[fltsim.0] title=SNA_Seawind sim=SNA_Seawind model= panel= sound= texture= kb_checklists= description=Aircraft produced by S.N.A. Inc. 4 place amphibean kitplane. When introduced the Seawind immediately took a strong following, due to its beautiful appearance and high performance. The Seawind is powered by a 300 HP engine which gives it, among flying boats/amphibeans, an impressive speed of 162 kts. The elegant Seawind is a kitplane - you build it yourself in your garage! ui_manufacturer=S.N.A. Inc. ui_type=Seawind ui_variation=4 seater atc_heavy=0 atc_id= atc_airline= atc_flight_number= [forcefeedback] gear_bump_nose_magnitude=6000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=6000 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=6000 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=3250 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 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 [fltsim.2] title= sim= panel= sound= texture= model= [fltsim.3] title= sim= panel= sound= texture= model= [fltsim.4] title= sim= panel= sound= texture= model= [fltsim.5] title= sim= panel= sound= texture= model= [fltsim.6] title= sim= panel= sound= texture= model= [fltsim.7] title= sim= panel= sound= texture= model= [fltsim.8] title= sim= panel= sound= texture= model= [fltsim.9] title= sim= panel= sound= texture= model= [General] performance=Length: 27 ft. 2 in\nSpan: 35 ft.\nWeight: 2300 lbs.\nPower: Lycoming IO-540, 300HP\nRange: 980 miles\nDate: 07\/07\/2000\nDetails: 4-place amphibian\nDesigner: Vaidas Masidlauskas atc_type= atc_model= [WEIGHT_AND_BALANCE] reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 1.500, 0.000, 0.000 max_number_of_stations= 50 station_load.0= 170.000, 4.000, 1.500, 0.000 empty_weight= 2300.000 empty_weight_roll_MOI= 3000.000 empty_weight_pitch_MOI= 8000.000 empty_weight_yaw_MOI= 10000.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 3400.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 station_load.1= 170.000, 4.000, -1.500, 0.000 station_load.2= 170.000, 1.000, 1.500, 0.000 station_load.3= 170.000, 1.000, -1.500, 0.000 [fuel] LeftMain= 0.000, -6.000, 0.000, 37.000, 0.000 RightMain= 0.000, 6.000, 0.000, 37.000, 0.000 fuel_type=1.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area= 160.000 wing_span= 35.000 wing_root_chord= 4.583 wing_dihedral= 4.000 wing_incidence= 3.000 wing_twist= -1.000 oswald_efficiency_factor= 0.600 wing_winglets_flag= 1 wing_sweep= 0.000 wing_pos_apex_lon= 0.000 wing_pos_apex_vert= 0.000 htail_area= 50.000 htail_span= 13.333 htail_pos_lon= -13.300 htail_pos_vert= 4.000 htail_incidence= -5.000 htail_sweep= 0.000 vtail_area= 40.000 vtail_span= 9.000 vtail_sweep= 45.000 vtail_pos_lon= -9.500 vtail_pos_vert= 2.000 elevator_area= 17.200 aileron_area= 20.813 rudder_area= 14.000 elevator_up_limit= 27.502 elevator_down_limit= 20.626 aileron_up_limit= 19.481 aileron_down_limit= 14.897 rudder_limit= 23.491 elevator_trim_limit= 19.481 spoiler_limit= 59.989 spoilerons_available= 0 aileron_to_spoileron_gain= 0.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 [contact_points] //0 Class (1=wheel, 2=scrape point, 3=skid, 4=floats) //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 / Water Rudder Effectiveness (0=Undamped, 1=Critically Damped) / 1.0 = normal //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) //Wheels point.0= 1.000, 7.083, 0.000, -4.200, 1600.000, 0.000, 0.520, 30.000, 0.320, 4.500, 1.640, 5.000, 5.000, 0.000, 0.000, 0.000 point.1= 1.000, -1.417, -4.500, -4.150, 1800.000, 1.000, 0.520, 0.000, 0.340, 2.500, 1.000, 5.000, 5.000, 2.000, 0.000, 0.000 point.2= 1.000, -1.417, 4.500, -4.150, 1800.000, 2.000, 0.520, 0.000, 0.340, 2.500, 1.000, 5.000, 5.000, 3.000, 0.000, 0.000 //SCRAPE point.3= 2.000, -1.500, -15.600, -1.100, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4= 2.000, -1.500, 15.600, -1.100, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5= 2.000, -11.000, 0.000, 1.000, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //Hull point.6= 4.000, 4.600, 0.000, -3.600, 6000.000, 0.000, 