Bombardier CRJ1000 vs. de Havilland Canada DHC-2 Beaver

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Bombardier CRJ1000 versus de Havilland Canada DHC-2 Beaver
39.1 m 128 ft 5 in length 13.56 m 44 ft 6 in
7.5 m 24 ft 7 in height 5 m 16 ft 5 in
26.2 m 86 ft wingspan 16.56 m 54 ft 4 in
2 GE CF34-8C5A1 turbofans engines 2 x Armstrong Siddeley Double Mamba turboprop engines
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 thrust per engine Approximately 3,100 hp (2,312 kW) each
27,260 lb of force or 121.2 kN at takeoff, 29,020 lb of force or 129 kN thrust APR Automatic Power Reserve total thrust Approximately 6,200 hp (4,624 kW) total
41,640 kg 91,800 lb MTOW 24,200 lb 10,977 kg
3,004 km 1,623 nm range 2,535 km 1,369 nm
515 mph 829 km/h cruise speed 228 mph 367 km/h
100 (common) capacity Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.