Installation Instructions

GTN 6XX/7XX AML STC Installation Manual 190-01007-A3
Page E-90 Rev. 4
P1001
AUTOPILOT
COMPUTER
SPZ-200A/500
J1A J1B
16 -
- 7
GTN 6XX/7XX
LATERAL SUPERFLAG OUT
13
32
VERTICAL SUPERFLAG OUT
LAT SUPERFLAG
G/S SUPERFLAG
22 -
LOC FREQ GROUND
56
ILS/GPS APPROACH*
20
21
-
-
LAT DEV +LT
LAT DEV +RT
49
68
MAIN LATERAL +LEFT OUT
MAIN LATERAL +RIGHT OUT
s
-
-
16
17
GS DEV +UP
GS DEV +DN
12
31
MAIN VERTICAL +UP OUT
MAIN VERTICAL +DOWN OUT
FZ-500
FD Computer
SPERRY
ALL WIRES 24 AWG OR LARGER UNLESS OTHERWISE SPECIFIED.
GROUND DESIGNATIONS: SHIELD BLOCK GROUND AIRFRAME GROUND
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.
1
2
3
NOTES:
s
s
LATERAL + LEFT
LATERAL + RIGHT
s
VERTICAL + UP
VERTICAL + DOWN
s
TO MAIN CDI
LATERAL SUPERFLAG
VERTICAL SUPERFLAG
s
4
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.
4
Figure E-41. GTN 6XX/7XX – Sperry Autopilot Interconnect