[fltsim.0]
title=M101T Sokol
sim=M101T
model=1
panel=
sound=
texture=Dexter
kb_checklists=
kb_reference=
atc_id=
atc_id_color=0xff000000
atc_parking_types=RAMP
ui_manufacturer=AI
ui_type="M101T Sokol 1"
ui_variation="BASE"
description=AI M101T. Visual model by Scorpio9999. Flight dynamics by Scorpio9999. Paintwork by Goffy & sib2217. Polys: LOD1-2822, LOD2-1597, LOD3-937, LOD4-314, LOD5-61
atc_parking_codes=

[fltsim.1]
title=M101T Sokol Dexter
sim=M101T
model=
panel=
sound=
texture=Dexter
kb_checklists=
kb_reference=
atc_id=
atc_id_color=0xff000000
atc_parking_types=RAMP
ui_manufacturer=AI
ui_type="M101T Sokol"
ui_variation="Dexter"
description=AI M101T. Visual model by Scorpio9999. Flight dynamics by Scorpio9999. Paintwork by Goffy & sib2217. Polys: LOD1-2554, LOD2-1501, LOD3-937, LOD4-314, LOD5-61
atc_parking_codes=

[General]
atc_type=Myasischev
atc_model=M101T
editable=0
performance="Maximum Speed 540 km/hr\nCruise Speed 420 km/hr\n\nEngine\nWalter, M-601F  \n\nPropeller\nFive-Bladed, Constant Speed, Full Feathering, Reversible  V510


[WEIGHT_AND_BALANCE]
max_gross_weight = 7202                          // (pounds)
empty_weight = 3128                              // (pounds)

// Distance from geometric center to 1/4 of chord
reference_datum_position     = 3.28, 0, 0       // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     = 2.0, 0, 0       // (feet) longitudinal, lateral, vertical distance from specified datum
//empty_weight_CG_position     = 4.92, 0, 0       // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 10

station_load.0 = "170,  1.31, -1.5, 0.0, Pilot 1"                   // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170,  1.31,  1.5, 0.0, Pilot 2"         // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI   = 4129.27	//8874.87
empty_weight_roll_MOI    = 3038.45	//6026.96
empty_weight_yaw_MOI     = 5762.72	//11858.54
empty_weight_coupled_MOI = 0.0

[flight_tuning]
cruise_lift_scalar     = 0.7	//0.6 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 = 11.8, 0.0, 0.0                       //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 11.8, 0.0, 0.0                       //fake engine for proper behaviour of NAV lights
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      = 7.54                  //Propeller Diameter, (feet)
propeller_blades        = 5                     //Number of propeller blades
propeller_moi           = 40		//200   //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    = 17.378                //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    = -20.0                 //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            = 36146                 //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          = 1475 		//2950  //Maximum torque available (ft-lbs)


[Flaps.0]
type=1
span-outboard=0.6       // Percent span for flap position
extending-time=10.0      // Seconds, time to fully extend
system_type=0           // 0 = electrical
damaging-speed  = 175                                  // KIAS
blowout-speed   = 175                                  // KIAS
lift_scalar=2.16		//3.0 2.7 2.5 2.2 2.0
drag_scalar=0.3		//0.6 0.4 0.5
pitch_scalar=0.1	//1.0 0.4 0.8 0.75
flaps-position.0= 0     // degrees
flaps-position.1=10     // degrees
flaps-position.2=20     // degrees
flaps-position.3=30     // degrees
flaps-position.4=40     // 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

[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          = 2, 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

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit            
light.0 = 1, -6.56,   0.00, -2.46,  fx_beacon ,
light.1 = 1, -4.92,   0.00,  2.46,  fx_beacon ,
light.2 = 2, -0.83, -21.32, -0.65,  fx_strobe ,
light.3 = 2, -0.83,  21.32, -0.65,  fx_strobe ,
light.4 = 3, -0.80, -21.32, -0.65,  fx_navred ,
light.5 = 3, -0.80,  21.32, -0.65,  fx_navgre ,
// smoke effects
//light.6  = 2, 9.34, -2.39, -0.09 , fx_M101T_smoke ,
//light.7  = 2, 9.34,  2.39, -0.09 , fx_M101T_smoke ,

[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


        //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,  7.87,   0.00, -5.4,  2500, 0, 0.66, 55.0, 0.5, 1.5, 0.9, 5.0, 6.0, 0
point.1 = 1, -1.2,   -4.92, -5.4,  2500, 2, 0.82,  0.0, 0.3, 2.0, 0.7, 5.0, 6.0, 2
point.2 = 1, -1.2,    4.92, -5.4,  2500, 2, 0.82,  0.0, 0.3, 2.0, 0.7, 5.0, 6.0, 3
point.3 = 2, -0.81, -21.31, -0.65, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5	//l_wing
point.4 = 2, -0.81   21.31, -0.65, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6	//r_wing
point.5=  2, -19.62,   0.0,  6.91, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9	//tail
point.6=  2,  13.08,   0.0,  0.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4	//nose
point.7=  2, -17.33,   0.0, -0.57, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7	//aux_greb

max_number_of_points = 10

static_pitch    = 0.2	//1.3  //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height= 5.0          //feet, altitude of CG when at rest on the ground
gear_system_type=0

[brakes]
parking_brake = 1        		//Parking brake available
toe_brakes_scale = 1.0	//0.3 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  = -0.5, -1.1, -1.7, 58.82, 0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -0.5,  1.1, -1.7, 58.82, 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

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tiremark_6, 1 //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               = 183.93                //Square feet
wing_span               = 42.62                 //Feet
wing_root_chord         = 4.02                  //Feet
wing_dihedral           = 6.0		//3.9   //Degrees
wing_incidence          = 5.0		//2.5   //Degrees
wing_twist              = 0.0		//-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       = 1.41                  //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = -1.23                 //Feet, vertical distance from reference point, positive going up
htail_area              = 15.38		//39.0  //Square feet
htail_span              = 14.16		//11.7  //Feet
htail_pos_lon           = -14.36	//-30.9 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 1.04		//0.0   //Feet, vertical distance from reference point, positive going up
htail_incidence         = 0.0		//2.0   //Degrees
htail_sweep             = 12.8		//5.0   //Degrees, horizontal tail leading edge
vtail_area              = 18.49		//18.0  //Square feet
vtail_span              = 5.22		//4.8   //Feet, tip to body
vtail_sweep             = 46.6		//45.0  //Degrees, vertical tail leading edge
vtail_pos_lon           = -12.695	//-28.8 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 1.98		//1.5   //Feet, vertical distance from reference point, positive going up
elevator_area           = 6.56		//16.6  //Square feet
aileron_area            = 7.06		//18.3  //Square feet
rudder_area             = 11.09		//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           = 0.0                   //Degrees
spoilerons_available    = 0                     //Spoilerons Available?
aileron_to_spoileron_gain = 0                   //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    = 61	//78.0          //Knots True (KCAS)
full_flaps_stall_speed  = 60.8                  //Knots True (KCAS)
cruise_speed            = 227                   //Knots True (KTAS)
max_mach                = 0.60
max_indicated_speed     = 300		//175	//Red line (KIAS)

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1000.0
autothrottle_available= 0
pitch_takeoff_ga=5.0				//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
[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000
[stall_warning]
type=1