Spoiler Position; Spoiler Color Coding; Pitch/Roll/Yaw Trim Display; Pitch Trim - Honeywell PRIMUS 1000 Pilot's Manual

Integrated avionics system for embraer 145
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PRIMUSr1000 Integrated Avionics System
Condition D
--Flaps position is as selected
NOTES:
1. When flap condition A or B exists, the flap position digital display
is boxed in the same color.
2. Only 0° , 9°,22° , 33° , 45°are displayed if flap control units are
valid (other positions are denoted by a dash (--)).
3. If either flap control unit fails, the actual flap position from the DAU
is displayed (0°to 47° ).
Spoiler Position -- The ground spoiler position is shown by a boxed
D
annunciation. Table 5--12 defines the color coding for the spoiler
position.

Spoiler Position

Closed
Open
NOTE: When the following conditions exist, the box and annunciation turn red:
-
Any spoilers switch sensed to be open
-
Weight on wheels (WOW)
-
Thrust lever angle > 60° .

PITCH/ROLL/YAW TRIM DISPLAY

The aircraft surface trim positions are shown in the lower right corner
of the EICAS. The symbols are described below.
Pitch Trim -- The pitch trim is indicated by digital and analog
D
displays. The digital display ranges from --10°(full nose down) to +4°
(full nose up). A green band is displayed to mark the takeoff trim
range. The color of the pointer and digital display are described in
table 5--13.
Engine Instrument and Crew Alerting System (EICAS)
5-16
Condition
Flaps Position Symbol Color
Table 5--11
Annunciation
CLD
OPN

Spoiler Color Coding

Table 5--12
Color Logic
Green
Color
White (see note)
Green (see note)
A28--1146--112--00

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