[fltsim.0]
title=S7
sim=S7
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=S7_ref
ui_manufacturer=Rans
ui_type=S-7C Courier
ui_variation=Yellow
description=Two seats in tandem, high wing, tractor, taildragger. Full enclosure with doors. Dope and fabric covering process. Standard engine, Rotax 912S-100hp. The aircraft is flown solo from the front seat. Full dual controls. Equipped with the Rotax 100 HP 912S engine, the Courier leaps into the air in less than 325 feet. Lifting off short means little if you can’t haul a load. 500 pounds of payload puts the Courier in the "do something, go somewhere" class. Tough spring steel gear and effective Cleveland Brakes let you do that something in places previously passed by. The gentle nature of this taildragger will encourages the newcomer and compliments the seasoned. Developed in the land of daily crosswinds (Kansas), the Courier is good for 20 KTS. at 90 degrees – more if you know a few tricks.

atc_id=N1205S
atc_airline=
atc_flight_number=

[fltsim.1]
title=S7paint1
sim=S7
model=
panel=
sound=
texture=1
kb_checklists=
kb_reference=S7_ref
ui_manufacturer=Rans
ui_type=S-7C Courier
ui_variation=Red
description=Two seats in tandem, high wing, tractor, taildragger. Full enclosure with doors. Dope and fabric covering process. Standard engine, Rotax 912S-100hp. The aircraft is flown solo from the front seat. Full dual controls. Equipped with the Rotax 100 HP 912S engine, the Courier leaps into the air in less than 325 feet. Lifting off short means little if you can’t haul a load. 500 pounds of payload puts the Courier in the "do something, go somewhere" class. Tough spring steel gear and effective Cleveland Brakes let you do that something in places previously passed by. The gentle nature of this taildragger will encourages the newcomer and compliments the seasoned. Developed in the land of daily crosswinds (Kansas), the Courier is good for 20 KTS. at 90 degrees – more if you know a few tricks.

atc_id=N3377C
atc_airline=
atc_flight_number=

[General]
atc_type=Experimental
atc_model=S7C
editable=0

performance=Span : 29' 0"\nLength : 22' 10" \nHeight : 6' 3"\nWeight empty :675lbs.\nWeight max : 1,200lbs. \nPower: 100hp Rotax 912s \nMax speed : 130mph.\nCruise speed: 118mph. \nRate of Climb: 1100ft\/min\nService Ceiling: 14,500ft.\nRange: 386miles\n

[WEIGHT_AND_BALANCE]
max_gross_weight = 1200  // (pounds)
empty_weight = 675       // (pounds)

reference_datum_position= 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline,waterline)
empty_weight_CG_position= 0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 50

station_load.0 = "200, 0.00, 0.00, 0.00 ,Pilot"//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "000,-3.00, 0.00, 0.00 ,CoPilot"//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "000,-6.00, 0.00, 0.00 ,Baggage"//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_roll_MOI=5343.0
empty_weight_pitch_MOI=5767.0
empty_weight_yaw_MOI=9367.0
empty_weight_coupled_MOI=0.0

[flight_tuning]
cruise_lift_scalar          = 0.4
parasite_drag_scalar        = 1.35
induced_drag_scalar         = 1.0
elevator_effectiveness      = 1.0
aileron_effectiveness       = 1.0
rudder_effectiveness        = 1.0
pitch_stability             = 1.0
roll_stability              = 1.0
yaw_stability               = 1.0
elevator_trim_effectiveness = 2.0
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0

[GeneralEngineData]
engine_type = 0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 6.13, 0.0, 0.0                       //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 0.77                          //Fuel flow scalar
min_throttle_limit=0.000000

[piston_engine]
power_scalar = 1.00                             //Piston power scalar
cylinder_displacement= 82.75                    //Cubic inches per cylinder
compression_ratio= 10.5                         //Compression ratio
number_of_cylinders=4                           //Number of cylinders
max_rated_rpm= 5800                             //Max rated RPM
max_rated_hp= 100                               //Max rated HP
fuel_metering_type= 1                           //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0                                 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.1                  //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 =1.00                             //Propeller thrust scalar
propeller_type= 1                               //0=Constant Speed,1=Fixed Pitch
propeller_diameter= 5.87                        //Propeller Diameter, (feet)
propeller_blades= 2                             //Number of propeller blades
propeller_moi= 3.78                             //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= 0.1                                    //Prop time-constant 
gear_reduction_ratio= 1.00                      //Propeller gear reduction ratio
fixed_pitch_beta= 13.75                         //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 in feather
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)

[electrical]
                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor         = 0, 5 , 17.0
gear_motor         = 0, 5 , 17.0
autopilot          = 0, 5 , 17.0
avionics_bus       = 0, 10, 17.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 20, 17.0
marker_beacon      = 1, 2 , 17.0
gear_warning       = 0, 2 , 17.0
fuel_pump          = 0, 5 , 17.0
starter1           = 0, 20, 17.0
light_nav          = 0, 5 , 17.0
light_beacon       = 0, 5 , 17.0
light_landing      = 0, 5 , 17.0
light_taxi         = 0, 5 , 17.0
light_strobe       = 0, 5 , 17.0
light_panel        = 0, 5 , 17.0

        //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               (0=Undamped, 1=Critically Damped)
        //11 Extension Time              (seconds)
        //12 Retraction Time             (seconds)
        //13 Sound Type


