[fltsim.0] title=Sikorsky S-39 New York American sim=Sikorsky S-39 New York American model= panel= sound= texture=NC14326 checklists= ui_manufacturer=Sikorsky ui_type=S-39C NC-14326 New York American ui_variation=All-white "New York American" description=Single-engined amphibian, used by New York American newspaper in 1930's to cover stories around the country. atc_heavy=0 atc_id= atc_airline= atc_flight_number= [forcefeedback] gear_bump_nose_magnitude=2000 gear_bump_nose_direction=18000 gear_bump_nose_duration=250000 gear_bump_left_magnitude=2000 gear_bump_left_direction=35500 gear_bump_left_duration=250000 gear_bump_right_magnitude=2000 gear_bump_right_direction=500 gear_bump_right_duration=250000 ground_bumps_magnitude1=1750 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 [General] performance=Maximum Speed\t120 kts\nCruise Speed\t100 kts\nMaximum Range\t400 nm\nService Ceiling\t18,000 ft\nMax Gross Weight\t4,000 lb\nSeating\t\t4\nUseful Load\t1,322 lb\n\n\n atc_type= atc_model= [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, 0.000, 0.000, -2.000 empty_weight=3150.000 empty_weight_roll_MOI=3872.000 empty_weight_pitch_MOI=3385.000 empty_weight_yaw_MOI=6135.000 empty_weight_coupled_MOI=0.000 max_gross_weight=4000.000 CG_forward_limit=0.000 CG_aft_limit=1.000 [fuel] LeftMain=-0.250, -2.100, 2.500, 32.500, 0.000 RightMain=-0.250, 2.100, 2.500, 32.500, 0.000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=350.000 wing_span=52.000 wing_root_chord=7.083 wing_dihedral=1.500 wing_incidence=0.000 wing_twist=0.000 oswald_efficiency_factor=0.686 wing_winglets_flag=0 wing_sweep=0.000 wing_pos_apex_lon=0.830 wing_pos_apex_vert=2.500 htail_area=39.000 htail_span=16.000 htail_pos_lon=-19.000 htail_pos_vert=0.000 htail_incidence=0.000 htail_sweep=0.000 vtail_area=18.000 vtail_span=4.837 vtail_sweep=0.000 vtail_pos_lon=-19.000 vtail_pos_vert=1.500 elevator_area=16.610 aileron_area=18.300 rudder_area=6.650 elevator_up_limit=28.000 elevator_down_limit=20.999 aileron_up_limit=19.996 aileron_down_limit=15.000 rudder_limit=23.995 elevator_trim_limit=19.498 spoiler_limit=0.000 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 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) point.0=1.000, -11.000, 0.000, -4.670, 1600.000, 0.000, 0.520, 30.000, 0.380, 2.500, 1.640, 5.000, 5.000, 1.000, 0.000, 0.000 point.1=1.000, 1.830, -5.000, -6.800, 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, 1.830, 5.000, -6.800, 1800.000, 2.000, 0.520, 0.000, 0.340, 2.500, 1.000, 5.000, 5.000, 3.000, 0.000, 0.000 point.3=4.000, -10.000, 0.000, -4.170, 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.4=4.000, 6.000, -2.500, -4.170, 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.5=4.000, 6.000, 2.500, -4.170, 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.6=4.000, 1.250, -8.330, -3.750, 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.7=4.000, 1.250, 8.330, -3.750, 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.8=2.000, 0.000, -8.330, -1.500, 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.9=2.000, 0.000, 8.330, -1.500, 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.10=2.000, -12.170, 0.000, 0.000, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 static_pitch=10.500 static_cg_height=6.100 gear_system_type=0 [GeneralEngineData] engine_type=0 Engine.0=2.000, 0.000, 2.500 fuel_flow_scalar=1.000 min_throttle_limit=0.000000 [piston_engine] power_scalar=1.0 //Piston power scalar cylinder_displacement=109.0 //Cubic inches per cylinder compression_ratio=6.0 //Compression ratio number_of_cylinders=9 //Number of cylinders max_rated_rpm=2300 //Max rated RPM max_rated_hp=300 //Max rated HP fuel_metering_type=1 //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter cooling_type=0 //0=Cooling type Air, 1=Cooling type Liquid normalized_starter_torque=0.3 //Starter torque factor turbocharged=0 //Is it turbocharged? 0=FALSE, 1=TRUE max_design_mp=0 //Max design manifold pressure, (inHg) min_design_mp=0 //Min design manifold pressure, (inHg) critical_altitude=0 //Altitude to which the turbocharger will provide max design manifold pressure (feet) emergency_boost_type=0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power emergency_boost_mp_offset=0 //Additional manifold pressure supplied by emergency boost emergency_boost_gain_offset=0 //Multiplier on manifold pressure due to emergency boost fuel_air_auto_mixture=0 //Automixture available? 0=FALSE, 1=TRUE auto_ignition=0 //Auto-Ignition available? 0=FALSE, 1=TRUE max_rpm_mechanical_efficiency_scalar=1.0 //Scalar on maximum RPM mechanical efficiency idle_rpm_mechanical_efficiency_scalar=1.0 //Scalar on idle RPM mechanical efficiency max_rpm_friction_scalar=1.0 //Scalar on maximum RPM friction idle_rpm_friction_scalar=1.0 //Scalar on idle RPM friction [propeller] thrust_scalar=1.0 //Propeller thrust scalar propeller_type=1 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=8.3 //Propeller Diameter, (feet) propeller_blades=2 //Number of propeller blades propeller_moi=5.0 //Propeller moment of inertia beta_max=0 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min=0 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm=0 //Miminum governed RPM prop_tc=0 //Prop time-constant gear_reduction_ratio=1.0 //Propeller gear reduction ratio fixed_pitch_beta=20 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available=0 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available=0 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available=0 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available=0 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather=0 //Minimum RPM for prop feathering beta_feather=0 //Feathering pitch angle (degrees) power_absorbed_cf=0 //Coefficient of friction for power absorbed by propeller defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available=0 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta=0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta=0 //Minimum pitch angle in reverse, (degrees) [Reference Speeds] flaps_up_stall_speed=54.000 full_flaps_stall_speed=54.000 cruise_speed=111.548 max_indicated_speed=160.000000 [keyboard_response] elevator=100.000000,180.000000 aileron=200.000000,1000.000000 rudder=200.000000,1000.000000 [Views] // longitudinal, lateral, vertical distance from datum point //eyepoint=0.3,-1.3,-0.9 eyepoint=-0.5,-1.2,-0.9 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 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 [direction_indicators] direction_indicator.0=1,0 [flight_tuning] cruise_lift_scalar=0.800 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 //parasite_drag_scalar=1.600 parasite_drag_scalar=1.800 induced_drag_scalar=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [Flaps.0] type=1 span-outboard=0.100 extending-time=1.000 system_type=0 damaging-speed=0.000 blowout-speed=0.000 lift_scalar=0.000 drag_scalar=0.000 pitch_scalar=0.000 flaps-position.0=0.000, 0.000 flaps-position.1=1.000, 0.000 [brakes] toe_brakes_scale=0.465407 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [exits] number_of_exits=3 exit_rate.0=0.2 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing // longitudinal, lateral, vertical distance from datum point light.0=4, 0.000, 0.000, -1.150, fx_vclighth, //high VC-lighting; adjust these positions as you would for the [Views] section light.1=4, 0.000, 0.000, -1.150, fx_vclight, //normal panel/VC-lighting; adjust these positions as you would for the [Views] section