[fltsim.0] title=H-295 sim=H-295 model = panel = sound = texture = panel_alias = sound_alias = kb_checklists = kb_reference = atc_id =N6295P atc_id_color = atc_parking_types = atc_parking_code = ui_manufacturer = Helio Aircraft ui_type = H-295 Super Courier ui_variation = U.S. Civil Register description = Rugged and dependable, the H-295 series Super Courier first flew in 1958, and also entered U.S. military use as the U-10. Combining large flaps, slats, and spoilers, the Courier could use the smallest of strips. [fltsim.1] title=U-10B sim=H-295 model =u10b panel =u10b sound = texture =u10b panel_alias = sound_alias = kb_checklists = kb_reference = atc_id = B-857 atc_id_color = atc_parking_types = atc_parking_code = ui_manufacturer = Helio Aircraft ui_type = U-10B Super Courier ui_variation = Air America description = Rugged and dependable, the H-295 series Super Courier first flew in 1958, and also entered U.S. military use as the U-10. Combining large flaps, slats, and spoilers, the Courier could use the smallest of strips. [General] atc_type = atc_model = editable = 1 visual_damage=1 performance = + Empty Weight: 2480 lbs + Max Power: 295 Hp + Maneuver speed: 113 mph @ 5.0 g + Max speed: 167 mph @ 8500 ft + Max speed at sea-level: 166 mph + Climb rate: 1150 ft/min @ 84 mph Flight Dynamics By: Tim Piglet Conrad Piglet's Peculiar Planes FD Build 3 - 11/11/04 04:24 AM Flight Dynamics Workbook V2.84.63 [pitot_static] vertical_speed_time_constant = 2 [WEIGHT_AND_BALANCE] max_gross_weight = 3400 empty_weight = 2080 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 CG_forward_limit = 0 CG_aft_limit = 1 max_number_of_stations = 4 station_load.0 = 200, 0, 0, 0, Pilot station_load.1 = 200, 0, 0, 0, co-pilot station_load.2 = 0, 0, 0, 0 station_load.3 = 0, 0, 0, 0 empty_weight_pitch_MOI = 6389 empty_weight_roll_MOI = 3250 empty_weight_yaw_MOI = 7343 empty_weight_coupled_MOI = 0 [flight_tuning] cruise_lift_scalar = 1 parasite_drag_scalar = 1 induced_drag_scalar = 1 elevator_effectiveness = 1 aileron_effectiveness = 1 rudder_effectiveness = 1 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 = 1 p_factor_on_yaw = 1 torque_on_roll = 1 gyro_precession_on_roll = 1 gyro_precession_on_yaw = 1 [GeneralEngineData] engine_type = 0 Engine.0 = 8.13, 0, 0 fuel_flow_scalar = 1 min_throttle_limit = 0 [piston_engine] power_scalar = 1 cylinder_displacement = 80 compression_ratio = 8.7 number_of_cylinders = 6 max_rated_rpm = 3000 max_rated_hp = 295 fuel_metering_type = 1 cooling_type = 1 normalized_starter_torque = 0.31 turbocharged = 0 max_design_mp = 29.9 min_design_mp = 9 critical_altitude = 8500 emergency_boost_type = 0 emergency_boost_mp_offset = 0 emergency_boost_gain_offset = 0 fuel_air_auto_mixture = 0 auto_ignition = 0 emergency_boost_duration = 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 = 14 beta_max = 65 beta_min = 15 min_gov_rpm = 450 prop_tc = 0.01 gear_reduction_ratio = 1.3 fixed_pitch_beta = 25 low_speed_theory_limit = 73.9697223927095 prop_sync_available = 0 prop_deice_available = 1 prop_feathering_available = 0 prop_auto_feathering_available = 0 min_rpm_for_feather = 700 beta_feather = 88.5 power_absorbed_cf = 0.9 defeathering_accumulators_available = 0 prop_reverse_available = 0 minimum_on_ground_beta = 1 minimum_reverse_beta = -14 rotation = 1 [TailHook] tailhook_length = 1 tailhook_position = 0, 0, -1 cable_force_adjust = 1 [contact_points] max_number_of_points = 6 point.0 = 1, -20, 0, -0.388, 2574.8, 0, 0.45, 45, 0.25, 2.5, 0.88, 0, 0, 0, 0, 0 point.1 = 1, 3.19, -4.622, -6.50, 2574, 1, 0.9, 0, 0.55, 2.5, 0.88, 0, 0, 2, 0, 0 point.2 = 1, 3.19, 4.622, -6.50, 2574, 2, 0.9, 0, 0.55, 2.5, 0.88, 0, 0, 3, 0, 0 point.3 = 2, -0.07, -19.05, 2.68, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 5 point.4 = 2, -0.07, 19.05, 2.68, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 6 point.5 = 2, 1.65, 0, -2.6, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 4 static_pitch= 14 static_cg_height= 6.0 gear_system_type = 1 tailwheel_lock = 1 [Views] eyepoint= -0.175, -0.794, 1.564 [flaps.0] //Trailing Edge Flaps type = 1 span-outboard = 0.75 extending-time = 5 flaps-position.0 = 0 flaps-position.1 = 11, 111 flaps-position.2 = 22, 106 