Specifications
| Variant | CRJ700 | CRJ705 | CRJ900 | CRJ1000 |
|---|---|---|---|---|
| Cockpit crew | Two | |||
| Seating capacity | 78 (1-class, maximum) 70 (1-class, typical) 66 (2-class, typical) |
90 (1-class, maximum) 86 (1-class, typical) 75 (2-class, typical) |
104 (1-class, maximum) 100 (1-class, typical) 86 (2-class, typical) |
|
| Length | 32.51 m (106 ft 8 in) | 36.40 m (119 ft 4 in) | 39.13 m (128 ft 4.7 in) | |
| Wingspan | 23.24 m (76 ft 3 in) | 24.85 m (81 ft 6 in) | 26.18 m (85 ft 10.6 in) | |
| Height | 7.57 m (24 ft 10 in) | 7.51 m (24 ft 7 in) | 7.50 m (24 ft 6 in) | |
| Wing area | 70.61 m² (760 ft²) | 77.4 m² (833 ft²) | ||
| Fuselage max diameter | 2.7 m (8 ft 10 in) | |||
| Maximum cabin width | 2.57 m (8 ft 5 in) | |||
| Cabin height | 1.89 m (6 ft 2 in) | |||
| Operating empty weight | 19,731 kg (43,500 lb) | 21,433 kg (47,250 lb) | 23,179 kg (51,100 lb) | |
| Max Zero Fuel Weight (ZFW) | 28,259 kg (62,300 lb) LR: 28,801 kg (63,495 lb) |
31,751 kg (70,000 lb) LR: 32,024 kg (70,600 lb) |
35,154 kg (77,500 lb) | |
| Maximum takeoff weight (MTOW) | 32,999 kg (72,750 lb) ER: 34,019 kg (75,000 lb) LR: 34,926 kg (77,000 lb) |
36,504 kg (80,500 lb) ER: 37,421 kg (82,500 lb) LR: 38,330 kg (84,500 lb) |
EuroLite: 38,995 kg (85,968 lb) 40,824 kg (90,000 lb) ER: 41,640 kg (91,800 lb) |
|
| Max payload weight | 8,527 kg (18,800 lb) LR: 9,070 kg (19,995 lb) |
10,319 kg (22,750 lb) LR: 10,591 kg (23,350 lb) |
11,975 kg (26,400 lb) | |
| Cargo capacity | 15.5 m3 (550 cu ft) | 16.8 m3 (590 cu ft) | 19.4 m3 (690 cu ft) | |
| Take off run at MTOW (ISA) | 1,564 m (5,131 ft) ER: 1,676 m (5,499 ft) LR: 1,851 m (6,073 ft) |
1,778 m (5,833 ft) ER: 1,861 m (6,106 ft) LR: 1,944 m (6,378 ft) |
EuroLite: 1,822 m (5,978 ft) 1,996 m (6,549 ft) ER: 2,079 m (6,821 ft) |
|
| Service ceiling | 12,497 m (41,000 ft) | |||
| Basic cruise speed | Mach 0.78 (829 km/h, 515 mph) | Mach 0.78 (829 km/h, 515 mph) | Mach 0.80 (850 km/h, 528 mph) | Mach 0.78 (827 km/h, 515 mph) |
| Maximum cruise speed | Mach 0.825 (876 km/h, 544 mph) | Mach 0.83 (885 km/h, 559 mph) | Mach 0.83 (881 km/h, 547 mph) | Mach 0.82 (870 km/h, 541 mph) |
| Maximum range | 1,434 nmi (2,656 km; 1,650 mi) ER: 1,732 nmi (3,208 km; 1,993 mi) LR: 2,002 nmi (3,708 km; 2,304 mi) |
1,719 nmi (3,184 km; 1,978 mi) ER: 1,963 nmi (3,635 km; 2,259 mi) LR: 1,999 nmi (3,702 km; 2,300 mi) |
1,350 nmi (2,500 km; 1,550 mi) ER: 1,593 nmi (2,950 km; 1,833 mi) LR: 1,828 nmi (3,385 km; 2,104 mi) |
EuroLite: 909 nmi (1,683 km; 1,046 mi) 1,345 nmi (2,491 km; 1,548 mi) ER: 1,535 nmi (2,843 km; 1,766 mi) |
| Maximum fuel load | 8,822 kg (19,450 lb) | |||
| Engines (2x) | GE CF34-8C5B1 | GE CF34-8C5 | GE CF34-8C5A1 | |
| Takeoff thrust (2x) | 56.4 kN (12,670 lbf) | 58.4 kN (13,123 lbf) | 59.4 kN (13,360 lbf) | 60.6 kN (13,630 lbf) |
| Thrust APR (2x) | 61.3 kN (13,790 lbf) | 63.4 kN (14,255 lbf) | 64.5 kN (14,510 lbf) | 64.5 kN (14,510 lbf) |
Sources: CRJ700, CRJ705, CRJ900, CRJ1000
Notes:
- Delta Connection branded CRJ900 aircraft seat 76 passengers and four crew members in a combined first/coach class configuration.
Read more about this topic: Bombardier CRJ700 Series