[fltsim.0]
title=Tupolev Tu-114 AA Hruschev
sim=Tupolev Tu-114
model=hruschev
panel=
sound=
texture=hruschev
kb_checklists=
description= The first produced unit CCCP-L5611. \nSamdim Design\n 
ui_manufacturer=Tupolev
ui_type=Tu-114
ui_variation=1959 Khruschev      

[fltsim.1]
title=Tupolev Tu-114 JAL
sim=Tupolev Tu-114
model=JAL
panel=
sound=
texture=JAL
kb_checklists=
description= Joint Aeroflot - Japan Air Lines livery  \nSamdim Design\n   
ui_manufacturer=Tupolev
ui_type=Tu-114
ui_variation=1967 Aeroflot and JAL       

[fltsim.2]
title=Tupolev Tu-114 AER70
sim=Tupolev Tu-114
model=aer70
panel=
sound=
texture=aer70
kb_checklists=
description= Standard Aeroflot livery in the 70-ies \nSamdim Design\n    
ui_manufacturer=Tupolev
ui_type=Tu-114
ui_variation=1973 Aeroflot 70-ies   
 
[fltsim.3]
title=Tupolev Tu-126
sim=Tupolev Tu-114
model=126
panel=126
sound=
texture=126
kb_checklists=
description= AWACS version    \nSamdim Design\n 
ui_manufacturer=Tupolev
ui_type=Tu-126
ui_variation=Soviet Army   

[General]
atc_type=TU
atc_model=TU-114
performance= Production: 33 units from 1958 to 1964\n Wing span  51.1m\n Length   54.1m\n Height  15.5m\n Wings surface  311.1m2\n Empty weight  93500kg\n Max takeoff weight  173500kg\n Engines  4x Kuznetsov NK-12MV\n Power  4x 14795hp\n Top speed  877km/h\n Cruise speed  770km/h\n  Maximum range  8800km\n Range with max payload  6200km\n Service ceiling  12000m\n Runway length  3500m\n  Crew  5\n Passengers  65-220\n Useful load  25000kg

[GeneralEngineData]
engine_type=1
Engine.0=-5.500000,-20.3333,-8.416667
Engine.1=-5.500000,20.3333,-8.416667
Engine.2=-5.000000,-42.000000,-8.416667
Engine.3=-5.000000,42.000000,-8.416667
fuel_flow_scalar=0.8//0.725//0.862//aav//1.00
min_throttle_limit=-0.270000

[TurbineEngineData]
fuel_flow_gain=0.002000
inlet_area=40.00//aav//113.0
rated_N2_rpm=29920.0
static_thrust=28000.//aav//65000.000000
afterburner_available=0
reverser_available=1.000000

[jet_engine]
thrust_scalar = 1.0

[flight_tuning]
cruise_lift_scalar     = 1.0
parasite_drag_scalar   = 0.65
induced_drag_scalar    = 1.3
elevator_effectiveness = 0.5
aileron_effectiveness  = 0.7
rudder_effectiveness   = 1.0
pitch_stability        = 0.7//1.0
roll_stability         = 0.7//1.0
yaw_stability          = 0.7//1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 0.1//aav//1.0


[TailHook]
tailhook_length=4                               ;(feet)
tailhook_position = -15.0, 0.0, -1.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust = 1.0

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, -35.20, -83.08, -3.98, fx_navredm
light.1 = 3, -35.20, 83.08, -3.98, fx_navgrem
light.2 = 3, -99.40, 0, 6.49, fx_navwhih
light.3 = 2, -73.88, 0, -1.73, fx_beaconb
light.4 = 1, -95.41, 0, 33.48, fx_beaconh
light.5 = 4, 67.28, 2.36, 4.50, fx_vclight_yellow
light.6 = 4, 67.28, -2.36, 4.50, fx_vclight_yellow
light.7 = 3, 67.28, 0, 4.50, fx_vclight_yellow
light.8 = 4, 70.91, 0.57, 2.73, fx_vclight_yellow

[smokesystem]
smoke.0 = -5.19, -30, 41.39, fx_smoke_rx
smoke.1 = -5.06, -32, 22.27, fx_smoke_rx
smoke.2 = -5.06, -32, -22.27, fx_smoke_rx
smoke.3 = -5.19, -30, -41.39, fx_smoke_rx

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_td, 1

[direction_indicators]
direction_indicator.0=3,0

[fuel]
//aav
//Center1=0.000000,0.000000,-4.000000,10400.000000,3.000000
//LeftMain=-7.000000,-35.000000,0.000000,14400.000000,3.000000
//RightMain=-7.000000,35.000000,0.000000,14400.000000,3.000000
//
Center1   =  0.00,   0.00,-4.00,6870.00,3.0
LeftMain  = -7.00, -35.00, 0.00,9000.0,3.0
RightMain = -7.00,  35.00, 0.00,9000.0,3.0
//
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=0

[airplane_geometry]
wing_area      = 3500.//aav//6700.000000
wing_span      = 180.//aav//233.250000
wing_root_chord= 22.//aav//29.666667
wing_dihedral  = 1.999512
wing_incidence = 0.137329
wing_twist     =-0.999756
oswald_efficiency_factor=0.7//aav//1.966913
wing_winglets_flag=0
wing_sweep        = 35.  //aav//0.000000  
wing_pos_apex_lon = 37.//25.//8.0  //aav//0.000000 - balans
wing_pos_apex_vert= 0.000000
htail_area        =  850.//1090.000000
htail_span        =  50.//aav//70.666667
htail_pos_lon     = -85. //aav//-121.000000
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep       = 40.  //aav//0.000000
vtail_area=573.000000
vtail_span=27.292856
vtail_sweep       = 35. //aav//0.000000
vtail_pos_lon     = -85.//aav//-108.333333
vtail_pos_vert=5.833333
elevator_area     = 100.//aav// 360.000000
aileron_area      = 80. //aav// 261.880000
rudder_area       = 150.//aav// 350.000000
elevator_up_limit   =14.772396
elevator_down_limit =21.772396
aileron_up_limit    =19.480565
aileron_down_limit  =19.480565
rudder_limit        =23.491270
elevator_trim_limit =19.996227
spoiler_limitn      =0
spoilerons_available=0
aileron_to_spoileron_gain=3.000000
min_ailerons_for_spoilerons=9.969466
min_flaps_for_spoilerons=15.000000
spoiler_limit=59.988681

