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
- PFD Screen
- MFD Screen
- Engine Data Modules
- Analog instruments
- Attitude Gyro and Indicator
- Directional Gyro / Heading Indicator
- Airspeed Indicator
- Altimeter
- Vertical Speed Indicator
- Turn and Slip Indicator
- Fuel Temp/Press Indicator
- Oil Temp/Press Indicators
- Fuel Level Indicator
- MAP
- RPM
- Vacuum Gauge
- Sensors
- Oil Temperature Sensor
- Carburator 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
- 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
- Tachometer
- Turn&Slip
- Vacuum Pump
- Contacts:
- Pitot Heater
- L/G
- Taxi Light
- Auxiliary Flight Control:
- Aileron Trim
- Elevator Trim
- Flap Position
- Electronic Simulation of Sensors:
- Oil Temperature Manifold Pressure
- Engine RPM • Oil Pressure
- Fuel Level
- Fuel Press
- Sender Selector Panel
- Fuel System
- Oil System
- Vacuum Control Panel
- Static System Instrument
- MAP
- Fuel Flow
Component Technical Specs
- 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
