[fltsim.0]
title=Mil Mi-26MCS Belorusii
sim=Mil Mi-26MCS Belorusii
model=
panel=
sound=
texture=
kb_checklists=
prop_anim_ratio=-1.06
atc_id=EW-260TF
atc_model=Mil Mi-26MCS Belorusii
ui_manufacturer=Kazan Helicopter Plant JSC
ui_type=Mil Mi-26MCS Belorusii
ui_variation=EW-260TF
atc_heavy=0
atc_airline=26MCS Belorusii
atc_flight_number=EW-260TF



[weight_and_balance]

// ACM V2.5
max_gross_weight = 123300
empty_weight = 62040
empty_weight_pitch_MOI = 1262059
empty_weight_roll_MOI = 357503
empty_weight_yaw_MOI = 1085773
empty_weight_coupled_MOI = 0
CG_forward_limit = 0.000
CG_aft_limit = 1.000
max_number_of_stations = 10

reference_datum_position     = 0.000, 0.000, 0.000
empty_weight_CG_position     = 9.709, 0.000, 0.000

max_number_of_stations = 50

station_load.0 =170.000000, 21.489000, -2.132000, -2.132000, Pilot
station_load.1 =170.000000, 21.489000, 2.135000, -2.132000, Co-Pilot
station_load.2 =170.000000, 20.177000, 0.000000, -2.130000, Engineer
station_load.3 =170.000000, 14.271000, -1.640000, -2.788000, Pass FrontLeft1
station_load.4 =170.000000, 14.271000, -3.280000, -2.788000, Pass FrontLeft2
station_load.5 =170.000000, 11.318000, -1.640000, -2.952000, Pass FRontLeft3
station_load.6 =170.000000, 11.318000, -3.280000, -2.952000, Pass FrontLeft4
station_load.7 =170.000000, 8.202000, -1.640000, -3.280000, Pass MiddleLeft
station_load.8 =170.000000, 8.202000, -3.280000, -3.280000, Pass MiddleLeft
station_load.9 =170.000000, 5.249000, -1.640000, -3.444000, Pass BackLeft1
station_load.10 =170.000000, 5.249000, -3.280000, -3.444000, Pass BackLeft2
station_load.11 =170.000000, 2.600000, -1.640000, -3.608000, Pass BackLeft3
station_load.12 =170.000000, 2.600000, -3.280000, -3.608000, Pass BackLeft4
station_load.13 =170.000000, 14.271000, 1.640000, -2.788000, Pass FrontRight
station_load.14 =170.000000, 14.271000, 3.280000, -2.788000, Pass FrontRight
station_load.15 =170.000000, 11.318000, 1.640000, -2.952000, Pass FRontRight
station_load.16 =170.000000, 11.318000, 3.280000, -2.952000, Pass FrontRight
station_load.17 =170.000000, 8.202000, 1.640000, -3.280000, Pass MiddleRigh
station_load.18 =170.000000, 8.202000, 3.280000, -3.280000, Pass MiddleRigh
station_load.19 =170.000000, 5.249000, 1.640000, -3.444000, Pass BackRight1
station_load.20 =170.000000, 5.249000, 3.280000, -3.444000, Pass BackRight2
station_load.21 =170.000000, 2.600000, 1.640000, -3.608000, Pass BackRight3
station_load.22 =170.000000, 2.600000, 3.280000, -3.608000, Pass BackRight4

;Moments of Inertia
empty_weight_roll_MOI= 50000.000
empty_weight_pitch_MOI= 50000.000
empty_weight_yaw_MOI= 106000.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000


[flight_tuning]
rudder_effectiveness=0.05
aileron_effectiveness= 1.0
elevator_effectiveness=1.3


[electrical]
                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot          = 4, 4 , 15.0
avionics           = 0, 5 , 15.0
pitot_heat         = 4, 2 , 15.0
additional_system  = 0, 2 , 15.0
marker_beacon      = 4, 2 , 10.0
fuel_pump          = 0, 5 , 17.0
starter1           = 0, 20, 24.0
starter2           = 0, 20, 24.0
starter3           = 0, 20, 24.0
light_nav          = 0, 5 , 10.0
light_beacon       = 4, 5 , 15.0
light_landing      = 4, 5 , 15.0
light_taxi         = 0, 5 , 15.0
light_strobe       = 0, 5 , 10.0
light_panel        = 0, 5 , 10.0
light_cabin        = 4, 5 , 10.0
light_logo         = 4, 5 , 10.0
light_recognition  = 4, 5 , 10.0
hydraulic_pump     = 0, 5 , 15.0
fuel_transfer_pump = 0, 5 , 15.0
max_battery_voltage = 38.0
generator_alternator_voltage = 208.0
max_generator_alternator_amps = 150.0


