[fltsim.0]
title=CR-32-Ter
sim=CR-32-Ter
model=
panel=
sound=
texture=
kb_checklists=
ui_manufacturer=FIAT AVIAZIONE
ui_type=CR 32-Ter 
ui_variation= ''Escuadrilla Cucaracha''
atc_heavy=0
atc_id=S21 
atc_airline=
atc_flight_number=
description=FIAT CR32 FIGHTER. Eng:Fiat A30RA  600 HP.\nA.M.I. Italian Museum\nPainting ''escuadrilla cucaracha''.
 
[fltsim.1]
title=CR-32-TerPAINT1935
sim=CR-32-Ter
model=
panel=
sound=
texture=1935
kb_checklists=
ui_manufacturer=FIAT AVIAZIONE
ui_type=CR 32-Ter 
ui_variation= "Squadriglia Folle"
atc_heavy=0
atc_id=S21 
atc_airline=
atc_flight_number=
description=FIAT CR32 FIGHTER. Eng:Fiat A30RA  600 HP.\nPainting 1935 "Squadriglia Folle".

[General]
atc_type=        
atc_model=
editable=0
performance=Superlative aerobatic performer biplane\nEng:Fiat A30RA 600 HP (C.C.W.propeller).\n Maxspeed:355Kmh\nThrust levers acted opposite.\nThe airplane really carried two airspeed indicators.\nModel textures and Panel by G. Quai\ngauges by I.D'Attomo. 
                        
Category=airplane

[WEIGHT_AND_BALANCE]
max_gross_weight = 2095                       
empty_weight = 1345                            

reference_datum_position     =  1.8, 0, 0       
empty_weight_CG_position     = -1.4, 0, 0      

max_number_of_stations = 50

station_load.0 = "170, -5.9, 0.0, 0.0, Pilot"           

;Moments of Inertia
empty_weight_pitch_MOI   = 717
empty_weight_roll_MOI    = 395
empty_weight_yaw_MOI     = 856
empty_weight_coupled_MOI = 0.0


[electrical]
max_battery_voltage = 12.0
generator_alternator_voltage = 13.8
max_generator_alternator_amps = 40.0

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

avionics_bus       = 0, 5 , 9.5
avionics           = 1, 5 , 9.5
additional_system  = 0, 2 , 9.5
marker_beacon      = 1, 2 , 9.0
fuel_pump          = 0, 5 , 9.0

[flight_tuning]
cruise_lift_scalar     = 1.0
parasite_drag_scalar   = 2.0
induced_drag_scalar    =1.2
elevator_effectiveness = 0.48
aileron_effectiveness  = 0.48
rudder_effectiveness   = 1.0
pitch_stability        = 1.0
roll_stability         = 1.2   
yaw_stability          = 1.0
elevator_trim_effectiveness =2.5 
aileron_trim_effectiveness  = 2.0
rudder_trim_effectiveness   = 2.0
p_factor_on_yaw          = 0.5
torque_on_roll           = 0.5

[flaps.0]       
type             = 0                                  
system_type      = 4                                   

[GeneralEngineData]
engine_type = 0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket,    5=Turboprop
Engine.0 = 3.5, 0.0, 0.60                    // vertical distance from reference datum
fuel_flow_scalar=1.00                        
min_throttle_limit = 0.0                     

[piston_engine]
power_scalar=1.0                     
cylinder_displacement=90.25          
compression_ratio=8.700                     
number_of_cylinders=6                          
max_rated_rpm=2700.00                       
max_rated_hp=300.00                             
fuel_metering_type=0
cooling_type=0
normalized_starter_torque=0.30                 
turbocharged=0 
max_design_mp=0.00
min_design_mp=0.00
critical_altitude=0.00
emergency_boost_type=0 
emergency_boost_mp_offset=0.00
emergency_boost_gain_offset=0.00
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar= 1.0     
idle_rpm_mechanical_efficiency_scalar= 1.0     
max_rpm_friction_scalar= 1.0                   
idle_rpm_friction_scalar= 1.0                 

