Specifications
| CS100 | CS100ER | CS300 | CS300XT | CS300ER | |
|---|---|---|---|---|---|
| Passengers | 125 (1-class, dense) 110 (1-class, standard) 100 (2-class, mixed) |
145 (1-class, dense) 130 (1-class, standard) 120 (2-class, mixed) |
|||
| Seat Pitch | 30 in (76 cm) (1-class, dense) 32 in (81 cm) (1-class, standard) 36 in (91 cm) & 32 in (81 cm) (2-class, mixed) |
||||
| Seat Width | 19 in (48 cm) | ||||
| Flight crew | 2 (pilot, co-pilot) | ||||
| Length | 34.9 m (115 ft) | 38.0 m (124.7 ft) | |||
| Wingspan | 35.1 m (115 ft) | ||||
| Wing Area (net) | 112.3 m2 (1,209 sq ft) | ||||
| Tail height | 11.5 m (38 ft) | ||||
| Cabin width | 3.27 metres (129 in) | ||||
| Cabin height | 2.13 metres (84 in) | ||||
| Fuselage max diameter | 3.7 m (12 ft) | ||||
| Max takeoff weight | 54,931 kg (121,100 lb) | 58,151 kg (128,200 lb) | 59,557 kg (131,300 lb) | 63,095 kg (139,100 lb) | |
| Max landing weight | 50,576 kg (111,500 lb) | 55,339 kg (122,000 lb) | |||
| Cargo Volume | 23.2 m3 (820 cu ft) | 30 m3 (1,100 cu ft) | |||
| Max range | 4,074 km (2,200 nmi) | 5,463 km (2,950 nmi) | 4,074 km (2,200 nmi) | 5,463 km (2,950 nmi) | |
| Max cruise speed | Mach 0.82 (870 km/h, 470 kn, 541 mph) | ||||
| Typical cruise speed | Mach 0.78 (828 km/h, 447 kn, 514 mph) | ||||
| Take off run at MTOW | 1,509 m (4,951 ft) | 1,902 m (6,240 ft) | 1,661 m (5,449 ft) | 1,890 m (6,200 ft) | |
| Landing field length | 1,350 m (4,430 ft) | 1,448 m (4,751 ft) | |||
| Service ceiling | 12,497 m (41,001 ft) | ||||
| Engines | 2 x Pratt & Whitney PW1500G | ||||
| Thrust per Engine | 93.4 kN (21,000 lbf) | 103.6 kN (23,300 lbf) | 93.4 kN (21,000 lbf) | 103.6 kN (23,300 lbf) | |
- Notes: Data are preliminary and may change. ER = Extended Range, XT = Extra Thrust.
- Sources: CSeries Family
Read more about this topic: Bombardier CSeries