1. ALL WIRES
24 AWG OR LARGER UNLESS OTHERWISE SPECIFIED
.
2.
GROUND DESIGNATIONS: SHIELD BLOCK GROUND AIRFRAME GROUND
3. AT THE GTN
, CONNECT SHIELD GROUNDS TO THE CONNECTOR BACKSHELL --
THE SHIELD LEADS MUST BE LESS THAN 3.
0". CONNECT OTHER SHIELD GROUNDS TO AIRCRAFT
GROUND WITH AS SHORT A CONDUCTOR AS PRACTICAL.
4. IF VLOC ANNUNCIATE SIGNAL IS USED ONLY BY AUTOPILOT
, THIS MAY BE CONNNECTED DIRECTLY. IF VLOC ANNUNCIATE SIGNAL IS REQUIRED BY OTHER SYSTEMS,
CONNECT AS SHOWN IN FIGURE LABELED “CONNECTION TO OTHER SYSTEMS”.
5.
CONNECT OTHER PINS THAT ARE NOT SHOWN IN ACCORDANCE WITH THE MANUFACTURER’S INSTRUCTIONS.
6.
IF GPS ANNUNCIATE SIGNAL IS USED ONLY BY AUTOPILOT, THIS MAY BE CONNECTED DIRECTLY
. IF GPS ANNUNCIATE SIGNAL IS REQUIRED BY OTHER SYSTEMS (I
.E.
CDI,
REMOTE ANNUNCIATOR
), CONNECT AS SHOWN IN FIGURE LABELED “CONNECTION TO OTHER SYSTEMS”.
7
. GPS TRACK GAIN IS USED TO IMPROVE TRACKING WHEN GPS IS SELECTED ON THE CDI AND THE AUTOPILOT IS IN ANALOG NAVIGATION MODE (AND ROLL STEERING IS NOT
ENGAGED).
8
. FOR CONVERTERS 01278
-() S
/N 600A AND ABOVE
.
9. FOR CONVERTERS 01278-()
S/N
599 AND BELOW.
10
. ONLY REQUIRED FOR GTN 650/750.
11
. ALL GAMA FORMAT CONFIGURATIONS OF THE GPS ARINC 429 OUTPUT PROVIDE DATA REQUIRED BY THE AUTOPILOT FOR GPSS.
THE ARINC 429 CONFIGURATION CANNOT BE
USED
. REFER TO SECTION 5.5.1.1 FOR CONFIGURATION SETTINGS.
12. THE SPLICE MUST BE PERFORMED AT THE CONNECTOR END OF THE WIRE
. SPLICE AS SHOWN:
s
NOTES:
PXX
s
s
LRU
13
. CONNECT TO AUTOPILOT CIRCUIT BREAKER FOR AIRCRAFT POWER.
14. AN ACCEPTABLE RELAY IS LEACH P/N WN460-( )( )( ).
15. 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.
16. REFER TO SHEET 1 OF THIS FIGURE FOR PINOUT INFORMATION
.
