[fltsim.0] title=Latecoere 38-0 sim=Latecoere 38-0 model= panel= sound= texture= checklists= description=Description: Twin-engined long-range flying boat. ui_manufacturer=Latecoere ui_type=Late38 description=Late38-0, test model\n(c) 2004-2007 Alexander Belov\n ui_variation= [General] performance=Date: 2007.02.16 atc_type=LATECOERE atc_model=late380 [contact_points] //0 Class (1=wheel, 2=scrape, 3=skid, 4=float, 5=waterrudder) //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) //Hull point.0=4.000, 16.840, 0.000, -12.500, 1800.000, 0.000, 0.000, 0.000, 0.400, 2.500, 0.520, 0.000, 0.000, 0.000, 0.000, 0.000 point.1=4.000, -8.850, -4.700, -12.000, 1800.000, 0.000, 0.000, 25.000, 0.400, 2.500, 0.520, 0.000, 0.000, 2.000, 0.000, 0.000 point.2=4.000, -8.850, 4.700, -12.000, 1800.000, 0.000, 0.000, 25.000, 0.400, 2.500, 0.520, 0.000, 0.000, 3.000, 0.000, 0.000 point.3=4.000, -19.540, 0.000, -10.450, 1800.000, 0.000, 0.000, 0.000, 0.400, 2.500, 0.520, 0.000, 0.000, 0.000, 0.000, 0.000 point.4=4.000, -6.310, -9.900, -11.850, 1300.000, 0.000, 0.000, 25.000, 0.400, 2.500, 0.750, 0.000, 0.000, 2.000, 0.000, 0.000 point.5=4.000, -6.310, 9.900, -11.850, 1300.000, 0.000, 0.000, 25.000, 0.400, 2.500, 0.750, 0.000, 0.000, 3.000, 0.000, 0.000 //scrape point.5=2.000, 0.980, -38.350, 3.070, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.6=2.000, 0.980, 38.350, 3.070, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.7=2.000, 16.860, 0.000, 1.000, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.8=2.000, -8.180, 0.000, 13.670, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000 point.9=2.000, -38.290, 0.000, -1.420, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //low wing static_pitch=-0.180 static_cg_height=11.850 gear_system_type=4 [Views] eyepoint=8.934, -1.577, -7.482 [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=170.000, 10.370, -1.265, -0.330, pilot station_load.1=170.000, 10.370, 1.265, -0.330, co-pilot station_load.2=170.000, 7.350, -1.366, -1.640, navigator //station_load.3=880.000, 4.350, -1.366, 0, payload empty_weight=11724.6 empty_weight_roll_MOI=70000.000 empty_weight_pitch_MOI=53084.000 empty_weight_yaw_MOI=62255.000 empty_weight_coupled_MOI=0.000 max_gross_weight=22600.000 CG_forward_limit=0.500 CG_aft_limit=-0.800 [fuel] //4000 kg full fuel load LeftMain = 4.92, -1.64, -9.84, 368.0, 0.00 LeftAux = -3.28, -1.64, -9.84, 368.0, 0.00 RightMain= 4.92, 1.64, -9.84, 368.0, 0.00 RightAux = -3.28, -1.64, -9.84, 368.0, 0.00 Center1 = 0.00, 0.00, 0.00, 1.00, 0.00 fuel_type=1.00 number_of_tank_selectors=1 electric_pump=0 [flight_tuning] cruise_lift_scalar=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.000 pitch_stability=1.100 roll_stability=1.100 yaw_stability=1.100 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.215 parasite_drag_scalar=0.900 induced_drag_scalar=1.000 rudder_effectiveness=1.000 [pitot_static] vertical_speed_time_constant=100 [airplane_geometry] //wing_area=1397.47 //wing only wing_area=1689.22 //wing and stummel wing_span=102.95 wing_root_chord=14.75 wing_dihedral=3.0 wing_incidence=7.800 wing_twist=0.000 wing_winglets_flag=0 wing_sweep=0.000 wing_pos_apex_lon=0.000 wing_pos_apex_vert=0.000 htail_area=341.8 htail_span=23.28 htail_pos_lon=-34.9 htail_pos_vert=-3.10 htail_incidence=0.000 htail_sweep=0.000 vtail_area=59.1 vtail_span=10.8 vtail_sweep=30.000 vtail_pos_lon=-34.9 vtail_pos_vert=3.330 elevator_area=96.75 aileron_area=39.340 rudder_area=10.62 elevator_up_limit=15.000 elevator_down_limit=15.000 aileron_up_limit=24.001 aileron_down_limit=18.999 rudder_limit=20.000 elevator_trim_limit=21.000 spoiler_limit=1.450 spoilerons_available=0 aileron_to_spoileron_gain=0.000 min_ailerons_for_spoilerons=0.000 min_flaps_for_spoilerons=0.000 oswald_efficiency_factor=0.85 [keyboard_response] elevator=350.000000,500.000000 aileron=450.000000,1000.000000 rudder=200.000000,1000.000000 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=400.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 use_no_default_pitch=1 use_no_default_bank=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=100.000000 default_pitch_mode=0 default_bank_mode=0 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 [EFFECTS] //wake=fx_wake_s water=fx_spray //water=fx_wake_s dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_wtrspray_s, 1 startup=fx_enginefailure, 2 [direction_indicators] direction_indicator.0=1,0 [GeneralEngineData] engine_type=0 Engine.0= 7.93, 0.0, 0.0 Engine.1=-7.80, 0.0, 0.0 fuel_flow_scalar=0.95 min_throttle_limit=0.100000 [piston_engine] cylinder_displacement=183.071 compression_ratio=6.2 number_of_cylinders=12 max_rated_rpm=2600.000 max_rated_hp=800.000 fuel_metering_type=1 cooling_type=1 normalized_starter_torque=0.085 turbocharged=0 max_design_mp=0.000 min_design_mp=0.000 critical_altitude=0.000 emergency_boost_type=0 emergency_boost_mp_offset=0.000 emergency_boost_gain_offset=0.000 fuel_air_auto_mixture=0 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=0.600 power_scalar=1.000 [propeller] propeller_type=1 propeller_diameter=13.11 propeller_blades=2 propeller_moi=34.000 beta_max=0.500 beta_min=0.500 min_gov_rpm=800.000 prop_tc=0.010 gear_reduction_ratio=1.0 fixed_pitch_beta=20.500 low_speed_theory_limit=80.000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.000 beta_feather=0.000 power_absorbed_cf=0.000 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.000 minimum_reverse_beta=0.000 thrust_scalar=1.100 // account for pusher prop [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=27000 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [Reference Speeds] flaps_up_stall_speed=66.000 full_flaps_stall_speed=66.000 cruise_speed=105.000 max_indicated_speed=259.000000 [Flaps.0] type=0 span-outboard=0.500000 extending-time=0 system_type=0 flaps-position.0= 0.0, 0.0 flaps-position.1= 0.0, 0.0 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=0 Com.1=1,0 Com.2=0,0 Nav.1=1,0,0 Nav.2=0,0,0 Adf.1=1,0 Transponder.1=0 Marker.1=0 [electrical] electric_always_available=0 //áûëî =1 ;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 pitot_heat=0, 2 , 17.0 additional_system=0, 20, 17.0 fuel_pump=0, 5 , 17.0 starter1=0, 20, 17.0 light_nav=0, 5 , 17.0 light_panel=0, 5 , 17.0 [LIGHTS] [SMOKESYSTEM] [brakes] toe_brakes_scale=1.000000 parking_brake=1 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
