Fully Authority Digital Engine Control Unit

The all-in-house-developed Engine Control Unit (ECU) is also configurable as a Full Authority Digital Engine Control Unit (FADEC). This product, made for low-power turbojet and turboprop engines, has completed MIL-STD qualification tests, over 1,000 hours of ground testing and over 100 hours of flight tests. It is qualified according to MIL-STD-461F for EMI/EMC and with MIL-STD-810G for environmental conditions.

Technical Features

• Isolated and ESD-protected interfaces (RS 422/485/232)
• EMI/EMC compatible with MIL-STD-461F
• Vibration and temperature resistance compatible with MIL-STD-810G
• Operating range between -40°C and +80°C
• In-device test and during operation test feature
• Data recording
• Configuration and debug modes
• Safety modes in case of failure
  • Temperature sensor error detection
  • Speed sensor error detection
  • Open-loop control mode
  • EGT hold mode
  • Transfer command standby mode