# Canadair CL-604 - Type: Aircraft model (FAA registry) - Registry code: 1900301 - Manufacturer (registry): CANADAIR - Model: CL-604 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-jet - Seats: 21 - Weight class: 12,500 to 19,999 lb - Certification: Not type certificated - Registered aircraft: 1 - Page: https://openairdocs.org/model/canadair-cl-604 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft (1) - [N559CB](https://openairdocs.org/aircraft/N559CB): [Aircarr Holdings LLC](https://openairdocs.org/faa-owner/AIRCARR%20HOLDINGS%20LLC), [Houston, TX](https://openairdocs.org/faa-place/TX/Houston), S/N 5335 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (220, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR U5OA_N36VV](https://openairdocs.org/sdr/U5OA_N36VV), Sep 18, 2022: ENGINE. LOW PRESSURE. ON 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 - [SDR RU3A2021040600010](https://openairdocs.org/sdr/RU3A2021040600010), Apr 6, 2021: FLAP SYSTEM. FAILED. FLAPS FAILED @ 43 DEGREES ON APPROACH @ KAFW. FULL STOP LANDING AND FLAP RESET SUCCESSFUL. - [SDR RU3A20190825043](https://openairdocs.org/sdr/RU3A20190825043), Aug 25, 2019: WARNING 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 COMP - [SDR CA190814005](https://openairdocs.org/sdr/CA190814005), Aug 9, 2019: OIL 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 A - [SDR CA190806003](https://openairdocs.org/sdr/CA190806003), Aug 1, 2019: RIB. 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 TRAILIN - [SDR CA190802010](https://openairdocs.org/sdr/CA190802010), Aug 1, 2019: COMPUTER. 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 - [SDR CA200114018](https://openairdocs.org/sdr/CA200114018), Jul 29, 2019: OUTFLOW 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 IND - [SDR CA190730002](https://openairdocs.org/sdr/CA190730002), Jul 29, 2019: CABIN PRESSURE. MALFUNCTIONED. (CAN) THE OPERATOR REPORTED A LOSS OF PRESSURIZATION AFTER LEVELING OFF AT FL350 FOLLOWING DEPARTURE FROM MURTALA MUHAMMED INTERNATIONAL AIRPORT (DNMM), LAGOS, - [SDR CA191022043](https://openairdocs.org/sdr/CA191022043), Jul 15, 2019: DOOR. 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 - [SDR CA190709004](https://openairdocs.org/sdr/CA190709004), Jun 5, 2019: LIMITER. 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 INDICAT - [SDR CA190614011](https://openairdocs.org/sdr/CA190614011), Jun 3, 2019: FLT 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 - [SDR CA191216019](https://openairdocs.org/sdr/CA191216019), May 27, 2019: CIRCUIT 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 CA190527011](https://openairdocs.org/sdr/CA190527011), May 25, 2019: HOSE. 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 - [SDR CA190510006](https://openairdocs.org/sdr/CA190510006), May 10, 2019: TORQUE 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 - [SDR CA190514008](https://openairdocs.org/sdr/CA190514008), May 8, 2019: MOTOR. 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 TH - [SDR CA190506011](https://openairdocs.org/sdr/CA190506011), Apr 30, 2019: PUMP. 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# 2019 - [SDR CA190430014](https://openairdocs.org/sdr/CA190430014), Apr 25, 2019: PDU. 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 - [SDR CA190410009](https://openairdocs.org/sdr/CA190410009), Apr 8, 2019: FLAP 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 AIRPOR - [SDR CA190402010](https://openairdocs.org/sdr/CA190402010), Mar 31, 2019: PITOT 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 PR - [SDR CA190401013](https://openairdocs.org/sdr/CA190401013), Mar 29, 2019: MOTOR. 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 NE - [SDR CA190820015](https://openairdocs.org/sdr/CA190820015), Mar 13, 2019: SERVO 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 DEF - [SDR CA191121013](https://openairdocs.org/sdr/CA191121013), Mar 7, 2019: SWITCH. 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 & - [SDR CA191121008](https://openairdocs.org/sdr/CA191121008), Feb 28, 2019: SWITCH. 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 - [SDR CA190913009](https://openairdocs.org/sdr/CA190913009), Feb 6, 2019: FLEX LINE. CRACKED. (CAN) CUSTOMER FOUND THAT ALL PSU PASSENGER OXYGEN MASK STOWAGE BOX FLEXIBLE HOSE LEAKING DURING MAINTENANCE TASKS. - [SDR CA190913006](https://openairdocs.org/sdr/CA190913006), Feb 6, 2019: FLEX 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 DE - [SDR CA190314018](https://openairdocs.org/sdr/CA190314018), Jan 14, 2019: ADC. 