Illustration Index - Elite Simulation
Illustration Index - Elite Simulation
Illustration Index - Elite Simulation
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<strong>Elite</strong> Evolution S923 FNPT II MCC<br />
©1990 - 2010, <strong>Elite</strong> <strong>Simulation</strong> Solutions AG, all rights reserved<br />
January 2010<br />
section page 38 of 58<br />
version<br />
The engine monitoring system has the capability of depicting a realistic representation of<br />
engine operations.<br />
Propeller control and operation are realistically simulated. This includes full range of pitch<br />
control, feathering and propeller governing.<br />
6.3.3 Fuel System<br />
The aircraft fuel system is simulated in accordance with aircraft data. The effects of fuel<br />
depletion is simulated. Fuel quantity indicators are simulated from aircraft data.<br />
6.3.4 Pitot Static System<br />
The aircraft pitot static system is simulated in accordance with aircraft data.<br />
6.3.5 Landing Gear, Brakes and Nose Wheel Steering Systems<br />
The normal landing gear system controls, indicators and warning sounds are simulated<br />
according to the aircraft data.<br />
The simulated aircraft brake system has a realistic force feel and also represents<br />
asymmetrical brake functionality. Parking brake control is simulated.<br />
Nose wheel steering is simulated. Steering forces are felt by the pilot through the rudder<br />
pedals when using a dynamic control loading unit.<br />
6.3.6 Flight Control System<br />
The flight controls are installed for a two Pilot (dual yoke) operations in the Cockpit and<br />
correspond according to the available aircraft data. Realistic force feel and dynamic<br />
response is achieved from aircraft data.<br />
The simulation of trim for elevator, rudder and aileron is provided. Trim position indicators –<br />
Software and Hardware are present for elevator and rudder and reflect system operation.<br />
The aircraft flaps operation is simulated and affects the aircraft’s performance.<br />
6.4 Avionics / Radio System <strong>Simulation</strong><br />
6.4.1 General<br />
All avionics operate as they would in the actual aircraft, except as explained in this section.<br />
Avionics operation is limited by the capabilities of the <strong>Elite</strong> Evolution S923 navigation system.<br />
The avionics of the <strong>Elite</strong> Evolution S923 include the following:<br />
� Audio control Console / Intercom<br />
� NAV/COM Receivers (Bendix/King KX 165 - 25)<br />
� ADF (Bendix/King KR 87)<br />
� DME (Bendix/King KN 62A)<br />
� Transponder (Bendix/King KT 70)<br />
� Autopilot KFC 150<br />
� Apollo GPS GX50, GX55, GX60 and GX65 or<br />
3.1
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