Integrated Avionics System IAS

The Integrated Avionics System IAS comprises a full set of instruments for ultralight aircrafts. It combines the flight data and the engine data systems. It provides the pilot with the following information (depending on product configuration you choose):

  • air speed;
  • altitude;
  • vertical speed;
  • 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.

Please note that the composition of data depends on the product configuration you choose (sets). We offer a number of configurations that differ in the selection of data, in the form they are displayed, and in the design of displays (single displays AM1 or quadruple displays AM4). Thus, the system is composed of one to five displays and two measurements modules: EMS DAQ R02.01, and AUX AVS 2.

NOTE: The type and number of information presentation depends on the types of monitors that are included in the sets.


Sets currently on offer:


 

Set IAS AM1 01 GR01

The Integrated Avionics System version IAS AM1 01 GR01 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 € 1 900 + VAT rate 23%

Price VAT inclusive € 2 337


 

Set IAS AM1 01 GR02

The Integrated Avionics System version IAS AM1 01 GR02 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 € 1 900 + VAT rate 23%

Price VAT inclusive € 2 337


 

Set IAS AM1 01 AR01

The Integrated Avionics System version IAS AM1 01 AR01 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 € 1 900 + VAT rate 23%

Price VAT inclusive € 2 337

Set IAS AM4 01 AR02

The Integrated Avionics System version IAS AM4 01 AR02 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 € 1 640 + VAT rate 23%

Price VAT inclusive € 2 017.20


System components:


 

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.

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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 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 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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Connectors

Each set comes complete with a set of connectors for attaching displays to measurement modules.

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Display brightness potentiometer

The potentiometer is to be mounted in the instrument board. It enables the user to adjust brightness of all system displays.

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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 FL02.01

This instrument presents altitude, climb rate and reference pressure.

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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 FL01.01

This instrument presents air speed.

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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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Measurement Module AUX AVS 2

This module measures air speed, altitude and climb rate.

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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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Display type EEM MOT 01 FE01.03

This instrument presents flight and engine parameters.

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