Specifications
| SSJ 100–75 | SSJ 100-75LR | SSJ 100–95 | SSJ 100-95LR | |
|---|---|---|---|---|
| Cockpit crew | 2 | |||
| Seating capacity | 83 (1-class, dense) 78 (1-class, standard) 68 (2-class, standard) |
103 (1-class, dense) 98 (1-class, standard) 86 (2-class, standard) |
||
| Seat pitch | 30 in (1-class, dense), 32 in (1-class, standard) 36 & 32 in (2-class, standard) |
31 in (1-class, dense), 32 in (1-class, standard) 36 & 32 in (2-class, standard) |
||
| Length | 26.44 m (86 ft 9 in) | 29.94 m (98 ft 3 in) | ||
| Wingspan | 27.80 m (91 ft 2 in) | |||
| Height | 10.28 m (33 ft 9 in) | |||
| Fuselage max diameter | 3.35 m (11 ft 0 in) | |||
| Cabin width | 3.236 m (127.4 in) | |||
| Cabin height | 2.12 m (6 ft 11 in) | |||
| Aisle width | 51 cm (20 in) | |||
| Seat width | 46.5 cm (18.3 in) | |||
| Volume bins per passenger | 0.07 m3 (2.5 cu ft) | |||
| Maximum take-off weight (MTOW) | 38,820 kg (85,600 lb) | 42,280 kg (93,200 lb) | 45,880 kg (101,100 lb) | 49,450 kg (109,000 lb) |
| Empty weight (OEW) | – | – | 25,100 kg (55,000 lb) | – |
| DOW | – | – | 26,600 kg (59,000 lb) | – |
| Maximum landing weight | 35,000 kg (77,000 lb) | 41,000 kg (90,000 lb) | ||
| Maximum payload | 9,130 kg (20,100 lb) | 12,245 kg (27,000 lb) | ||
| Maximum fuel capacity | 13,135 L (10,600 kg or 23,370 lb) | 13,135 L (10,600 kg or 23,370 lb) | ||
| Cargo capacity | 15.01 m3 (530 cu ft) | 21.97 m3 (776 cu ft) | ||
| Takeoff run at MTOW | 1,515 m (4,970 ft) | 1,731 m (5,679 ft) | 2,052 m (6,732 ft) | |
| Maximum flight altitude | 12,500 m (41,000 ft) | |||
| Cruising speed | Mach 0.78 (828 km/h/511 mph / 448knots at 11,000 m/36,000 ft) | |||
| Maximum cruise speed | Mach 0.81 (870 km/h/ 541 mph / 469knots at 11,000 m/36,000 ft) | |||
| Range (full passenger payload) | 2,900 km (1,800 mi) | 4,550 km (2,830 mi) | 3,048 km (1,894 mi) | 4,578 km (2,845 mi) |
| Engine (x 2) | PowerJet SaM146 | |||
| Takeoff thrust (x 2) | 13,500 lbf (60 kN) | 15,400 lbf (69 kN) | ||
| APR thrust (x 2) | 15,400 lbf (69 kN) | 17,500 lbf (78 kN) | ||
| Fan tip diameter | 1.22 m (48 in) | |||
| Engine length | 2.07 m (81 in) | |||
Sources: Sukhoi Civil Aircraft Company, Superjet International, PowerJet.
Read more about this topic: Sukhoi Superjet 100