[fltsim.0]
title=Casa 235 pkit
sim=Casa 235
model=
panel=MIO
sound=
texture=pkit
kb_checklists=
ui_manufacturer=CASA
ui_type=CASA CN235
ui_variation=pkit
atc_heavy=0
atc_id=
atc_airline=casa
atc_flight_number=
description=




[General]
atc_type=CASA
atc_model=CN235
editable=1
performance=CASA CN-235 - Span: 84.8 ft Length: 70.2 ft Height: 26.1 ft Weight: 36,380 lbs. max.  Engines: 2 x General Electric CT7-9C3 turboprops, 1,750 hp each Crew: 3/4 Maximum speed: 260 mph. Cruising speed: 245 mph. Range: 2,730 miles Service Ceiling: 25,000 ft.
Category=airplane

; Length  70 ft 2 in  
; Wingspan  84 ft 8 in  
; Operational specifications   
; Maximum takeoff weight  36,376 lb  
; Maximum landing weight  36,376 lb  
; Maximum payload  13,227 lb  
; Maximum cruising speed  245 ktas.  
; Takeoff distance at 50 ft (S/L, ISA, MTOW)  2,075 ft  
; Landing distance from 50 ft (S/L, ISA, MTOW)  2,365 ft  
; MTOW (Lb) 36,376 
; MLW (Lb) 36,376  //no weight restriction to landing
; Max payload (Lb)  13,100  
; Max fuel capacity (Lb)  9,150 (1,380 gal) 


[WEIGHT_AND_BALANCE]
max_gross_weight = 36376.000
empty_weight     = 14802.000

reference_datum_position     = 0.000, 0.000, 0.000
empty_weight_CG_position     = 0.000, 0.000, 0.000

max_number_of_stations = 20

station_load.0 = 340.00, 18.00, 0.00, 0.00, Pilot & co-pilot


;Moments of Inertia
empty_weight_pitch_MOI  = 139480.000
empty_weight_roll_MOI   = 83661.000
empty_weight_yaw_MOI    = 98435.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[flight_tuning]
cruise_lift_scalar     =1.000
parasite_drag_scalar   =1.000
induced_drag_scalar    =1.000
elevator_effectiveness =1.000
aileron_effectiveness  =1.000
rudder_effectiveness   =1.000
pitch_stability        =1.000
roll_stability         =1.000
yaw_stability          =1.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness  =1.000
rudder_trim_effectiveness   =1.000

[GeneralEngineData]
engine_type = 5
Engine.0 = 8.300, -11.010, 1.500
Engine.1 = 8.300, 11.010, 1.500
fuel_flow_scalar   = 0.760
//fuel_flow_scalar   = 0.560
min_throttle_limit = -0.25        //Minimum percent throttle.  Generally negative for turbine reverser

[propeller]
thrust_scalar           =1.000
propeller_type          = 0
propeller_diameter      = 10.010
propeller_blades        = 4
propeller_moi           = 115.000
beta_max                = 62.000
beta_min                = 5.000
min_gov_rpm             = 1700.000
prop_tc                 = 0.004
gear_reduction_ratio    = 14.200
fixed_pitch_beta        = 0.000
low_speed_theory_limit  = 80.000
prop_sync_available     = 1
prop_deice_available    = 1
prop_feathering_available= 1
prop_auto_feathering_available= 1
min_rpm_for_feather     = 700.000
beta_feather            = 86.000
power_absorbed_cf       = 0.900
defeathering_accumulators_available= 1 
prop_reverse_available  = 1.000
minimum_on_ground_beta  = 1.000
minimum_reverse_beta    = -14.000

[TurbineEngineData]
fuel_flow_gain          = 0.011
inlet_area              = 1.000
rated_N2_rpm            = 33000.000  
static_thrust           = 186.000
afterburner_available   = 0

[turboprop_engine]
power_scalar            =1.000
maximum_torque          = 5500.860
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[exits]
number_of_exits = 3
exit_rate.0 = 0.30                               ;Percent per second
exit_rate.1 = 0.10                               ;Percent per second

[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, 5 , 17.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 2 , 17.0
marker_beacon      = 1, 2 , 17.0
gear_warning       = 0, 2 , 17.0
fuel_pump          = 0, 5 , 17.0
starter1           = 0, 55, 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                        <0=none,1=wheel, 2=scrape, 3=float>
        //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)


[contact_points]
//point.0= 1.0, 21.95,  0.00, -8.30, 1481.0, 0.0, 0.75, 60.0, 0.296, 2.5, 0.952, 4.0, 4.0, 0.0, 210.0, 235.0
point.0= 1.0, 21.95, 0.00, -8.30, 1481.0, 0.0, 0.75, 60.0, 0.296, 2.5, 0.815, 4.000, 4.000, 0.000, 210.000, 235.000
point.1= 1.0, -2.00, -6.580, -8.740, 1574.000, 1.000, 0.980, 0.000, 0.642, 2.500, 0.815, 4.500, 4.500, 2.000, 210.000, 235.000
point.2= 1.000, -2.000, 6.580, -8.740, 1574.000, 2.000, 0.980, 0.000, 0.642, 2.500, 0.815, 4.500, 4.500, 3.000, 210.000, 235.000
point.3= 2.000, 0.000, -42.400, 4.700, 787.000, 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, 0.000, 42.400, 4.700, 787.000, 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, -26.700, 0.000, 0.000, 787.000, 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, 23.550, 0.000, -5.200, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.7= 2.000, 0.000, -6.600, -6.200, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 
point.8= 2.000, 0.000, 6.600, -6.200, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_pitch = -0.550
static_cg_height = 8.220
gear_system_type=1      //Hydraulic

