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STALL PROTECTION SYSTEM (CONT'D)
SPS Ground Testing
Preflight testing of the system is accomplished by SPS TEST switches on the miscellaneous
test panel, located on the center pedestal. Either the L (R) SPS TEST switch will cause the
system to progressively sweep through the AOA range from no stall to full stall, as indicated on
the SPS test indicator, activating ignition (blue arc) and shaker/autopilot disconnect (yellow arc).
This is followed by red flashing STALL annunciation on the PFD, and an aural warbler warning.
If both switches are activated simultaneously, the stick pusher will activate (red arc).
Pusher disconnects can then be tested by pushing, in sequence, the pilot’s AP/SP DISC, the
copilot’s AP/SP DISC and the G-switch.
CAUTION
See the Airplane Flight Manual for full testing procedures. Ignition
is activated during the test, and may pose a hazard in enclosed
areas.
CONTROLS AND INDICATORS
Primary and secondary flight controls and indicators are accessible from both pilot seats. Warning,
caution, advisory and status messages are presented on the EICAS page and on the FLIGHT
CONTROLS synoptic page.
FLIGHT CONTROLS
Description
Vol. 2 10−10−19
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
CONTROLS AND INDICATORS (CONT'D)
Primary Flight Controls
Pitch, Roll and Yaw Controls
Figure 10−10−13
FLIGHT CONTROLS
Description
Vol. 2 10−10−20
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
CONTROLS AND INDICATORS (CONT'D)
Stab Trim, Aileron Trim, Rudder Trim
Trim Controls
Figure 10−10−14
FLIGHT CONTROLS
Description
Vol. 2 10−10−21
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
CONTROLS AND INDICATORS (CONT'D)
Flaps, Spoilers
Flap and Spoiler Controls
Figure 10−10−15
FLIGHT CONTROLS
Description
Vol. 2 10−10−22
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
CONTROLS AND INDICATORS (CONT'D)
Stall Protection System
Stall Protection System
Figure 10−10−16
FLIGHT CONTROLS
Description
Vol. 2 10−10−23
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
CONTROLS AND INDICATORS (CONT'D)
EICAS Flight Controls Indications (Ground Spoilers)
Figure 10−10−17
FLIGHT CONTROLS
Description
Vol. 2 10−10−24
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
CONTROLS AND INDICATORS (CONT'D)
EICAS Flight Controls Indications (Flight Spoilers)
Figure 10−10−18
FLIGHT CONTROLS
Description
Vol. 2 10−10−25
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
CONTROLS AND INDICATORS (CONT'D)
EICAS Flight Controls Indications (Flaps)
Figure 10−10−19
FLIGHT CONTROLS
Description
Vol. 2 10−10−26
REV 1, Dec 21/06
CL−605 Flight Crew Operating Manual
PSP 605−6
CONTROLS AND INDICATORS (CONT'D)
EICAS Flight Controls Indications (Trim)
Figure 10−10−20
FLIGHT CONTROLS
Description
Vol. 2 10−10−27
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
CONTROLS AND INDICATORS (CONT'D)
EICAS Flight Controls Indications (Aileron, Elevator, Rudder)
Figure 10−10−21
FLIGHT CONTROLS
Description
Vol. 2 10−10−28
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
EICAS MESSAGES
MESSAGE MEANING
AURAL WARNING
(IF ANY)
CONFIG FLAPS Flaps are not set at 20° with the aircraft in takeoff
mode.
“CONFIG FLAPS”
CONFIG SPOILERS Spoilers are not stowed with the aircraft in takeoff
mode.
“CONFIG SPOILERS”
CONFIG STAB Pitch trim is not set in the green band with the aircraft
in takeoff mode
“CONFIG TRIM”
AILERON PCU One or both ailerons have a jammed power control unit.
ALT COMP FAIL The left or right altitude compensation circuit of the stall protection computer
has failed.
ELEVATOR SPLIT Indicates >5 degrees difference between left and right elevator surface
position.
FLAPS FAIL Either both flap motors are overheated or the flaps have failed.
FLT SPLRS DEPLOY Flight spoilers are deployed with either the radio altitude between 10’ – 300’ or
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