# Service difficulty reports: Canadair CL-604

A list on [Canadair CL-604](https://openairdocs.org/model/canadair-cl-604.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 5 · 220 reports

- [SDR U5OA_N36VV](https://openairdocs.org/sdr/U5OA_N36VV.md): Engine · low pressure · Sep 18, 2022 · N36VV · Cndair CL604 · Engine Oil Indicating System
  > 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 PRESS CONTINUED TO DROP, WHEN PRESS READING DROPPED TO 25 PSI THE CAS MSG R LOW OIL PRESS ILLUMINATE
- [SDR RU3A2021040600010](https://openairdocs.org/sdr/RU3A2021040600010.md): Flap System · failed · Apr 6, 2021 · N88 · Cndair CL604 · Trailing Edge Flap Control System
  > FLAPS FAILED @ 43 DEGREES ON APPROACH @ KAFW. FULL STOP LANDING AND FLAP RESET SUCCESSFUL.
- [SDR RU3A20190825043](https://openairdocs.org/sdr/RU3A20190825043.md): Warning System · false activation · Aug 25, 2019 · N88 · Cndair CL604 · Landing Gear Position and Warning
  > "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 CONTINU
- [SDR CA190814005](https://openairdocs.org/sdr/CA190814005.md): Oil System · low pressure · Aug 9, 2019 · Cndair CL604 · Engine Oil 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 ENGIN
- [SDR CA190806003](https://openairdocs.org/sdr/CA190806003.md): Rib · cracked · Aug 1, 2019 · Cndair CL604 · Wing, Rib/Bulkhead
  > (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 CA190802010](https://openairdocs.org/sdr/CA190802010.md): Computer · malfunctioned · Aug 1, 2019 · Cndair CL604 · Stall Warning System
  > (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 CA200114018](https://openairdocs.org/sdr/CA200114018.md): Outflow Valve · malfunctioned · Jul 29, 2019 · Cndair CL604 · Pressure Regulator/Outflow Valve
  > (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 CA190730002](https://openairdocs.org/sdr/CA190730002.md): Cabin Pressure · malfunctioned · Jul 29, 2019 · Cndair CL604 · Cabin Pressure Control System
  > (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 VALUE
- [SDR CA191022043](https://openairdocs.org/sdr/CA191022043.md): Door · unknown · Jul 15, 2019 · Cndair CL604 · Passenger/Crew Doors
  > (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 CA190709004](https://openairdocs.org/sdr/CA190709004.md): Limiter · damaged · Jun 5, 2019 · Cndair CL604 · Spoilers
  > (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 AIRCRAFT
- [SDR CA190614011](https://openairdocs.org/sdr/CA190614011.md): Flt Controls · binding · Jun 3, 2019 · Cndair CL604 · Flight Control System
  > (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 LOAD
- [SDR CA191216019](https://openairdocs.org/sdr/CA191216019.md): Circuit Card · faulted · May 27, 2019 · Cndair CL604 · Autopilot System
  > (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.md): Hose · leaking · May 25, 2019 · Cndair CL604 · Passenger Oxygen System
  > (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 OXYGE
- [SDR CA190510006](https://openairdocs.org/sdr/CA190510006.md): Torque Tube · damaged · May 10, 2019 · Cndair CL604 · Passenger/Crew Doors
  > (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 INTE
- [SDR CA190514008](https://openairdocs.org/sdr/CA190514008.md): Motor · failed · May 8, 2019 · Cndair CL604 · Trailing Edge Flap Actuator
  > (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 CA190506011](https://openairdocs.org/sdr/CA190506011.md): Pump · failed · Apr 30, 2019 · Cndair CL604 · Hydraulic Pump (Electric/Engine), Main
  > (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 CA190430014](https://openairdocs.org/sdr/CA190430014.md): Pdu · overheated · Apr 25, 2019 · Cndair CL604 · Trailing Edge Flap Control System
  > (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 CA190410009](https://openairdocs.org/sdr/CA190410009.md): Flap System · failed · Apr 8, 2019 · Cndair CL604 · Trailing Edge Flap Control System
  > (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 GROU
- [SDR CA190402010](https://openairdocs.org/sdr/CA190402010.md): Pitot System · contaminated · Mar 31, 2019 · Cndair CL604 · Pitot/Static System
  > (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 DISENGA
- [SDR CA190401013](https://openairdocs.org/sdr/CA190401013.md): Motor · overheated · Mar 29, 2019 · Cndair CL604 · Trailing Edge Flap Control System
  > (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 CA190820015](https://openairdocs.org/sdr/CA190820015.md): Servo Valve · defective · Mar 13, 2019 · Cndair CL604 · Landing Gear Steering System
  > (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 RESPONS
- [SDR CA191121013](https://openairdocs.org/sdr/CA191121013.md): Switch · failed · Mar 7, 2019 · Cndair CL604 · Stabilizer Control System
  > (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 CA191121008](https://openairdocs.org/sdr/CA191121008.md): Switch · failed · Feb 28, 2019 · Cndair CL604 · Stabilizer Control System
  > (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 CA190913009](https://openairdocs.org/sdr/CA190913009.md): Flex Line · cracked · Feb 6, 2019 · Cndair CL604 · Passenger Oxygen System
  > (CAN) CUSTOMER FOUND THAT ALL PSU PASSENGER OXYGEN MASK STOWAGE BOX FLEXIBLE HOSE LEAKING DURING MAINTENANCE TASKS.
- [SDR CA190913006](https://openairdocs.org/sdr/CA190913006.md): Flex Line · cracked · Feb 6, 2019 · Cndair CL604 · Passenger Oxygen System
