Analogue Cockpit Instrumentation System Trainer

quick overview :

Features:

1. The system combines Cockpit analog flight instrumentation and engine instrumentation.
2. Three degrees of freedom instrument panel permits full demonstration of attitude and directional gyro functions.
3. Functional engine instrumentation system be connected to engine sensors.
4. All analog instruments operate manually
5. 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.
6. Provision of engine sensor simulation.
7. Pitot-static system.
8. Instructor’s Panel for fault insertion

Components:

1. Analog instruments
• Attitude Gyro and Indicator
• Directional Gyro / Heading Indicator
• Airspeed Indicator
• Altimeter
• Vertical (Upload speed) Speed Indicator
• Turn and Slip Indicator
• Fuel Temp/Press Indicator
• Oil Temp/Press Indicators
• Fuel Level Indicator
• MAP
• RPM / engine tachometer
• Vacuum Gauge
2. Sensors:
• Oil Temperature Sensor
• Manifold Pressure Sensor
• Fuel Level Sensor
• Oil Pressure Sensor
• Fuel Pressure Sensor
• Engine RPM Sensor
• Ammeter Shunt
• Pitot Tube
• Static Port
3. Aircraft circuit breakers.
4. Throttle Lever
5. Pitot-Static System:
• Pitot Tube
• Fuselage Static Port
• Alternate Static Port
• Static Source Selector Switch
• Two Test Ports for Pitot-Static Test Set
6. Power
• Main Power
• Tachometer
• Turn & Slip
• Vacuum Pump