SMELL OF FUEL WHEN MAIN CABIN DOOR WAS OPENED. LT MAIN GEAR WAS SITTING IN A PUDDLE OF FUEL. FOUND ENGINE FUEL FEED AUX TANK LINE RUPTURED. (IPC 28-21-16 NR 285) (TC NR 20061221005)SDR CA070115009Fuel Line · torn(CAN) FUEL LEAK WAS FOUND FROM HOSE ASSEMBLY P/N AE7010000N0130 ON THE SECOND ENGINE RUN AFTER THAT HOSE WAS REPLACED. NOTE: THIS LINE WAS REPLACED AS REQUESTED BY MFG (DISCLOSURE LETTER), BATCH RECALL DUE TO DEFECTIVE HOSE (BATCH NR 840850). (TC NR 20070115SDR CA061222002Hose · torn(CAN) FUEL LEAK WAS FOUND FROM HOSE ASSY P/N AE7010000N0130 AFTER THE SECOND ENGINE RUN. NOTE: PRIOR RUN, LINE WAS REPLACED IAW (DISCLOSURE LETTER), BATCH RECALL DUE TO DEFECTIVE HOSE (BATCH NR 8740850) (TC NR 20061222002)SDR CA070109001Tube · blocked(CAN) AUTO SHUTOFF DID NOT OCCUR DURING PRESSURE REFUELING OPERATIONS RESULTING IN FUEL SPILL ON RAMP. OPERATOR REPORTED SIMILAR PROBLEMS SINCE TAKING DELIVERY OF NEW AIRCRAFT. IT WAS FOUND THAT A NUMBER OF LT AND RT WING TRANSFER AND BALANCING PIPES (TUBES) HSDR CA061025002Switch · inoperative(CAN) WHILE CARRYING OUT A 12 MONTH CABIN OXYGEN FUNCTIONAL TEST, FOUND THE OXYGEN CONTROL PANEL SEMI-FUNCTIONAL. THE ROTARY KNOB WOULD NOT GO TO THE "CLOSED" POSITION WITHOUT EXCESSIVE FORCE. ROTATING TO THE "OVERRIDE" POSITION FUNCTIONED PROPERLY BUT OXYGEN SDR 2006FA0000836Unknown · unknownREASON REMOVED, PRESSURIZATION CLIMBS AFTER T/O UP TO 2000 FPM. THEN CATCHES AND WORKS DURING FLIGHT. PRIOR TO INSTALLATION IN THE AIRCRAFT, THIS COMPONENT WAS INSPECTED, UNDER WO NR U22732, DATED MAR 30, 2006. COMPONENT WAS INSTALLED ON 06/09/2006. (K)SDR CA060504007Bracket · fracturedPRIOR TO A/C DEPARTURE, AND DURING A GROUND CHECK OF THE FLIGHT SPOILERS, THE LT SPOILER INDICATED IT WAS EXTENDED WHILE SURFACE WAS PHYSICALLY IN STOWED POSITION (AS COMMANDED BY SPOILER LEVER). FLIGHT SPOILER POSITION TRANSMITTER WAS INSPECTED AND FOUND TO SDR CA060403003Outflow Valve · failed(CAN) ON A FLIGHT DURING CLIMB OUT AT FL 110 AND CLEARED FOR FL150 A (CABIN ALT) EICAS MESSAGE POSTED. THE CREW OBSERVED THAT CABIN ALTITUDE WAS CLIMBING IN AN UNUSUAL HIGH RATE. WHEN CABIN ALTITUDE REACHED 10000 FEET CREW DECIDED TO CONTROL IN MANUAL MODE. NOSDR CA060228001Windshield · crackedWHILE CRUISING THE LT WINDSHIELD OUTER PLY CRACKED. THE AIRCRAFT CONTINUE INTO WHERE A NEW WINDSHIELD WAS INSTALLED.SDR 545412132005Landing Gear · obstructedON TAKEOFF, NOSE GEAR WOULD NOT RETRACT. RETURNED TO DEPARTURE POINT WITH UNEVENTFUL LANDING. MAINTENANCE FOUND LARGE TRAFFIC CONE STUCK BETWEEN THE TWO NOSE WHEELS WHICH PREVENTED RETRACTION. NO DAMAGE TO AIRCRAFT. OPERATIONAL TEST PERFORMED OF LANDING GESDR 545412022005Carbon Seal · leakingSTRONG OIL SMELL NOTICED IN COCKPIT DURING CLIMB-OUT. MAINTENANCE WAS ABLE TO VERIFY DISCREPANCY AND FOUND THE NR 1 CARBON SEAL ON THE LEFT ENGINE FAILED. REPLACED SEAL, OPS CHECK NORMAL.
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