IFD5XX Installation Manual
600-00299-000
Page 153 of 198
Revision: 02
B end i x / K i ng
K I 2 0 8 A
P 2 0 8 A 1
20
21
43
42
48
3
9
50
2
15
14
Navigation
Indicator
LNAV LATERAL DEV +LT IN
LNAV LATERAL DEV +RT IN
LNAV +TO IN
LNAV +FROM IN
LNAV LFLAG IN
LNAV LATERAL -FLAG IN
LNAV FCS LOC ENGAGE IN
OBS RETURN
LNAV OBS EXCITATION IN
LNAV OBS SIN OUT
LNAV OBS COS OUT
RELAY ENGAGE
IFD540
MAIN +LEFT
MAIN +RIGHT
MAIN +TO
MAIN +FROM
MAIN LFLAG
MAIN LATERAL -FLAG
APPROACH ANNUNCIATE
MAIN OBS ROTOR H
MAIN OBS ROTOR C
MAIN OBS ROTOR D
MAIN OBS ROTOR E
MAIN OBS ROTOR F
MAIN OBS ROTOR G
GPS ANNUNCIATE
P1001
21
22
25
26
23
24
5
32
31
33
34
35
36
2
NOTES:
1.
ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED.
TO CONNECT THE IFD540 TO A KI209A INDICATOR, ADD TWO 10K OHM, ¼ WATT RESISTORS AS SHOWN.
3.
REFER TO MANUFACTURER’S DOCUMENTATION FOR COMPLETE PINOUT AND INTERCONNECT INFORMATION. PINOUTS OF OTHER UNITS
SHOWN FOR REFERENCE ONLY.
4.
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.
PROPER CONNECTION OF THE RELAY ENGAGE INPUT OF THE KI 208A IS DEPENDENT ON ITS POWER SUPPLY VOLTAGE. REFER TO KI 208A
DOCUMENTATION FOR PROPER CONNECTION.
IF THE IFD540 IS INSTALLED, AND ANOTHER VOR/ILS RECEIVER IS AVAILABLE TO DRIVE THE NAVIAGATION INDICATOR, AN EXTERNAL
SOURCE SELECTION SWITCH MUST BE USED IN LIEU OF THE GPS ANNUNICATE OUTPUT.
10k OHM
10k OHM
VOR/ILS
GPS
6
P1006
8
29
VOR/LOC COMPOSITE OUT
ILS ENERGIZE
5
6
10
VOR/LOC COMPOSITE
NAV LOC ENGAGE IN
2
5
6
2
Figure D - 17: Main Indicator KI208 Interconnect
Summary of Contents for IFD540
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