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000   // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=1.600000,0.000000,0.000000   // (feet) longitudinal, lateral, vertical distance from specified datum
//
empty_weight     = 208000.//aav//600000.000000
max_gross_weight = 408000.//400000.//aav//800136.500000
//
empty_weight_pitch_MOI   =  10000000.  //aav// 43510000.000000
empty_weight_roll_MOI    =  4000000. //aav// 21215562.000000
empty_weight_yaw_MOI     =  8000000.  //aav// 39439242.000000
empty_weight_coupled_MOI =  0.        //aav// 1000.000000



max_number_of_stations = 50

station_load.0 =  "170.0,  80.0,  -2.0,    0.0, Pilot"                  //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 =  "170.0,  80.0,   2.0,    0.0, Co-Pilot"               //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 =  "170.0,  85.0,   0.0,    0.0, Navigator"              //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 =  "850.0,   0.0,   0.0,    0.0, Crew"                   //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 =  "850.0,  32.0,   0.0,    0.0, First Class"            //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = "5100.0,  11.0,   0.0,    0.0, Business Class"         //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = "12000.0,-10.0,   0.0,    0.0, Coach 1-16"             //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = " 850.0, -52.5,   0.0,    0.0, Coach 16-29"            //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = "2000.0,  12.0,   0.0,   -6.0, Forward Cargo"          //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.9 = "10000.0,-27.0,   0.0,   -6.0, Aft Cargo"              //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)




[brakes]
toe_brakes_scale=0.3//aav//0.4500000
parking_brake=1

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=14.000000
system_type=0
flaps-position.0=0.000, 0
flaps-position.1=5.000
flaps-position.2=10.000
flaps-position.3=15.000
flaps-position.4=20.000
flaps-position.5=25.000
flaps-position.6=30.000
lift_scalar=1.1//aav//0.76 - theory .0   0.24 - .1
drag_scalar=0.8 //- theory .0    0.6  - .1


[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
//eyepoint=99.732406,-1.896736,7.099943
eyepoint=64.64,-1.996736,6.01

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1200.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=2.000000
max_pitch=5.000000
max_pitch_acceleration=10.000000
max_pitch_velocity_lo_alt=0.80000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=6000.000000
max_pitch_velocity_hi_alt_breakpoint=20000.000000
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

[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,1
normal_pressure=3000.000000

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0


[contact_points]

point.0 = 1, 60.41, 0.00, -16.61,   2000.0, 0, 2.0, 70.0, 1.50, 1.67, 0.900,  9.0,  8.0, 0, 220, 250
point.1 = 1, -6.35, -22.25, -16.12, 3000.0, 1, 2.0, 0.0,  1.25, 1.11, 0.900, 9.0,  9.0, 2, 220, 250
point.2 = 1, -6.35, 22.25, -16.12,  3000.0, 2, 2.0, 0.0,  1.25, 1.11, 0.900, 9.0,  9.0, 3, 220, 250
point.3 = 2.000000,-14.166667,-47.333333,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4 = 2.000000,-14.166667,47.333333,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5 = 2.000000,-83.333333,0.000000,2.500000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6 = 2.000000,42.666667,0.000000,-3.750000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
point.7 = 5, -30.9, -5.25, -7.30,1600, 0, 0.00, 50.0, 0.0,  0.0,       1.00, 8.0, 8.2, 0, 0.0, 0.0

//point.0 = 1, 45.41, 0.00, -16.61,   2000.0, 0, 2.0, 70.0, 1.50, 1.67, 0.900,  12.0,  9.0, 0, 220, 250
//point.1 = 1, -10.35, -22.25, -15.92, 3000.0, 1, 2.0, 0.0,  1.25, 1.11, 0.900, 14.0,  10.0, 2, 220, 250
//point.2 = 1, -10.35, 22.25, -15.92,  3000.0, 2, 2.0, 0.0,  1.25, 1.11, 0.900, 14.0,  10.0, 3, 220, 250
//point.3 = 1.000000,-5.666667,21.283333,-18.150000,1574.803150,1.000000,6.716506,0.000000,  2.270603,2.500000,1.556694, 10.000000,9.000000,2.000000,220.000000,250.000000
//point.4 = 1.000000,-5.666667,-20.083333,-18.150000,1574.803150,2.000000,6.716506,0.000000, 2.270603,2.500000,1.556694, 11.000000,8.000000,3.000000,220.000000,250.000000
//point.5 = 2.000000,-14.166667,-47.333333,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
//point.6 = 2.000000,-14.166667, 47.333333,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
//point.7 = 2.000000,-83.333333,  0.000000,2.500000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
//point.8 = 2.000000,42.666667,   0.000000,-3.750000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000

static_pitch=0
static_cg_height=17
gear_system_type=0


[Reference Speeds]
flaps_up_stall_speed   = 155.0//aav//145.000000
full_flaps_stall_speed = 125.0 //aav//115.000000
cruise_speed           = 416.//aav//460
max_indicated_speed    = 485.//aav//390.000000
max_mach=0.850000