Roll Gain Adjustment; Overstabilization In A Right Roll - Honeywell PRIMUS 660 Pilot's Manual

Primus digital weather radar system
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ROLL GAIN ADJUSTMENT

This in–flight adjustment is made in a bank when the ground returns do
not remain symmetrical during turns. The procedure is listed in table
7–6.
Step
1
If two controllers are installed, one must be turned off. If an
indicator is used as the controller, the procedure is the
same as given below.
2
Fly to an altitude of 10,000 feet AGL or greater.
3
Set range to 50 NM.
4
Adjust the tilt down until a solid band of ground returns are
shown on the screen. Then adjust the tilt until the green
region of the ground returns start at about 40 NM.
5
Select STAB (STB) 4 times within 3 seconds. A display
with text instructions for roll offset is shown.
A28–1146–111
REV 2
PRIMUS

Overstabilization in a Right Roll

Figure 7–8
Roll Gain Adjustment Procedure
Table 7–6 (cont)
R
660 Digital Weather Radar System
40
20
Procedure
100
80
60
AD–17722–R2@
In–Flight Adjustments
7-11

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