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Elite Evolution S923 FNPT II MCC ©1990 - 2010, Elite Simulation Solutions AG, all rights reserved January 2010 section page 36 of 58 6 Description of Simulation 6.1 Aerodynamic and Performance version The aerodynamic flight simulation will widely reproduce the flight characteristics of a twin engine aircraft. The simulation of the flight performance is based on an accurate mathematics model. Full consideration is given to all variable surfaces and their effects. Simulation does include: � Variation of aircraft longitudinal, lateral and directional stability with altitude, airspeed and gross weight � Stall characteristics � 1-Engine in op. characteristics � Ground handling characteristics 6.1.1 Wind Effects The effect of wind from any direction, at speeds from zero to sixty knots is realistically simulated and controlled by the instructor. The wind does show the correct effect on the ground track display during in-flight operation of the Elite Evolution S923 FNPT II MCC. 6.1.2 Atmosphere Variation of temperature, pressure and density with altitude does follow the ISA standard model. 6.1.3 On Ground Handling Simulation does include turning effects due to rudders, brakes and A/C wheel steering, representative flare and touch down effects. Also asymmetric thrust effects are simulated. 6.1.4 Take-Off and Climb-Out With parking brake set and applied power, proper aircraft pitch effects are simulated. During take-off, heading control is accomplished via the use of wheel steering and/or rudder. 6.1.5 Stalls There is full representation of the ”approach to stall” and the recovery from it. Stall is simulated by Cockpit instruments and associated flight characteristics. The influence of aircraft attitude, gross weight, configuration and altitude is also simulated. 6.1.6 One Engine Inoperative Performance Full representation of 1-Engine in op. characteristics and performance are implemented. 6.1.7 Landing The following is simulated during the landing phase: � Rate of descent versus speed, power setting and wind conditions � Control approach response 3.1
Elite Evolution S923 FNPT II MCC ©1990 - 2010, Elite Simulation Solutions AG, all rights reserved January 2010 section page 37 of 58 � Stall speeds in the approach and landing configuration � Ground roll and deceleration version Ground effects (including wind effects) and air to ground transients are simulated to the best available data, representative of the in-ground effect characteristics of the actual flight. 6.1.8 Instrument Responses Instrument responses to actual aircraft responses do reflect: � Aircraft slip and rate of turn � Rate of turn, as a function of bank angle and airspeed � Attitude, altitude, rate of climb and trim changes with gear position and flap setting changes � Pitch attitude, as a function of gross weight and airspeed 6.2 Radio Navigation Simulation 6.2.1 Radio Navigation Computation In order to execute the radio navigation simulation function, real world Navigation Databases are used. Periodical updates are available if necessary. Modification of existing and creation of new facilities are done using the modification page. Elite is updating on a regular basis the Navigation Database. However, the manufacturer cannot assure, that on the date of delivery, the Navigation Database is current. In case of an obsolete Navigation Database, the operator is asked to modify the facilities using Elite’s modification page. Alternatively, Elite can upload current Navigation data's via remote access to the customers FNPT II MCC device. 6.3 Aircraft Systems Simulation 6.3.1 Electrical System Changing the status of electricity consumers in the Cockpit (e. g. switching on / off Avionics panel) are reflected in the consumption of electricity. Should the aircraft’s electrical systems run on battery only without being constantly fed by the alternator, battery load will decrease. When running on Standby generator only Nav1 and Comm1 will work. 6.3.2 Engine System The engine and the associated controls and indicators are simulated as described in the aircraft data. The basis for the engine and aircraft model is a King Air B200. Simulation of the power plants include engine start on the ground and in the air, normal- and emergency handling, acceleration, deceleration and shut-down. Variations of the effects of altitude, airspeed and ambient temperature are included in the performance computations. Characteristics for the applicable engine and their effect on the flight path are reproduced in response to engine control selections. 3.1
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