[fltsim.0] title=Tornado_ADV-21° sim=Tornado_ADV-21° model= panel= sound= texture= checklists= ui_manufacturer=Panavia ui_type=ADV ui_variation=ADV 21° Tiger-Group. description=Tornado ADV is the Air Defence Variant of Tornado optimised for long range interception. Built by the Panavia consortium of three nations industries, British Aerospace-DASA (Germany)- Alenia (Italy).First flight, 27 October 1979.\nDesigner (visual FSDS model and texture): Giovanni Clemente. Country: Novara ITALY. Web: WWW.GIOCLEM:COM\nem@il: fsgioclem@virgilio.it Giugno 2002. Credit: Maxtac atc_heavy=0 atc_id= atc_airline= atc_flight_number= [forcefeedback] gear_bump_nose_magnitude=6000 gear_bump_nose_direction=18000 gear_bump_nose_duration=250000 gear_bump_left_magnitude=6000 gear_bump_left_direction=35500 gear_bump_left_duration=250000 gear_bump_right_magnitude=6000 gear_bump_right_direction=00500 gear_bump_right_duration=250000 ground_bumps_magnitude1=3250 ground_bumps_angle1=8900 ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ground_bumps_angle2=9100 ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 crash_direction1=01000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=2500000 [fltsim.1] Title= sim= Panel= Sound= texture= model= [fltsim.2] Title= sim= Panel= Sound= texture= model= [fltsim.3] Title= sim= Panel= Sound= texture= model= [fltsim.4] Title= sim= Panel= Sound= texture= model= [fltsim.5] Title= sim= Panel= Sound= texture= model= [fltsim.6] Title= sim= Panel= Sound= texture= model= [fltsim.7] Title= sim= Panel= Sound= texture= model= [fltsim.8] Title= sim= Panel= Sound= texture= model= [fltsim.9] Title= sim= Panel= Sound= texture= model= [WEIGHT_AND_BALANCE] reference_datum_position=0.000, 0.000, 0.000 empty_weight_CG_position=0.000, 0.000, 0.000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight=28000.000 empty_weight_roll_MOI=238163.000 empty_weight_pitch_MOI=270219.000 empty_weight_yaw_MOI=383883.000 empty_weight_coupled_MOI=1300.000 max_gross_weight=45420.000 CG_forward_limit=0.000 CG_aft_limit=1.000 [fuel] LeftMain=0.000, 0.000, 0.000, 1000.000, 0.000 LeftAux=0.000, 0.000, 0.000, 300.000, 0.000 RightMain=0.000, 0.000, 0.000, 1000.000, 0.000 RightAux=0.000, 0.000, 0.000, 300.000, 0.000 fuel_type=2.000 number_of_tank_selectors=1 [airplane_geometry] wing_area=525.000 wing_span=38.333 wing_root_chord=13.667 wing_dihedral=2.999 wing_incidence=-0.494 wing_twist=-1.000 oswald_efficiency_factor=0.750 wing_winglets_flag=0 wing_sweep=0.000 wing_pos_apex_lon=0.000 wing_pos_apex_vert=0.000 htail_area=80.000 htail_span=16.667 htail_pos_lon=-23.333 htail_pos_vert=0.000 htail_incidence=0.000 htail_sweep=0.000 vtail_area=60.000 vtail_span=8.832 vtail_sweep=0.000 vtail_pos_lon=-20.000 vtail_pos_vert=5.833 elevator_area=20.000 aileron_area=21.000 rudder_area=10.200 elevator_up_limit=27.502 elevator_down_limit=20.626 aileron_up_limit=19.481 aileron_down_limit=14.897 rudder_limit=23.491 elevator_trim_limit=19.481 spoiler_limit=59.989 spoilerons_available=0 aileron_to_spoileron_gain=0.000 min_ailerons_for_spoilerons=0.000 min_flaps_for_spoilerons=0.000 [contact_points] point.0=1.00, 12.75, 0.00, -7.20, 1574.80, 0.0, 0.780208,42.00, 0.45, 2.50, 0.90, 4.0, 4.0, 0.0, 200.00, 200.00 point.1=1.00, -5.917,-5.25, -7.05, 1574.80, 1.00,0.780208, 0.00, 0.50, 2.50, 0.85, 5.0, 5.0, 2.0, 200.00, 200.00 point.2=1.00, -5.917, 5.25, -7.05, 1574.80, 2.00,0.780208, 0.00, 0.50, 2.50, 0.85, 5.0, 5.0, 3.0, 200.00, 200.00 point.3=2.000000,-18.083333,-15.583333,-0.166667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.000000,-18.083333,15.583333,-0.166667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.000000,-24.250000,0.000000,-2.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,26.750000,0.000000,-2.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 static_pitch=0.000 static_cg_height=7.259 [GeneralEngineData] engine_type=1 Engine.0=-13.333, -2.500, -1.667 Engine.1=-13.333, 2.500, -1.667 fuel_flow_scalar=1.000 [TurbineEngineData] fuel_flow_gain=0.002 inlet_area=21.520 rated_N2_rpm=29920.000 static_thrust=17933.300 afterburner_available=0 reverser_available=1 [Reference Speeds] flaps_up_stall_speed=120.000 full_flaps_stall_speed=96.000 cruise_speed=756.622 [keyboard_response] elevator=150.000, 250.000 aileron=150.000, 250.000 rudder=150.000, 250.000 [Views] eyepoint=13.561, 0.00, 3.373 [General] performance=Length:18.68m Span:min 8.60 m \/ max 13.91 m\nWeight: MTOW 27986 kg - Empty 14502 kg\nPower:2 Turbo Union RB-199 Turbofan\nDesigner (visual FSDS model and texture): Giovanni Clemente. Country: Novara ITALY. Web: WWW.GIOCLEM:COM\nem@il: fsgioclem@virgilio.it Febbraio 2002. Credit: Maxtac for the spectacular mouving parts. WWW.MAXTAC.IT \n\n atc_type= atc_model= [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=1800.000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000 pitch_takeoff_ga=8.000 [Flaps.0] type=1 span-outboard=0.500000 extending-time=5.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=15.996982,0.000000 flaps-position.2=39.992454,0.000000 [smokesystem] smoke.0=-1.00, -2.00, 3.750, fx_smoke_rx smoke.1=-1.00, -2.00, -3.750, fx_smoke_rx [LIGHTS] //types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing //(feet) longitudinal, lateral, vertical distance from reference datum light.0=3, 5.817, 5.840, 1.462, fx_navgreh , light.1=3, 5.817, -5.840, 1.462, fx_navredh , light.2=3,-30.273, 0.073, 11.941, fx_navwhih , light.3=3,-30.273, -0.073, 11.941, fx_navwhih , light.4=1, 7.850, 0.00, -2.845, fx_beaconh , light.5=1, -2.388, 0.00, 4.207, fx_beaconh , [direction_indicators] direction_indicator.0=3,0