[fltsim.0] title=Robin HR200 sim=hr200 model= panel= sound= texture= kb_checklists= kb_reference= atc_id=N20TMB ui_manufacturer=Robin ui_type=HR200 ui_variation=Private description=" " atc_heavy=0 atc_airline= atc_flight_number= atc_id_color=0x00000000 atc_id_font=Verdana,-11,1,600,0 visual_damage=0 [General] atc_type=ROBINSON atc_model= editable=1 performance=Speed: 260 km/h 140 kts; Service Ceiling: 5.000 m 16.404 ft; Range: 935 km 505 nm. Category=airplane [weight_and_balance] // ACM V2.5 max_gross_weight = 1670.00 empty_weight = 1100.00 reference_datum_position = 0.00, 0.00, 0.00 empty_weight_CG_position = 0.00, 0.00, 0.00 empty_weight_pitch_MOI = 1900.00 empty_weight_roll_MOI = 800.00 empty_weight_yaw_MOI = 1600.00 empty_weight_coupled_MOI = 0.00 CG_forward_limit = 0.00 CG_aft_limit = 1.00 max_number_of_stations = 2 station_load.0 =170.00, 0.00, -1.50, 0.00, Pilot station_load.1 =170.00, 0.00, 1.50, 0.00, Station 2 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, 0.76, -13.66, 0.31, fx_navred , light.1 = 3, 0.76, 13.66, 0.31, fx_navgre , light.2 = 2, -5.79, 0.00, 2.21, fx_strobe , light.3=4, 0.50, 0.00, 2.40, fx_vclight [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 0 fuel_flow_scalar = 1.00 min_throttle_limit = 0.0 engine.0 = 5.50, 0.00, 0.90 [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn_s, 1 windshield_rain_effect_available = 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 1 number_of_tank_selectors = 1 electric_pump = 1 LeftMain= 0.00, -5.00, 0.00, 15.00, 0.00 RightMain= 0.00, 5.00, 0.00, 15.00, 0.00 [contact_points] static_pitch = 0.00 static_cg_height = 2.80 tailwheel_lock = 0 gear_system_type = 4 max_number_of_points = 17 point.0=1, 4.00, 0.00, -2.80, 1200.00, 0.00, 0.50, 35.00, 0.12, 2.50, 0.80, 0.00, 0.00, 0.00, 0.00, 0.00 point.1=1, -1.00, -4.50, -2.80, 1600.00, 1.00, 0.50, 0.00, 0.15, 2.50, 0.80, 0.00, 0.00, 2.00, 0.00, 0.00 point.2=1, -1.00, 4.50, -2.80, 1600.00, 2.00, 0.50, 0.00, 0.15, 2.50, 0.80, 0.00, 0.00, 3.00, 0.00, 0.00 point.3=2, -0.50, -13.60, 0.30, 1574.80, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00, 0.00, 0.00 point.4=2, -0.50, 13.60, 0.30, 1574.80, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 6.00, 0.00, 0.00 point.5=2, -13.90, 0.00, -0.30, 1574.80, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 9.00, 0.00, 0.00 point.6=2, 6.80, 0.00, 0.90, 1574.80, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00 [keyboard_response] elevator = 100, 180 aileron = 100, 200 rudder = 100, 200 [forcefeedback] gear_bump_nose_magnitude = 3000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 2700 gear_bump_left_direction = 35500 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 2700 gear_bump_right_direction = 00500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 1300 ground_bumps_angle1 = 08900 ground_bumps_intercept1 = 3.0 ground_bumps_slope1 = 0.20 ground_bumps_magnitude2 = 200 ground_bumps_angle2 = 09100 ground_bumps_intercept2 = 1.075 ground_bumps_slope2 = 0.035 crash_magnitude1 = 10000 crash_direction1 = 01000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000 [airplane_geometry] wing_area = 135.00 wing_span = 27.50 wing_root_chord = 4.30 wing_dihedral = 4.50 wing_incidence = 2.00 wing_twist = -1.00 oswald_efficiency_factor = 0.70 wing_winglets_flag = 0 wing_sweep = 0.00 wing_pos_apex_lon = 1.30 wing_pos_apex_vert = -0.80 htail_area = 24.00 htail_span = 10.20 htail_pos_lon = -10.50 htail_pos_vert = 0.40 htail_incidence = 0.00 htail_sweep = 0.00 vtail_area = 10.00 vtail_span = 2.80 vtail_sweep = 37.00 vtail_pos_lon = -10.80 vtail_pos_vert = 1.40 elevator_area = 20.00 aileron_area = 9.00 rudder_area = 6.00 elevator_up_limit = 20.00 elevator_down_limit = 16.00 aileron_up_limit = 20.00 aileron_down_limit = 15.00 rudder_limit = 24.00 elevator_trim_limit = 15.00 