Bombardier CRJ Second Gen

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Bombardier CRJ Second Gen at a Glance
Role Regional jet
Country of Origin {{{country}}}
Manufacturer Bombardier Aerospace
Status In production
Number Built 56
Unit Cost 33.000.000v$

The Bombardier CRJ 900 is a regional airliner that was developed from the Bombardier CRJ 200.

Specifications

Variant CRJ700
CRJ705 CRJ900 CRJ1000
Crew 4 (2 pilots + flight attendants)
Seating capacity 70 75 86-90* 100-104
Length
Wing span
Height
32.51 m (106 ft 8 in)
23.24 m (76 ft 3 in)
7.57 m (24 ft 10 in)
36.40 m (119 ft 4 in)
24.85 m (81 ft 6 in)
7.51 m (24 ft 7 in)
39.13 m (128 ft 4.7 in)
26.18 m (85 ft 10.6 in)
7.13 m (23 ft 4.8 in)
Wing area 70.61 m² (760 ft²) 70.61 m² (760 ft²)
Fuselage max diameter 2.69 m (8 ft 10 in)
Engines (2x)
Takeoff thrust (2x)
Thrust APR (2x)
GE CF34-8C1
56.4 kN (12,670 lbf)
61.3 kN (13,790 lbf)
GE CF34-8C5
58.4 kN (13,123 lbf)
63.4 kN (14,255 lbf)
GE CF34-8C5A1

60.63kN (13,630 lbf)

Max Zero Fuel Weight (ZFW) 28,801 kg (63,495 lb) 31,751 kg (70,000 lb) 35,154 kg (77,500 lb)
Max payload weight 8,527 kg (18,800 lb) 10,319 kg (22,750 lb) 12,156 kg (26,800 lb)
Maximum range 3,121 km (1,939 mi)
ER: 3,676 km (2,284 mi)
3,591 km (2,231 mi)
ER/LR: 3,773 km (2,344 mi)
2,956 km (1,837 mi)
ER: 3,408 km (2,117 mi)
LR: 3,660 km (2,274 mi)
2,761 km (1,491 mi)
ER: 3,131 km (1,691 mi)
Basic cruising speed Mach 0.79 (810 km/h, 503 mph) Mach .80 (838 km/h, 521 mph) Mach .82 (877 km/h, 545 mph) Mach .85 max or 330 kts indicated
Service ceiling 12,496 m (41,000 ft)
Turning circle 22.86 m (75 ft)
Number of Orders 253 168* 38
23 Options
Certification Date Dec 2000 Sept 2002 4th Quarter 2009