[fltsim.0]
title=Mil Mi8MT "Hip" RU Air Force
sim=Mi8MT
model=
panel=
sound=
texture=
checklists=
kb_checklists=
kb_reference=
atc_id=VVS09
atc_airline=RU VVS
atc_flight_number=VVS40RU
ui_manufacturer=Mil
ui_type=Mi8MT
ui_variation=VVS
visual_damage=1 
description=Mil Mi-8, Power installation: 2 xGDT TV2-117A  power on 1250kVt, diameter of carrying screw: 21.29m, length of fuselage: 18.17m, height: 4.38m, widthof fuselage: 2.5m, take-off weight: 12000kg, weight start: 6625kg,maximum velocity: 250km/h, max velocity: 225km/h, dynamicceiling: 4500m, range of flight: 425-480km, service load: 4000kg.

[fltsim.1]
title=Mil Mi8MT "Hip" UA Air Force
sim=Mi8MT
model=
panel=
sound=
texture=1
checklists=
kb_checklists=
kb_reference=
atc_id=VVS09
atc_airline=UA VPS
atc_flight_number=VPS31UA
ui_manufacturer=Mil
ui_type=Mi8MT
ui_variation=VPS
visual_damage=1 
description=Mil Mi-8, Power installation: 2 xGDT TV2-117A  power on 1250kVt, diameter of carrying screw: 21.29m, length of fuselage: 18.17m, height: 4.38m, widthof fuselage: 2.5m, take-off weight: 12000kg, weight start: 6625kg,maximum velocity: 250km/h, max velocity: 225km/h, dynamicceiling: 4500m, range of flight: 425-480km, service load: 4000kg.

[fltsim.2]
title=Mil Mi8T Aeroflot
sim=Mi8T
model=1
panel=
sound=
texture=2
checklists=
kb_checklists=
kb_reference=
atc_id=AF09
atc_airline=Aeroflot
atc_flight_number=AF22186
ui_manufacturer=Mil
ui_type=Mi8T
ui_variation=Aeroflot
visual_damage=1 
description=Mil Mi-8T, Power installation: 2 xGDT TV2-117A  power on 1250kVt, diameter of carrying screw: 21.29m, length of fuselage: 18.17m, height: 4.38m, widthof fuselage: 2.5m, take-off weight: 12000kg, weight start: 6625kg,maximum velocity: 250km/h, max velocity: 225km/h, dynamicceiling: 4500m, range of flight: 425-480km, service load: 4000kg.

[fltsim.3]
title=Mil Mi8T Russian Ministry of Emergency (MChS)
sim=Mi8T
model=1
panel=
sound=
texture=3
checklists=
kb_checklists=
kb_reference=
atc_id=mcs80199
atc_airline=MChS
atc_flight_number=mcs80199
ui_manufacturer=Mil
ui_type=Mi8T
ui_variation=MCS
visual_damage=1 
description=Mil Mi-8T, Power installation: 2 xGDT TV2-117A  power on 1250kVt, diameter of carrying screw: 21.29m, length of fuselage: 18.17m, height: 4.38m, widthof fuselage: 2.5m, take-off weight: 12000kg, weight start: 6625kg,maximum velocity: 250km/h, max velocity: 225km/h, dynamicceiling: 4500m, range of flight: 425-480km, service load: 4000kg

[contact_points]
point.0=1.000000,33.333333,0.000000,-8.666667,3003.698634,0.000000,0.520132,54.000000,1.120889,2.500000,1.260614,5.000000,5.000000,0.000000,0.000000,0.000000
point.1=1.000000,-8.333333,-8.333333,-6.500000,3003.698634,1.000000,0.520132,0.000000,1.002901,2.500000,1.416001,8.000000,8.000000,2.000000,0.000000,0.000000
point.2=1.000000,-8.333333,8.333333,-6.500000,3003.698634,2.000000,0.520132,0.000000,1.002901,2.500000,1.416001,9.000000,9.000000,3.000000,0.000000,0.000000
point.3=2.000000,0.000000,-125.000000,50.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,0.000000,125.000000,50.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-50.000000,0.000000,-1.666667,1802.219181,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,12.500000,0.000000,-2.083333,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
point.7=4.000, -7.000, -4.250, -5.000, 1068.000, 0.000, 0.512, 20.000, 0.800, 2.500, 0.700, 0.000, 0.000, 0.000, 0.000, 0.0
point.8=4.000, -7.000, 4.250, -5.000, 1068.000, 0.000, 0.512, 20.000, 0.800, 2.500, 0.700, 0.000, 0.000,1.000, 0.000, 0.0
point.9=4.000, 5.350, -4.250, -5.300, 1068.000, 1.000, 0.512, 0.000, 0.800, 2.500, 0.700, 0.000, 0.000, 2.000, 0.000, 0.0
point.10=4.000, 5.350, 4.250, -5.300, 1068.000, 2.000, 0.512, 0.000, 0.800, 2.500, 0.700, 0.000,0.000, 3.000, 0.000, 0.0
static_pitch=2.3
static_cg_height=6.0