0.000, 0.000, 0.700, 1.000, 0.850, 0.000, 0.000, 1.000, 0.000, 0.000 point.7= 4.000, -11.000, 0.000, -2.400, 6000.000, 0.000, 0.000, 0.000, 0.500, 1.000, 0.650, 0.000, 0.000, 1.000, 0.000, 0.000 point.8= 4.000, -1.450, -15.600, -1.400, 6000.000, 0.000, 0.000, 0.000, 0.750, 2.500, 0.550, 0.000, 0.000, 1.000, 0.000, 0.000 //PONTOONS point.9= 4.000, -1.450, 15.600, -1.400, 6000.000, 0.000, 0.000, 0.000, 0.750, 2.500, 0.550, 0.000, 0.000, 1.000, 0.000, 0.000 static_pitch= 2.000 static_cg_height= 3.300 /point.0= 1.000, 4.083, 0.000, -3.167, 1181.102, 0.000, 0.521, 0.000, 0.334, 2.500, 1.032, 3.500, 3.500, 0.000, 0.000, 0.000 /point.1= 1.000, -1.417, -4.500, -3.167, 1574.803, 1.000, 0.521, 0.000, 0.221, 2.500, 0.912, 4.700, 4.700, 2.000, 0.000, 0.000 /point.2= 1.000, -1.417, 4.500, -3.167, 1574.803, 2.000, 0.521, 0.000, 0.221, 2.500, 0.912, 5.200, 5.200, 3.000, 0.000, 0.000 /point.3= 2.000, 0.000, -17.917, 2.083, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 /point.4= 2.000, 0.000, 17.917, 2.083, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 /point.5= 2.000, -16.333, 0.000, 0.833, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 /point.6= 2.000, 0.000, 0.000, -3.400, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //Grumman Duck Contact /points //FLOAT /point.7=4.000, -4.000, 0.000, -3.200, 6000.000, 0.000, 0.000, 30.000, 0.450, 2.500, 0.650, 0.000, 0.000, 1.000, 0.000, 0.000 /point.8=4.000, -7.500, -2.500, -3.500, 6000.000, 0.000, 0.000, 0.000, 0.950, 2.500, 0.650, 0.000, 0.000, 2.000, 0.000, 0.000 /point.9=4.000, -7.500, 2.500, -3.500, 6000.000, 0.000, 0.000, 0.000, 0.950, 2.500, 0.650, 0.000, 0.000, 2.000, 0.000, 0.000 //PONTOONS /point.10=4.000, -12.000, -15.600, -2.100, 6000.000, 0.000, 0.000, 0.000, 0.750, 2.500, 0.650, 0.000, 0.000, 3.000, 0.000, 0.000 /point.11=4.000, -12.000, 15.600, -2.100, 6000.000, 0.000, 0.000, 0.000, 0.750, 2.500, 0.650, 0.000, 0.000, 3.000, 0.000, 0.000 /[contact_points] /Orig Seawind ///Hull /Foreplane /point.7= 4.000, -3.000, 0.000, -3.200, 6000.000, 0.000, 0.000, 0.000, 0.450, 2.500, 0.650, 0.000, 0.000, 1.000, 0.000, 0.000 /Aft plane /point.8= 4.000, -20.000, 0.000, -3.200, 6000.000, 0.000, 0.000, 0.000, 0.950, 2.500, 0.650, 0.000, 0.000, 1.000, 0.000, 0.000 ///Floats /Left /point.9= 4.000, -12.000, -17.917, -2.100, 6000.000, 0.000, 0.000, 0.000, 0.950, 2.500, 0.650, 0.000, 0.000, 2.000, 0.000, 0.000 /Right /point.10= 4.000, -12.000, 17.917, -2.100, 6000.000, 0.000, 0.000, 0.000, 0.950, 2.500, 0.650, 0.000, 0.000, 3.000, 0.000, 0.000 static_pitch=0.000000 static_cg_height=2.853557 [GeneralEngineData] engine_type= 0 Engine.0= -0.167, 0.000, 4.330 fuel_flow_scalar= 1.000 [piston_engine] max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 cylinder_displacement= 93.500 compression_ratio= 8.600 number_of_cylinders= 6 max_rated_rpm= 2400.000 max_rated_hp= 300.000 fuel_metering_type= 1 cooling_type= 0 normalized_starter_torque= 0.300 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 power_scalar=1.071 [propeller] propeller_type= 0 propeller_diameter= 6.833 propeller_blades= 3 propeller_moi= 7.840 beta_max= 34.000 beta_min= 15.000 min_gov_rpm= 1000.000 prop_tc= 0.100 gear_reduction_ratio= 1.000 fixed_pitch_beta= 20.000 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=1.500 [Reference Speeds] flaps_up_stall_speed= 62.000 full_flaps_stall_speed= 49.600 cruise_speed= 164.399 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=0.422921,-1.255947,1.922367 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 [direction_indicators] direction_indicator.0=1,0 [flight_tuning] cruise_lift_scalar=1.381 pitch_stability=1.213 roll_stability=1.000 yaw_stability=1.500 parasite_drag_scalar=0.851 induced_drag_scalar=0.851 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 elevator_trim_effectiveness=1.341 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 5.000 system_type= 0 damaging-speed= 0.000 blowout-speed= 0.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 13.331, 0.000 flaps-position.2= 26.662, 0.000 flaps-position.3= 39.992, 0.000