600840-000031 Stratus ES/ESG Installation Instructions
Rev. 2.1
Last Revised: June 22, 2017
Page 21 of 44
18
External GPS Common
Ground
-
18
AUX Ground
-
19
AUX +5V Power
Out
19
AUX +5V Power
Out
20
Aircraft Ground
-
20
Aircraft Ground
-
21
Aircraft Power
-
21
Aircraft Power
-
22
RS232-TX Maintenance
Out
22
RS232-TX Maintenance
Out
23
RS232-TX AUX
Out
23
RS232-TX AUX
Out
24
RS232-TX Altitude
Out
24
RS232-TX Altitude
Out
25
External IDENT
In
25
External IDENT
In
26
External Squat Switch
In
26
External Squat Switch
In
27
Altitude D4
In
27
Altitude D4
In
28
Altitude A2
In
28
Altitude A2
In
29
Altitude B1
In
29
Altitude B1
In
30
Altitude B4
In
30
Altitude B4
In
31
Altitude C2
In
31
Altitude C2
In
32
External Suppress I/O
I/O
32
External Suppress I/O
I/O
33
14V Lighting Bus HI
In
33
14V Lighting Bus HI
In
34
-
-
34
-
-
35
-
-
35
-
-
36
Aux +5V Power
Out
36
Aux +5V Power
Out
37
Altitude Common (GND)
-
37
Altitude Common (GND)
-
Table 14: Pin assignments
Figure 2: Pin-out
Refer to the wiring diagrams in Stratus ES/ESG Installation and Wiring Drawings (601837-
000024) to complete wiring. The sections below describe the function of each pin in more detail.
Power
Stratus ES/ESG requires a 5 amp circuit breaker. A minimum of 2 ground pins should be tied.
Pin #
Pin Name
I/O
1
Aircraft Ground
-
2
Aircraft Power
-
20
Aircraft Ground
-
21
Aircraft Power
-
Table 15: Power pin assignments
