Canadair 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 U5OA_N36VVEngine · low pressureON A PART 91 TRIP SCHEDULED FROM KAUS TO KVNY CREW NOTICED THE RH ENG OIL PRESS FLUCTUATING BETWEEN 31 AND 39 PSI AT CRUISE FL340, AS FLIGHT PROGRESSED THE OIL PRESS CONTINUED TO DROP, WHEN PRESS READING DROPPED TO 25 PSI THE CAS MSG R LOW OIL PRESS ILLUMINATESDR RU3A2021040600010Flap System · failedFLAPS FAILED @ 43 DEGREES ON APPROACH @ KAFW. FULL STOP LANDING AND FLAP RESET SUCCESSFUL.SDR RU3A20190825043Warning System · false activation"WOW OUTPUT" CAUTION & "GND SPLR NOT ARMED" ADVISORY IN FLIGHT. WOW OUTPUT EXTINGUISHED IN 5 MIN THEN SPLR MSG STAYED ON UNTIL ENGINE SHUTDOWN. MAINTENANCE COMPLIED WITH GROUND CHECKS, SPOILERS, NO DEFECT WAS FOUND. NO FAULT INDICATED AT POWER UP. WILL CONTINUSDR CA190814005Oil System · low pressure(CAN) AIRCRAFT HAD AN ENGINE SHUT DOWN IN FLIGHT, DECLARED A PAN PAN AND DIVERTED INITIAL INFORMATION IS THAT DURING FLIGHT OIL PRESSURE DROPPED ON ONE ENGINE AND AFTER THEY THROTTLED BACK IT STABILIZED ABIT BUT THEN CONTINUED TO DROP. CREW SHUT DOWN THE ENGINSDR CA190806003Rib · cracked(CAN) L/H WING @ WS112.3, CANTED RIB, DRAWING #600-10332, IPC 57-51-01, P8 (ITEM 75) FOUND CRACKED, 1` LONG WITH SPIDER CRACKING AND 2 RIVETS SHEARED AT TRAILING EDGE GUSSET , IPC 57-51-001 (ITEM 155). (TC# 20190806003)SDR CA190802010Computer · malfunctioned(CAN) STALL ALT COMP LIGHT AND STALL FAIL ARE ANNUNCIATIED. FIELD SERVICE REPRESENTATIVE INPUT AUG 1, 2019: FAULT CLEARED THE NEXT MORNING. ADVISED CUSTOMER TO REPLACE THE STALL COMPUTER. (TC# 20190802010)SDR CA200114018Outflow Valve · malfunctioned(CAN) THE PRESSURISATION SYSTEM PRE-PRESSURISED FOR TAKEOFF, POSITIVE DIFFERENTIAL VALUES WERE OBSERVED IN THE CLIMB WITH BOTH CABIN ALTITUDE AND CABIN RATE INDICATING 0 AS OBSERVED UP TILL ABOUT 5,000 FT AFTER WHICH THE CABIN ALTITUDE AND RATE VALUES STARTED SDR CA190730002Cabin Pressure · malfunctioned(CAN) THE OPERATOR REPORTED A LOSS OF PRESSURIZATION AFTER LEVELING OFF AT FL350 FOLLOWING DEPARTURE FROM MURTALA MUHAMMED INTERNATIONAL AIRPORT (DNMM), LAGOS, NIGERIA. THE AIRCRAFT PRE-PRESSURIZED, AS IT SHOULD, PRIOR TO TAKEOFF. POSITIVE DIFFERENTIAL VALUESDR CA191022043Door · unknown(CAN) FAILED TO PRESSURIZE AFTER TAKE-OFF IN AUTO & MANUAL. DURING DESCENT AT 7000 FT THE PASSENGER DOOR HANDLE CAS MESSAGE ILLUMINATED CREW CONFIRMED THERE WAS NOISE FROM THE DOOR INITIAL REPORT WITHOUT REMOVING ANY PANELS "I HAVE JUST BEEN TO TAKE A LOOK SDR CA190709004Limiter · damaged(CAN) CREW REPORTED THAT WHEN DEPLOYING SPOILERS THEY DEPLOYED ASYMMETRICALLY AND THE AIRCRAFT ROLLED