[fltsim.0]
title=Beechcraft King Air 200
sim=200
model=
panel= 
sound=
texture=
kb_checklists=
ui_manufacturer=Beechcraft
ui_type=Super King Air 200
ui_variation=Blue and White
atc_heavy=0
atc_id=N200KA
atc_airline=
atc_flight_number=
description=Beechcraft's original Super King Air 200 by Dee Waldron. (Full flying version.) The 100 series airframe was completly redesigned and became the "Super King Air 200".\nOriginal B200 models (for AI use) by Henry Tomkiewicz.

[General]
atc_type=KingAir
atc_model=BE20
editable=1
performance=Maximum speed 249 kts, Maximum Range 1340 nm


[WEIGHT_AND_BALANCE]
max_gross_weight=12500                        // (pounds)
empty_weight=7315                          // (pounds)


reference_datum_position=0.0, 0, 0       // (ft) distance from FS Ref position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0.0, 0, 0       // (ft) long, lat, vert distance from specified datum

max_number_of_stations=50

station_load.0=190,  5.0, -2.0, 0.0           //Pilot           Weight (lbs), long, lat, vert positions from datum (ft)
station_load.1=190,  5.0,  2.0, 0.0           //Co-Pilot        Weight (lbs), long, lat, vert positions from datum (ft)
station_load.2=185, -2.1, -2.0, 0.0           //Passenger       Weight (lbs), long, lat, vert positions from datum (ft)
station_load.3=135, -2.1,  2.0, 0.0           //Passenger       Weight (lbs), long, lat, vert positions from datum (ft)
station_load.4=195, -5.3, -2.0, 0.0           //Passenger       Weight (lbs), long, lat, vert positions from datum (ft)
station_load.5=140, -5.3,  2.0, 0.0           //Passenger       Weight (lbs), long, lat, vert positions from datum (ft)


;Moments of Inertia
empty_weight_pitch_MOI=30000
empty_weight_roll_MOI=18200
empty_weight_yaw_MOI=36500
empty_weight_coupled_MOI=0.0


[fuel]
LeftMain=0.0, -14.5, -1.0, 185.0, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux=0.0,  -6.0, -1.5,  70, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=0.0,  14.5, -1.0, 185.0, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux=0.0,   6.0, -1.5,  70, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=2                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1                    
electric_pump=1

//Maximum Fuel Load 544 US Gallons, 3644 LB. Mains 185 US Gallons Aux 87 US Gallons
// 8 passenger seats

[airplane_geometry]
wing_area=303                
wing_span=54.5              
wing_root_chord=3.50	 	                   
wing_dihedral=6.0                   
wing_incidence=1.66		 
wing_twist=0			 
wing_pos_apex_lon=1.4                 
wing_pos_apex_vert=-1                  
oswald_efficiency_factor=0.725
wing_winglets_flag=0                
wing_sweep=0.0              
htail_area=68
htail_span=18.42
htail_pos_lon=-15.0
htail_pos_vert=1.0
htail_incidence=0.0
htail_sweep=20.0                  
vtail_area=52.3
vtail_span=7.4                  
vtail_sweep=40.0                  
vtail_pos_lon=-20.5                
vtail_pos_vert=4.1                   
elevator_area=17.0                  
aileron_area=13.5                  
rudder_area=7.3                   
elevator_up_limit=20.0                 
elevator_down_limit=14.0                 
aileron_up_limit=25.0                
aileron_down_limit=15.0                  
rudder_limit=25.0                 
elevator_trim_limit=18.8                 
spoiler_limit=90.0                  
spoilerons_available=0                     
aileron_to_spoileron_gain=0                 
min_ailerons_for_spoilerons=0                
min_flaps_for_spoilerons=0           
    
[Reference Speeds]
flaps_up_stall_speed=99.0                  
full_flaps_stall_speed=76.0                 
cruise_speed=278.0                 
max_indicated_speed=259.937500
max_mach=0.520000


[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
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=1.2
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0

[GeneralEngineData]
engine_type=5                                 
Engine.0=-8.3, -8.6, 0.5                      
Engine.1=-8.3,  8.6, 0.5                    
fuel_flow_scalar=0.95
min_throttle_limit=-0.25          

[TurbineEngineData]
fuel_flow_gain=0.011           
inlet_area=0.38                      
rated_N2_rpm=29920                
static_thrust=140              

[turboprop_engine]
power_scalar=1.0               
maximum_torque=2305


[propeller]
thrust_scalar=1.000
propeller_type=0                     
propeller_diameter=8.2
propeller_blades=3                  
propeller_moi=20                    
gear_reduction_ratio=14.96	
beta_max=40                  
beta_min=15.2    
minimum_on_ground_beta=4
prop_reverse_available=1                   
minimum_reverse_beta=-30	
min_gov_rpm=25000         
prop_tc=0.004               
fixed_pitch_beta=0                  
low_speed_theory_limit=80                   
prop_sync_available=1                   
prop_deice_available=1                   
prop_feathering_available=1                    
prop_auto_feathering_available=1              
min_rpm_for_feather=700                  
beta_feather=86.0              
power_absorbed_cf=0.9                
defeathering_accumulators_available=0         


