McDonnell Douglas A-4 Skyhawk vs. Canadair CL-415

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McDonnell Douglas A-4 Skyhawk versus Canadair CL-415
12.19 m 40 ft 0 in length 19.82 m 65 ft 0 in
4.57 m 15 ft height 8.66 m 28 ft 5 in
8.08 m 26 ft 6 in wingspan 28.6 m 93 ft 1
1x Pratt & Whitney J52-P-6A Jet engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
8,500 pound-force thrust per engine 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
8,500 pound-force total thrust 4,300 to 4,760 shaft horsepower
11,113 kg 24,500 lb MTOW 19,733 kg 43,525 lb
3,222 km 1,739 nm range 1,600 km 864 nm
586 kts 364 mph cruise speed 290 km/h 180 mph
Up to 9,155 pounds of weapons on 5 hardpoints 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.