Honeywell PRIMUS 1000 - Pitch Trim Color Description; Roll Trim; Yaw Trim

PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
5-17
Engine Instrument and Crew Alerting System (EICAS)
NOTES: 1. When the pitch trim is > +1°, UP is annunciated
above the digital display.
2. When the pitch trim is < --1°, DN is annunciated
above the digital display.
3. When pitch trim is < --1°, the minus (--) sign is
removed.
Condition
Digits and Pointer
Color
Condition A
--Weight--on--wheels (WOW)
--Trim out of takeoff range
--Trust lever angle >60°
Red
Condition B
--Weight--on--wheels (WOW)
--Trim out of takeoff range
--Trust lever angle <60°
Amber
Condition C
--Airborne
Green
NOTE: Digits are also enclosed in a box of the same color.
Pitch Trim Color Description
Table 5--13
D Roll Trim -- An analog roll trim scale displays the current roll trim.
The green trim arrow indicates the trim position. An amber mistrim
arrow is displayed when the autopilot is engaged and the ailerons
must be retrimmed. The mistrim arrow indicates the direction ofthe
trim required to retrim the aircraft.
D Yaw Trim -- Rudder trim is displayed with an analog scale and a
green pointer. The pointer indicates the current trim position.