Год создания  1957 
Экипаж 5-6 человек 
Скорость максимальная 780 км/ч  
Скорость крейсерская  570 км/ч  
Наивыгоднейшая высота полета 8500 м. 
Практический потолок 10200 м. 
Дальность перегоночная 6200 км. 
Дальность действия 3600 км 
Длина разбега 1230 м. 
Длина пробега ( при посадочной массе 58т.) 1125 м. 
Аэронавигационный запас топлива 1600 кг/час 
Расход авиатоплива в крейсерском режиме 2,3 т/час 
Максимальный взлетная масса 61000 кг 
Нормальная взлетная масса 55100 кг 
Максимальный посадочная масса 61000 кг 
Максимальная масса платной загрузки 17 000 кг 
Масса снаряженного самолета 35340 кг 
Масса пустого самолета 34580 кг 
Размах крыльев 38 м 
Длина самолета 33,1 м 
Высота самолета 10,53 м 
Максимальный запас топлива 22066 кг. 
Двигатель, тип ТВД АИ-20М 
Двигатель, мощность 4*3128 кВт 


[contact_points]


        //0  Class                        <0=none,1=wheel, 2=scrape, 3=float>
        //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)

point.0=1.000000,31.000000,0.000000,-11.000,1574.803150,0.000000,1.251998,45.320000,0.840046,2.500000,0.95296,9.000000,7.000000,0.000000,220.000000,250.000000
point.1=1.000000,-7.000000,-7.500000,-9.8200000,1574.803150,1.000000,1.251998,0.000000,0.847366,2.500000,0.95121,12.000000,10.000000,2.000000,220.000000,250.000000
point.2=1.000000,-7.000000,8.000000,-9.8200000,1574.803150,2.000000,1.251998,0.000000,0.847366,2.500000,0.95121,12.000000,10.000000,3.000000,220.000000,250.000000
point.3=1.000000,-3.000000,-7.500000,-9.8200000,1574.803150,1.000000,1.251998,0.000000,0.847366,2.500000,0.95121,12.000000,10.000000,2.000000,220.000000,250.000000
point.4=1.000000,-3.000000,8.000000,-9.8200000,1574.803150,2.000000,1.251998,0.000000,0.847366,2.500000,0.95121,12.000000,10.000000,3.000000,220.000000,250.000000

point.5=2.000000,-5.500000,-61.000000,4.666667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.6=2.000000,-5.500000,61.000000,4.666667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.7=2.000000,-59.000000,0.000000,4.666667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.8=2.000000,31.000000,0.000000,4.666667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000

static_pitch=2.15000                     //1.35000  
static_cg_height=9.30000                 //9.10000
gear_system_type=0




[GeneralEngineData]
engine_type=5
Engine.0=0.333333,-18.833333,0.000000
Engine.1=0.333333,18.833333,0.000000
Engine.2=0.000000,-35.000000,0.000000
Engine.3=0.000000,35.000000,0.00000
fuel_flow_scalar=1.000000
min_throttle_limit=-0.10000000


[Flaps.0]
type=1
span-outboard=0.500000
extending-time=14.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=1.665409,0.000000
flaps-position.2=5.330818,0.000000
flaps-position.3=10.996227,0.000000
flaps-position.4=12.661636,0.000000
flaps-position.5=18.327045,0.000000
flaps-position.6=22.327045,0.000000
flaps-position.7=27.327045,0.000000
flaps-position.8=30.327045,0.000000