Page D-8
GTN 725/750 TSO Installation Manual
Rev. A
190-01007-02
P1001
GTN 7XX
NOTES:
1. ALL WIRES 24 AWG OR LARGER UNLESS OTHERWISE SPECIFIED.
2. GROUND DESIGNATIONS: SHIELD BLOCK GROUND AIRFRAME GROUND
3. ALL POWER LEADS AND GROUND LEADS ARE REQUIRED.
4. CONFIGURATION MODULE IS MOUNTED IN THE BACKSHELL OF THE P1001 CONNECTOR.
5. CONFIGURATION MODULE HARNESS USES 28 AWG WIRES. CONTACTS SUPPLIED WITH CONFIGURATION MODULE
MUST BE USED FOR CONNECTING CONFIGURATION MODULE HARNESS TO P1001.
6. OPTIONAL CONNECTION. LIGHTING CAN BE CONTROLLED BY THE INTEGRATED PHOTOCELL, A SINGLE LIGHTING
BUS, OR DUAL LIGHTING BUSES. REFER TO SECTION
TBD
FOR MORE DETAILS.
7. CIRCUIT BREAKER SHOULD BE LABELED AS SHOWN.
8. CIRCUIT BREAKER SHOULD BE LABELED AS: “GPS” FOR THE GTN 725, AND “NAV/GPS” FOR THE GTN 750
s
CONFIG MODULE POWER
CONFIG MODULE GND
CONFIG MODULE DATA
CONFIG MODULE CLOCK
4
1
3
2
RED
BLK
YEL
WHT
LIGHTING BUS 1 HI
LIGHTING BUS 1 LO
TO AIRCRAFT
LIGHTING BUS
65
64
62
63
18
17
NAV/GPS
AIRCRAFT POWER
AIRCRAFT POWER
AIRCRAFT GND
AIRCRAFT GND
5A (28 VDC)
ESSENTIAL BUS
AIRCRAFT
GROUND
7.5A (14 VDC)
20 AWG
20
19
78
77
AIRCRAFT POWER
AIRCRAFT POWER 43
30
AIRCRAFT GND
AIRCRAFT GND 38
37
44
40
P1003
5A (28 VDC)
ESSENTIAL BUS
10A (14 VDC)
AIRCRAFT POWER
AIRCRAFT GND
COM
LIGHTING BUS 2 LO
LIGHTING BUS 2 HI 61
42
P1004
AIRCRAFT POWER
AIRCRAFT POWER
AIRCRAFT GND
AIRCRAFT GND
52
51
62
61
20 AWG
20 AWG
AIRCRAFT
GROUND
20 AWG (5A C/B, 28VDC)
18 AWG (10A C/B, 14 VDC)
AIRCRAFT
GROUND
20 AWG (5A C/B, 28VDC)
18 AWG (10A C/B, 14 VDC)
20 AWG
3
3
3
4
6
8
5
7
Figure D-4. GTN Power Lighting Configuration Interconnect
Sheet 1 of 2
Summary of Contents for GTN 725
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