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 - [SDR CA191203014](https://openairdocs.org/sdr/CA191203014), Jan 14, 2019: TIRE. 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 AFTE - [SDR RU3A201807232031](https://openairdocs.org/sdr/RU3A201807232031), Jul 22, 2018: WARNING SYSTEM. ACTIVATED. RIGHT 14TH STAGE DUCT FAIL LIGHT ILLUMINATED IN FLIGHT. - [SDR CA160302012](https://openairdocs.org/sdr/CA160302012), Mar 2, 2016: FITTING. 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 - [SDR CA160225002](https://openairdocs.org/sdr/CA160225002), Feb 25, 2016: CDU. 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 - - [SDR CA160127002](https://openairdocs.org/sdr/CA160127002), Jan 24, 2016: STRUT. LEAKING. (CAN) AIRCRAFT ENCOUNTERED RETRACTION PROBLEMS (NLG TRANSIT LIGHT WOULD NOT EXTINGUISHED) AND HAD TO COMPLETE ITS FLIGHT WITH GEAR DOWN AND CONFIRMED LOCKED. FO - [SDR CA160111007](https://openairdocs.org/sdr/CA160111007), Jan 7, 2016: OUTLET. 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 CA151203011](https://openairdocs.org/sdr/CA151203011), Nov 29, 2015: FIRE 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 - [SDR CA151203017](https://openairdocs.org/sdr/CA151203017), Nov 24, 2015: FIRE 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. - [SDR CA151118008](https://openairdocs.org/sdr/CA151118008), Nov 13, 2015: BRACKET. CHAFED. (CAN) NLG CHANNEL 600-33045 CHAFED BY RH EDGE OF DOWN LOCK SWITCH BRACKET 20046-101. - [SDR CA150925017](https://openairdocs.org/sdr/CA150925017), Sep 23, 2015: WHEEL. MISSING. (CAN) DOM REPORTED THAT CREW NOTICED THE RT OUTBOARD WHEEL ASSEMBLY MISSING UPON LANDING. - [SDR CA150828010](https://openairdocs.org/sdr/CA150828010), Aug 10, 2015: RIBBON HEATER. OVERHEATED. (CAN) DURING AN INSPECTION, THE OPERATOR NOTICED THAT THE INSULATION INSTALLED OVER THE HEATED SILICONE GALLEY DRAIN HOSE (INSTALLED BY MODIFICATION DATA SUMMAR - [SDR CA150806004](https://openairdocs.org/sdr/CA150806004), Aug 4, 2015: CDU. 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 CA150703005](https://openairdocs.org/sdr/CA150703005), Jun 30, 2015: STAB 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 - [SDR CA150611003](https://openairdocs.org/sdr/CA150611003), Jun 11, 2015: CONVERTER. FAILED. (CAN) AOA SIGNAL CONVERTER INFLIGHT POWER INTERRUPTIONS ABNORMAL SIGNAL BEHAVIOR WAS OBSERVED WHEN ANALYZING FLIGHT TEST DATA FROM INSTRUMENTATION. ABNORMAL AOA - [SDR CA150527002](https://openairdocs.org/sdr/CA150527002), May 27, 2015: BUSHING. MIGRATED. (CAN) LEFT & RIGHT MAIN GEAR AFT MOUNTING BUSHINGS MIGRATING. DISCOVERED DURING SCHEDULED INSPECTION. MANUFACTURER CORRESPONDENCE HAS INDICATED THAT NO MIGRATIO - [SDR CA150327005](https://openairdocs.org/sdr/CA150327005), Mar 11, 2015: PANEL. 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 CA150304006](https://openairdocs.org/sdr/CA150304006), Mar 2, 2015: FLEX 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 - [SDR CA150217002](https://openairdocs.org/sdr/CA150217002), Feb 14, 2015: CONNECTOR. 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 - [SDR CA150128006](https://openairdocs.org/sdr/CA150128006), Jan 27, 2015: ELEMENT. 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 I - [SDR CA150115003](https://openairdocs.org/sdr/CA150115003), Jan 15, 2015: MICROWAVE 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 - [SDR CA150113028](https://openairdocs.org/sdr/CA150113028), Jan 11, 2015: MANIFOLD. 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 P - [SDR CA150106006](https://openairdocs.org/sdr/CA150106006), Jan 6, 2015: WIRE. 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 CRIM - [SDR CA150106005](https://openairdocs.org/sdr/CA150106005), Jan 6, 2015: DRAIN 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 - [SDR CA141219008](https://openairdocs.org/sdr/CA141219008), Dec 16, 2014: WINDSHIELD. 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 DE All 220: https://openairdocs.org/model/canadair-cl-604/reports.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Bombardier CL-604](https://openairdocs.org/model/bombardier-cl-604): 0 registered aircraft, registry code 1390017 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.