Bombardier CRJ1000 vs. Cessna O-2 Skymaster

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Bombardier CRJ1000 versus Cessna O-2 Skymaster
39.1 m 128 ft 5 in length 8.9 m 29 ft 2 in
7.5 m 24 ft 7 in height 2.87 m 9 ft 5 in
26.2 m 86 ft wingspan 11.58 m 38 ft
2 GE CF34-8C5A1 turbofans engines Two 210-hp Continental IO-360s
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 210 hp
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 420 hp
41,640 kg 91,800 lb MTOW 5,400 lb 2,449 kg
3,004 km 1,623 nm range 1,705 km 921 nm
515 mph 829 km/h cruise speed 144 mph 232 km/h
100 (common) capacity 2
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.