Aircraft EFIS + EICAS Trainer

Description

Features

• This training system combines “Cockpit analog flight instrumentation”, “primary flight instrumentation”, “aircraft systems instrumentation” and “engine instrumentation”.
• The Trainer use Digital ADAHRS (Air Data and Attitude Heading and Reference Systems.
• “Air Data and Attitude Heading and Reference Systems” provide highly accurate and reliable referencing of aircraft position, rate, vector and acceleration data.
• Three degrees of freedom instrument panel permits full demonstration of attitude and directional gyro functions.
• Functional engine monitoring system be connected to engine sensors.
• All analog instruments operate manually
• Primary flight display be mounted on a panel that can simulate roll, pitch, and yaw movements controlled by a mechanism operated by a control yoke.
• Provision of engine sensor simulation.
• Pitot-static system to conduct pitot static system checks for digital instrument at the trainer.
• Instructor’s Panel for fault insertion.

Components

• Smart PFD-MFD Screen
• Engine Data Modules
• Sensors
  • Oil Temperature Sensor
  • Carburetor Air Temp Sensor
  • Manifold Pressure Sensor
  • Fuel Level Sensor
  • Oil Pressure Sensor
  • Fuel Pressure Sensor
  • Engine RPM Sensor
  • Fuel Flow Sensor
  • Ammeter Shunt
  • CHT Thermocouples (Qty 4)
  • EGT Thermocouples (Qty 4)
  • OAT Sensor • Pitot Tube
  • Static Port
  • Inductive sensor
• GPS receiver / antenna
• Aircraft circuit breakers
• Throttle Lever
• Propeller Lever
• Pitot-Static System:
  • Pitot Tube
  • Fuselage Static Port
  • Alternate Static Port
  • Static Source Selector Switch
  • Two Test Ports for Pitot-Static Test Set
• Power
  • Main Power
  • PDF
  • Tachometer
  • Vacuum Pump
• Contacts:
• • Pitot Heater
  • L/G
  • Taxi Light

Component Technical Specs

• Smart PFD-MFD Screen
  • NOTE: Smart PFD-MFD Screen brand/model and some technical specs can be change due to market availability ( Dynon-Bendix-Garmin or similar )
  • Screen is very bright and high-resolution driven by advanced graphics processors create highly visible and readable display.
  • Display is 1280 x 800 pixel, 1200+ nit TFT active-matrix capacitive multi- touch LCD screen.
  • High-Definition Touch Screen
  • Display Connectors Specification
• PFD-MFD Screen
• PFD Page Layout have at least the following:
• Airspeed Indicator
  • Ground Speed (GS)
  • True Airspeed (TAS)
• Airspeed Bug
• Airspeed Trend Rate
• Attitude Indicator
• Flight Path Marker
• Altimeter
  • Setting Barometer (BARO)
• Altitude Bug
• Altitude Trend Rate
• Barometer Setting, and Density Altitude
• Vertical Speed Indicator
• Vertical Speed (VS) BUG
• Heading Indicator/Directional Gyro