Avidyne IFD540 Installation Manual page 136

IFD 540 #1
GPS ARINC 429 IN 1 A
GPS ARINC 429 IN 1 B
GPS ARINC 429 OUT A
GPS ARINC 429 OUT B
VOR/ILS ARINC 429 OUT A
VOR/ILS ARINC 429 OUT B
IFD 540 #2
GPS ARINC 429 IN 1 A
GPS ARINC 429 IN 1 B
GPS ARINC 429 OUT A
GPS ARINC 429 OUT B
VOR/ILS ARINC 429 OUT A
VOR/ILS ARINC 429 OUT B
NOTES:
1. ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED.
2. AT IFD540 UNIT, TERMINATE SHIELD GROUNDS TO THE CONNECTOR BACKSHELL OR
USE CARD-EDGE CONNECTOR TO TERMINATE SHIELD GROUNDS TO BACK PLATE –
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. IF THE GPS ARINC 429 IN 1 PORT (P1001-48 AND -49) IS ALREADY USED FOR ANOTHER
PURPOSE, THE GPS ARINC 429 IN 2 PORT (P1001-50 AND -51) MAY BE CONNECTED
INSTEAD.
THE DEPICTED COLLINS EFIS-84 INTERFACE DOES NOT SUPPORT SELECTION OF THE
4
GPS COURSE VIA THE EFIS CONTROL PANEL A GARMIN. A GAD 42 IS REQUIRED FOR
GPS SELECTED COURSE.
REFER TO MANUFACTURER'S DOCUMENTATION FOR COMPLETE PINOUT AND
5.
INTERCONNECT INFORMATION. PINOUTS OF OTHER UNITS SHOWN FOR REFERENCE
ONLY.
600-00299-000
P1001
48
49
46
47
P1006
24
23
P1001
48
49
46
47
P1006
24
23
Figure D - 4: EFIS Interconnect
Page 136 of 198
IFD5XX Installation Manual
ARINC 429 EFIS
Collins Bendix/King
DISPLAY #1
EFIS-84 EFS 40/50
DPU-84 SG 465
P1 P4652A P4652B
47 LNAV TRANSMITTER A
4
20 LNAV TRANSMITTER B
142 67 LRN/LNAV 1 RECEIVER A
53 LRN/LNAV 1 RECEIVER B
138
64 LRN/LNAV 2 RECEIVER A
122
126 63 LRN/LNAV 2 RECEIVER B
16 NAV 1 RECEIVER A
125
29 NAV 1 RECEIVER B
129
38 NAV 2 RECEIVER A
25 NAV 2 RECEIVER B
ARINC 429 EFIS
Collins Bendix/King
DISPLAY #2
EFIS-84 EFS 40/50
DPU-84 SG 465
P1 P4652A P4652B
LNAV TRANSMITTER A
47
4
LNAV TRANSMITTER B
20
LRN/LNAV 1 RECEIVER A
142
67
LRN/LNAV 1 RECEIVER B
138
53
122 LRN/LNAV 2 RECEIVER A
64
126 LRN/LNAV 2 RECEIVER B
63
NAV 1 RECEIVER A
16
NAV 1 RECEIVER B
29
125 NAV 2 RECEIVER A
38
129 NAV 2 RECEIVER B
25
Revision: 02