[propeller]
thrust_scalar=1.83                          
propeller_type= 0                              
propeller_diameter=6.0                     
propeller_blades= 2                       
propeller_moi= 5.9                           
beta_max= 34                                   
beta_min= 17                                   
min_gov_rpm= 1400                             
prop_tc= 0.1                                    
gear_reduction_ratio= 1.0                       
fixed_pitch_beta= 0                            
low_speed_theory_limit= 80  
prop_sync_available= 0                          
prop_deice_available= 0                        
prop_feathering_available= 0                   
prop_auto_feathering_available= 0               
min_rpm_for_feather= 0                         
beta_feather= 0                                
power_absorbed_cf= 0                           
defeathering_accumulators_available= 0         
prop_reverse_available= 0                       
minimum_on_ground_beta= 0                      
minimum_reverse_beta= 0                        

[contact_points]
point.0=1, -16.50,   0.00, -1.36, 1977.95,  0, 0.4100, 50.0, 0.4, 2.5, 0.9, 0.0, 0.0, 0.0, 0.0, 0.0
point.1=1,  -0.05,  -2.92, -4.5, 1968.50,  1, 1.1660,   0.0, 0.6, 2.5, 0.9, 0.0, 0.0, 2.0, 0.0, 0.0
point.2=1,  -0.05,   2.92, -4.5, 1968.50,  2, 1.1660,   0.0, 0.6, 2.5, 0.9, 0.0, 0.0, 3.0, 0.0, 0.0

point.3=2,  -1.80, -12.25, -1.17,  787.40, 0, 0.0000,   0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0
point.4=2,  -1.80,  12.25, -1.17,  787.40, 0, 0.0000,   0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0
point.5=2, -15.80,   0.00,  4.33,  787.40, 0, 0.0000,   0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0
point.6=2,   1.67,   0.00, -1.83,  787.40, 0, 0.0000,   0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0

static_pitch = 10.54
static_cg_height =3.80 

[brakes]
parking_brake = 1      
toe_brakes_scale = 0.6  
differential_braking_scale = 1.0       

[hydraulic_system]
normal_pressure = 0.0   

[Views]
eyepoint = -3.70, 0.00, 2.35

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

[SMOKESYSTEM]                //for FSX
smoke.0=0.00, -15.0, 0.0, fx_smoke_r
smoke.1=0.00, 15.0, 0.0, fx_smoke_w      

//[SMOKESYSTEM]        //double bar the above for FSX than remouve the double bar on the left for FS2004
smoke.0=0.00, 0.00,15.00, fx_smoke_w  
smoke.1=0.00, 0.00,-15.00, fx_smoke_r


[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 = 140,  240
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

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=1,0

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit        
//light.0 =3,  -1.62, -13.28,-0.15, fx_navred
//light.1 =3,  -1.62,  13.28,-0.15, fx_navgre
light.2 = 4, -3.5, 0.00, 1.20, fx_vclighth 

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

[fuel]
Center1   = -2.6,  0.0,  0.0, 11.1, 0.0      
Center2   = -0.6,  0.0,  0.0,  2.3, 0.0       
LeftMain  = -1.8, -2.1, -0.8, 15.9, 0.0       
RightMain = -1.8,  2.1, -0.8, 15.9, 0.0      
fuel_type = 1                                
number_of_tank_selectors = 1                    
electric_pump=1

[airplane_geometry]
wing_area               = 112.0                
wing_span               = 24.6                 
wing_root_chord         = 4.8                   
wing_dihedral           = 2.6                  
wing_incidence          = 0.0                   
wing_twist              = 0.0                  
oswald_efficiency_factor= 0.6                  
wing_winglets_flag      = 0                    
wing_sweep              = 3.0                   
wing_pos_apex_lon       = -0.2    
wing_pos_apex_vert      = 0.0                   
htail_area              = 28.0                 
htail_span              = 10.5                 
htail_pos_lon           = -13.1                 
htail_pos_vert          = 0.0                   
htail_incidence         = 0.0                  
htail_sweep             = 10.0                   
vtail_area              = 15.0                 
vtail_span              = 4.4                   
vtail_sweep             = 20.0                
vtail_pos_lon           = -14.3                 
vtail_pos_vert          = 1.5                  
elevator_area           = 10.0                 
aileron_area            = 18.4               
rudder_area             = 7.0                
elevator_up_limit       = 26.0               
elevator_down_limit     = 26.0                  
aileron_up_limit        = 30.0                  
aileron_down_limit      = 30.0                  
rudder_limit            = 30.0                 
elevator_trim_limit     = 15.0               
spoiler_limit           = 0.0                 
spoilerons_available    = 0                     
aileron_to_spoileron_gain = 0                  
min_ailerons_for_spoilerons = 0               
min_flaps_for_spoilerons = 0                   
auto_spoiler_available=0
positive_g_limit_flaps_up=10.00
positive_g_limit_flaps_down=10.00
negative_g_limit_flaps_up=-10.00
negative_g_limit_flaps_down=-10.00

