[fltsim.0]
title=Sikorsky C-6A
sim=Sikorsky S-38C VarA
model=
panel=
sound=
texture=C-6A
checklists=
description=The Sikorsky C-6A was the US Army's version of the S-38. Used 1931-33 as coastal patrol or VIP transport.
atc_id=0397
ui_manufacturer=Sikorsky
ui_type=USAAF C-6A 
ui_variation=USAAF olive drab, chrome yellow
visual_damage=1
atc_heavy=0
atc_airline=Army
atc_flight_number=0397

[fltsim.1]
title=Sikorsky S-38 Spirit of Carnauba
sim=Sikorsky S-38C VarA
model=
panel=
sound=
texture=Carnauba
checklists=
atc_id=NC6V
ui_manufacturer=Sikorsky
ui_type=S-38 Spirit of Carnauba
ui_variation=Red, black, silver, yellow
description=Twin-engined biplane amphibian. Used by S.C. Johnson to explore South America for source of raw materials.
atc_heavy=0
atc_airline=S.C. Johnson
atc_flight_number=NC6V

[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=450
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\t125 mph\nCruise Speed\t110 mph\nMaximum Range\t700 mi\nService Ceiling\t18,000 ft\nMax Gross Weight\t10.840 lb\nSeating\t\t8 passengers, 2 crew\nUseful Load\t3800 lb\n\n\n\n
[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, -16.00,  0.0,  -5.00,  1600, 0, 0.57, 22.00, 0.30, 2.5, 0.80, 4.00, 4.00, 0, 0.0, 0.0
point.1=1,   2.00, -5.00, -7.50,  1600, 1, 0.57,  0.00, 0.20, 2.5, 0.80, 4.00, 4.00, 2, 0.0, 0.0
point.2=1,   2.00,  5.00, -7.50,  1600, 2, 0.57,  0.00, 0.20, 2.5, 0.80, 4.00, 4.00, 3, 0.0, 0.0
point.4=4, -16.00,  0.0,  -5.00,  1600, 0, 0.0,   0.0,  0.55, 2.5, 0.65, 0.0,  0.0,  0, 0.0, 0.0
point.5=4,   6.00, -3.00, -5.00,  1600, 1, 0.0,   0.0,  0.95, 2.5, 0.65, 0.0,  0.0,  2, 0.0, 0.0
point.6=4,   6.00,  3.00, -5.00,  1600, 2, 0.0,   0.0,  0.95, 2.5, 0.65, 0.0,  0.0,  3, 0.0, 0.0
point.7=4,   2.00,-12.50, -4.50,  1600, 0, 0.0,   0.0,  0.85, 2.5, 0.65, 0.0,  0.0,  3, 0.0, 0.0
point.8=4,   2.00, 12.50, -4.50,  1600, 0, 0.0,   0.0,  0.85, 2.5, 0.65, 0.0,  0.0,  3, 0.0, 0.0
point.9=2,   1.00,-12.50, -0.50,  1800, 0, 0.0,   0.0,  0.0,  0.0, 0.0,  0.0,  0.0,  5, 0.0, 0.0
point.10=2,  1.00, 12.50, -0.50,  1800, 0, 0.0,   0.0,  0.0,  0.0, 0.0,  0.0,  0.0,  6, 0.0, 0.0
point.11=2, -16.00, 0.0,   0.0,   1800, 0, 0.0,   0.0,  0.0,  0.0, 0.0,  0.0,  0.0,  9, 0.0, 0.0
point.12=2,  9.00,  0.0,  -0.50,  1800, 0, 0.0,   0.0,  0.0,  0.0, 0.0,  0.0,  0.0,  4, 0.0, 0.0
static_pitch=7.498169
static_cg_height=6.908612

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=3.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=12.666187,0.000000
flaps-position.2=25.332374,0.000000
flaps-position.3=37.998561,0.000000

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=6500.000000
empty_weight_roll_MOI=33554.000000
empty_weight_pitch_MOI=40000.000000
empty_weight_yaw_MOI=53266.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=8084.000

[fuel]
LeftMain=-4.000000,-8.000000,4.000000,132.000000,0.000000
RightMain=-4.000000,8.000000,4.000000,132.000000,0.000000
fuel_type=1.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=720.000000
wing_span=71.666667
wing_root_chord=8.333333
wing_dihedral=0.000000
wing_incidence=2.499390
wing_twist=0.000000
oswald_efficiency_factor=0.983303
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=51.000000
htail_span=18.000000
htail_pos_lon=-23.333333
htail_pos_vert=0.000000
htail_incidence=0.417480
htail_sweep=0.000000
vtail_area=15.000000
vtail_span=4.415880
vtail_sweep=0.000000
vtail_pos_lon=-23.333333
vtail_pos_vert=6.666667
elevator_area=36.550000
aileron_area=37.400000
rudder_area=31.850000
elevator_up_limit=27.501974
elevator_down_limit=20.626481
aileron_up_limit=19.480565
aileron_down_limit=14.896903
rudder_limit=23.491270
elevator_trim_limit=19.480565
spoiler_limit=0.000057
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000

[GeneralEngineData]
engine_type=0
Engine.0=0.000000,-5.166667,0.500000
Engine.1=0.000000,5.166667,0.500000
fuel_flow_scalar=1.000000

[piston_engine]
cylinder_displacement=109.440000
compression_ratio=6.700000
number_of_cylinders=9
max_rated_rpm=2250.000000
max_rated_hp=450.000000
fuel_metering_type=2
cooling_type=0
normalized_starter_torque=0.155000
turbocharged=1
max_design_mp=36.999999
min_design_mp=1.000000
critical_altitude=5000.000000
emergency_boost_type=0
emergency_boost_mp_offset=0.000000
emergency_boost_gain_offset=0.000000
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000

[propeller]
propeller_type=0
propeller_diameter=8.500000
propeller_blades=2
propeller_moi=8.000000
beta_max=34.000000
beta_min=11.000000
min_gov_rpm=1400.000000
prop_tc=0.100000
gear_reduction_ratio=1.000000
fixed_pitch_beta=0.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000000
beta_feather=0.000000
power_absorbed_cf=0.000000
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000

[Reference Speeds]
flaps_up_stall_speed=54.000000
full_flaps_stall_speed=54.000000
cruise_speed=115.130319

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

[Views]
eyepoint=1.935183,-1.422552,-1.179236

[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

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