[fltsim.0]
title=Sikorsky S-39C NC55V
sim=Sikorsky S-39C NC55V
model=
panel=
sound=
texture=
checklists=
ui_manufacturer=Sikorsky
ui_type=S-39C "Amphibion" NC55V
ui_variation=Varney Speed Lines white and blue
description=Light transport parasol monoplane. Flight model by Alexander Belov updated with data from Paul Matt Historic Aviation Album vol 14.  Wheeled version of NC55V used by Varney Air Ferries in San Francisco in 1932.\n
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=


[forcefeedback]
gear_bump_nose_magnitude=3000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=3000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=3000
gear_bump_right_direction=500
gear_bump_right_duration=250000
ground_bumps_magnitude1=1250
ground_bumps_angle1=8900
ground_bumps_intercept1=5#
ground_bumps_slope1=0.48
ground_bumps_magnitude2=350
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

[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, -6.780, 1600.000, 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, -6.580, 1600.000, 2.000, 0.520, 0.000, 0.340, 2.500, 1.000, 5.000, 5.000, 3.000, 0.000, 0.000

point.4=4.000,-10.000, 0.000, -3.670, 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.5=4.000, 6.000, -2.500, -3.670, 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, 6.000, 2.500, -3.670, 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.7=4.000, 1.250, -8.330, -3.250, 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=4.000, 1.250, 8.330, -3.250, 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.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, 5.000, 0.000, 0.000
point.10=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.11=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
point.12=2.000, 5.000, 0.000, -2.000, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_pitch=9.000
static_cg_height=6.0

[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
atc_type=
atc_model=

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_tchdrt
touchdown=fx_tchdwn, 1

[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=0.000000,0.000000,0.000000,0.000000
empty_weight=3115.000
empty_weight_roll_MOI=3830.000
empty_weight_pitch_MOI=4026.000
empty_weight_yaw_MOI=6667.000
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, 33.000, 0.000
RightMain=-0.250, 2.100, 2.500, 33.000, 0.000
fuel_type=1.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=350.000
wing_span=52.000
wing_root_chord=7.083
wing_dihedral=1.500
wing_incidence=0.500
wing_twist=0.000
oswald_efficiency_factor=0.908
wing_winglets_flag=0
wing_sweep=0.000
wing_pos_apex_lon=0.830
wing_pos_apex_vert=2.000
htail_area=39.000
htail_span=16.000
htail_pos_lon=-19.000
htail_pos_vert=0.000
htail_incidence=0.417
htail_sweep=0.000
vtail_area=6.000
vtail_span=2.793
vtail_sweep=0.000
vtail_pos_lon=-19.000
vtail_pos_vert=1.667
elevator_area=16.610
aileron_area=18.300
rudder_area=18.650
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=0.000
spoilerons_available=0
aileron_to_spoileron_gain=0.000
min_ailerons_for_spoilerons=0.000
min_flaps_for_spoilerons=0.000

[GeneralEngineData]
engine_type=0
Engine.0=2.000, 0.000, 2.917
fuel_flow_scalar=1.000

[piston_engine]
cylinder_displacement=109.000
compression_ratio=8.500
number_of_cylinders=9
max_rated_rpm=2400.000
max_rated_hp=300.000
fuel_metering_type=2
cooling_type=0
normalized_starter_torque=0.155
turbocharged=1
max_design_mp=35.000
min_design_mp=1.000
critical_altitude=5000.000
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=1.000
power_scalar=1.000

[propeller]
propeller_type=0
propeller_diameter=8.030
propeller_blades=2
propeller_moi=8.000
beta_max=65.000
beta_min=11.000
min_gov_rpm=1400.000
prop_tc=0.100
gear_reduction_ratio=1.000
fixed_pitch_beta=0.000
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=1.000

[Reference Speeds]
flaps_up_stall_speed=52.000
full_flaps_stall_speed=52.000
cruise_speed=101.524

[keyboard_response]
elevator=100.000000,180.000000
aileron=200.000000,1000.000000
rudder=200.000000,1000.000000

[Views]
eyepoint=0.333210,-0.999631,-0.499815

[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=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
parasite_drag_scalar=1.000
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=0.500
extending-time=3.000
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=12.666, 0.000