Specifications

Prime contractor	Antonov
Primary task	Medium range cargo transport
Type airplane	Military tactical airplane
Length	33.10 meters
Height	10.53 meters
Wingspan	38.00 meters
Wing area	121.7 square meters
Aspect Ratio
Angle of sweep
Dihedral / Anhedral
Engines	4x AI-20 turboprop
Thrust	4250 hp
Weight (empty)
Weight (start, maximum (MTOW))	61,000 kg
Weight (landing, maximum)
Required runway length (start)	850 meters
Required runway length (landing)	860 meters
Cruise speed	600 km/h
Maximum speed	640 km.h
Ceiling	33,465 ft (10.200 meters)
Maximum range	5500 km
Fuel tank quantity (Max. trip fuel)
Air-to-air-refueling (ATAR) capability	no
Passengers	100 troops or 130 passengers
Freight capacity
Armament	2x 23mm NR-23 cannons in the tail
Maximum weapon load
Maximum G resistance
Radar
Sensors
Avionics
Type flight controls
Type landing gear
Versions
Produced	+/- 900
Crew	3-6
Costs
Flight hour life
First flight	March 1957
Operational since
Successor of the
Similar airplane	C-130 Hercules, C-160 Transall
Operators (past and presently)	Afghanistan, CIS-states, Sovjet Union, Ukraine