flaps-position.3 = 33, 101 flaps-position.4 = 45, 97 damaging-speed = 111 blowout-speed = 120 system_type = 3 lift_scalar = 0 drag_scalar = 0 pitch_scalar = 1 [flaps.1] //Leading Edge Flaps type = 2 span-outboard = 0.75 extending-time = 5 flaps-position.0 = 0 flaps-position.1 = 11 flaps-position.2 = 22 flaps-position.3 = 33 flaps-position.4 = 45 damaging-speed = 111 blowout-speed = 120 system_type = 3 lift_scalar = 1 drag_scalar = 0 pitch_scalar = 0 [flaps.2] //Leading Edge Flaps type = 2 span-outboard = 0.75 extending-time = 5 flaps-position.0 = 0 flaps-position.1 = 11 flaps-position.2 = 22 flaps-position.3 = 33 flaps-position.4 = 45 damaging-speed = 111 blowout-speed = 120 system_type = 3 lift_scalar = 0 drag_scalar = 1 pitch_scalar = 0 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 50 electric_always_available = 0 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 10, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 20, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 17 starter2 = 0, 20, 17 starter3 = 0, 20, 17 starter4 = 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 prop_sync = 0, 15, 17 auto_feather = 0, 15, 17 auto_brakes = 0, 15, 17 standby_vacuum = 0, 15, 17 hydraulic_pump = 0, 2, 17 fuel_transfer_pump = 0, 5, 17 propeller_deice = 0, 5, 17 light_recognition = 0, 5, 17 light_wing = 0, 5, 17 light_logo = 0, 5, 17 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0 = 3, 0.07, -19.62, 2.91, fx_navred light.1 = 3, 0.07, 19.62, 2.91, fx_navgre light.2 = 1, -12.81, 0, 2.62, fx_beacon light.3 = 4, 0, 0, 0, fx_vclight_yellow [Radios] // availiable, standby frequency, has glide slope Audio.1 = 1 Com.1 = 1, 1 Com.2 = 1, 1 Nav.1 = 1, 1, 1 Nav.2 = 1, 1, 0 Adf.1 = 1 Transponder.1 = 1 Marker.1 = 1 [keyboard_response] elevator = 350, 500 aileron = 450, 1000 rudder = 200, 1000 [direction_indicators] direction_indicator.0 = 1, 0 [exits] number_of_exits = 2 exit_rate.0 = 0.8 exit_rate.1 = 0.8 [EFFECTS] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn, 1 [autopilot] autopilot_available = 1 flight_director_available = 0 default_vertical_speed = 1000 autothrottle_available = 0 autothrottle_arming_required = 0 autothrottle_max_rpm = 90 autothrottle_takeoff_ga = 1 pitch_takeoff_ga = 8 max_pitch_velocity_hi_alt = 1.5 max_pitch_velocity_lo_alt_breakpoint = 20000 max_pitch_velocity_hi_alt_breakpoint = 28000 max_pitch = 10 max_pitch_acceleration = 1 max_pitch_velocity_lo_alt = 2 max_bank= 25 max_bank_acceleration = 1.8 max_bank_velocity = 3 max_throttle_rate = 0.1 nav_proportional_control = 9 nav_integrator_control = 0.25 nav_derivative_control = 0 nav_integrator_boundary = 2.5 nav_derivative_boundary = 0 gs_proportional_control = 9.52 gs_integrator_control = 0.26 gs_derivative_control = 0 gs_integrator_boundary = 0.7 gs_derivative_boundary = 0 yaw_damper_gain = 0 [fuel] LeftMain = 0, -5.1, 2.3, 60, 0 RightMain = 0, 5.1, 2.3, 60, 0 fuel_type = 1 number_of_tank_selectors = 1 electric_pump=1 [airplane_geometry] wing_area = 231 wing_span = 39 wing_root_chord = 5.92307692307692 wing_dihedral = 1 wing_incidence = 0 wing_twist = 0 oswald_efficiency_factor = 0.873292267437662 wing_winglets_flag = 0 wing_sweep = 0 wing_pos_apex_lon = 1.48076923076923 wing_pos_apex_vert = 0 htail_area = 0 htail_span = 13.7 htail_pos_lon = -18.33 htail_pos_vert = 0 htail_incidence = 0 htail_sweep = 0 vtail_area = 15.2 vtail_span = 6.4 vtail_sweep = 0 vtail_pos_lon = -19.31 vtail_pos_vert = 0 elevator_area = 37.5 aileron_area = 20.7 rudder_area = 10.6 elevator_up_limit = 30 elevator_down_limit = 20 aileron_up_limit = 15 aileron_down_limit = 15 rudder_limit = 30 elevator_trim_limit = 18 spoiler_limit = 45 spoilerons_available = 1 aileron_to_spoileron_gain = 4 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 [Reference Speeds] flaps_up_stall_speed = 43.4 full_flaps_stall_speed = 37.4 cruise_speed = 143 max_indicated_speed = 174 max_mach = 0.2628 [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 [gear_warning_system] gear_warning_available = 0 pct_throttle_limit = 0.1 flap_limit_idle = 33.75 flap_limit_power = 16.875 [brakes] toe_brakes_scale = 0.7 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 = 2, 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