Figure H-25. Autopilot Interconnect - Garmin GPS 400W Installation Manual

GNS 400W
MAIN LATERAL +FLAG
MAIN LATERAL - FLAG
MAIN +LEFT
MAIN +RIGHT
MAIN VERTICAL +FLAG
MAIN VERTICAL -FLAG
MAIN +UP
MAIN +DOWN
GPS ARINC 429 OUT
4
ILS/GPS APPROACH
NOTES:
1. ALL WIRES 24 AWG OR LARGER UNLESS OTHERWISE SPECIFIED.
2. AT GNS 400W SERIES UNIT, TERMINATE SHIELD GROUNDS TO THE CONNECTOR BACKSHELL OR USE CARD-EDGE
CONNECTOR TO TERMINATE SHIELD GROUNDS TO BACKPLATE. THE SHIELD LEADS MUST BE LESS THAN 3.0 INCHES.
CONNECT OTHER SHIELD GROUNDS TO AIRCRAFT CHASSIS WITH AS SHORT A CONDUCTOR AS PRACTICAL.
3. ONLY CONNECTIONS SUPPORTED BY THE AUTOPILOT ARE REQUIRED
4. ALL "GAMA 429" CONFIGURATIONS OF THE GPS ARINC 429 OUTPUT PROVIDE DATA REQUIRED BY THE AUTOPILOT FOR
GPSS. THE "ARINC 429" CONFIGURATION CANNOT BE USED.
5. GNS 400 SERIES SETUP ITEMS
MAIN SYSTEM CONFIG PAGE: DISCRETES - ILS/GPS APR: APPROACH ONLY
Page H-38
Rev. G
TO MAIN CDI
5
P4001
23
24
21
22
29
30
27
28
A 46
B 47
14

Figure H-25. Autopilot Interconnect

AUTOPILOT
COMPUTER
LAT DEV FLAG+
LAT DEV FLAG-
LAT DEV +LT
LAT DEV +RT
GS DEV FLAG+
GS DEV FLAG-
GS DEV +UP
GS DEV +DOWN
A
429 GPS IN
B
ILS ENERGIZE (A/P IN)
GNS 400W Series Installation Manual
190-00356-08