PRIMUSr 880 Digital Weather Radar System

PITCH GAIN ADJUSTMENT

This in- flight adjustment is made in a bank when the ground returns do not follow the contours of the range arcs during turns. The procedure is listed in table 5- 10.

Step

Procedure

 

 

 

 

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 25 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 20

 

NM.

 

 

5

On the WC controller, select variable gain (pull), WX

 

and REACT OFF. VAR shows on the display.

 

 

6

Push STAB (STB) 4 times within 3 seconds. A display

 

with text instruction is shown.

 

 

7

From the roll offset entry menu, push the STAB (STB)

 

button 3 more times to bring up the pitch gain entry

 

menu.

 

 

8

To change the pitch gain value, pull out the GAIN knob

 

and rotate it. The pitch gain adjustment range is from

 

90 to 110%.

9

While flying with a steady pitch angle of >5°, adjust so

 

the contour of the ground returns follow the contour of

 

the range arcs as closely as possible.

10

When change is completed, push in the GAIN knob.

 

The display returns to the previous message.

 

 

11

Push the STAB button to exit the mode and save the

 

value in nonvolatile memory.

 

Pitch Gain Adjustment

 

Table 5- 10

Radar Facts

A28- 1146- 102- 00

5-30

 

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Image 80
Honeywell 880 manual Pitch Gain Adjustment