//--------------------------Designed by Flysimware! 2012----------------------------




[fltsim.0]

title=Cessna 195 YELLOW

sim=C195

model=YellowRed
panel=

sound=

texture=Yellow

kb_checklists=Cessna195_check

kb_reference=Cessna195_check

ui_manufacturer="Cessna"

ui_type="195"

ui_variation="Yellow/Red"

ui_typerole="Single Engine Prop"

ui_createdby="Flysimware"

atc_id_color="yellow/red"

atc_id="N9833A"
description="Cessna 195"





[fltsim.1]

title=Cessna 195 Red

sim=C195

model=Red

panel=

sound=

texture=Red

kb_checklists=Cessna195_check
kb_reference=Cessna195_check

ui_manufacturer="Cessna"

ui_type="195"
ui_variation="Red"

ui_typerole="Single Engine Prop"

ui_createdby="Flysimware"

atc_id_color="red"

atc_id="FLYSIM"

description="Cessna 195"





[fltsim.2]

title=Cessna 195 Chrome

sim=C195

model=Chrome

panel=

sound=

texture=chrome

kb_checklists=Cessna195_check

kb_reference=Cessna195_check

ui_manufacturer="Cessna"
ui_type="195"

ui_variation="Chrome"

ui_typerole="Single Engine Prop"

ui_createdby="Flysimware"

atc_id_color="Chrome"

atc_id="N553CA"

description="Cessna 195"





[CameraDefinition.0]

Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = 7.5, 0.75, 0
InitialPbh = 5, 0, 270
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum


[CameraDefinition.1]
Title = "Left Wing"
Guid = {3A09FD6C-D406-4d8f-A5CD-789F5E0C14ED}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = -7.9, 0.75, -0.9
InitialPbh = 5, 0, 90
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum


[CameraDefinition.2]
Title = "Engine"
Guid = {D8D64955-2E9B-4e75-9D8B-789FBBFAC74A}
Description = View from the engine looking at the prop
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .50
ShowWeather = Yes
InitialXyz = 1.0, 1.4, 1.4
InitialPbh = 46, -20 , 302
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum


[CameraDefinition.3]
Title = "Tail"
Guid = {D8D67955-2E9B-4e75-9D8B-789FBBFAC64A}
Description = Looking forward from the tip of the vertical stabilizer
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.75
ShowWeather = Yes
InitialXyz = -1.3, -0.2, -7.65
InitialPbh = 5, 06, 12
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum


[CameraDefinition.001]
Title = "Right Seat"
Guid = {195EAB58-9E4A-1E2A-A34C-7899D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = 0.34
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=100
InitialXyz=0.64, 0.02, 0.05
InitialPbh=0, 0, 0


[CameraDefinition.002]
Title = "Radio Stack"
Guid = {195EAB58-9E4A-2E2A-A34C-7899D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.7
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=100
InitialXyz=0.29, -0.088, -0.1
InitialPbh=12, 0, 4


[CameraDefinition.003]
Title = "Circuit Box"
Guid = {195EAB58-9E4A-3E2A-A34C-7899D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.7
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=100
InitialXyz=-0.1, -0.42, -0.1
InitialPbh=2, 0, 2


[General]
atc_type=CESSNA
atc_model=C195
performance=
Category=airplane



[flight_tuning]

cruise_lift_scalar=1.0 

parasite_drag_scalar=0.6

induced_drag_scalar=0.6

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=1.0

aileron_trim_effectiveness=1.0 

rudder_trim_effectiveness=1.0 






[weight_and_balance]

max_gross_weight = 3400

empty_weight = 2050

reference_datum_position = 0.0, 0, 0

empty_weight_CG_position = 0.0, 0, 0


empty_weight_pitch_MOI = 3600

empty_weight_roll_MOI = 2537

empty_weight_yaw_MOI = 2200

empty_weight_coupled_MOI = 0




max_number_of_stations = 6


station_name.0 = "Pilot"    
station_name.1 = "Co Pilot"       
station_name.2 = "Passenger1" 
station_name.3 = "Passenger2"  
station_name.4 = "Passenger3"
station_name.5 = "Luggage"
station_load.0 = 170,   1.10, -0.80,  1.50
station_load.1 = 170,   1.00,  0.80,  1.50
station_load.2 = 0.00,  -1.00, -0.80, -1.50
station_load.3= 0.00,  -1.00,  0.00, -1.70
station_load.4= 0.00,  -1.00,  0.80, -1.70
station_load.5 = 0.00,  -3.00,  0.00, -2.60



