Aircraft for sale: Sale of several units/ The CRJ200 - medium-haul passenger aircraft for local airlines, developed by the Canadian company Bombardier Regional Aircraft (included in the corporation Bombardier Aerospace). The aircraft is an upgraded model of the passenger aircraft Canadair Regional Jet CRJ-100. The aircraft is new turbofan engines General Electric CF34-3B1 (38.81 kN thrust and ARM system - 41 kN) with reduced fuel consumption and the possibility of exploitation at an air temperature of 35 ° C. As a result of this modification can be operated at high altitudes and hot climate . . Aircraft showed better performance characteristics than the CRJ-100. The first planes were delivered to the airline Tyrolean Airways January 15, 1996. By the end of 1999 it was produced 303 aircraft CRJ200.
Specifications
Variant CRJ-200 ER/LR
Crew 3-4 (2 pilots + 1-2 cabin crew)
Seating capacity 50
44 (CRJ-440)
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
LR: 3,713 km (2,307 mi, 2,004 nmi)
Normal cruising speed Mach .74 (785 km/h)
Maximum cruising speed Mach .81 (859 km/h)
Flight ceiling 12,496 m (41,000 ft)
