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The ROLL SPOILERS switch is located on the center pedestal. If the jam is in the pilot’s wheel, raising the guarded switch and pressing OFF disables the roll assist function. A ROLL SPOILERS OFF (C) will be illuminated on the EICAS. A ROLL SPOILERS OFF (S) is illuminated when the roll spoilers have been turned off and the roll disconnect has been ac-tivated. Pressing the switch again, reengages the roll assist function and extinguishes the CAS message
PILOT COPILOT
CONTROL CONTROL
WHEEL ROLL SPOILERS WHEEL
MIC D
ROLL
ID MIC
OFF
DISCONNECT SWITCH
RVDTS RVDTS
SECU1
SECU2
COMMAND MONITOR
COMMAND
MONITOR
ARINC 429
CFO1005002_005
Volume 2 Flight Crew Operating Manual Sep 13/2004 CSP 100-6 REV 1
10-02-10 SECONDARY FLIGHT CONTROLS (Cont) FLIGHT SPOILER SCHEMATIC
Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6
10-02-11 SECONDARY FLIGHT CONTROLS (Cont)
GROUND SPOILERS DESCRIPTION
After touchdown or during a rejected takeoff, the inboard and outboard ground spoilers in conjunction with the multifunc-tion spoilers are extended to spoil lift and increase drag to assist in aircraft braking. The ground spoilers function is nor-mally automatic but can be activated manually by the pilot. The ground spoilers have no in-flight function.
COMPONENTS AND OPERATION
The ground spoiler function is selected by the three position GND SPOILERS switch as follows:
-OFF — Disables the ground spoilers by disarming the function -AUTO — Automatically arms the ground spoilers for landing and rejected takeoff in conjunction with throttle lever angle, wheel speed, weight on wheels and radio altitude -MANUAL ARM — Arms the ground spoilers regardless of the inputs required to arm in the AUTO position
When deployed, the ground spoiler panels extend to 60° and the multifunctional panels extend to 45°, however, only the multifunction panels respond to control wheel roll assist inputs. Ground spoilers deploy when the inputs for ground spoiler deploy logic are throttles at IDLE, and 2 of the 3 following criteria are met: radio altitude less than 7 ft, weight on wheels, and wheelspeed greater than 16 kt.
The position of all panels are shown on the EICAS FLIGHT CONTROLS synoptic page. Green arrows and position scales indicate relative deflection of the surfaces.
Inboard and outboard ground spoilers are limited to two positions, either up or down. The spoilers are continuously monitored and any fault detected is displayed on the appropriate EICAS screen.
Volume 2 Flight Crew Operating Manual Sep 13/2004 CSP 100-6 REV 1
10-02-12 SECONDARY FLIGHT CONTROLS (Cont) TAKEOFF CONFIGURATION WARNING SYSTEM
DESCRIPTION
The takeoff configuration warning system monitors the position of the flaps, flight spoilers, parking brake, autopilot, aile-ron, rudder, roll and pitch disconnect, and horizontal stabilizer trims, to ensure that they are in a safe configuration for take-off.
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