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RESPONSE TIME 4 4
SLOPE 50 50
MINIMUM 080 040
OFFSET 50 50
DATE/TIME SETUP page
UTC DATE UTC TIME
Enter UTC (Universal Time Coordinated) date Enter UTC time
MAIN DISCRETE INPUTS page
Make sure the decoded altitude displayed on display is correct
MAIN CDI/OBS CONFIG page
Perform OBS calibration of CDI/HSI with the "SELECTED COURSE" field
COM SETUP page
SPACING 25,0 KHz
Store Calibration ? Select the field and press "ENT"
VOR/LOC/GS CDI page
Perform CDI calibration with the "SELECTED COURSE" field
Pages configuration — OPT10-23-004 -A
Table 501A
AAAA
Validity : GNS 430 34-57-00(BA) 04
(BA) JUN5 04
MAIN ARINC 429 CONFIG page
SPEED DATA
IN 1 LOW OFF
IN 2 LOW OFF
OUT LOW OFF or GAMA 429 (1)
SDI COMMON
MAIN RS 232 CONFIG page
INPUT OUTPUT
CHAN 1 OFF or SHADIN FUEL (2) OFF or AVIATION (2)
CHAN 2 OFF OFF
CHAN 3 OFF or CROSSFILL (3) OFF or CROSSFILL (3)
CHAN 4 OFF OFF
MAIN LIGHTING page
DISPLAY KEY
LIGHTING XXXX XXXX
SOURCE PHOTO 28V DC
RESPONSE TIME 4 4
SLOPE 50 50
MINIMUM 080 040
OFFSET 50 50
Pages configuration — OPT10-23-006-A
Table 501B
"GAMA 429" with A/P KFC225.
"Shadin Fuel - Aviation" with OPT. SHADIN (Microflo-L) and/or OPT. KMD 550.
"CROSSFILL - CROSSFILL" with OPT. GNS430 # 2.
AAAA
Validity : GNS 430 34-57-00 Page 505
(BA) JUN 04
PAGE INTENTIONALLY LEFT BLANK
AAAA
Validity : GNS 430 Na ev50016
34-57-00 (BA) Page
GLOBAL POSITIONING SYSTEM (GPS)
ADJUSTMENT / TEST
1. OPERATIONAL TEST OF THE GLOBAL POSITIONING SYSTEM
Tools and consumable material
- Ground power unit
Procedure
Park the aircraft on a clear area.
Make sure that the main switch-breaker is open.
Connect the ground power unit - refer to 24-40-00.
Make sure the A78 GPS receiver is not energized ("PUSH-ON" button in pulled-out position).
Close the main switch-breaker.
Set the radio master switch to "ON".
Interfaced-with-HSI version
If necessary, select GPS function on the HSI indicator with the "NAV GPS" or "NAV1 GPS1" annunciator/switch of the advisory panel.
All
Press "PUSH-ON" button of GPS receiver to energize it.
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