[fltsim.0]
title=Teletica Kingair B200
sim=RFDS_King_Air_B200C
model=
panel=
sound=
texture=
kb_checklists=RFDS_King_Air_B200_check
kb_reference=RFDS_King_Air_B200_ref
atc_id_color=0xffffffffff
atc_id=TI-TCT
ui_manufacturer=Beechcraft
ui_type=King Air B200
ui_variation=Teletica TI-TCT
visual_damage=1
description=The King B200 Owned By Teletica, One Of The Best TV Stations in Costa Rica, Was Purchased About 1 Year Ago. It is in Perfect Condition. Teletica Bought the King Air B200 Because of Its Versatility. Telectica Currently Owns a Hughes 500, a Schewizer 300, a Falcon 100 Jet, a Beechcraft Bonanza and of Course, The King Air B200. They Currently Use this Aircraft for Flights Within Costa Rica, Where the Landing Strips are Not In Ver Good Conditon and Which Are Small, the King Air B200 Is Specially Designed for Those Types of Landing Areas.
atc_heavy=0
atc_airline=
atc_flight_number=
[General]
atc_type=KINGAIR
atc_model=BE20
performance=Cruise Speed\t\n240 kts 276 mph 444 km\/h\n\nEngines\t\nPratt & Whitney PT6A-42 850 shp\n\nMaximum Range\t\n1,765 nm 2,031 m\t 3,269 km\n\nService Ceiling\t\n35,000 ft 10,668 m\n\nFuel Capacity\t\n539 U.S. gal 2,040 L\n\nMaximum Takeoff Weight \n12,500 lb\t 5,666 kg\n\nLength\t\n43.75 ft\t 13.33 m\n\nWingspan\t\n54.5 ft\t 16.6 m\n\nHeight\t\n14.5 ft\t 4.41 m\n\nSeating\t\nUp to 7 in emergency configuration\n\nUseful Load\t\n2,513 lb\t 1,138 kg
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
[folding_wings]
wing_fold_system_type = 4 ;0=None
fold_rates = 0.12,0.11 ;Percent per second
[TailHook]
tailhook_length=4 ;(feet)
tailhook_position = -15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust = 1.0
[WEIGHT_AND_BALANCE]
max_gross_weight = 12500.000
empty_weight = 9357.500
reference_datum_position = 15.833, 0.000, 0.000
empty_weight_CG_position = -15.743, 0.000, 0.000
max_number_of_stations = 50
station_load.0 = 286.000, -10.750, -2.000, 0.000
station_load.1 = 190.000, -18.166, -2.000, 0.000
station_load.2 = 100.000, -27.083, 0.000, 0.000
station_load.3 = 190.000, -18.166, -2.000, 0.000
station_load.4 = 100.000, -27.083, 0.000, 0.000
station_load.5 = 100.000, -27.083, 0.000, 0.000
station_load.6 = 100.000, -27.083, 0.000, 0.000
station_load.7 = 100.000, -27.083, 0.000, 0.000
station_load.8 = 0.000, -18.916, 0.000, 0.000
;Moments of Inertia
empty_weight_pitch_MOI = 22110.960
empty_weight_roll_MOI = 14862.360
empty_weight_yaw_MOI = 29325.877
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, -4.800, 0.500
Engine.1 = -8.300, 4.800, 0.500
fuel_flow_scalar = 0.740
min_throttle_limit=-0.250000
[propeller]
thrust_scalar =1.000
propeller_type = 0
propeller_diameter = 7.750
propeller_blades = 4
propeller_moi = 24.000
beta_max = 45.000
beta_min = 18.200
min_gov_rpm = 22875.000
prop_tc = 0.004
gear_reduction_ratio = 15.000
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 = 87.900
power_absorbed_cf = 0.900
defeathering_accumulators_available= 0
prop_reverse_available = 1
minimum_on_ground_beta = 1.000
minimum_reverse_beta = -14.000
[TurbineEngineData]
fuel_flow_gain = 0.011
inlet_area = 0.562
rated_N2_rpm = 33000.000
static_thrust = 158.000
afterburner_available= 0
[turboprop_engine]
power_scalar =1.000
maximum_torque = 2230.000
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
[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
