| Crew | 2
|
| Max | 52-64
|
| Dimensions: |
|
| Wingspan | (m) 30
|
| Length | (m) 26,877
|
| Height | (m) 9,324
|
| Wing area | (kv.m) 81,9
|
| stabilizer | 11.10 m
|
| minimum distance from the earth before the end of propeller blades | (mm) 500
|
| Diameter of a fuselage | (m) 2,86
|
| Dimensions of the passenger cabin: |
|
| Length | (m) 19,93
|
| Width | (m) 2,64
|
| Height | (m) 1,92
|
| Weights and loadings: |
|
| Maximum take-off weight | (kg) 23500
|
| Maximum landing weight | (kg) 23500
|
| maximum mass without fuel | (kg) 22600
|
| Aircraft without fuel | (t) 21,5
|
| Weight curb aircraft (with crew) | (kg) 16100
|
| Mass of empty aircraft | (kg) 15540
|
| Maximum fuel | (t) 8360
|
| Maximum weight of a commercial load | (kg) 6500
|
| maximum mass of fuel (at P = 0793 g / cm 3) | (kg) 6960
|
| Flight characteristics: |
|
| Cruising speed | (km / h) 550
|
| maximum number of passenger seats | 64
|
| Range (km): |
|
| 64 passengers 2200 km
|
| 52 passengers 3100 km
|
| height of flight | (m) 7600
|
| Take-off distance during take-off weight of 21800kg | (m) 950
|
| Take-off distance during take-off weight of 23500kg | (m) 1250
|
| Landing distance when landing weight 21800kg | (m) 900
|
| Landing distance when landing weight 23000kg | (m) 1050
|
