[fltsim.0] title=Giles G-300 fs9 sim=g3009m model= panel= sound= texture= checklists= ui_manufacturer=Acrotech description=Notes: [General] performance=Wingspan (ft) 22 \nLength (ft) 20.5 \nHeight (in) 67 \nEmpty Weight (lb) 1100 \nGross Weight (lb) 1400 \nPower (hp) 330+ \nStall Speed (kts)* 52 \nMaximum Speed (kts) 220 \nVertical Penetration, Vne (ft) 3000+ \nPilot Size Range 5' 2'' to 6' 4'' \nPilot Weight Range (lb) 100 to 245 \nFuel Capacity (US gal) 18 \n [pitot_static] vertical_speed_time_constant = 2 [WEIGHT_AND_BALANCE] max_gross_weight = 1600 empty_weight = 1025 reference_datum_position = 0, 0, 0 empty_weight_CG_position = -0.3, 0, 0 CG_forward_limit = 0 CG_aft_limit = 1 max_number_of_stations = 12 station_load.0 = 170, -3.1, 0, -0.5, Pilot empty_weight_pitch_MOI = 700 empty_weight_roll_MOI = 600 empty_weight_yaw_MOI = 950 empty_weight_coupled_MOI = 0 [flight_tuning] cruise_lift_scalar = 1 parasite_drag_scalar = 1 induced_drag_scalar = 1 elevator_effectiveness = 1 aileron_effectiveness = 3 rudder_effectiveness = 0.5 pitch_stability = 1 roll_stability = 1 yaw_stability = 1 elevator_trim_effectiveness = 1 aileron_trim_effectiveness = 1 rudder_trim_effectiveness = 1 hi_alpha_on_roll= 1 hi_alpha_on_yaw= 0.5 p_factor_on_yaw = 0.5 torque_on_roll = 0.5 gyro_precession_on_roll = 0.5 gyro_precession_on_yaw = 0.5 [GeneralEngineData] engine_type = 0 Engine.0 = 6, 0, 0 fuel_flow_scalar = 1 min_throttle_limit = 0 [piston_engine] power_scalar = 1 cylinder_displacement = 110 compression_ratio = 8 number_of_cylinders = 6 max_rated_rpm = 2900 max_rated_hp = 300 fuel_metering_type = 0 cooling_type = 0 normalized_starter_torque = 0.32 turbocharged = 1 max_design_mp = 0 min_design_mp = 0 critical_altitude = 0 emergency_boost_type = 0 emergency_boost_mp_offset = 0 emergency_boost_gain_offset = 0 fuel_air_auto_mixture = 0 auto_ignition = 0 max_rpm_mechanical_efficiency_scalar = 1 idle_rpm_mechanical_efficiency_scalar = 1 max_rpm_friction_scalar = 1 idle_rpm_friction_scalar = 1 [propeller] thrust_scalar = 1 propeller_type = 0 propeller_diameter = 8 propeller_blades = 3 propeller_moi = 11.0 beta_max = 40 beta_min = 15 min_gov_rpm = 1200 prop_tc = 0.1 gear_reduction_ratio = 1 fixed_pitch_beta = 0 low_speed_theory_limit = 80 prop_sync_available = 0 prop_deice_available = 0 prop_feathering_available = 0 prop_auto_feathering_available = 0 min_rpm_for_feather = 700 beta_feather = 1 power_absorbed_cf = 0 defeathering_accumulators_available = 0 prop_reverse_available = 0 minimum_on_ground_beta = 0 minimum_reverse_beta = 0 rotation = 1 [TailHook] tailhook_length = 4 tailhook_position = -15, 0, -1 cable_force_adjust = 1 [contact_points] max_number_of_points = 11 point.0 = 1, -10, 0, -2.0, 8000.000, 0.000, 0.238, 60.000, 0.300, 2.5, 0.800, 0.000, 0.000, 0.000, 0.000, 0.000 point.1 = 1, 1.0, -3, -4.58, 7600, 1, 0.709, 0, 0.323, 2.1, 0.8, 0, 0, 2, 0, 0 point.2 = 1, 1.0,3, -4.58, 7600, 2, 0.709, 0, 0.323, 2.1, 0.8, 0, 0, 3, 0, 0 point.3 = 1, 5.0, 3.5, -3.60, 7600, 0, 0.709, 0, 0.223, 2.1, 0.8, 0, 0, 2, 0, 0 point.4 = 1, 5.0,-3.5, -3.60, 7600, 0, 0.709, 0, 0.223, 2.1, 0.8, 0, 0, 3, 0, 0 point.5 = 1, 3.0, 12.5, -2.10, 7600, 0, 0.709, 0, 0.223, 2.1, 0.8, 0, 