[Views]
eyepoint=0,-0.8,0.9


[fuel]

fuel_type = 1

number_of_tank_selectors = 1

electric_pump = 1

LeftMain =1.0, -3.0, 0.65, 41.1, 1  

RightMain =1.0, 3.0, 0.65, 41.1, 1





[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop


engine_type = 0
fuel_flow_scalar = 1.100000
min_throttle_limit = 0.000000

engine.0 = 8.0, 0.000000, 0.000000





[piston_engine]

power_scalar = 1.0                                      //Piston power scalar

cylinder_displacement= 86.0                     	//Cubic inches per cylinder

compression_ratio= 8.5         				//Compression ratio

number_of_cylinders=7                           	//Number of cylinders

max_rated_rpm= 2600                                    //Max rated RPM

max_rated_hp= 400                           

           //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= 0.3                          //Starter torque factor

turbocharged= 0                                         //Is it turbocharged? 0=FALSE, 1=TRUE

max_design_mp= 39.5                                     //Max design manifold pressure, (inHg)

min_design_mp= 10                                       //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= 1.1                          //Scalar on idle RPM friction





[propeller]

thrust_scalar = 1.0                                  //Propeller thrust scalar

propeller_type= 0                                   //0=Constant Speed, 1=Fixed Pitch

propeller_diameter= 6.5                             //Propeller Diameter, (feet)

propeller_blades= 2                                 //Number of propeller blades

propeller_moi= 11.9                                 //Propeller moment of inertia

beta_max= 50.0                                      //Maximum blade pitch angle for constant speed prop, (degrees)

beta_min= 10.0                                      //Minimum blade pitch angle for constant speed prop, (degrees)

min_gov_rpm= 700                                    //Miminum governed RPM

prop_tc= 0.1                                       //Prop time-constant

gear_reduction_ratio= 0.69                         //Propeller gear reduction ratio

fixed_pitch_beta= 0                             //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= 1                         //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= 0.0                       //Miminum pitch angle on ground, (degrees)

minimum_reverse_beta= 0.0                         //Minimum pitch angle in reverse, (degrees)







[electrical]

max_battery_voltage = 24.0

generator_alternator_voltage = 28.0

max_generator_alternator_amps = 100.0

      

;BusType, MaxAmpLoad, MinVoltage   BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus 	   = 0, 10 , 15.0

avionics           = 1, 10 , 15.0

pitot_heat         = 0, 5 , 10.0

additional_system  = 0, 25 , 15.0

marker_beacon      = 1, 10 , 10.0

fuel_pump          = 0, 25 , 20.0

starter1           = 0, 40,  20.0

light_nav          = 0, 10 , 15.0

light_beacon       = 0, 10 , 15.0

light_landing      = 0, 15 , 15.0

light_taxi         = 0, 15 , 15.0

light_panel        = 0, 15 , 15.0

light_cabin        = 0, 2 , 5.0

light_recognition    = 0, 2 , 5.0


        


        //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                  (seconds)
        //14 Airspeed limit for retraction     (KIAS)
        //15 Airspeed that gear gets damage at (KIAS)





[contact_points]

point.0 = 1, -17.70,   0.00,   -1.519,   2574.8, 0, 0.45, 68, 0.15, 5.5, 0.50, 5, 5, 0, 0, 0

point.1 = 1,   1.70,  -3.85,   -5.800,   1574.8, 1, 0.8,  0,  0.15, 4.5, 0.80, 5, 5, 0, 0, 0

point.2 = 1,   1.70,   3.85,   -5.800,   1574.8, 2, 0.8,  0,  0.15, 4.5, 0.80, 5, 5, 0, 0, 0

point.3 = 2,  -1.40,  -18.4,    0.244,   1574.8, 0, 0,    0,  0,      0, 0, 0, 0, 5, 0, 0

point.4 = 2,  -1.40,   18.4,    0.244,   1574.8, 0, 0,    0,  0,      0, 0, 0, 0, 5, 0, 0

point.5 = 2, -19.10,   0.00,    -0.010,  1574.8, 0, 0,    0,  0,      0, 0, 0, 0, 9, 0, 0

point.6 = 2,    7.3,   0.00,   -2.970,   1574.8, 0, 0,    0,  0,      0, 0, 0, 0, 4, 0, 0





max_number_of_points = 21


static_pitch = 12.6

static_cg_height = 5.24

tailwheel_lock = 1

gear_system_type = 1

max_number_of_points = 7



[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=taxi, 7=recognition, 8=wing, 9=logo, 10=cabin  
     



light.1 = 10,  -2.2,      0.00,   -0.3,  fx_vclighthLow

light.3 = 9,    1.5,     1.4,    -0.3,   fx_vclightRed

light.4 = 7,    1.5,     -1.4,    -0.3,   fx_vclightRed




[brakes]

toe_brakes_scale=1.0

parking_brake=1
differential_braking_scale = 1.0





[smokesystem]


smoke.0 =   2.3,  -1.2, -0.8, fx_smokecustom





[Radios]


