Engine Data System EDS

The Engine Data System EDS is a part of the Integrated Avionics System IAS, but may be used as an independent system to provide the pilot with basic information on:

  • engine speed;
  • rotor speed;
  • inlet air pressure;
  • inlet air temperature;
  • oil pressure;
  • oil temperature;
  • cylinder head temperature;
  • exhaust gas temperature;
  • supply voltage;
  • trim (pitch and roll) signal;
  • fuel level;
  • engine operation time;
  • total engine operation time (HOBBS).

 

The system was designed for comfortable use and straightforward mounting. Care was taken to provide maximum readability of the instruments’ displays. The system’s functions include automatic data analysis and recording to facilitate aircraft maintenance procedures. A detailed characteristics of the system’s properties is provided on the About system page.

We offer a number of configurations of the system. Depending on the configuration you choose, system would comprise one to four displays and the measurements module EMS DAQ R02.01.

PLEASE NOTE: the selection of data and the form they are displayed depends on the display types in the sets.


Sets currently on offer:


 

Set EDS AM1 GR01

The EDS AM1 GR01 Engine Data System is recommended for ultralight autogyros and helicopters equipped with ROTAX engines type 912 UL, ULS, 914, or their modifications. It comprises the following modules:

Module details are described below.

While placing order, please state units of measurement and threshold values for the flight and engine parameters applicable for your aircraft.

Price VAT exclusive € 999 + VAT rate 23%

Price VAT inclusive PLN 1 228.77


 

Set EDS AM1 GR02

The EDS AM1 GR02 Engine Data System is recommended for ultralight autogyros and helicopters equipped with ROTAX engines type 912 UL, ULS, 914, or their modifications. It comprises the following modules:

Module details are described below.

While placing order, please state units of measurement and threshold values for the flight and engine parameters applicable for your aircraft.

Price VAT exclusive € 999 + VAT rate 23%

Price VAT inclusive € 1 228.77


 

Set EDS AM1 AR01

The EDS AM1 GR02 Engine Data System is recommended for ultralight fixed-wing aircrafts equipped with ROTAX engines type 912 UL, ULS, 914, or their modifications. It comprises the following modules:

Module details are described below.

While placing order, please state units of measurement and threshold values for the flight and engine parameters applicable for your aircraft.

Price VAT exclusive € 999 + VAT rate 23%

Price VAT inclusive € 1 228.77


System components:


 

Display type EEM MOT 01 FE01.03

This instrument presents basic engine parameters: engine speed, cylinder head temperature (for two cylinders), and exhaust gas temperature (two points).

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Measurement Module EMS DAQ R2

This module measures engine operation parameters, and collects and records engine and airframe operation data.

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Display type EEM MOT 01 FE01.01

This instrument presents basic engine parameters: engine speed, inlet air pressure, oil pressure, and oil temperature.

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Display type EEM MOT 01 FE02.01

This instrument presents further data on engine operation: rotor speed, supply voltage, inlet air temperature, cylinder head temperature (for two cylinders), and exhaust gas temperature (two points).

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Display type EEM MOT 01 FE03.01

This instrument presents additional data of the aircraft: fuel level, two trimers’ positions, engine operation time and total engine operation time.

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Display type EEM MOT 01 FE01.02

This instrument presents basic engine parameters: engine speed, rotor speed, cylinder head temperature (for two cylinders), and exhaust gas temperature (two points).

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Display type EEM MOT 01 FE02.02

This instrument presents basic engine parameters: inlet air pressure, inlet air temperature, oil pressure, and oil temperature.

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Display type EEM MOT 01 FE03.02

This instrument presents additional data of the aircraft: fuel level, two trimers’ positions, voltage, engine operation time, total engine operation time, number of recorded threshold crossings.

Read more