Installation Instructions
GTN 6XX/7XX AML STC Installation Manual 190-01007-A3
Page E-23 Rev. 4
GTN 6XX/7XX
P1001
9
2
15
50
14
MAIN OBS ROTOR C
MAIN OBS STATOR D
MAIN OBS STATOR E (GND)
MAIN OBS STATOR F
MAIN OBS STATOR G (GND)
MAIN OBS ROTOR H (GND)
20
21
MAIN LATERAL +LEFT OUT
MAIN LATERAL +RIGHT OUT
43
42
MAIN +TO OUT
MAIN +FROM OUT
48
3
MAIN LATERAL +FLAG OUT
MAIN LATERAL -FLAG OUT
ILS/GPS APPROACH
6
GPS ANNUNCIATE*
NAVIGATION
INDICATOR
LNAV FCS LOC ENGAGE IN
OBS RETURN
LNAV OBS EXCITATION IN
LNAV OBS SIN OUT
LNAV OBS COS OUT
RELAY ENGAGE
LNAV LATERAL DEV +LEFT IN
LNAV LATERAL DEV +RIGHT IN
LNAV +TO IN
LNAV +FROM IN
LNAV LATERAL +FLAG IN
LNAV LATERAL -FLAG IN
VOR/LOC COMPOSITE
NAV LOC ENGAGE IN
BENDIX/KING
KI 208A
P208A1
1
21
40
2
41
60
49
68
11
30
50
69
56
15
VOR/LOC COMPOSITE OUT
ILS ENERGIZE
10
P1004
8
29
N/C
6
5
s
s
s
s
s
s
s
GPS
VOR/ILS
7
1. ALL WIRES 24 AWG OR LARGER UNLESS OTHERWISE SPECIFIED.
2. GROUND DESIGNATIONS: SHIELD BLOCK GROUND AIRFRAME GROUND
3. AT GTN 6XX/7XX, CONNECT SHIELD GROUNDS TO THE CONNECTOR BACKSHELL -- THE SHIELD TERMINATION
LEADS MUST BE LESS THAN 3.0". CONNECT OTHER END OF THE SHIELD PER THE REMOTE EQUIPMENT
INSTALLATION REQUIREMENTS. IF NO SHIELD TERMINATION REQUIREMENT EXISTS FOR THE REMOTE
EQUIPMENT, TERMINATE SHIELDS AS SHORT AS POSSIBLE, NOT TO EXCEED 3.0". SEE SECTION 2.4.11.4.
4. REFER TO MANUFACTURERS DOCUMENTATION FOR COMPLETE PINOUT AND INTERCONNECT INFORMATION.
PINOUTS OF OTHER UNITS SHOWN FOR REFERENCE ONLY.
5. 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.
6. IF THE GTN 625/635/725 IS INSTALLED, AND ANOTHER VOR/ILS RECEIVER IS AVAILABLE TO DRIVE THE
NAVIGATION INDICATOR, AN EXTERNAL SOURCE SELECTION SWITCH MUST BE USED IN LIEU OF THE GPS
ANNUNCIATE OUTPUT. AN ACCEPTABLE SWITCH IS CARLINGSWITCH P/N 112-A-63. LABEL AS SHOWN. REFER
TO SECTION 2.4.8 FOR ADDITIONAL SWITCH INSTALLATION REQUIREMENTS.
7. THESE CONNECTIONS ARE USED ON THE GTN 650/750 ONLY.
8. FOR IFR-CERTIFIED COMPOSITE AIRCRAFT ONLY (EACH AIRCRAFT IN APPENDIX G THAT REQUIRES
OVERBRAID OVER THE GPS/WAAS CABLE): ANY LRU (I.E. CDI, AUTOPILOT) THAT CONNECTS TO THE GTN’S
P1001 MAIN CDI/VDI OUTPUTS MUST BE MOUNTED TO THE INSTRUMENT PANEL OR COCKPIT CENTER
CONSOLE WITH ELECTRICAL BONDING EQUAL TO OR LESS THAN 20 MILLIOHMS BETWEEN THE EQUIPMENT
AND THE INSTRUMENT PANEL.
s
NOTES:
N/C
N/C
8
Figure E-10. GTN 6XX/7XX – Bendix King KI 208A Interconnect