Bombardier CRJ1000 vs. Beechcraft T-34 Mentor

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Bombardier CRJ1000 versus Beechcraft T-34 Mentor
39.1 m 128 ft 5 in length 7.92 m 25 ft 11 in
7.5 m 24 ft 7 in height 2.95 m 9 ft 8 in
26.2 m 86 ft wingspan 10.03 m 32 ft 11 in
2 GE CF34-8C5A1 turbofans engines 1 x Continental Motors IO-520 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 300 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 300 hp
41,640 kg 91,800 lb MTOW 3,100 lb 1,406 kg
3,004 km 1,623 nm range 1,111 km 600 nm
515 mph 829 km/h cruise speed 190 mph 306 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.