Bombardier CRJ1000 vs. North American T-6 Texan

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Bombardier CRJ1000 versus North American T-6 Texan
39.1 m 128 ft 5 in length 9.0 m 29 ft 6 in
7.5 m 24 ft 7 in height 3.56 m 11 ft 8 in
26.2 m 86 ft wingspan 12.8 m 42 ft
2 GE CF34-8C5A1 turbofans engines 1 x Pratt & Whitney R-1340-AN-1 radial 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 thrust per engine Approximately 600 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 Approximately 600 hp
41,640 kg 91,800 lb MTOW 5,617 lb 2,548 kg
3,004 km 1,623 nm range 1,175 km 634 nm
515 mph 829 km/h cruise speed 145 mph 233 km/h
100 (common) capacity Pilot and one passenger
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.