        //0  Class                        <0=none,1=wheel, 2=scrape, 3=skid>
        //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]
static_pitch = 2.7
static_cg_height = 6.3
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 10
point.0= 1.000, 18.864, 0.000, -14.100, 1574.000, 0.000, 0.984, 35.000, 0.760, 1.300, 0.750, 0.000, 0.000, 0.000, 0.000, 0.000
point.1= 1.000, 4.757, -7.381, -14.200, 1600.000, 1.000, 1.476, 0.000, 0.800, 1.300, 0.850, 0.000, 0.000, 2.000, 0.000, 0.000
point.2= 1.000, 4.757, 7.381, -14.200, 1600.000, 2.000, 1.476, 0.000, 0.800, 1.300, 0.850, 0.000, 0.000, 3.000, 0.000, 0.000
point.3= 2.000, 25.754, 0.000, -4.101, 100.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.4= 2.000, -2.460, 0.000, -6.233, 100.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.5= 2.000, -27.887, 0.000, -4.800, 600.000, 0.000, 0.000, 0.000, 0.600, 1.500, 0.850, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 42.800, 0.000, 6.560, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
point.7= 2.000, -27.060, 0.000, 6.560, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000
point.8= 2.000, -7.830, -34.930, 6.560, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.9= 2.000, -7.830, 34.930, 6.560, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.10= 2.000, -32.800, -0.820, -2.460, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
point.11= 2.000, -39.360, -0.820, 3.930, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000


[brakes]
parking_brake = 1      //Parking brake available
toe_brakes_scale = 0.3  //Brake scalar


[hydraulic_system]
normal_pressure=797.700
engine_map=1,0,0,0
electric_pumps=1


[Views]
eyepoint = 29.4, 0.00, -0.55


[exits]
number_of_exits=4
exit_rate.0=0.4                                                           
exit_rate.1=0.4      
exit_rate.2=0.4
exit_rate.3=0.4


[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


[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.
//NOTE: These map to cyclic (fore/aft), cyclic (left/right), and anti-torque
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=2,0


[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2 


[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, 5=landing, 8=wing
light.0 = 3, 12.10, -6.50, -5.65,  fx_navgre ,
light.1 = 3, 12.10, 5.78, -5.65,  fx_navred ,
light.2 = 1, 21.90,  1.00, -9.40,  fx_DAFokker_beacon ,
light.3 = 1, -37.00,  0.69, 4.10,  fx_DAFokker_beacon ,
light.4 = 5, 38.30, 0.30, -6.50, fx_landing ,
light.5 = 5, 38.30, -1.15, -6.50, fx_landing ,
light.6 = 4, 33.10,   2.30, -2.8,  fx_vclight    ; Pilots
light.7 = 4, 33.10,  -2.30, -2.8,  fx_vclight    ; Pilots
light.8 = 4, 33.10,  0.00, -2.8,  fx_vclight    ; Pilots
light.9 = 4, 32.10,  0.00,  -1.6,  fx_vclight    ; EXT
light.10 = 4, 30.10,  -1.00,  -1.6,  fx_vclight    ; EXT
light.11 = 4, 30.10,  1.00,  -1.6,  fx_vclight    ; EXT


[effects]
wake = fx_wake
water = fx_spray
concrete = fx_sparks
windshield_rain_effect_available = 1
landrotorwas=fx_rtr_lnd

[fuel]
Center1 = 6.889, 0.000, 2.296, 117.000, 0.000
fuel_type = 2                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors =3                    
electric_pump=1
External1= 8.366, -4.920, -4.757, 179.000, 0.000
External2= 9.350, 4.920, -4.757, 196.000, 0.000


[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 1.00
min_throttle_limit = 0.0
max_contrail_temperature = -60.0
master_ignition_switch = 1
engine.0 = 5, -3, 6.8, 
engine.1 = 5, 3, 6.8, 




[propeller]
thrust_scalar=1.0 
propeller_type=0
propeller_diameter=6.883000
propeller_blades=3
propeller_moi=8.559780
beta_max=0.000000
beta_min=15.000000
min_gov_rpm=0.000000
prop_tc=0.100000
gear_reduction_ratio=1.000000
fixed_pitch_beta=20.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000000
beta_feather=0.000000
power_absorbed_cf=0.000000
defeathering_accumulators_available=0
prop_reverse_available=0.000000
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000


[Reference Speeds]
cruise_speed            = 129.0                 //Knots True (KTAS)
max_indicated_speed     = 134.0                   //Red line (KIAS)


[Helicopter]
low_realism_stability_scale=1.0, 1.0, 1.0 
reference_length = 110.7
right_trim_scalar=1.0
rotor_brake_scalar=1.0
governor_pid=0.4,0,0.1,0,0.2
governed_pct_rpm_ref=1.04
torque_scalar=0.9
cyclic_roll_control_scalar=3.0
cyclic_pitch_control_scalar=3.0
pedal_control_scalar=1.2
collective_on_rotor_torque_scalar=1.0
side_aero_center = -10.5
rotor_brake_scalar     = 1.0
correlator_available   = 1


[fuselage_aerodynamics]
drag_force_cf=1.000000
side_drag_force_cf=10.000000
pitch_damp_cf=-2.00000
roll_damp_cf=-2.000000
yaw_damp_cf=-0.500000
yaw_stability_cf=0.70


[MainRotor]
Position = -12.5, 0, 17
Radius = 34.931
max_disc_angle = 7.0
RatedRpm = 510
Number_of_blades = 8
weight_per_blade = 250.0
Weight_to_moi_factor = 0.80
inflow_wel_reference =35.0
 

[SecondaryRotor]
TailRotor = 1
Position = -83.776, 0.5, 19.101
Radius = 9.397 

[Reference Speeds]
cruise_speed=140.0                 //Knots True (KTAS)
max_indicated_speed     = 180.0                   //Red line (KIAS)


[yaw_string]
yaw_string_available=1


[smokesystem]
smoke.0 = 9.28, -6.39, -7, fx_smkpuff_m
smoke.1 = 9.28, -6.39, 7, fx_smkpuff_m

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90.000000
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