TO THE RIGHT. THE CREW NOTED THAT ON THE EICAS THE INDICATION SHOWED THAT THE RH SPOILER HAD EXTENDED FURTHER THAN THE LEFT. ENGINEERS REVISITED THE AIRCRAFTSDR CA190614011Flt Controls · binding(CAN) THE CREW NOTED THE FLIGHT CONTROLS WERE EXTREMELY STIFF ABOUT PITCH AND ROLL AXIS WITH OR WITHOUT AIR LOAD. THE AIRCRAFT HYDRAULIC PRESSURE SHOWED NORMAL IN ALL THREE SYSTEMS. UPON LANDING THE FLIGHT CREW VERIFIED THE PROBLEM PERSISTED WITHOUT AIR LOADSDR CA191216019Circuit Card · faulted(CAN) YAW OSCILLATION PERCEIVED BY FLIGHT CREW. YD DISENGAGED WHICH RESOLVED THE OSCILLATION CONDITION. FCC CARD FOUND CAUSING THE ISSUE. (TC# 20191216019)SDR CA190527011Hose · leaking(CAN) APPROX 100PSI O2 LEAK OVERNIGHT. LOCATED LEAK AT BASE OF HOSE FITTING UNDER CO-PILOTS SIDE PANEL. FURTHER INVESTIGATION ALSO REVEALED THE HOSE WAS BULGING AT SAME LOCATION. ATTACHMENT POINT FOR THIS LINE IS TO THE `IN` PORT FITTING OF THE PASSENGER OXYGESDR CA190510006Torque Tube · damaged(CAN) QUALITY ESCAPE DISCLOSURE LETTER: MISSING CAD PLATING ON THE INSIDE BORE FOR PART NUMBER 600-31944-5. PART SHOULD BE MANUFACTURED AS PER DRAWING 600-31944-5 REV BB, EDL REV 01. AFFECTS CHALLENGER 650 AIRCRAFT SERIAL NUMBERS 6117 TO 6147. BOMBARDIER INTESDR CA190514008Motor · failed(CAN) DURING PRE-FLIGHT, TECHNICIAN NOTICED THE #2 FLAP MOTOR C/B (CB2-B5) TRIPPED. PUSH C/B BACK IN AND SELECTED FLAPS TO 20 DEG. ONCE FLAPS STARTED TO MOVE THE C/B TRIPPED AGAIN. FLAP MOTOR REPLACED. (TC# 20190514008)SDR CA190506011Pump · failed(CAN) AIRCRAFT HAD AN INFLIGHT SYSTEM 3 HYDRAULIC PRESSURE LOW INDICATION IN FLIGHT AND DIVERTED FOR LANDING CREW INFORMED THAT CB HYD 3 A WAS POPPED. (TC# 20190506011)SDR CA190430014Pdu · overheated(CAN) FLAP MOTOR 1 AND 2 OVERHEAT AT THE SAME TIME. CARRIED OUT OPS TESTS FLAPS AND CB PULLED OUT ONE BY ONE OF THE FLAP MOTORS. AND OPS CHECK ON ONE MOTOR EACH TIME. NO OVERHEAT OCCURRED. ALL SATISFACTORY DUE TO BOTH FLAP MOTORS OVERHEAT AT THE SAME TIME IT SDR CA190410009Flap System · failed(CAN) FLAP FAIL ON DESCENT , FLAPS SELECTED TO 20 FROM ZERO. FLAPS FAILED WITHOUT MOVING. PILOTS DECLARED AN EMERGENCY. DIVERTED FOR LANDING AT ALTERNATE AIRPORT. UNEVENTFUL LANDING. TECHNICIANS TOWED AIRCRAFT INTO HANGAR TO TROUBLESHOOT. ON POWER UP WITH GROUSDR CA190402010Pitot System · contaminated(CAN) AIRPLANE DIVERTED FOR UNSCHEDULED LANDING WITH FOLLOWING ISSUE: AT FLIGHT LEVEL CRUISE AT FL370 WITH MODERATE RAIN AND BUMPINESS THE AIRSPEED OF THE LH PRIMARY FLIGHT DISPLAY (PFD) STARTED GRADUALLY DECREASING,LH 200 KTS AND RH 280 KTS. MACH TRIM DISENGASDR CA190401013Motor · overheated(CAN) FLAP MOTOR OVERHEAT