[fltsim.0] title=Heli Agusta 109 Vistas Pint ge-gr sim=Heli Agusta 109 Vistas visual_damage=1 prop_anim_ratio=1.41 model= panel= sound= texture=ge-gr kb_checklists= atc_id=D-HHBE ui_manufacturer=Aerospitale ui_type="Agusta A109" ui_variation="AirStar Helicopters" description=Grand Canyon Sightseeing - AirStar Helicopters [General] atc_type=Aerospitale editable=1 performance=keine Angaben atc_model=Agusta A1 [turboprop_engine] power_scalar=50.0 [propeller] thrust_scalar=9.0 propeller_type=1 propeller_diameter=6.883000 propeller_blades=4 propeller_moi=5.706520 beta_max=0.000000 beta_min=15.000000 min_gov_rpm=0.000000 prop_tc=0.100000 gear_reduction_ratio=1.000000 fixed_pitch_beta=20.000000 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.000000 beta_feather=0.000000 power_absorbed_cf=0.000000 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000 //Dampers are set to our mormal standards of flight [ground_reaction] //main_gear_static_compression = 5.2 // (feet), The distance the main gear strut is compressed when at rest on the ground center_gear_static_compression = 5.2 // (feet), The distance the center gear strut is compressed when at rest on the ground //main_gear_damping_ratio = 0.7 // Main gear strut damping, 0 = undamped osciallations, 1 = critically damped center_gear_damping_ratio = 1.0 // Center gear strut damping, 0 = undamped osciallations, 1 = critically damped [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= 1000.000 empty_weight_roll_MOI= 4000.000 empty_weight_pitch_MOI= 6000.000 empty_weight_yaw_MOI= 10000.000 empty_weight_coupled_MOI= 1200.000 max_gross_weight= 8250.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [fuel] Center1= 0.000, 0.000, 0.000, 91.000, 0.000 fuel_type=2.000 number_of_tank_selectors=1 electric_pump=0 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) avionics_bus=0, 10, 17.0 avionics=1, 5 , 17.0 gear_motor=0, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 20, 17.0 marker_beacon=1, 2 , 17.0 fuel_pump=0, 5 , 17.0 starter1=0, 20, 17.0 light_nav=0, 5 , 17.0 light_beacon=0, 5 , 17.0 light_landing=0, 5 , 17.0 light_taxi=0, 5 , 17.0 light_strobe=0, 5 , 17.0 light_panel=0, 5 , 17.0 //1 Class <0=none,1=wheel, 2=scrape, 3=skid> //1 Longitudinal Position (feet) //2 Lateral Position (feet) //3 Vertical Position (feet) //4 Impact Damage Threshold (Feet Per Minute) //5 Brake Map (0=None, 1=Left, 2=Right) //6 Wheel Radius (feet) //7 Steer Angle (degrees) //8 Static Compression (feet) (0 if rigid) //9 Max/Static Compression Ratio //10 Damping Ratio (0=Undamped, 1=Critically Damped) //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) [contact_points] point.0= 1.000, 3.000, 0.000, -3.100, 2200.000, 0.000, 0.400, 45.000, 0.500, 0.750, 0.850, 4.000, 4.000, 0.000, 0.000, 0.000 point.1= 1.000, -2.900, -4.110, -3.100, 2200.000, 1.000, 0.500, 0.000, 0.500, 0.750, 0.850, 4.000, 4.000, 0.000, 0.000, 0.000 point.2= 1.000, -2.900, 4.110, -3.100, 2200.000, 2.000, 0.500, 0.000, 0.500, 0.750, 0.850, 4.000, 4.000, 0.000, 0.000, 0.000 point.3 = -2.30, -3.74, -1.96, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.4 = -2.30, 3.61, -1.96, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.5 = 9.46, 0.10, -1.89, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.6 = -2.18, -3.74, -3.30, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.7 = -2.18, 3.61, -3.30, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.8 = 9.58, 0.10, -3.24, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.9 = -2.18, -3.74, -2.87, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.10 = -2.18, 3.61, -2.87, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.11 = 9.58, 0.10, -2.81, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.12 = -2.18, -3.74, -2.87, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.13 = -2.18, 3.61, -2.87, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.14 = 9.58, 0.10, -2.81, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.15 = -2.18, -3.74, -2.87, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.16 = -2.18, 3.61, -2.87, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.17 = 9.58, 0.10, -2.81, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.18 = -2.18, -3.74, -2.87, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.19 = -2.18, 3.61, -2.87, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.20 = 9.58, 0.10, -2.81, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.21 = -2.18, -3.74, -2.87, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.22 = -2.18, 3.61, -2.87, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.23 = 9.58, 0.10, -2.81, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 static_cg_height= 2.843 static_pitch = -0.298 gear_system_type=0 [Views] eyepoint= 5.95, 1.00, 2.06 //(feet) longitudinal, lateral, vertical distance from reference datum [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 1 Com.2=0, 0 Nav.1=1, 1, 1 Nav.2=0, 1, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [keyboard_response] elevator=100.000, 180.000 aileron=200.000, 1000.000 rudder=200.000, 1000.000 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0 = 3, -15.7, -4.4, 2.0, fx_navred , light.1 = 3, -15.7, 4.4, 2.0, fx_navgre , light.2 = 3, -22.5, 0.0, 8.4, fx_navwhi, light.3 = 1, -22.5, 0.0, 8.4, fx_beacon , light.4 = 4, -22.5, 0.0, 8.4, fx_vclight , light.5 = 2, -22.5, 0.0, 8.4, fx_beacon , light.6 = 4, 0.0, 0.0, -1.9, fx_vclight , light.7 = 3, -1.5, 0.0, -1.9, fx_beacon , light.8 = 2, -1.5, 0.0, -1.9, fx_beacon , light.9 = 2, -2.0, 0.0, -1.9, fx_strobe , [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type= 3 Engine.0= 0.000, 0.000, 3.300 fuel_flow_scalar=1.000 min_throttle_limit=0.000000 [Reference Speeds] flaps_up_stall_speed=54.000 full_flaps_stall_speed=43.200 cruise_speed=0.000 max_indicated_speed=190.000000 [SMOKESYSTEM] smoke.0= 0.00, -5.00, -4.00, fx_flare smoke.1= 0.00, -5.00, 4.00, fx_flare [exits] number_of_exits=2 exit_rate.0=0.8 exit_rate.1=0.8 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=1800.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 [direction_indicators] direction_indicator.0=3,0 [brakes] toe_brakes_scale=1.000031 parking_brake=0 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [hydraulic_system] normal_pressure=0.000000 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0