600840-000031 Stratus ES/ESG Installation Instructions
Rev. 2.2
Last Revised: February 20, 2018
Page 20 of 45
2.6.
Circuit protective device marking
If Stratus ES/ESG is replacing an existing transponder, ensure that the circuit protective device
is sufficiently marked.
If Status ES/ESG is a new installation, ensure that the labeling is in accordance with AC 43.13-
2B, Chapter 2, Section 207, Sub-Section f., Paragraph (4).
3. Cabling and wiring
This section describes cabling and wiring specifications, pin-out information, and antenna and
GPS position source connection procedures.
3.1.
Cabling and wiring specifications
Wiring is not supplied by Appareo. Use 22 gauge wire and install wiring in accordance with FAA
AC 43.13-1B and AC 43.13-2B. Wire length and routing will vary by installation. See
Stratus ES/ESG Installation and Wiring Drawings (601837-000024) for exact specifications.
Re-use of existing wiring is permitted, but it must be in compliance with these installation
instructions and with the Stratus ES/ESG wiring diagrams.
NOTE:
Previously installed equipment may have additional components inline that could
impede the function of Stratus ES/ESG. Removal of those components is required.
CAUTION:
Remove aircraft power before wiring to avoid damaging the device.
3.2.
Pins
The following are the pin assignments and pin-out for Stratus ES/ESG.
NOTE:
Not all pins will be used for all configurations. See the sub-sections below to determine
which pins will be used for your installation.
Stratus ES
Stratus ESG
Pin #
Pin Name
I/O
Pin #
Pin Name
I/O
1
Aircraft Ground
-
1
Aircraft Ground
-
2
Aircraft Power
-
2
Aircraft Power
-
3
RS232-RX
External GPS input
In
3
RS232-RX Maintenance
In
4
-
-
4
-
-
5
RS232-RX Altitude
In
5
RS232-RX Altitude
In
6
RS232-TX GPS 1PPS
Out
6
RS232-TX GPS 1PPS
Out
7
External Standby
In
7
External Standby
In
8
Software Update Enable
In
8
Software Update Enable
In
9
Altitude A1
In
9
Altitude A1
In
