Airbus A330-300 vs. Bombardier CRJ1000

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Airbus A330-300 versus Bombardier CRJ1000
63.66 m 208 ft 9 in length 39.1 m 128 ft 5 in
16.79 m 55 ft 1 in height 7.5 m 24 ft 7 in
60.3 m 197 ft 9 in wingspan 26.2 m 86 ft
General Electric CF6-80E, Pratt & Whitney PW4000 series, Rolls-Royce Trent 700 engines 2 GE CF34-8C5A1 turbofans
311.4 kN (Pratt & Whitney PW4170), 304.7 kN (General Electric CF6-80E1A3), 316.3 kN (Rolls-Royce Trent 772C-60) thrust per engine 13,630 lb of force or 60.6 kN at takeoff, 14,510 lb of force or 64.5 kN thrust APR Automatic Power Reserve
Depends on the engine type total thrust 27,260 lb of force or 121.2 kN at takeoff, 29,020 lb of force or 129 kN thrust APR Automatic Power Reserve
242,000 kg 533,600 lb MTOW 41,640 kg 91,800 lb
11,750 km 6,346 nm range 3,004 km 1,623 nm
900 km/h 559 mph cruise speed 515 mph 829 km/h
250-290 capacity 100 (common)
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.