MC21 / MS21
| MS-21 -100 | MS-21 -200 | MS-21 -300 | MS-21 -400 | |
|---|---|---|---|---|
Dimensions (external) | ||||
| wing span (m) | 35,25 | |||
| length (overall) (m) | 35,01 | 38,25 | 40,68 | 40.68 |
Engines | ||||
| type | By-pass turbojet engine | |||
| number of engines (pcs) | 2 | |||
| take-off thrust (kg) | 11000-12000 | |||
| traction on takeoff mode (MCA, H = 0) (kg) | 2 x 10.8 | 2 x 12.8 | 2 x 15.5 | |
| thrust-to-weight | 0.36 | 0.36 | 0.36 | |
| Fuel consumption per passenger-kilometer (G / Pass-km) | 15.05 | 15.1 | 14.3 | |
Weights and Volumes | ||||
| max take-off weight (t) | 65.8 | 65.8 | 71.1 | 72.0 |
| curb weight of the aircraft (t) | 37.0 | 38.6 | 39.9 | |
| estimated payload (t) | 12,54 | 14,82 | 16,53 | 16.53 |
| maximum mass of fuel (l) | 22.0 | |||
Performance | ||||
| cruise speed (km/h) | 850 | |||
| range with payload (km) | 4700 | 5500 | 4500 | 4500 |
| max flight altitude (m) | 11600 | |||
| runway length (m) | 2100 | 2400 | 2400 | 2400-2500 |
Seats | ||||
| flight crew | 2 | |||
| passengers | 132 | 150 | 180 | 210 |
Service Life | ||||
| calendar | 25 years | |||
| flights | 30000 | |||
| flight hours | 60000 | |||
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