SIZES:
span clearance (m) 50,5
aircraft length (m) 46,6
aircraft altitude (m) 14,76
wing size (m2) 300
fuselage diameter (m) 4,8
MAIN POWER GENERATOR CHARACTERISTICS
type, model of power generator TRDD, D-30KP, 2
power generator quantity (pcs) 4
supreme takeoff power rating (MCA, H=0) 4×12000
normality ICAO point 16, chapter 2
MASS CHARACTERISTICS
supreme takeoff mass (t) 190
supreme disposable load (t) 50
supreme reservoir tankage (l) 109500
NAVIGABLE TECHNICAL CHARACTERISTICS
Course speed (km/h) 750-780 km/h
flying range with supreme charge (km) 3700
flight elevation (m) 9000-12000
unstick distance (m) 1700
landing roll (m) 1000
SPACE QUANTITY
flying crew 6
Cargo hold sizes:
foorlights length (m) 24,54
width (m) 3,45
altitude (m) 3,4
volume (cubic meter) 321
