 |
|
| Engines: | |
type (series)
| D-36-(3A)
| D-36-(3A)
| D-36-(4A)
| |
thrust, kgf
| 2 x 6500
| 2 x 6500
| 2 x 6500
| | Cargo capacity, t
| 10
| (up to 2300 kg in cargo compartment)
| 10
| | Passengers, pers.
| 52
| 9-29
| 52
| | Cruising speed, km/h
| 580-700
| 580-700
| 600-740
| | Flight altitude, m
| 10100
| 10100
| 10100
| | Range,km: | |
with max load
| 950
| —
| 1450
| |
with passengers
| 2750
| 3300 (9 pass.+ 2.3 t)
| 3600
| |
with max fuel load (cargo, t)
| 4250(1.8)
| 4400 (8 pass.)
| 5050(2.5)
| | Required runway, m
| 2050
| 2050
| 1900
| | Crew, pers.
| 4/2
| 2
| 2
| | Cargo compartment dimensions, m | |
floor width
| 2.1
| 2.15
| 2.15
| |
hight
| 2.08
| 2.2
| 2.2
| |
lenght
| 9.8
| 5
| 9.8
|
|
|