CAS MSG POSTED. AIRCRAFT HAD TO LAND WITHOUT FLAP EXTENDED AT DIFFERENT AIRPORT INSTEAD OF DESTINATION AIRPORT DUE TO LONGER RUNWAY NEEDED. CIRCUIT BREAKER OF MOTOR TRIPPED DURING THE FLIGHT AS WELL.SDR CA190820015Servo Valve · defective(CAN) AC LANDED AT AIRPORT AND AFTER TOUCH DOWN, AT AROUND 80-60 KTS, NOSE WHEEL STEERING (NWS) FAILED. AC STOPPED ON RUNWAY AND NOSE WHEEL WAS FOUND 90 DEG DEFLECTED. MAINTENANCE MANAGED TO GET THE AC OFF RUNWAY AND INTO FACILITY. BOMBARDIER, CUSTOMER RESPONSSDR CA191121013Switch · failed(CAN) DURING CRUISE AN (AMBER) "STAB TRIM" & (AMBER) "MACH TRIM" CAS MESSAGES POSTED ON EICAS & AUTOPILOT KICKED OFF LINE. CREW WAS ABLE TO CLEAR CAS MESSAGE & RE-ENGAGE THE AUTOPILOT AFTER MESSING AROUND WITH THE STAB TRIM DISCONNECT SWITCHES ON THE PILOT`S &SDR CA191121008Switch · failed(CAN) CUSTOMER REPORTING AIRCRAFT DEPARTED AND THE CREW COULD NOT GET THE STAB TRIM TO ENGAGE. CREW WILL DIVERT FOR LANDING. BOTH PILOT AND CO-PILOT PITCH TRIM SWITCHES REPLACED.SDR CA190913009Flex Line · cracked(CAN) CUSTOMER FOUND THAT ALL PSU PASSENGER OXYGEN MASK STOWAGE BOX FLEXIBLE HOSE LEAKING DURING MAINTENANCE TASKS.SDR CA190913006Flex Line · cracked(CAN) DURING A 36 MONTH INSPECTION ON CL605 THE FOLLOWING DEFECT WAS FOUND ON THE PASSENGER EMERGENCY OXYGEN SYSTEM. (PASSENGER EMERGENCY OXYGEN MASKS FAILED DEPLOYMENT AS REQUIRED) 1). 35-00-00-204, AMM TASK 35-20-00-710-801 OPERATIONAL CHECK OF THE PASSENGSDR CA190314018Adc · malfunctioned(CAN) OPERATOR REPORTED HAVING TWO UNRELIABLE AIRSPEED EVENTS ON THE SAME AIRCRAFT WITHIN TWO WEEKS, IN DECEMBER 2018 AND JANUARY 2019. THE FIRST EVENT OCCURRED ON DECEMBER 28TH, 2018, EN ROUTE PRIOR TO TOP OF DESCENT AT FL400. THE CREW RECEIVED AN EFIS COMP MSDR CA191203014Tire · failed(CAN) AFTER DE-ICE, THEY INITIATE TAXIING IN NORMAL CONDITION. DURING TAXIING THEY NOTICED AN ANTI-SKID INBD CAS MSG AND DISAPPEAR AFTER 2 SEC. ALL TAXIING AFTER WAS NORMAL. THEY DO A ROLLING T/O WITHOUT PROBLEM NOTICED AT POWER UP AND AT V1, THEY START TO FESDR RU3A201807232031Warning System · activatedRIGHT 14TH STAGE DUCT FAIL LIGHT ILLUMINATED IN FLIGHT.SDR CA160302012Fitting · vibration(CAN) SHANKING CONDITION ON DIVAN FLOOR FITTING BETWEEN FS449 AND FS525, BL27 AND BL35.40, RH, WL73.5. FOR DIVAN FRAME INSTALLATION (604DX2529032). QUANTITY 10 DIVAN FLOOR FITTINGS (2523.500.02-4295/-4297/-4299/-4301/-4303/-4307) RECEIVED NOT AS PER DRAWING.SDR CA160225002Cdu · unknown(CAN) CDU-6200/RTA-4114 NON-COMPLIANCE TO DO-160() SECTION 22, B3K33 Ï¿½PIN INJECTION LIGHTNINGÏ¿½ DUE TO TRIMMED RESISTOR WHAT IS THE POTENTIAL SAFETY IMPACT - LOSS OF ALL