Honeywell BENDIX/KING RDR 2000 Installation Manual page 62

BENDIX/KING
6. Proceed to Step N.
N. ROLL OFFSET
1. Set the tilt table for 0
ROLL OFFSET page (see
2. Press the WxA to display brackets around the ROLL value. Adjust the TILT knob
for a ROLL value of 0.0 ± 1.0
3. Set the tilt table to 10
4. Set the tilt table to 10
5. Set the tilt table to 0
6. Proceed to Step O.
O. PITCH GAIN
1. Press the GND MAP button to obtain the PITCH GAIN page on the display (see
figure 2-14). Set the TILT knob for a value of 0.0.
2. Set the tilt table for 5
3. Press the WxA button again to display brackets around the PITCH value. Adjust
the TILT knob for a reading of 10.0U ± 1.0
button again will remove the brackets.
4. Set the tilt for 5
5. Proceed to Step P.
P. ROLL GAIN
1. Set the tilt table to 0
GAIN page on the display (see
2. In determining the tilt of the table use the standard rate turn for the aircraft being
aligned.
3. Press the WxA button again to display brackets around the ROLL value. Adjust the
TILT knob for a reading of 10.0R ± 1.0
again will remove the brackets.
4. Set the tilt table for a standard rate turn for the aircraft being aligned. Repeat Step
3.
5. Proceed to Step S.
Q. ARINC 429 PITCH OFFSET
1. Set the tilt table for 0
PITCH OFFSET page (see
2. Press the WxA to display brackets around the PITCH value. Adjust the TILT knob
for a PITCH value of 0.0 ± 1.0
Page 2-32
°
pitch and roll. Press the GND MAP button to display the
figure 2-17).
°
. Press the WxA button to deselect the brackets.
°
roll right. The value should be 10.0R ± 1.0
°
roll left. The value should be 10.0L ± 1.0
°
roll. The value should be 0.0 ± 1.0
°
pitch up.
°
PITCH DOWN. Repeat Step 3.
°
pitch and roll. Press the GND MAP button to obtain the ROLL
figure
°
pitch and roll. Press the GND MAP button to display the 429
figure 2-18).
°
. Press the WxA button to deselect the brackets.
00643I05.TDC
°
.
°
in the PITCH field. Pressing the WxA
2-16). Set the TILT knob for a value of 0.0.
°
in the ROLL field. Pressing the WxA button
RDR 2000
°
.
°
.
Rev 7, July/2002