[fltsim.0]
title=Cessna 195 CC-FCC
sim=c195
model=
panel=
sound=
texture=CC-FCC
panel_alias =
sound_alias =
kb_checklists=
kb_reference=
atc_id=CC-FCC
ui_manufacturer=Cessna
ui_type=195
ui_variation=CC-FCC
description=Este es el esquema real de pintura del CC-FCC, actualmente, en la realidad, este avión se encuentra en el Museo Aeronautico Nacional, ubicado en el Aeropuerto de Los Cerrillos (SCTI), en Santiago de Chile. Existe un avión gemelo de este en el Aeropuerto Internacional Carriel Sur de la Ciudad de Concepción (SCIE).
atc_heavy=0
atc_airline=
atc_flight_number=CC-FCC


[General]
atc_type=CESSNA
atc_model=195
editable=1
performance=son más o menos las mismas performances de un C206 con la salvedad de un motor radial y patín de cola, espero encontrar performances originales en algún momento.


[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               (0=Undamped, 1=Critically Damped)
        //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)
//GEAR
point.0 = 1.000, -18.000, 0.000, -1.500, 1600.000, 0.000, 0.250, 80.000, 0.200, 2.500, 0.700, 0.000, 0.000, 0.000, 0.000, 0.000
point.1 = 1.000, 2.000, -4.000, -5.900, 1600.000, 1.000, 0.600, 0.000, 0.300, 2.500, 0.700, 0.000, 0.000, 2.000, 0.000, 0.000
point.2 = 1.000, 2.000, 4.000, -5.900, 1600.000, 2.000, 0.600, 0.000, 0.300, 2.500, 0.700, 0.000, 0.000, 3.000, 0.000, 0.000
//SCRAPES
point.3= 2.000, -0.180, -18.060, 1.400, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, -0.180, 18.060, 1.400, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -20.000, 0.000, 0.600, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 8.200, 0.000, -1.300, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_pitch = 12.000
static_cg_height = 5.000

[exits]
number_of_exits=2
exit_rate.0=0.8 //opens using shift+e and part name passenger_door
exit_rate.1=0.8 //opens using shift+e+2 and part name cargo_door

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3,  -0.18, -18.06,  1.40, fx_navredh ,
light.1 = 3,  -0.18,  18.06,  1.40, fx_navgreh ,
light.2 = 3, -19.90,   0.00,  0.62, fx_navgreh ,
light.3 = 2,  -0.18, -18.06,  1.40, fx_strobeh ,
light.4 = 2,  -0.18,  18.06,  1.40, fx_strobeh ,
light.5 = 1,  -9.79,   0.00,  1.20, fx_beaconh ,
light.6 = 4,   0.56,   0.00,  1.25, fx_vclight,

[fuel]
LeftMain=-0.25,-7.5,2.5,44.0,2.5    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons),
RightMain=-0.25,7.5,2.5,44.0,2.5    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons),
fuel_type=1.000000
number_of_tank_selectors=1

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 700.0
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

[brakes]
toe_brakes_scale=1.000000
parking_brake=1

[stall_warning]
type=1






[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

[WEIGHT_AND_BALANCE]
empty_weight=2228		

reference_datum_position=0.0, 0, 0	
empty_weight_CG_position=0.0, 0, 0
max_number_of_stations=50

station_load.0=170,  3.0, -1.5, 0.0		//Pilot    # 1        
station_load.1=170,  3.0,  1.5, 0.0		//Co-Pilot # 2
station_load.2=160,  0.2, -1.5, 0.0		//Rear Pax # 3
station_load.3=160,  0.2,  1.5, 0.0		//Rear Pax # 4
station_load.4=0, -3.4, -1.5, 0.0		//Rear Pax # 5
station_load.5=0, -3.4,  1.5, 0.0		//Rear Pax # 6
station_load.6=100, -4.5,  0.0, 0.0		//Baggage Aft 100Lbs max 
empty_weight_roll_MOI=4200.000000
empty_weight_pitch_MOI=9900.000000
empty_weight_yaw_MOI=7200.000000
empty_weight_coupled_MOI=0.000000

[ground_reaction]
main_gear_damping_ratio=1.0
center_gear_damping_ratio=1.0

[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

[airplane_geometry]
wing_area=182.000000
wing_span=39.666667
wing_root_chord=4.916670
wing_dihedral=2.999268
wing_incidence=0.900879
wing_twist=-0.999756
oswald_efficiency_factor=0.815740
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=1.229000
wing_pos_apex_vert=0.000000
htail_area=46.000000
htail_span=14.500000
htail_pos_lon=-15.833333
htail_pos_vert=0.000000
htail_incidence=3.246460
htail_sweep=0.000000
vtail_area=18.000000
vtail_span=4.837355
vtail_sweep=0.000000
vtail_pos_lon=-14.583333
vtail_pos_vert=4.666667
elevator_area=17.500000
aileron_area=14.000000
rudder_area=11.000000
elevator_up_limit=25.000001
elevator_down_limit=20.000001
aileron_up_limit=20.000001
aileron_down_limit=15.000001
rudder_limit=27.000001
elevator_trim_limit=20.000001
spoiler_limit=0.000000
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000

[Flaps.0]
type=1                                                 // 1 - tail, 2 - lead
span-outboard=0.5                                      // 0.0 .. 1.0
extending-time=8.0                                     // seconds
system_type=0
flaps-position.0=0.0,0.0                               // degrees
flaps-position.1=10.0,0.0                              // degrees
flaps-position.2=20.0,0.0                              // degrees
flaps-position.3=40.0,0.0                              // degrees
damaging-speed=250                                     // KIAS
blowout-speed=300                                      // KIAS
system_type=0                                          //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None


[GeneralEngineData]
engine_type=0
Engine.0=6.666667,0.0,0.0
fuel_flow_scalar=1.0

[piston_engine]
cylinder_displacement=87.000000
compression_ratio=8.000000
number_of_cylinders=6
max_rated_rpm=2700                                     //Max rated RPM
max_rated_hp=310                                       //Max rated HP   285 continuous, 310 takeoff
fuel_metering_type=0
cooling_type=0
normalized_starter_torque=0.300000
turbocharged=1                                        //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=36.5                                    //Max design manifold pressure, (inHg)
min_design_mp=1.000000
critical_altitude=27000
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=6.750000
propeller_blades=2
propeller_moi=5.000000
beta_max=50.000000
beta_min=12.000000
min_gov_rpm=1100.000000
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=56.000000
full_flaps_stall_speed=44.800000
cruise_speed=134

[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

[keyboard_response]
elevator=150.00,250.00
aileron=150.00,250.00
rudder=150.00,250.00

[Views]
eyepoint=-1.871104,-1.076526,1.460999

[direction_indicators]
direction_indicator.0=1,0