PRIMARY CDU RADIO TUNING CONTROL. - LOSS OF FMS CONTROL, FMS WILL CONTINUE TO FLY CURRSDR CA160127002Strut · leaking(CAN) AIRCRAFT ENCOUNTERED RETRACTION PROBLEMS (NLG TRANSIT LIGHT WOULD NOT EXTINGUISHED) AND HAD TO COMPLETE ITS FLIGHT WITH GEAR DOWN AND CONFIRMED LOCKED. FOLLOWING SUCCESSFUL LANDING AND PRELIMINARY INVESTIGATION THE NLG ASSY WAS FOUND DEFLATED AND COULD SDR CA160111007Outlet · arced(CAN) THE CABIN OUTLET AT THE LT FORWARD SEAT WHEN THE TABLET CHARGER WAS PLUGGED IN THE OUTLET, CHARGER HAD ELECTRICAL ARCHING AND SMOKE.SDR CA151203011Fire Warning · false activation(CAN) DURING CLIMBOUT, THE RT ENGINE FIRE WARNING TRIPPED OFF WITH RED, RT ENGINE FIRE, POSTED. CREW SHUTDOWN THE RT ENGINE AND WARNING WENT OUT. ACFT DECLARED EMERGENCY AND DIVERTED, LANDING WITHOUT INCIDENT. CREW DID NOT NOTICE ANY EVIDENCE OF A FIRE FROMSDR CA151203017Fire Loop · failed(CAN) IT WAS REPORTED TO THE CUSTOMER RESPONSE CENTER (CRC) THAT THE CREW OBSERVED A FIRE INDICATION FOR THE RIGHT-HAND ENGINE AS THE AIRCRAFT WAS CLIMBING OUT. THE CREW FOLLOWED THE CHECKLIST. THE CREW THEN SHUT DOWN THE ENGINE AND THE FIRE INDICATION WENT OUSDR CA151118008Bracket · chafed(CAN) NLG CHANNEL 600-33045 CHAFED BY RH EDGE OF DOWN LOCK SWITCH BRACKET 20046-101.SDR CA150925017Wheel · missing(CAN) DOM REPORTED THAT CREW NOTICED THE RT OUTBOARD WHEEL ASSEMBLY MISSING UPON LANDING.SDR CA150828010Ribbon Heater · overheated(CAN) DURING AN INSPECTION, THE OPERATOR NOTICED THAT THE INSULATION INSTALLED OVER THE HEATED SILICONE GALLEY DRAIN HOSE (INSTALLED BY MODIFICATION DATA SUMMARY D48100) SHOWED SIGNS OF OVERHEATING. AFTER REMOVING THE INSULATION, IT WAS DISCOVERED THAT THE RIBSDR CA150806004Cdu · overheated(CAN) CREW REPORT THAT SMOKE CAME FROM FMS CDU NR 2 WHILE ON THE RAMP. CIRCUIT BREAKER DID NOT TRIP. CDU HAS BEEN ELECTRICALLY DISCONNECTED AND MELED.SDR CA150703005Stab System · failed(CAN) AFTER DEPARTURE, HAD THE STAB TRIM AMBER CAS MESSAGE POST ON THE EICAS. CONTINUOUSLY RE-EVALUATED THE SITUATION AND EXPLORED SOME POTENTIAL OPTIONS. FLEW AT A REDUCED ALTITUDE AND AIRSPEED AND REMAINED CLEAR OF RVSM AIRSPACE. MAINTENANCE REPORTED FAUSDR CA150611003Converter · failed(CAN) AOA SIGNAL CONVERTER INFLIGHT POWER INTERRUPTIONS ABNORMAL SIGNAL BEHAVIOR WAS OBSERVED WHEN ANALYZING FLIGHT TEST DATA FROM INSTRUMENTATION. ABNORMAL AOA SIGNALS ARE SEEN AS SPIKES IN THE AOA VALUE, UP TO 60 DEG & OR DOWN TO -15DEG. THIS BEHAVIOR IS CSDR CA150527002Bushing · migrated(CAN) LEFT & RIGHT MAIN GEAR AFT MOUNTING BUSHINGS MIGRATING. DISCOVERED DURING SCHEDULED INSPECTION. MANUFACTURER CORRESPONDENCE HAS INDICATED THAT