[contact_points]
point.0=1,  -15.00,    0.0, -1.25, 1574.80, 0.00, 0.20, 60.00, 0.30, 2.50, 0.65, 0.00, 0.00, 0.00, 0.00, 0.00
point.1=1,    1.24,   -3.0, -4.22, 1574.80, 1.00, 0.51,  0.00, 0.30, 2.50, 0.65, 0.00, 0.00, 2.00, 0.00, 0.00
point.2=1,    1.24,    3.0, -4.22, 1574.80, 1.00, 0.51,  0.00, 0.30, 2.50, 0.65, 0.00, 0.00, 2.00, 0.00, 0.00
point.3=2,   -2.28,  14.68,  2.34,  800.00, 0.00, 0.00,  0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00
point.4=2,   -2.28, -14.68,  2.34,  800.00, 0.00, 0.00,  0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00
point.5=2,  -15.00,   0.00,  0.38,  800.00, 0.00, 0.00,  0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00
point.6=2,    3.60,   0.00, -1.60,  800.00, 0.00, 0.00,  0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00
point.7=2,  -15.00,   0.00,  4.57,  800.00, 0.00, 0.00,  0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00

static_pitch = 11.64
static_cg_height = 3.75

[Views]
eyepoint = -1.00, 0.00, 1.86           //(feet) longitudinal, lateral, vertical distance from reference datum

[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1       = 1
Com.1         = 1, 1
Com.2         = 1, 1
Nav.1         = 1, 1, 1
Nav.2         = 1, 1, 0
Adf.1         = 1
Transponder.1 = 1
Marker.1      = 1

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit        
light.0 = 2,  -1.63, -14.75,  2.37, fx_strobe
light.1 = 2,  -1.63,  14.75,  2.37, fx_strobe
light.2 = 2,  -5.79,  0.000, -1.08, fx_beacon
light.3 = 4,   0.50,  0.000,  1.20, fx_vclightwhi
               
[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to  1/2 and 1/8 respectively.
elevator = 100,  180
aileron  = 200, 1000
rudder   = 200, 1000

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=1,0

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

[fuel]
LeftMain  = -1.5, -2.7, 2.4, 9.0, 0.3  //Longitudinal(feet),Lateral(feet),Vertical(feet),Usable(gallons),Unusable(gallons)
RightMain = -1.5,  2.7, 2.4, 9.0, 0.3  //Longitudinal(feet),Lateral(feet),Vertical(feet),Usable(gallons),Unusable(gallons)
fuel_type = 1                          //Fuel type: 1 = Avgas,2 = JetA
number_of_tank_selectors=1                    
electric_pump=1

[airplane_geometry]
wing_area               = 147.1                 //Square feet
wing_span               = 29.4                  //Feet
wing_root_chord         = 5.0                   //Feet
wing_dihedral           = 1.1                   //Degrees
wing_incidence          = 2.5                   //Degrees
wing_twist              = 0.0                   //Degrees
oswald_efficiency_factor= 0.8                   //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 0                     //Degrees, wing leading edge
wing_pos_apex_lon       = -2.4                  //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = 0.0                   //Feet, vertical distance from reference point, positive going up
htail_area              = 39.0                  //Square feet
htail_span              = 11.7                  //Feet
htail_pos_lon           = -18.3                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 0.0                   //Feet, vertical distance from reference point, positive going up
htail_incidence         = 3.2                   //Degrees
htail_sweep             = 10.0                  //Degrees, horizontal tail leading edge
vtail_area              = 18.0                  //Square feet
vtail_span              = 4.8                   //Feet, tip to body
vtail_sweep             = 40.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -16.2                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 1.5                   //Feet, vertical distance from reference point, positive going up
elevator_area           = 16.6                  //Square feet
aileron_area            = 18.3                  //Square feet
rudder_area             = 6.7                   //Square feet
elevator_up_limit       = 28.0                  //Degrees
elevator_down_limit     = 17.0                  //Degrees
aileron_up_limit        = 20.0                  //Degrees
aileron_down_limit      = 14.0                  //Degrees
rudder_limit            = 16.0                  //Degrees
elevator_trim_limit     = 19.5                  //Degrees
spoiler_limit           = 1.0                   //Degrees
spoilerons_available    = 0                     //Spoilerons Available?
aileron_to_spoileron_gain = 0                   //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0                 //Degrees
min_flaps_for_spoilerons = 0                    //Minimum flap handle position when spoilerons activate

[flaps.0]
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.5                                  // 0.0 .. 1.0
extending-time   = 5                                    // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 10                                   // degrees
flaps-position.2 = 20                                   // degrees
flaps-position.3 = 30                                   // degrees
damaging-speed   = 100                                 // KIAS
blowout-speed    = 120                                  // KIAS
lift_scalar = 1.0                                       
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 3                                         //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None

[Reference Speeds]
flaps_up_stall_speed    = 40.00                //Knots True (KTAS)
full_flaps_stall_speed  = 35.65                //Knots True (KTAS)
cruise_speed            = 102.6                //Knots True (KTAS)
max_indicated_speed      =135.0                //Knots True (KTAS)

[autopilot]
autopilot_available= 1
flight_director_available= 0
default_vertical_speed=1100.0
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

[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

[brakes]
parking_brake = 1                       //Parking brake available
toe_brakes_scale=1.0                    //Brake scalar
differential_braking_scale = 1.0        //Delta on the amount of brake when the rudder pedals deflected

[hydraulic_system]
normal_pressure=0.000000

[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0