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Dynon Avionics SkyView Classic - Example Engine Sensor and Transducer Installations

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SV-EMS-220/221 Installation and Configuration
7-20 SkyView System Installation Guide - Revision AA
this section are designed to not exceed these current limitations. However, more complex and
installations that differ significantly from these standard installations should be designed to not
exceed the following current limitations:
EMS
Module
Output
Pin
Output
Current
Limit
Wire Color
Current Draw of Sensors that Use This Output
12V
15
80mA
Red
FloScan Fuel Flow Sensor (100403-001): 50mA
EI Fuel Flow Sensor P/N 100403-003: 15mA
UMA Differential Fuel Pressure: 10mA
Rotax Honeywell Oil Pressure Sensor: 20mA
Rotax Oil Pressure Sensor P/N 456180: 20mA
Dynon Avionics Capacitance to Voltage
Converter: 25mA
5V
18
300mA
(Limited
by
internal
self-
resetting
fuse)
White/Red
Kavlico pressure sensors: 5mA
3
rd
party trim and flaps position: 5mA
Manifold pressure sensor P/N 100434-000:
10mA
Table 32 EMS Module Current Draw Limits for 12V (Pin 15) and 5V (Pin 18) Outputs
Example Engine Sensor and Transducer Installations
This section contains example engine sensor and transducer installations for popular engines.
Each engine subsection listed on the following pages contains tables for each SV-EMS-220/221
connector and suggests a way to connect that engine’s required sensors to the EMS module.
These tables are based on the downloadable mapping and settings files available from Dynon
Avionics’ support forums and may need to be modified based on your particular installation.

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