spoiler_limit = 0.00 aileron_to_spoileron_gain = 0.00 spoiler_handle_available = 0 min_ailerons_for_spoilerons = 0.00 min_flaps_for_spoilerons = 0.00 spoilerons_available = 0 auto_spoiler_available=0 positive_g_limit_flaps_up=6.000000 positive_g_limit_flaps_down=4.000000 negative_g_limit_flaps_up=-4.500000 negative_g_limit_flaps_down=-3.500000 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 60 engine_generator_map = 1 electric_always_available = 0 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 5, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 2, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 17 light_nav = 0, 5, 17 light_beacon = 0, 5, 17 light_landing = 0, 5, 17 light_taxi = 0, 5, 17 light_strobe = 0, 5, 17 light_panel = 0, 5, 17 [pitot_static] vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI pitot_heat=1.000000 [flight_tuning] cruise_lift_scalar=1.00 parasite_drag_scalar=1.00 induced_drag_scalar=1.00 elevator_effectiveness=1.00 aileron_effectiveness=1.00 rudder_effectiveness=1.00 pitch_stability=1.00 roll_stability=1.00 yaw_stability=1.00 elevator_trim_effectiveness=1.00 aileron_trim_effectiveness=1.00 rudder_trim_effectiveness=1.00 [piston_engine] power_scalar=1.00 cylinder_displacement= 80.00 compression_ratio= 8.00 number_of_cylinders= 4 max_rated_rpm= 2675.00 max_rated_hp= 160.0 fuel_metering_type= 0 cooling_type= 0 normalized_starter_torque= 0.30 turbocharged= 0 max_design_mp= 0.00 min_design_mp= 0.00 critical_altitude= 0.00 emergency_boost_type= 0 emergency_boost_mp_offset= 0.00 emergency_boost_gain_offset= 0.00 fuel_air_auto_mixture= 0 auto_ignition= 0 max_rpm_mechanical_efficiency_scalar=1.00 idle_rpm_mechanical_efficiency_scalar=1.00 max_rpm_friction_scalar=1.00 idle_rpm_friction_scalar=1.00 [propeller] thrust_scalar=1.00 propeller_type= 1 propeller_diameter= 6.00 propeller_blades= 2 propeller_moi= 4.00 beta_max= 0 beta_min= 0 min_gov_rpm=0.00 prop_tc= 0.10 gear_reduction_ratio= 1.00 fixed_pitch_beta= 20.00 low_speed_theory_limit= 80.00 prop_sync_available= 0 prop_deice_available= 1 prop_feathering_available= 0 prop_auto_feathering_available= 0 min_rpm_for_feather= 0.00 beta_feather= 0.00 power_absorbed_cf= 0.00 defeathering_accumulators_available= 0 prop_reverse_available= 0.00 minimum_on_ground_beta= 0.00 minimum_reverse_beta= 0.00 [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 0.0 //Flap angle that activates warning at idle flap_limit_power = 16.0 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 1.0 //Brake scalar [hydraulic_system] normal_pressure = 0.0 //PSI [Views] eyepoint=-0.20, 0.80, 2.40 [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [direction_indicators] //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another //2 Indicator number of slaving indicator if Type = 4 direction_indicator.0=1,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=1,1 //Turn AND Bank [Reference Speeds] flaps_up_stall_speed= 60.00 full_flaps_stall_speed= 50.00 cruise_speed= 126.00 //116 knots indicated at 5,000 ft. max_indicated_speed = 160 //Red line (KIAS) max_level_speed=138 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=500.0 autothrottle_available=0 pitch_takeoff_ga=8.0 max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=9.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain = 0.0 [stall_warning] type=2 stick_shaker=1 [Flaps.0] type= 1 span-outboard= 0.60 extending-time= 3.00 system_type= 0 damaging-speed= 250.00 blowout-speed= 300.00 lift_scalar= 1.00 drag_scalar= 1.00 pitch_scalar= 0.50 flaps-position.0= 0.00, 0.00 flaps-position.1= 15.00, 0.00 flaps-position.2= 30.00, 0.00 [vacuum_system] max_pressure=5.15 vacuum_type=1 electric_backup_pressure=4.90 engine_map=1,0,0,0 [pneumatic_system] max_pressure=0.00 bleed_air_scalar=0.00 [deice_system] structural_deice_type=0