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=2100.000000
empty_weight_roll_MOI=45000.000000
empty_weight_pitch_MOI=60000.000000
empty_weight_yaw_MOI=35000.000000
empty_weight_coupled_MOI=0.000000



[GeneralEngineData]
engine_type=1
Engine.0=0.000000,0.000000,0.000000
Engine.1=0.000000,0.000000,0.000000
fuel_flow_scalar=1.000000

[Reference Speeds]
flaps_up_stall_speed=0.000000
full_flaps_stall_speed=0.000000
cruise_speed=0.000000

[keyboard_response]
elevator=0.000000,20480.000000
aileron=0.000000,20480.000000
rudder=0.000000,20480.000000

[Views]
eyepoint=0.495386,0.00,12.499815


[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
autoland_available=0

[direction_indicators]
direction_indicator.0=3,0

[airplane_geometry]
wing_area=1500.000000
wing_span=125.000000
wing_root_chord=16.666667
wing_dihedral=1.999512
wing_incidence=-0.494385
wing_twist=-0.999756
oswald_efficiency_factor=0.250329
wing_winglets_flag=1
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=1850.000000
htail_span=154.166667
htail_pos_lon=-20.833333
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=100.000000
vtail_span=11.401754
vtail_sweep=0.000000
vtail_pos_lon=-20.000000
vtail_pos_vert=5.833333
elevator_area=100.500000
aileron_area=97.760000
rudder_area=87.000000
elevator_up_limit=27.501974
elevator_down_limit=20.626481
aileron_up_limit=19.480565
aileron_down_limit=14.896903
rudder_limit=23.491270
elevator_trim_limit=19.480565
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000


[TurbineEngineData]
fuel_flow_scalar=1.000000
fuel_flow_gain=0.002170
inlet_area=7.217160
rated_N2_rpm=29920.000000
static_thrust=6514.300000
afterburner_available=0
reverser_available=0

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=5.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=3.999245,0.000000
flaps-position.2=7.998491,0.000000
flaps-position.3=11.997736,0.000000
flaps-position.4=15.996982,0.000000
flaps-position.5=19.996227,0.000000
flaps-position.6=23.995472,0.000000
flaps-position.7=27.994718,0.000000
flaps-position.8=31.993963,0.000000
flaps-position.9=35.993209,0.000000
flaps-position.10=39.992454,0.000000

[fuel]
Center1=0.000000,0.000000,0.000000,250.000000,0.000000
LeftMain=0.000000,0.000000,0.000000,250.000000,0.000000
LeftAux=0.000000,-16.583333,0.000000,60.000000,0.000000
RightMain=0.000000,0.000000,0.000000,250.000000,0.000000
RightAux=0.000000,16.583333,0.000000,60.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1

[LIGHTS]        
light.0=3, 22.84, -4.3,  -1.6, fx_navredm ,
light.1=3,22.84,  4.3, -1.6, fx_navgrem ,
//light.2=2, -9,   0.00,  3.52,   fx_beaconb ,
light.3=2, -23.72, 0, 8, fx_strobeh ,
light.4=2, -30.22,  0, 8, fx_strobeh ,
light.5=2,  -4.35,   0.00, -3.9, fx_beaconb ,

[General]
performance=Power installation: 2 xGDT TV2-117A  power on 1250kVt, diameter of carrying screw: 21.29m, length of fuselage: \nAutor Vlad Zhyhulskiy