[fltsim.0]
title=Cessna Grand Caravan TOS
sim=AI Cessna C208B
model=cp
panel=
texture=1
ui_manufacturer=Active Korea FS Traffic
ui_type=C208B Grand Caravan
ui_variation=Tropic Air
atc_airline=TROPISER
atc_flight_number=208
atc_parking_codes=
atc_parking_types=GATE
description=AI Cessna C208B Grand Caravan by Henry Tomkiewicz
[fltsim.1]
title=Cessna C208 Grand Caravan C208 LAP
sim=AI Cessna C208B
model=CP
sound=
texture=
ui_manufacturer=Active Korea FS Traffic
ui_type=C208B Grand Caravan
ui_variation=TAM Mercosur
atc_airline=TAM
atc_parking_types=GATE, RAMP
description=AI Cessna C208B Grand Caravan by Henry Tomkiewicz, TAM Mercosur Repaint by Rodrigo Flores
[General]
atc_type=Cessna
atc_model=C208
editable=0
performance="Maximum Speed\n175 kts            324 km\/hr\n\nCruise Speed\n164 kts \t        305 km\/hr at 20,000 ft\n\nEngine\nPratt & Whitney Canada, Inc., PT6A-114A Free Turbine Flat Rated at 675 Shaft hp  \n\nPropeller\nThree-Bladed, Constant Speed, Full Feathering, Reversible  McCauley, 106-inch diameter\n\nMaximum Endurance\n5.1 hours maximum cruise at 10,000 ft\n6.6 hours maximum cruise at 18,000 ft\n6.4 hours maximum range at 10,000 ft\n7.2 hours maximum range at 18,000 ft\n\nService Ceiling\n22,800 ft            6,949 m\n\nFuel Capacity\n335  gal              1,268 L\n\nEmpty Weight\n4,575 lb              2,075 kg\n\nMaximum Gross Weight\n8,785 lb\t            3,985 kg\n\nUseful Load\n4,000 lb\t            1,814 kg\n\nLength\n41 ft, 7 in             12.7 m\n\nWingspan\n52 ft, 1 in\t            15.8 m\n\nHeight\n15 ft, 5-1\/2 in      4.8 m\n\nSeating\nUp to 14"
[WEIGHT_AND_BALANCE]
max_gross_weight = 8785                          // (pounds)
empty_weight = 4575                              // (pounds)
reference_datum_position     =  16.2, 0, 0       // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     = -15.4, 0, 0       // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = "170, -11.3, -1.5, 0.0, Pilot"                   // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170, -11.3,  1.5, 0.0, Passenger 2"         // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "0,   -13.9, -1.5, 0.0, Passenger 3"          // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "0,   -13.9,  1.5, 0.0, Passenger 4"          // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "170, -17.2, -1.5, 0.0, Passenger 5"          // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = "170, -17.2,  1.5, 0.0, Passenger 6"          // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = "150, -20.2, -1.5, 0.0, Passenger 7"          // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = "150, -20.2,  1.5, 0.0, Passenger 8"          // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = "0,   -23.2, -1.5, 0.0, Passenger 9"          // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.9 = "0,   -23.2,  1.5, 0.0, Passenger 10"         // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.10= "0,   -10.6,  0.0,-5.0, Cargo Pod 1"          // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.11= "0,   -15.2,  0.0,-5.0, Cargo Pod 2"          // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.12= "50,  -19.4,  0.0,-5.0, Cargo Pod 3"          // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.13= "50,  -24.6,  0.0,-5.0, Cargo Pod 4"          // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI   = 8874.87
empty_weight_roll_MOI    = 6026.96
empty_weight_yaw_MOI     = 11858.54
empty_weight_coupled_MOI = 0.0
[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          = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0
[GeneralEngineData]
engine_type = 5                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -2.4, 0.0, 0.0                       //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar        = 1.12                  //Scalar for fuel flow efficiency
min_throttle_limit = -0.25                      //Minimum percent throttle.  Generally negative for turbine reverser
[propeller]
thrust_scalar           = 1.0                   //Propeller thrust scalar
propeller_type          = 0                     //0=Constant Speed, 1=Fixed Pitch
propeller_diameter      = 8.8                   //Propeller Diameter, (feet)
propeller_blades        = 3                     //Number of propeller blades
propeller_moi           = 19                    //Propeller moment of inertia
beta_max                = 45                    //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min                = 15.6                  //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm             = 25520                 //Miminum governed RPM
prop_tc                 = 0.004                 //Prop time-constant
gear_reduction_ratio    = 17.4                  //Propeller gear reduction ratio
fixed_pitch_beta        = 0                     //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit  = 80                    //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available     = 0                     //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available    = 1                     //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 1                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available= 1               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather     = 700                   //Minimum RPM for prop feathering
beta_feather            = 88.0                  //Feathering pitch angle (degrees)
power_absorbed_cf       = 0.9                   //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available= 0          //Defeathering accumulators available? 0=FALSE, 1=TRUE 
prop_reverse_available  = 1                     //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta  = 1.0                   //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta    = -14.0                 //Minimum pitch angle in reverse, (degrees)
[TurbineEngineData]
fuel_flow_gain          = 0.011                 //Gain on fuel flow
inlet_area              = 1.0                   //Square Feet, engine nacelle inlet area
rated_N2_rpm            = 33000                 //RPM, second stage compressor rated value
static_thrust           = 158                   //Lbs, max rated static thrust at Sea Level
[turboprop_engine]
power_scalar            = 1.0                   //Scalar on Turboprop power
maximum_torque          = 1865                  //Maximum torque available (ft-lbs)