// Radio Type=availiable, standby frequency, has glide slope


Audio.1=1 

Com.1=1, 1 

Nav.1=1, 1, 1 

Transponder.1=1




[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

windshield_rain_effect_available = 1





[airplane_geometry]
wing_area = 218.000000

wing_span = 36.2

wing_root_chord = 8.21

wing_dihedral = 0.2

wing_incidence = 0.0

wing_twist = 0.0

oswald_efficiency_factor = 0.5

wing_winglets_flag = 0

wing_sweep = 0.0

wing_pos_apex_lon = 0.65

wing_pos_apex_vert = 2.1


htail_area = 29.0

htail_span = 9.0

htail_pos_lon = -16.71

htail_pos_vert = 0.4

htail_incidence = 0.0
htail_sweep = 1.8


vtail_area = 17.000000

vtail_span = 4.22

vtail_sweep = 1.0

vtail_pos_lon = -16.60

vtail_pos_vert = 0.3


elevator_area = 16.60

aileron_area = 20.300000

rudder_area = 14.60

elevator_up_limit = 42.0

elevator_down_limit = 34.0

aileron_up_limit = 25.0

aileron_down_limit = 20.0

rudder_limit = 40.0

elevator_trim_limit = 35.0

spoiler_limit = 0.0


aileron_to_spoileron_gain = 0.000000

spoiler_handle_available = 0

min_ailerons_for_spoilerons = 0.000000

min_flaps_for_spoilerons = 0.000000

spoilerons_available = 0

auto_spoiler_available=0
positive_g_limit_flaps_up=4.000000

positive_g_limit_flaps_down=2.000000

negative_g_limit_flaps_up=-1.500000

negative_g_limit_flaps_down=-1.500000





[Reference Speeds]
flaps_up_stall_speed=69.000000 

full_flaps_stall_speed=62.000000 

cruise_speed=170.0 

max_indicated_speed=250.000000





[exits]

number_of_exits = 2

exit_rate.0 = 0.4  ;Percent per second

exit_rate.1 = 0.4  ;Percent per second




[autopilot]

autopilot_available=0
flight_director_available=0 
default_vertical_speed=500.000000 
autothrottle_available=0 
pitch_takeoff_ga=8.000000 
use_no_default_pitch=0          

use_no_default_bank=1
default_bank_mode=0
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=0.00000
yaw_damper_gain=1.000000

[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=1
stick_shaker=0



[attitude_indicators]
attitude_indicator.0=1



[turn_indicators]

//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro

turn_indicator.0=1,1    //Turn AND Bank

[pitot_static]
pitot_heat=1.000000




[vacuum_system]

max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,0,0,0




[pneumatic_system]

max_pressure=0.000000
bleed_air_scalar=0.000000





[deice_system]

structural_deice_type=0

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





[forcefeedback]

gear_bump_nose_magnitude = 1000
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 = 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 = 2000
crash_direction1 = 1000
crash_magnitude2 = 2000
crash_direction2 = 9000
crash_period2 = 7500
crash_duration2 = 2500000





[flaps.0]       //Trailing Edge Flaps



type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.5                                  // 0.0 .. 1.0

extending-time   = 9                                    // seconds

flaps-position.0 = 0                                    // degrees

flaps-position.1 = 10                                   // degrees

flaps-position.2 = 15                                   // degrees

flaps-position.3 = 20                                   // degrees

flaps-position.4 = 25                                   // degrees

flaps-position.5 = 30                                   // degrees

flaps-position.6 = 35                                   // degrees

flaps-position.7 = 40                                   // degrees

flaps-position.8 = 45                                   // degrees

flaps-position.9 = 50                                   // degrees

flaps-position.10 = 55                                  // degrees

damaging-speed   = 170                                  // KIAS

blowout-speed    = 190                                  // KIAS

lift_scalar = 0.8

drag_scalar = 0.8
pitch_scalar= 0.3
system_type = 0                                       //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None