  > (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 PASSENG
- [SDR CA190314018](https://openairdocs.org/sdr/CA190314018.md): Adc · malfunctioned · Jan 14, 2019 · Cndair CL604 · Airspeed/Mach Indicator
  > (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 M
- [SDR CA191203014](https://openairdocs.org/sdr/CA191203014.md): Tire · failed · Jan 14, 2019 · Cndair CL604 · Tire
  > (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 FE
- [SDR RU3A201807232031](https://openairdocs.org/sdr/RU3A201807232031.md): Warning System · activated · Jul 22, 2018 · N88 · Cndair CL604 · Bleed Air Indicating System
  > RIGHT 14TH STAGE DUCT FAIL LIGHT ILLUMINATED IN FLIGHT.
- [SDR CA160302012](https://openairdocs.org/sdr/CA160302012.md): Fitting · vibration · Mar 2, 2016 · Cndair CL604 · Fuselage Main, Attach Fittings
  > (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 CA160225002](https://openairdocs.org/sdr/CA160225002.md): Cdu · unknown · Feb 25, 2016 · Cndair CL604 · Navigation System
  > (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 CURR
- [SDR CA160127002](https://openairdocs.org/sdr/CA160127002.md): Strut · leaking · Jan 24, 2016 · Cndair CL604 · Nose/Tail Landing Gear Strut/Axle
  > (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 CA160111007](https://openairdocs.org/sdr/CA160111007.md): Outlet · arced · Jan 7, 2016 · Cndair CL604 · Passenger Compartment Equipment
  > (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.md): Fire Warning · false activation · Nov 29, 2015 · Cndair CL604 · Fire Detection
  > (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 FROM
- [SDR CA151203017](https://openairdocs.org/sdr/CA151203017.md): Fire Loop · failed · Nov 24, 2015 · Cndair CL604 · Fire Detection
  > (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 OU
- [SDR CA151118008](https://openairdocs.org/sdr/CA151118008.md): Bracket · chafed · Nov 13, 2015 · Cndair CL604 · Main Landing Gear
  > (CAN) NLG CHANNEL 600-33045 CHAFED BY RH EDGE OF DOWN LOCK SWITCH BRACKET 20046-101.
- [SDR CA150925017](https://openairdocs.org/sdr/CA150925017.md): Wheel · missing · Sep 23, 2015 · Cndair CL604 · Wheel/Ski/Float
  > (CAN) DOM REPORTED THAT CREW NOTICED THE RT OUTBOARD WHEEL ASSEMBLY MISSING UPON LANDING.
- [SDR CA150828010](https://openairdocs.org/sdr/CA150828010.md): Ribbon Heater · overheated · Aug 10, 2015 · Cndair CL604 · Buffet/Galleys
  > (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 RIB
- [SDR CA150806004](https://openairdocs.org/sdr/CA150806004.md): Cdu · overheated · Aug 4, 2015 · Cndair CL604 · Central Display
  > (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.md): Stab System · failed · Jun 30, 2015 · Cndair CL604 · Stabilizer Control System
  > (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 FAU
- [SDR CA150611003](https://openairdocs.org/sdr/CA150611003.md): Converter · failed · Jun 11, 2015 · Cndair CL604 · Stall Warning System
  > (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 C
- [SDR CA150527002](https://openairdocs.org/sdr/CA150527002.md): Bushing · migrated · May 27, 2015 · Cndair CL604 · Fuselage, Landing Gear Attach Fittings
  > (CAN) LEFT & RIGHT MAIN GEAR AFT MOUNTING BUSHINGS MIGRATING. DISCOVERED DURING SCHEDULED INSPECTION. MANUFACTURER CORRESPONDENCE HAS INDICATED THAT NO MIGRATION IS ALLOWED.
- [SDR CA150327005](https://openairdocs.org/sdr/CA150327005.md): Panel · corroded · Mar 11, 2015 · Cndair CL604 · Fuselage Miscellaneous Structure
  > (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.md): Flex Drive · cracked · Mar 2, 2015 · Cndair CL604 · Engine Thrust Reverser
  > (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 TH
- [SDR CA150217002](https://openairdocs.org/sdr/CA150217002.md): Connector · melted · Feb 14, 2015 · Cndair CL604 · Light System Wiring
  > (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 CA150128006](https://openairdocs.org/sdr/CA150128006.md): Element · damaged · Jan 27, 2015 · Cndair CL604 · Overheat Detection
  > (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. WE
- [SDR CA150115003](https://openairdocs.org/sdr/CA150115003.md): Microwave Oven · malfunctioned · Jan 15, 2015 · Cndair CL604 · Buffet/Galleys
  > (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 CA150113028](https://openairdocs.org/sdr/CA150113028.md): Manifold · failed · Jan 11, 2015 · Cndair CL604 · Drag Control Actuator
  > (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 P
- [SDR CA150106006](https://openairdocs.org/sdr/CA150106006.md): Wire · misinstalled · Jan 6, 2015 · Cndair CL604 · Fuel System Wiring
  > (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 AWG
- [SDR CA150106005](https://openairdocs.org/sdr/CA150106005.md): Drain Line · misrouted · Jan 6, 2015 · Cndair CL604 · Wing Miscellaneous Structure
  > (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 CA141219008](https://openairdocs.org/sdr/CA141219008.md): Windshield · cracked · Dec 16, 2014 · Cndair CL604 · Flight Compartment Windows
  > (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

Next page: https://openairdocs.org/model/canadair-cl-604/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/model/canadair-cl-604/reports

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