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    =  0.0     //Flap angle that activates warning at idle
flap_limit_power   = 20.0     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1        //Parking brake available
toe_brakes_scale = 1.0   //Brake scalar
auto_brakes=4

[hydraulic_system]
normal_pressure = 3000.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,0,0   //pumps on Eng1,2

[Views]
eyepoint = 20.00, -1.8, 1.5   

[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, 1
Adf.1         = 1, 1
Adf.2         = 1, 1
Transponder.1 = 1
Marker.1      = 1

[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 = 150, 250
aileron  = 150, 250
rudder   = 150, 250

[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=3,0

[airspeed_indicators]
//airspeed_indicator.0 = 1.060,  -2.00

[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,  -4.00, -42.30,  5.05, fx_navred ,
light.1 = 3,  -4.00,  42.30,  5.05, fx_navgre ,
light.2 = 3, -43.40,   0.00,  4.00, fx_navwhi ,
light.3 = 2,  -4.00, -42.30,  5.00, fx_strobe ,
light.4 = 2,  -4.00,  42.30,  5.00, fx_strobe ,
light.5 = 1, -39.00,   0.00, 20.00, fx_beacon ,
light.6 = 1,   9.15,   0.00, -5.60, fx_beacon ,
light.7 = 2, -43.30,   0.00,  5.00, fx_strobe ,
light.8 = 4,  21.80,   0.00,  1.60, fx_vclight,
light.9 = 5,   7.10,  -6.55, -5.58, fx_landing
light.10= 5,   7.10,   6.55, -5.58, fx_landing

[EFFECTS]
WheelSnowSpray=fsfx_PFX_M_WheelSnowSpray //FSFX_PFX_Effect
SnowEngineWash=fsfx_PFX_M_SnowEngineWash //FSFX_PFX_Effect
WheelWetSpray=fsfx_PFX_M_WheelWetSpray //FSFX_PFX_Effect
WetEngineWash=fsfx_PFX_M_WetEngineWash //FSFX_PFX_Effect
SkidPavement=fsfx_PFX_M_skidmark //FSFX_PFX_Effect
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
//touchdown=fx_tchdwn_s, 1
touchdown=fx_tchdwn, 1

[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = 0.000, -4.500, -1.000, 875, 7
RightMain= 0.000, 4.500, -1.000, 875, 7
fuel_type= 2                                //Fuel type: 1 = Avgas, 2 = JetA 
number_of_tank_selectors = 2                    
electric_pump=1

[airplane_geometry]
wing_area               = 636.000
wing_span               = 84.600
wing_root_chord         = 8.990
wing_dihedral           = 2.000
wing_incidence          = 2.000
wing_twist              = -1.500
oswald_efficiency_factor= 0.700
wing_winglets_flag      = 0
wing_sweep              = 1.000
wing_pos_apex_lon       = 2.100
wing_pos_apex_vert      = 4.000

htail_area              = 80.000
htail_span              = 26.200
htail_pos_lon           = -36.800
htail_pos_vert          = 2.000
htail_incidence         = 0.500
htail_sweep             = 3.000

vtail_area              = 60.100
vtail_span              = 9.400
vtail_sweep             = 20.000
vtail_pos_lon           = -35.000
vtail_pos_vert          = 4.200

elevator_area           = 31.700
aileron_area            = 36.000
rudder_area             = 49.100

elevator_up_limit       = 17.000
elevator_down_limit     = 15.000
aileron_up_limit        = 18.000
aileron_down_limit      = 18.000
rudder_limit            = 25.000
elevator_trim_limit     = 12.000
spoiler_limit           = 0.000
spoilerons_available    = 0
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
auto_spoiler_available=0
positive_g_limit_flaps_up=3.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-1.299145
negative_g_limit_flaps_down=-1.099359

[Reference Speeds]
flaps_up_stall_speed    = 131.000
full_flaps_stall_speed  = 98.800
cruise_speed            = 245.000
max_mach                = 0.58
max_indicated_speed     = 276                   //Red line (KIAS)

//[TailHook]
//tailhook_length=1                              ;(feet)
//tailhook_position= -21.0, 0.0, -3.0            ;(feet) longitudinal, lateral, vertical positions from datum
//cable_force_adjust= 0.0

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=0
yaw_damper_gain = 1.0
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=1
autothrottle_max_rpm=105.000
pitch_takeoff_ga=8.000
use_no_default_pitch=1 // 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank=1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode.
default_pitch_mode=0
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=0.000000

[forcefeedback]
stick_shaker_magnitude=3000             ; 0 - 10000
stick_shaker_direction=0                ; 0 - 35999 degrees
stick_shaker_period=111111              ; in microseconds
gear_bump_nose_magnitude=2000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=2700           ; 0 - 10000
gear_bump_left_direction=9000           ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=27000         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=1300            ; 0 - 10000
ground_bumps_angle1=08900               ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200             ; 0 - 10000
ground_bumps_angle2=09100               ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
crash_magnitude1=5000                   ; 0 - 10000
crash_direction1=01000                  ; 0 - 35999 degrees
crash_magnitude2=5000                   ; 0 - 10000
crash_direction2=9000                   ; 0 - 35999 degrees
crash_period2=75000                     ; in microseconds
crash_duration2=2500000                 ; in microseconds

[stall_warning]
type=2
stick_shaker=1

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 12.000
system_type= 1
damaging-speed= 235.000
blowout-speed= 260.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 35.000, 0.000

[pitot_static]
pitot_heat=1.000000

[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0

[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000

[deice_system]
structural_deice_type=2