7-3-7
Indication / Warning
Symbolic aircraft views of the trim positions for the aileron trim tab (roll), rudder trim tab (yaw)
and horizontal stabilizer (pitch) are shown in the TRIM window of the systems MFD. In flight,
the trim indications are shown in white. An invalid trim status will be shown with an amber
cross. On the ground, the trim logic changes and the colors change based on the trim position.
The neutral trim positions change to green and the pitch trim also has a green diamond (aft
cg). The aircraft symbols change to green when each trim position is correctly set for takeoff. If
the trim position is not correctly set, the aircraft symbol will be white and a CAS
Takeoff
Configuration
will be displayed on the CAS window. A green trim in motion indicator will
show when the autopilot is moving the rudder and horizontal stabilizer trim. An invalid autopilot
trim parameter will be shown with an amber cross over the indicator.
Flap position is shown in the FLAP window of the systems MFD by a white symbolic flap
pointer which moves in relation to flap movement. The window is marked in white with the
positions 0, 15, 30 and 40. The pointer and the degree position mark will change to green
when the pointer reaches the selected flap position and is adjacent to the mark. When the
aircraft is on ground and flaps are at 40° the pointer will show white and a CAS
Takeoff
Configuration
will be displayed on the CAS window. When airborne and the flaps are up, the
flap indications change from their default white to a grey color after 20 seconds. An invalid flap
condition or status related to the flap position will be shown by an amber cross.
If the airspeed goes above the maximum limit for the current flap setting, the Flight Alerting
System (FAS) will initiate an “Overspeed” warning on the Primary Flight Display (PFD) and a
“Speed” voice callout will be heard. A red Vconstraint bar will be shown on the right side of the
PFD ASI tape and the airspeed digital readout will change to red.
If a stabilizer trim runaway of the main system is sensed, a CAS
Pitch Trim Runaway
will
be displayed and a “Trim Runaway” voice callout will be heard.
If a rudder trim runaway is sensed, a CAS
Yaw Trim Runaway
will be displayed and a “Trim
Runaway” voice callout will be heard.
In case of a pitch or yaw trim runaway, take action in accordance with Section 3, Emergency
Procedures,
On the ground and with weight on the wheels the aircraft is monitored for Takeoff Configuration
by the Monitoring Warning System (MWS). The MWS monitors the position of the trim tabs,
horizontal stabilizer, flaps, and the engine and airspeed conditions. If any of the trims or the
flap position are not in the takeoff range with the engine running,
Takeoff Configuration
will
be shown in the CAS window of the systems MFD. If any of the trims or the flap position are
not in the takeoff range, and the engine torque is increased more than 20 psi with an airspeed
of less than 50 KIAS, the FAS will initiate a NO TAKEOFF warning on the PFD and a “No
Takeoff” voice callout will be heard.
Section 7 - Airplane and Systems Description
Indication / Warning
Pilot's Operating Handbook
Report No: 02406
Issue date: Mar 06, 2020
Page 7-3-4
12-C-A15-00-0703-00A-043A-A
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GENERAL
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