Bombardier Canadair CRJ-700 Lufthansa D-ACPA at Apron C 06 Terminal 3

     
 
Variant CRJ700 CRJ705 CRJ900 CRJ1000
Cockpit crew Two
Seating capacity 78 (1-class, maximum)
70 (1-class, typical)
66 (2-class, typical)
74 (1-class, typical)
75 (2-class, typical)
90 (1-class, maximum)
88 (1-class, typical)
79 (2-class, typical)
104 (1-class, maximum)
100 (1-class, typical)
93 (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 m (760 ft) 77.4 m (833 ft)
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 (43,499 lb) 21,433 kg (47,252 lb) 23,179 kg (51,101 lb)
Max Zero Fuel Weight (ZFW) 28,259 kg (62,300 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)
 
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)
 
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)
 
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 0.85 (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 1,218 nmi (2,256 km; 1,402 mi)
ER: 1,504 nmi (2,785 km; 1,731 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)
1,048 nmi (1,941 km; 1,206 mi)
ER: 1,283 nmi (2,376 km; 1,476 mi)
LR: 1,515 nmi (2,806 km; 1,743 mi)
EuroLite: 971 nmi (1,798 km; 1,117 mi)
1,425 nmi (2,639 km; 1,640 mi)
ER: 1,622 nmi (3,004 km; 1,867 mi)
Maximum fuel load 8,887 kg (19,592 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)

 

 

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