Bombardier CRJ1000 vs. Beechcraft T-6 Texan II
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Bombardier CRJ1000 |
versus |
Beechcraft T-6 Texan II |
39.1 m |
128 ft 5 in |
length |
10.18 m |
33 ft 4 in |
7.5 m |
24 ft 7 in |
height |
3.29 m |
10 ft 10 in |
26.2 m |
86 ft |
wingspan |
10.21 m |
33 ft 6 in |
2 GE CF34-8C5A1 turbofans |
engines |
1 x Pratt & Whitney Canada PT6A-68 |
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 |
1100 lbs |
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 |
1100 lbs |
41,640 kg |
91,800 lb |
MTOW |
6,250 lb |
2,835 kg |
3,004 km |
1,623 nm |
range |
900 nm |
1,667 km |
515 mph |
829 km/h |
cruise speed |
320 kts |
199 mph |
100 (common) |
capacity |
2 |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.