//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= 1.000, -2.560, 0.000, -4.200, 1181.000, 0.000, 0.596, 39.900, 0.296, 2.500, 0.952, 4.800, 4.800, 0.000, 0.000, 0.000
point.1= 1.000, -17.733, -8.580, -4.900, 1574.000, 1.000, 0.596, 0.000, 0.642, 2.500, 0.815, 4.500, 5.200, 2.000, 0.000, 0.000
point.2= 1.000, -17.733, 8.580, -4.900, 1574.000, 2.000, 0.596, 0.000, 0.642, 2.500, 0.815, 4.800, 4.900, 3.000, 0.000, 0.000
point.3= 2.000, -15.938, -27.329, 2.380, 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, -15.938, 27.329, 2.380, 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, -40.940, 0.000, 2.620, 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, -1.610, 0.000, 1.125, 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 = -1.000
static_cg_height = 4.300
gear_system_type=0
[Views]
eyepoint = -11.28, -1.279, 3.707
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 0
Com.2 = 1, 0
Nav.1 = 1, 0, 1
Nav.2 = 1, 0, 0
Adf.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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, -15.833, -27.26, 2.26, fx_navred ,
light.1 = 3, -15.833, 27.26, 2.26, fx_navgre ,
light.2 = 3, -45.483, 0.00, 9.69, fx_navwhi ,
light.3 = 2, -15.633, -27.26, 2.26, fx_strobe ,
light.4 = 2, -15.633, 27.26, 2.26, fx_strobe ,
light.5 = 1, -41.213, 0.00, 10.44, fx_beacon ,
light.6 = 2, -21.343, 0.00, -1.19, fx_strobe ,
light.7 = 4, -9.923, 0.00, 1.64, fx_vclight,
[EFFECTS]
wake=fx_wake
water=fx_spray
//dirt=fx_tchdrt
dirt=fx_landdust_red
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
LeftMain = -15.416, -14.500, -1.000, 194.000, 0.000
LeftAux = -17.000, -6.000, -1.500, 79.200, 0.000
RightMain = -15.416, 14.500, -1.000, 194.000, 0.000
RightAux = -17.000, 6.000, -1.500, 79.200, 0.000
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=0
[airplane_geometry]
wing_area = 303.000
wing_span = 54.500
wing_root_chord = 5.400
wing_dihedral = 6.000
wing_incidence = 1.000
wing_twist = -1.500
oswald_efficiency_factor= 0.700
wing_winglets_flag = 0
wing_sweep = 1.000
wing_pos_apex_lon = -13.856
wing_pos_apex_vert = 0.000
htail_area = 67.000
htail_span = 18.500
htail_pos_lon = -39.304
htail_pos_vert = 9.842
htail_incidence = 0.500
htail_sweep = 20.000
vtail_area = 42.000
vtail_span = 7.400
vtail_sweep = 40.000
vtail_pos_lon = -33.202
vtail_pos_vert = 3.868
elevator_area = 17.000
aileron_area = 13.500
rudder_area = 7.300
elevator_up_limit = 17.000
elevator_down_limit = 15.500
aileron_up_limit = 18.000
aileron_down_limit = 18.000
rudder_limit = 30.000
elevator_trim_limit = 15.000
spoiler_limit = 60.000
spoilerons_available = 0
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
[Reference Speeds]
flaps_up_stall_speed = 94.000
full_flaps_stall_speed = 76.800
cruise_speed = 240.000
max_indicated_speed=259.000000
max_mach=0.579980
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
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
[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
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 0
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 20.000, 0.000
flaps-position.2= 40.000, 0.000
[Flaps.1]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 0
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 20.000, 0.000
flaps-position.2= 40.000, 0.000
[brakes]
toe_brakes_scale=1.000000
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=15.011494
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
