[fltsim.0] title=T-28D Intromet sim=T-28D_FS model = panel = sound = texture =itm panel_alias = sound_alias = kb_checklists = kb_reference = atc_id = atc_id_color = atc_parking_types = atc_parking_code = ui_manufacturer =North American Aviation ui_type =T-28D ui_variation =Intromet description =A T-28D modified to do weather research in the tropics for The Institute of Tropical Meteorology\n Original model by Tim Corad and panel by Michael Vader\n Adapted and painted by Luiz Alvarenga visual_damage=1 atc_flight_number= atc_airline= atc_type= atc_model= performance=+ Empty Weight: 6824 lbs + Max Power: 1425 Hp + Maneuver speed: 202 mph @ 6.0 g + Max speed: 346 mph @ 10000 ft + Max speed at sea-level: 332 mph + Climb rate: 1000 ft/min @ 111 mph Flight Dynamics By: Tim Piglet Conrad Piglet's Peculiar Planes FD Build 8 - 7/8/04 05:10 PM Flight Dynamics Workbook V2.84.65 [General] atc_type = atc_model = editable = 1 visual_damage=1 performance = + Empty Weight: 6824 lbs + Max Power: 1425 Hp + Maneuver speed: 202 mph @ 6.0 g + Max speed: 346 mph @ 10000 ft + Max speed at sea-level: 332 mph + Climb rate: 1000 ft/min @ 111 mph Flight Dynamics By: Tim Piglet Conrad Piglet's Peculiar Planes FD Build 8 - 7/8/04 05:10 PM Flight Dynamics Workbook V2.84.65 [pitot_static] vertical_speed_time_constant = 2 [WEIGHT_AND_BALANCE] max_gross_weight = 7886 empty_weight = 6424 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0.05, 0, 0 CG_forward_limit = 0 CG_aft_limit = 1 max_number_of_stations = 13 station_load.0 = 200, 0.32, 0, 1.89, Pilot empty_weight_pitch_MOI = 9544 empty_weight_roll_MOI = 4111 empty_weight_yaw_MOI = 12785 empty_weight_coupled_MOI = 0 [flight_tuning] cruise_lift_scalar = 1 parasite_drag_scalar = 1 induced_drag_scalar = 1 elevator_effectiveness = 1 aileron_effectiveness = 1.5 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 = 9.38, 0, 0 fuel_flow_scalar = 1 min_throttle_limit = 0 [piston_engine] power_scalar = 1.3 cylinder_displacement = 202.222222222222 compression_ratio = 6 number_of_cylinders = 9 max_rated_rpm = 2700 max_rated_hp = 1425 fuel_metering_type = 2 cooling_type = 0 normalized_starter_torque = 0.065 turbocharged = 1 max_design_mp = 52 min_design_mp = 9 critical_altitude = 10000 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 = 10 propeller_blades = 3 propeller_moi = 30 beta_max = 65 beta_min = 15 min_gov_rpm = 405 prop_tc = 0.01 gear_reduction_ratio = 1.1 fixed_pitch_beta = 25 low_speed_theory_limit = 80 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 [contact_points] max_number_of_points = 7 point.0 = 1, 6.0118, 0, -6.05, 1500, 0, 0.9, 45, 0.2, 2, 0.8, 5, 6, 0, 140.8, 176 point.1 = 1, -1.76, -6.05, -5.7, 1500, 1, 1.1, 0, 0.3, 1.2, 0.8, 5, 6, 2, 140.8, 176 point.2 = 1, -1.76, 6.05, -5.7, 1500, 2, 1.1, 0, 0.3, 1.2, 0.8, 6, 7, 3, 140.8, 176 point.3 = 2, -1.78, -19.434, 0.858, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 5 point.4 = 2, -1.78, 19.434, 0.858, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 6 point.5 = 2, -19.758, 0, -1.97, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 9 point.6 = 2, 6.835, 0, -2.692, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 4 static_pitch= 2 static_cg_height= 5.7 gear_system_type = 1 [Views] eyepoint= 0.382, 0, 4.088 [flaps.0] //Trailing Edge Flaps type = 1 span-outboard = 0.5 extending-time = 6 flaps-position.0 = 0 flaps-position.1 = 15, 152 flaps-position.2 = 25, 145 flaps-position.3 = 40, 139 damaging-speed = 156 blowout-speed = 173 system_type = 1 lift_scalar = 1 drag_scalar = 1 pitch_scalar = 1 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 160 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, -1.608, -19.901, 1.203, fx_navred light.1 = 3, -1-608, 19.901, 1.203, fx_navgre light.2 = 1, -12.931, 0, 2.543, fx_beacon light.3 = 1, -12.294, 0, -2.253, fx_beacon [Radios] // 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 [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 = 0.2 [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, -8, 0, 88.5, 0 RightMain = 0, 8, 0, 88.5, 0 fuel_type = 1 number_of_tank_selectors = 1 electric_pump=1 [airplane_geometry] wing_area = 268 wing_span = 40.0833333333333 wing_root_chord = 6.68607068607069 wing_dihedral = 7 wing_incidence = 0 wing_twist = 0 oswald_efficiency_factor = 0.890246175335343 wing_winglets_flag = 0 wing_sweep = 0 wing_pos_apex_lon = 1.72151767151767 wing_pos_apex_vert = 0 htail_area = 33.5 htail_span = 13.7 htail_pos_lon = -18.83 htail_pos_vert = 0 htail_incidence = 0 htail_sweep = 0 vtail_area = 16.25 vtail_span = 6.4 vtail_sweep = 0 vtail_pos_lon = -20 vtail_pos_vert = 0 elevator_area = 20.5 aileron_area = 22.5 rudder_area = 19.75 elevator_up_limit = 30 elevator_down_limit = 20 aileron_up_limit = 18 aileron_down_limit = 18 rudder_limit = 40 elevator_trim_limit = 18 spoiler_limit = 45 spoilerons_available = 0 aileron_to_spoileron_gain = 0 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 [Reference Speeds] flaps_up_stall_speed = 71.3 full_flaps_stall_speed = 60 cruise_speed = 122 max_indicated_speed = 304 max_mach = 0.5914 [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 = 1 pct_throttle_limit = 0.1 flap_limit_idle = 30 flap_limit_power = 15 [brakes] toe_brakes_scale = 0.740889 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 = 2000 [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