Tu-324 / Tu-414
| Geometric characteristics |
TU-324
|
TU-324A
|
TU-414
|
TU-414A
|
| A/c length, m |
25,5
|
25,5
|
31,85
|
31,85
|
| A/c Height, m |
7,3
|
7,3
|
8,3
|
8,3
|
| Wing span, m |
23,2
|
23,2
|
27,7
|
27,7
|
| Fuselage cross section, m |
2,8õ3,14
|
2,8õ3,14
|
2,8õ3,14
|
2,8õ3,14
|
| Weight characteristics | ||||
| Max takeoff weight, t |
23,7
|
23,7
|
38,15
|
40,35
|
| Maximal fuel reserve, t |
6,0
|
9,0
|
12,63
|
16,3
|
| Maximal payload, t |
5,5
|
1,8
|
8,0
|
2,5
|
| Passenger capacity |
52-56
|
8-19
|
72-76
|
8-26
|
| Flight range at maximal passenger capacity |
2500
|
7500
|
3500
|
8410
|
| Cruising speed, km/h |
810-870
|
870
|
850-900
|
900-950
|
| Field length, m |
1800
|
1800
|
1800
|
1800
|
| Engines |
AI-22
|
AI-22
|
BR-710
|
BR-710
|
| Passenger cabin | ||||
| Length, m |
10,26
|
10,26
|
19,7
|
19,7
|
| Width, m |
2,64
|
2,64
|
2,64
|
2,64
|
| Height, m |
1,92
|
1,92
|
1,92
|
1,92
|
|
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