0, 2, 0, 0 point.6 = 1, 3.0,-12.5, -2.10, 7600, 0, 0.709, 0, 0.223, 2.1, 0.8, 0, 0, 3, 0, 0 point.7 = 2, 9.0, 0, -2, 9100, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.8 = 2, 2.8, 12.50, -1.5, 4100, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.9 = 2, 2.8, -12.50,-1.5, 4100, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.10 = 2, -10, 0, 3, 3100, 0, 0, 0, 0, 0, 0, 0, 0, 0 static_pitch= 12 static_cg_height= 5.0 gear_system_type = 1 tailwheel_lock = 1 [Views] eyepoint = -2.6, 0.0, 1.3 [flaps.0] //Trailing Edge Flaps type = 1 system_type = 4 [electrical] //BusType, MaxAmpLoad, MinVoltage max_battery_voltage=38.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=160.0 electric_always_available=0 [Radios] // availiable, standby frequency, has glide slope Com.1 =1,1 Transponder.1 =1 Marker.1 =0 [keyboard_response] elevator = 350, 500 aileron = 450, 1000 rudder = 200, 1000 [direction_indicators] direction_indicator.0 = 1, 0 [exits] number_of_exits = 1 exit_rate.0 = 0.4 [EFFECTS] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown=fx_tchdwn_s, 1 [autopilot] autopilot_available =0 [fuel] Center1 = 1.7, 0, 0, 25, 0 fuel_type = 1 number_of_tank_selectors = 1 electric_pump=0 [airplane_geometry] wing_area = 125 wing_span = 24.6 wing_root_chord = 6.276 wing_dihedral = 1 wing_incidence = 0 wing_twist = 0 oswald_efficiency_factor = 0.964 wing_winglets_flag = 0 wing_sweep = 0 wing_pos_apex_lon = 1.27 wing_pos_apex_vert = 0 htail_area = 12 htail_span = 7.6 htail_pos_lon = -10 htail_pos_vert = 0 htail_incidence = 0 htail_sweep = 0 vtail_area = 4 vtail_span = 3.5 vtail_sweep = 0 vtail_pos_lon = -10.5 vtail_pos_vert = 0 elevator_area = 12 aileron_area = 14 rudder_area = 5 elevator_up_limit = 27 elevator_down_limit = 20 aileron_up_limit = 26 aileron_down_limit = 22 rudder_limit = 35 elevator_trim_limit = 18 spoiler_limit = 0 spoilerons_available = 0 aileron_to_spoileron_gain = 0 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 [Reference Speeds] flaps_up_stall_speed = 50.4 full_flaps_stall_speed = 50.4 cruise_speed = 150 max_indicated_speed = 300 max_mach = 1.0 [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 = 500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 3250 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5 ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 750 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.075 ground_bumps_slope2 = 1 crash_magnitude1 = 10000 crash_direction1 = 1000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000 stick_shaker_magnitude = 5000 stick_shaker_direction = 0 stick_shaker_period = 111111 [brakes] toe_brakes_scale = 0.6408 parking_brake = 1 [stall_warning] // 0 = None, 1 = Suction, 2 = Electric. type = 1 [hydraulic_system] electric_pumps = 0 engine_map = 1, 0, 0, 0 normal_pressure = 1000 [attitude_indicators] // 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] // 0=None, 1=Electric Gyro, 2=Vacuum Gyro turn_indicator.0 = 1, 0 [direction_indicators] // 0=None, 1=Vac Gyro, 2=Elec Gyro, 3=EM Slave Compass, 4=Slave to other ind direction_indicator.0 = 1, 0 [airspeed_indicators] airspeed_indicator.0 = 1, 0 [smokesystem] smoke.0 = 0, 0, 0, fx_smoke_w.fx