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The MASTER CAUTION pushlight works in conjunction with the "amber" CAS messages. The MASTER WARNING pushlight works in conjunction with the "redr" CAS messages. The MASTER WARNING pushlight works in conjunction with the "redr" CAS messages. PFD controller - Click for more information Reversionary Panel - click for more information Reversionary Panel - Click for more information Displays the APU amperage Displays the cabin rate-of-climb/descent based on feet-per-minute. It is a direct reading instrument that requires no electrical power. The cabin altitude/differential pressure indicator requires no electrical power to function. The outer scale provides a visual indication of cabin altitude in thousands of feet. The inner scale provides differential pressure taken from the inside and the outside ambient pressure taken from the co-pilot static port. Pressurization Panel - Click for more information Hobbs meter Audio Panel - Click for more information Audio Panel - Click for more information The light comes on at approximately 500 F to warn the pilots of a possible bleed leak or fire. The BOTTLE 1 ARMED PUSH will illuminate when either LH or RH ENG FIRE PUSH switchlight has been push. The BOTTLE 2 ARMED PUSH will illuminate when either LH or RH ENG FIRE PUSH switchlight has been push. The light comes on at approximately 500 F to warn the pilots of a possible bleed leak or fire. The MASTER CAUTION pushlight works in conjunction with the "amber" CAS messages. PFD Controller - Click for more information AFCS - Click for more information Annunciators - Click for more information The APU FIRE PUSH switchlight comes on when the APU detects a fire. Open the cover and press to activate the fire extinguisher. The APU will automatically activate the fire extinguisher within 8 seconds. The BAG FIRE PUSH comes on when either or both smoke detectors sense a fire in the baggae compartment. By lifting the cover and push the switchlight, the HDR fire extinguisher (shared with APU) will release its content in the baggage area as well as the MDR (nose compartment) fire extinguisher which will be released within a period of 180 minutes. Power will be removed from the normally closed baggage heat shutoff valve. If the APU is running, it will be automatically shut down. The SEC BAG BOTTLE PUSH will illuminate when the aircraft descents thru FL250 to remind the pilots to push it. By pushing it, it will allow the MDR fire extinguisher to release its content at a highr rate. Standby Flight Display - Click for more information DU 1. It is the PFD for the pilot. The DU is made of an active matrix liquid crystal display. DU 2. It can serve several purposes. 1) EICAS 2) MFD 3) PFD in case of DU 1 failure DU 3. It can serve several purposes. 1) EICAS 2) MFD 3) PFD in case of DU 4 failure DU 4. It is the PFD for the co-pilot. The DU is made of an active matrix liquid crystal display. Oxygen panel - Click for more information Bleed Air System panel - Click for more information temperature controller panel - Click for more information power quadrant - Click for more information Guarded switch for the rudder bias system. Once pressed, The O'RIDE function is powered by the emergency bus to move the actuator to its minimum position. Use when uncommanded rudder bias movement or when the checklist calls for it. The PITCH WHEEL controls the rate of climb/descent in feet per minute if using the V/S mode. Start panel - Click for more information Engine system panel - Click for more information Electrical panel - Click for more information MCDU 1. It is the display for FMS, radio tuning, avionics setup and system test. MCDU 2 Lighting panel - Click for more details Gust lock. Pulling on the handle locks the primary flight controls in neutral. Also, the left throttle is limited to half travel between IDLE and CRU detent. Secondary trim panel - Click for more information Thrust reverser emer stow - Click for more details Landing panel - Click for more information Anti-ice panel - Click for more information Emergency brake handle. Pulling on the handle, it allows a control release of the nitorgen that is stored in the pneumatic bottle located in the left nose compartment. The nitrogen is release directly in all four wheel brake assemblies. Constant pressure is recommended, otherwise the bottle will deplete quickly. Use when hydraulic failure. Landing distance must be increased per the checklist. Nose wheel steering. The tiller needs main DC power for the NWS steering unit to operate. in the event of a loss of hydraulic pressure, pneumatic back will allow the rudder to make two 90 degrees sweeps. Enough to clear the runway. The NWS unit can be disabled at anytime using the AP/TRIM/NWS disconnect on either yoke. Neither the tiller or the pneumatic back will be available in the event of a DC power loss. Emergency gear blowdown. Pulling the knob allows a pneumatic bottle (2050 psi in the left nose compartment) filled with nitrogen to release its content in the hydraulic lines to drive the landing gears uplocks and actuators open and let the gears free fall. Use when the checklist calls for it. Nose gear manual release. Pulling on the D ring will manually release the nose gear uplocks. To be use if the emergency blowdown failed and the checklist has called for it. The main gears manual release is located in the kick panel below the aft bulkhead closet. Flap handle. It must be pushed down in order to move it. The preset position are 0, 7, 15 and 35 degrees. The flaps are electrically activated via a mechanical drive. All functions are controlled and monitored by the flap controller. The controller drives the power drive unit (motor). It receives seperate RH and LH flaps position from the resolvers (jackscrews). if faults is detected, the system shuts down automatically and apprpriate warning are displayed. The IDENT bottom activates the IDENT feature of the transponder. The IDENT bottom activates the IDENT feature of the transponder. Depressing the TCS touch control steering will momentarily disconnect the autopilot while the switch is held down. As soon as it is released, the autopilot re-engages. Depressing the TCS touch control steering will momentarily disconnect the autopilot while the switch is held down. As soon as it is released, the autopilot re-engages. Depressing the AP/TRIM/NWS disconnect disconnects the autopilot and yaw damper. It also allows the nose wheel to caster freely. (hydraulic pressure removed) Depressing the AP/TRIM/NWS disconnect disconnects the autopilot and yaw damper. It also allows the nose wheel to caster freely. (hydraulic pressure removed) The switch controls the movement of the stabilizer via the primary trim system. Main DC system must be operational to use. The switch controls the movement of the stabilizer via the primary trim system. Main DC system must be operational to use. Cockpit lighting - Click for more information Push to talk switch. Pushing the switch allows communication with atc. Pulling the switch aft allows communication between pilots. Neutral is off. Push to talk switch. Pushing the switch allows communication with atc. Pulling the switch aft allows communication between pilots. Neutral is off. The knob controls the rheostat for chart light. WX radar controller - Click for more information CCD controllers - Click for more information PARK BRAKE knob. To set it, brake pedals must be pressed before pulling the knob. Hydraulic pressure must be above 2300 psi to be set. Pressure can cmoe from either engine driven hyrdraulic pumps or the electrical auxiliary hydraulic pump. Pulling on the knob traps fluid by way of a set of one-way check valves to the wheel brake assemblies. Click for more information EROS mask - Click for more information EROS mask - Click for more information Airshow controller. It controls the various airshow menus as well as the passenger briefing system.
LH CB panel
APU panel
RH CB panel
ELT panel

 

Left Circuit Breakers panel Right Circuit Breakers panel ELT panel - Click for more information APU panel - Click for more information