[Flaps.0]
type=1
span-outboard=0.5       // Percent span for flap position
extending-time=5.7      // Seconds, time to fully extend
system_type=0           // 0 = electrical
damaging-speed  = 175                                  // KIAS
blowout-speed   = 175                                  // KIAS
flaps-position.0= 0     // degrees
flaps-position.1=10,175     // degrees
flaps-position.2=20,150     // degrees
flaps-position.3=30,125     // degrees
[pitot_static]
vertical_speed_time_constant = 1.0              //Increasing this value will cause a more instantaneous reaction in the VSI
[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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit            
light.0 = 3, -16.00, -26.41,  3.85,  fx_navred,
light.1 = 3, -16.00,  26.41,  3.85,  fx_navgre,
light.2 = 3, -41.60,   0.00,  1.90,  fx_navwhi,
light.3 = 2, -16.20, -26.51,  3.85,  fx_strobeh,
light.4 = 2, -16.20,  26.51,  3.85,  fx_strobeh,
light.5 = 1, -39.80,   0.00, 10.01,  fx_beaconb,
[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 = 100,  180
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=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
[airspeed_indicators]
airspeed_indicator.0 = 1.183, -24.75
[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, 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
        //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
[contact_points]
point.0 = 1,  -4.70,  0.00, -5.250, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 0.0, 0.0, 0
point.1 = 1, -18.00, -6.00, -5.250, 2500, 1, 0.5,  0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 2
point.2 = 1, -18.00,  6.00, -5.250, 2500, 2, 0.5,  0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 3
point.3 = 2, -15.90, -26.0,  3.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5
point.4 = 2, -15.90   26.0,  3.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6
point.5=  2, -39.23,   0.0,  0.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9
point.6=  2,  -2.50,   0.0, -2.17, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4
point.7=  2, -42.00,   0.0, 10.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7
max_number_of_points = 21
static_pitch    = 0.24          //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height= 5.11          //feet, altitude of CG when at rest on the ground
[brakes]
parking_brake = 1        //Parking brake available
toe_brakes_scale = 0.68  //Brake scalar
[hydraulic_system]
normal_pressure = 3000.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,0,0,0   //pump on Eng1
[Views]
eyepoint= -12.1, -1.4, 2.12     //(feet) longitudinal, lateral, vertical distance from reference datum
[fuel]
LeftMain  = -17.0, -1.1, 2.5, 166.0, 3.6     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -17.0,  1.1, 2.5, 166.0, 3.6     //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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[exits]
number_of_exits = 2
exit_rate.0 = 0.4                               ;Percent per second
exit_rate.1 = 0.4                               ;Percent per second
[airplane_geometry]
wing_area               = 279.0                 //Square feet
wing_span               = 52.1                  //Feet
wing_root_chord         = 6.4                   //Feet
wing_dihedral           = 3.9                   //Degrees
wing_incidence          = 2.5                   //Degrees
wing_twist              = -1.7                  //Degrees
oswald_efficiency_factor= 0.7                   //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 0.0                   //Degrees, wing leading edge
wing_pos_apex_lon       = -14.5                 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = 0.0                   //Feet, vertical distance from reference point, positive going up
htail_area              = 39.0                  //Square feet
htail_span              = 11.7                  //Feet
htail_pos_lon           = -30.9                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 0.0                   //Feet, vertical distance from reference point, positive going up
htail_incidence         = 2.0                   //Degrees
htail_sweep             = 5.0                   //Degrees, horizontal tail leading edge
vtail_area              = 18.0                  //Square feet
vtail_span              = 4.8                   //Feet, tip to body
vtail_sweep             = 45.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -28.8                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 1.5                   //Feet, vertical distance from reference point, positive going up
elevator_area           = 16.6                  //Square feet
aileron_area            = 18.3                  //Square feet
rudder_area             = 6.7                   //Square feet
elevator_up_limit       = 28.0                  //Degrees
elevator_down_limit     = 21.0                  //Degrees
aileron_up_limit        = 20.0                  //Degrees
aileron_down_limit      = 15.0                  //Degrees
rudder_limit            = 24.0                  //Degrees
elevator_trim_limit     = 19.5                  //Degrees
spoiler_limit           = 20.0                  //Degrees
spoilerons_available    = 1                     //Spoilerons Available?
aileron_to_spoileron_gain = 1                   //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0                 //Degrees
min_flaps_for_spoilerons = 0                    //Minimum flap handle position when spoilerons activate
spoiler_handle_available = 0                    //Defaults to True if spoiler limit > 0, else False.  Should be False for spoilerons only
[Reference Speeds]
flaps_up_stall_speed    = 78.0                  //Knots True (KCAS)
full_flaps_stall_speed  = 60.8                  //Knots True (KCAS)
cruise_speed            = 155.0                 //Knots True (KTAS)
max_mach                = 0.60
max_indicated_speed     = 175                   ////Red line (KIAS)
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1000.0
autothrottle_available= 0
pitch_takeoff_ga=8.0
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 0.0
[forcefeedback]
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=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=00500         ; 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
[stall_warning]
type=2