Specifications
Variant | CRJ100 ER/LR | CRJ200 ER/LR |
---|---|---|
Crew | 3-4 (2 pilots + 1-2 cabin crew) | |
Seating capacity | 50 | |
Length Wing span Height |
26.77 m (87 ft 10 in) 21.21 m (69 ft 7 in) 6.22 m (20 ft 5 in) |
|
Wing area (net) Fuselage maximum diameter Turning circle |
48.35 m2 (520.4 sq ft) 2.69 m (8 ft 10 in) 22.86 m (75 ft 0 in) |
|
Engines (2x) Takeoff thrust (2x) Thrust APR (2x) |
GE CF34-3A1 38.83 kN (8,729 lbf) 41.01 kN (9,220 lbf) |
GE CF34-3B1 38.83 kN (8,729 lbf) 41.01 kN (9,220 lbf) |
Max Zero Fuel Weight (ZFW) | 19,958 kg (44,000 lb) | |
Max payload weight | 6,124 kg (13,500 lb) | |
Max Take Off Weight (MTOW) | 24,041 kg (53,000 lb) | |
Maximum range | ER: 3,000 km (1,864 mi, 1,620 nmi) LR: 3,710 km (2,305 mi, 2,003 nmi) |
ER: 3,045 km (1,895 mi, 1,644 nmi) LR: 3,713 km (2,307 mi, 2,004 nmi) |
Basic cruising speed | Mach .78 (593.74 mph ground, 516 knots ground) | |
Flight ceiling | 12,496 m (41,000 ft) | |
Number of Orders | 1054 | |
Certification Date | unknown | July 1992 |
Read more about this topic: Bombardier CRJ200