| 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 |
