1.
ALL WIRES
24 AWG OR LARGER UNLESS OTHERWISE SPECIFIED
.
2
. GROUND DESIGNATIONS
:
SHIELD BLOCK GROUND AIRFRAME GROUND
3.
AT GTN
6XX
/7
XX
, 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.
THE CENTURY IV REQUIRES AN ISOLATION DIODE TO BE INSTALLED ON THE LOCALIZER SWITCHING INPUT AS SHOWN BELOW.
s
NOTES
:
AUTOPILOT
CENTURY
IV
CD66
LOC SWITCH
44
GTN
6XX
/
7XX
P1001
ILS/GPS APPROACH
*
56
1
N4444 OR
EQUIV
.
6
. THE GTN CAN BE CONFIGURED TO ANY GPS ARINC 429 OUTPUT TO PROVIDE GPSS DATA.
REFER TO SECTION 5.5.1
.1 FOR CONFIGURATION SETTINGS
.
7. REFER TO MANUFACTURERS DOCUMENTATION FOR COMPLETE PINOUT AND INTERCONNECT INFORMATION
. PINOUTS OF OTHER UNITS SHOWN FOR REFERENCE ONLY.
8. THE SPLICE MUST BE PERFORMED AT THE CONNECTOR END OF THE WIRE
. SPLICE AS SHOWN:
Century AK 1081
GPSS converter
CD
278
1
2
ARINC 429 IN A
ARINC 429 IN B
8
4
NAV SELECTED
10
29
ARINC
429 OUT 1
A
ARINC 429 OUT 1B
52
VLOC ANNUNCIATE*
3 SHIELD GND
5 ARINC
429 IN B SPD SELECT
ARINC
429 IN A SPD SELECT
s
P1001
6
5
GTN
6XX/
7XX
5.
INSTALL JUMPER AS REQUIRED TO SET AK 1081 ARINC 429
SPEED TO MATCH THE GTN OUTPUT SETTING. REFER TO MANUFACTURER’S DOCUMENTATION FOR ADDITIONAL
DETAILS.
9. 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 P
1001 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.
PXX
s
s
LRU