[Reference Speeds]
flaps_up_stall_speed    = 55.0                 
full_flaps_stall_speed  = 55.0                 
cruise_speed            = 150.0                
max_indicated_speed     = 220                  

[autopilot]
autopilot_available=1 //0
flight_director_available= 0
default_vertical_speed=700.00
autothrottle_available=0
pitch_takeoff_ga=8.00
max_pitch=10.000000
max_pitch_acceleration=1.00
max_pitch_velocity_lo_alt=2.00
max_pitch_velocity_hi_alt=1.50
max_pitch_velocity_lo_alt_breakpoint=20000.00
max_pitch_velocity_hi_alt_breakpoint=28000.00
max_bank_acceleration=1.80
max_bank_velocity=3.00
max_throttle_rate=0.100
nav_proportional_control=9.00
nav_integrator_control=0.250
nav_derivative_control=0.000
nav_integrator_boundary=2.500
nav_derivative_boundary=0.000
gs_proportional_control=9.520
gs_integrator_control=0.260
gs_derivative_control=0.000
gs_integrator_boundary=0.700
gs_derivative_boundary=0.000
yaw_damper_gain=0.000

[forcefeedback]
ground_bumps_magnitude1=3000            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=4.0
ground_bumps_slope1=0.25
ground_bumps_magnitude2=350             ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=0.7
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

[stall_warning]
type=2
stick_shaker=0

[pitot_static]
pitot_heat=0.000000
[vacuum_system]
max_pressure=5.150
vacuum_type=1
electric_backup_pressure=0.000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=0.000
bleed_air_scalar=1.000
[deice_system]
structural_deice_type=0


[CameraDefinition.0]
Title = "Landing Gear"
Guid = {96873AAD-621B-4C45-8A58-DEF7B7FCB051}
Description = View of the landing gear and left wing inboard flaps
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .52
ShowWeather = Yes
InitialXyz = -3.1, 0.7, -13
InitialPbh = 0, 0, 17
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.1]
Title = "Tail"
Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description = Looking forward from behind the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .75
ShowWeather = Yes
InitialXyz = 0.7, 2.5, -19.0
InitialPbh = 5, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.2]
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 = 0.5
ShowWeather = Yes
InitialXyz =12.8, 1.6, 0.3
InitialPbh = 6, 0, 270
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum

[CameraDefinition.3]
Title = "Left Wing"
Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
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 = 0.5
ShowWeather = Yes
InitialXyz = -12.8, 1.6, 0.3
InitialPbh = 6, 0, 90
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = No
ClipMode=Minimum

[CameraDefinition.4]
Title = "Nose"
Guid = {3208BD74-1898-2743-A507-826C97B75E1B}
Description =Offset from the nose looking back at the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .8
ShowWeather = Yes
InitialXyz = -1.5,0.5,16.0
InitialPbh = 0,0,175
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum


[CameraDefinition.001]
Title = "VC view"
Guid = {8ff6c134-098d-409f-baec-caba3f683f98}
Origin = Virtual Cockpit
MomentumEffect = YES
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = .6
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-0.15, 0.20, -0.10   
InitialPbh=18, 0, 0        

[CameraDefinition.002]
Title = "VC other view"
Guid = {8ff6c134-098d-409f-baec-caba3f683f98}
Origin = Virtual Cockpit
MomentumEffect = YES
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = .6
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-0.21, 0.02, -0.09
InitialPbh=16, 0, 0