[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