[electrical]	
flap_motor=0, 5,  17
gear_motor=2, 5,  17
autopilot=0, 5,  17
avionics_bus=2, 10, 17
avionics=1, 5,  17
pitot_heat=0, 2,  17
additional_system=0, 20, 17
marker_beacon=0, 2,  17
gear_warning=0, 2,  17
fuel_pump=0, 5,  17
starter1=0, 20, 17
starter2=0, 20, 17
light_nav=0, 5,  17
light_beacon=0, 5,  17
light_landing=0, 5,  17
light_taxi=0, 5,  17
light_strobe=0, 5,  17
light_panel=0, 5,  17
light_cabin = 0, 5 , 17
prop_sync=0, 15, 17
auto_feather=0, 15, 17
standby_vacuum=0, 15, 17
hydraulic_pump=0, 2,  17
fuel_transfer_pump=0, 5,  17
propeller_deice=0, 14, 17
light_recognition=0, 5,  17
light_wing=0, 5,  17
light_logo=0, 5,  17
max_battery_voltage=24
generator_alternator_voltage=28
max_generator_alternator_amps=250
electric_always_available=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]
//Gear
point.0=1,  13.00,   0.00, -4.80, 1181, 0, 0.600, 60.0, 0.500, 1.0, 3.0,  5.8,  5.8, 0, 181.0, 204.0
point.1=1,  -2.10,  -8.58, -4.60, 1574, 1, 0.600,  0.0, 0.500, 2.5, 0.8,  5.2,  5.2, 2, 181.0, 204.0
point.2=1,  -2.10,   8.58, -4.60, 1574, 2, 0.600,  0.0, 0.500, 2.5, 0.8,  4.8,  4.8, 3, 181.0, 204.0

//Scrape
point.3=2,  -2.00, -27.00, 2.50,  787, 0, 0.000,  0.0, 0.000, 0.0, 0.0000,  0.0,  0.0, 5, 0.0, 0.0
point.4=2,  -2.00,  27.00, 2.50,  787, 0, 0.000,  0.0, 0.000, 0.0, 0.0000,  0.0,  0.0, 6, 0.0, 0.0
point.5=2, -24.50,   0.00,  2.00,  787, 0, 0.000,  0.0, 0.000, 0.0, 0.0000,  0.0,  0.0, 9, 0.0, 0.0
point.6=2,  14.10,   0.00,  0.25,  787, 0, 0.000,  0.0, 0.000, 0.0, 0.0000,  0.0,  0.0, 4, 0.0, 0.0

static_pitch=-0.4
static_cg_height=4.2
gear_system_type=0


[Views]
eyepoint=3.58, -1.22, 3.52


[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=20                                   // degrees
flaps-position.2=40                                   // degrees
damaging-speed=250                                  // KIAS
blowout-speed=300                                  // KIAS

[Radios]

Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 1, 1 
Nav.2=1, 1, 1 
Adf.1=1
Adf.2=1
Transponder.1=1, 1
Marker.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=3,0

[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,  -0.40, -27.21,  1.95, fx_navred ,
light.1=3,  -0.40,  27.21,  1.95, fx_navgre ,
light.2=3, -29.60,   0.00, 10.53, fx_navwhi ,
light.3=2,  -0.11, -26.82,  1.96, fx_strobe ,
light.4=2,  -0.11,  26.82,  1.96, fx_strobe ,
light.5=1, -25.41,   0.00, 10.88, fx_beacon ,
light.6=2,  -5.80,   0.00, -1.28, fx_beaconb ,
light.7=4,   3.95,   0.00,  3.40, fx_vclight,

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

[autopilot]
use_no_default_pitch=1
use_no_default_bank=1
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=1800
autothrottle_available=0 
autothrottle_arming_required=0
autothrottle_max_rpm=0
autothrottle_takeoff_ga=0
max_throttle_rate=0.10
pitch_takeoff_ga=8 
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000
max_pitch_velocity_hi_alt_breakpoint=28000
max_pitch=10
max_pitch_acceleration=1
max_pitch_velocity_lo_alt=2
max_bank=25
max_bank_acceleration=1.8
max_bank_velocity=3
max_throttle_rate=0.1
nav_proportional_control=9
nav_integrator_control=0.25
nav_derivative_control=0
nav_integrator_boundary=2.5
nav_derivative_boundary=0
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0
gs_integrator_boundary=0.7
gs_derivative_boundary=0
yaw_damper_gain=1.5
default_pitch_mode=0
default_bank_mode=0



[brakes]
toe_brakes_scale=1.000000
parking_brake=1

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.091553
flap_limit_power=11.459156
flap_limit_idle=0.000000
[hydraulic_system]
normal_pressure=0.000000
[stall_warning]
type=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

[forcefeedback]
stick_shaker_magnitude=5000             ; 0 - 10000
stick_shaker_direction=0                ; 0 - 35999 degrees
stick_shaker_period=111111              ; in microseconds
gear_bump_nose_magnitude=3000           ; 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=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