NO MIGRATION IS ALLOWED.SDR CA150327005Panel · corroded(CAN) MULTIPLE PANELS IN ACFT WERE FOUND CORRODED. CORROSION REMOVED, SOME OF THE CORROSION HAS GONE ENTIRELY THROUGH THE SURFACE OF THE HONEYCOMB PANEL.SDR CA150304006Flex Drive · cracked(CAN) FOUND DURING INSPECTION, 4 FLEX SHAFT ASSEMBLIES CRACKED ON THE SWAGED FITTING ENDS ON 2 THRUST REVERSERS ON OUR ACFT. 2 WERE FOUND ON THE LT ENGINE AND 2 ON THE RT ENGINE. 3 WERE PN 121754-2 AND ONE 121754-3. LOOKING AT THE FAILED PARTS IT APPEARS THSDR CA150217002Connector · melted(CAN) THE LAVATORY VANITY MIRROR HAS 3 LIGHTING ASSEMBLIES POWERED BY SEPARATE BALLASTS, PRECISION WINDING, PN 6900054-003. THEY ARE MOUNTED IN PROXIMITY OF THE HAND SOAP DISPENSER RESERVOIR. AN OVERFLOW OF THE SOAP DISPENSER RESERVOIR TOOK PLACE EITHER DUE SDR CA150128006Element · damaged(CAN) WE COMPLETED THE PREFLIGHT AND DEPARTED AS SCHEDULED. EVERYTHING WAS NORMAL, UNTIL AROUND 1530Z, ABOUT 10-15 MILES AWAY FROM CALLS (A FIX ON THE ILS 11L IN TUS), WE GOT THE RED L 14TH DUCT, CAS MESSAGE, AND THE OVERHEAD RED 14TH STAGE DUCT FAIL LIGHT. WESDR CA150115003Microwave Oven · malfunctioned(CAN) WHILE IN CRUISE FLIGHT AT 40,000, ONE OF THE PASSENGERS WAS USING THE GALLEY MICROWAVE OVEN. WHILE IN USE, THE MICROWAVE P/N 400-2577-01 STARTED SPARKING AND SMOKING. THE CB TRIPPED STOPPING THIS NOTED ACTION. CB WAS LEFT OUT DURING THE REMAINDER OF THE SDR CA150113028Manifold · failed(CAN) CREW REPORTED ON TAXI CHECK OUT OF VANCOUVER GROUND SPOILERS WOULD NOT RETRACT - TROUBLESHOOTING CARRIED OUT USING CL605 WM 27-61-00 AND ROCKWELLCOLLINS PSEU SENSOR DISCRETE DATA LABEL 271-274, LABEL 274 BIT 28 FOUND AT 0 INDICATING NO RETURN HYDRAULIC PSDR CA150106006Wire · misinstalled(CAN) BAD CRIMPING ON THE FUEL TRANSFER SHUTOFF VALVES WIRES ON THE WIRES THAT COME FROM FUEL TRANSFER SHUTOFF VALVE V3QA, V4QA & V5QA , PRODUCTION DID NOT CRIMP CONTACTS M39029/58-363 (12X) AND LUGS B0808005-006N (3X) AS PER BOMBARDIER STANDARDS. WIRES 24 AWGSDR CA150106005Drain Line · misrouted(CAN) IN THE WHEEL-WELL AREA, THE FUEL DRAIN TUBES WERE MISLOCATED. THEY WERE INVERTED AT THE ATTACHMENT ON THE TWO BUTTERFLY CLAMPS. THIS DISCREPANCY CAUSES A LOW CLEARANCE OR CONTACT BETWEEN THE TUBES AND THE AILERON QUADRANT LEVER DURING THE TRAVELLING OF SDR CA141219008Windshield · cracked(CAN) LEFT WINDSHIELD SURFACE FACE PLY CRACKED IN CRUISE. AS A RESULT RAPID DELAMINATION OCCURRED, WHICH LEAD TO THE BREAKUP OF THE FACE PLY. FACE PLY PIECES DEPARTED THE WINDSHIELD MAKING CONTACT WITH THE LEADING EDGE OF THE VERTICAL & HORIZONTAL STABILIZER
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