Bombardier CRJ1000 vs. Grumman OV-1 Mohawk

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Bombardier CRJ1000 versus Grumman OV-1 Mohawk
39.1 m 128 ft 5 in length 12.52 m 41 ft 1 in
7.5 m 24 ft 7 in height 3.89 m 12 ft 9 in
26.2 m 86 ft wingspan 14.63 m 48 ft
2 GE CF34-8C5A1 turbofans engines 2 x Lycoming T53 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 1,100 hp 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 2,200 hp total
41,640 kg 91,800 lb MTOW 14,950 lb 6,781 kg
3,004 km 1,623 nm range 1,690 km 913 nm
515 mph 829 km/h cruise speed 230 mph 370 km/h
100 (common) capacity Pilot and observer
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.