Bombardier CRJ1000 vs. Lockheed P-38 Lightning

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Bombardier CRJ1000 versus Lockheed P-38 Lightning
39.1 m 128 ft 5 in length 11.53 m 37 ft 10 in
7.5 m 24 ft 7 in height 3.91 m 12 ft 10 in
26.2 m 86 ft wingspan 15.85 m 52 ft
2 GE CF34-8C5A1 turbofans engines Engines: Two Allison V-1710-111/113 V-12 supercharged 4-stroke liquid-cooled 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 1,425 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 2,850 hp
41,640 kg 91,800 lb MTOW 9,798 kg 21,600 lb
3,004 km 1,623 nm range 1,100 nm 2,037 km
515 mph 829 km/h cruise speed 239 knots 139 mph
100 (common) capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.