Installation Instructions

GTN 6XX/7XX AML STC Installation Manual 190-01007-A3
Page E-22 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
23
22
MAIN VERTICAL
+
FLAG OUT
MAIN VERTICAL -FLAG OUT
27
26
MAIN VERTICAL
+
UP OUT
MAIN VERTICAL +DOWN 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
LNAV VERTICAL
-
FLAG IN
LNAV VERTICAL
+FLAG IN
LNAV VERTICAL +UP IN
LNAV VERTICAL
+
DOWN IN
NAV VERTICAL +UP IN
VOR/LOC COMPOSITE
NAV LOC ENGAGE IN
BENDIX
/KING
KI 209A
P209A1
NAV VERTICAL +DOWN IN
NAV VERTICAL -FLAG IN
NAV VERTICAL +FLAG IN
25
24
1
21
40
2
41
60
49
68
11
30
50
69
70
12
31
56
15
51
VOR/LOC COMPOSITE OUT
ILS ENERGIZE
GLIDESLOPE +UP
28
29
10
GLIDESLOPE +DOWN
GLIDESLOPE +FLAG
P
1004
32
55
34
8
29
53
5
N/C
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 MANUFACTURER’S 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 209A IS DEPENDENT ON THE POWER SUPPLY VOLTAGE.
REFER TO KI 209A 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:
s
s
s
s
s
s
s
s
s
s
s
VOR/ILS
GPS
GLIDESLOPE
-FLAG
N
/
C
N/C
8
6
7
Figure E-9. GTN 6XX/7XX – Bendix King KI 209A Interconnect