McDonnell Douglas F-4 Phantom II vs. Aero Commander 520

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McDonnell Douglas F-4 Phantom II versus Aero Commander 520
19.2 m 63 ft 0 in length 11.18 m 36 ft 8 in
5.03 m 16 ft 6 in height 3.45 m 11 ft 4 in
11.72 m 38 ft 5 in wingspan 14.28 m 46 ft 1
Two General Electric J79s engines 2 x Lycoming IO-540
17,900 lbs thrust per engine 400 lbs
35,800 lbs total thrust 800 lbs
27,965 kg 61,700 lb MTOW 8,500 lb 3,856 kg
3,031 km 1,636 nm range 850 nm 1,574 km
Mach 2.2 2,717 km/h cruise speed 210 kts 130 mph
Up to 16,000 lbs of externally carried ordnance capacity 5
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.