Appareo Systems LLC 1505005 Benutzerhandbuch
600840-000031 Stratus ESG Installation Instructions
Rev. 1.1
Last Revised: January 6, 2016
Page 17 of 42
Additional parts:
Item
Appareo Part
Number
Commercial Part
Number
Quantity
#6-32 Self-Locking Nut
-
MS21042 or other
approved fastener
approved fastener
6
#6-32 x 100° Flat Head SS
Screw
Screw
-
MS24693, AN507R or
other approved
fastener
other approved
fastener
6
Table 11: Required hardware (additional parts)
1.11.
Compatible equipment
Stratus ESG requires input from a GPS antenna, transponder antenna, and altitude encoder.
This section describes the requirements for the antennas and altitude encoders that must be
installed on the aircraft.
This section describes the requirements for the antennas and altitude encoders that must be
installed on the aircraft.
Antennas
The GPS and transponder antennas
should be installed using the antenna manufacturer’s
instructions. Wiring must be installed in accordance with FAA AC 43.13-1B and AC 43.13-2B.
1.11.1.1. GPS antenna
Stratus ESG requires an active antenna with the specifications of either TSO-C190 or
TSO-C144.
TSO-C144.
If meeting the specifications of TSO-C190, the GPS antenna must meet the following:
Powered at 5 Volts
Gain of 30 dB +- 5 dB
Qualified DO-160E Lightning, Zone 2A
Qualified DO-160E Icing, Category C
Alternatively, the following TSO-C144 antenna is compatible:
Manufacturer
Part Number
AntCom
42G15A-XT-1
Table 12: Compatible GPS antenna
The antenna should be installed using the antenna manufacturer’s instructions. The antenna
must also be installed at least 2 feet away from any other comm transmitter or transmitter
antenna in a location that does not break line of sight with satellites. Typical installation
locations are on the top of the aircraft or on the empennage with consideration for line of sight
with satellites.
must also be installed at least 2 feet away from any other comm transmitter or transmitter
antenna in a location that does not break line of sight with satellites. Typical installation
locations are on the top of the aircraft or on the empennage with consideration for line of sight
with satellites.
All wiring should have a minimum of 3 dB loss and a maximum of 7 dB loss. Each BNC or TNC
connection is estimated to have a 0.2 dB loss.
connection is estimated to have a 0.2 dB loss.