McDonnell Douglas F-4 Phantom II vs. Aero Commander 560

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McDonnell Douglas F-4 Phantom II versus Aero Commander 560
19.2 m 63 ft 0 in length 10.88 m 35 ft 8 in
5.03 m 16 ft 6 in height 3.6 m 11 ft 10 in
11.72 m 38 ft 5 in wingspan 15.02 m 49 ft 3 in
Two General Electric J79s engines 2 x Lycoming TIO-540
17,900 lbs thrust per engine 340 lbs
35,800 lbs total thrust 680 lbs
27,965 kg 61,700 lb MTOW 6,000 lb 2,722 kg
3,031 km 1,636 nm range 1,200 nm 2,222 km
Mach 2.2 2,717 km/h cruise speed 210 kts 130 mph
Up to 16,000 lbs of externally carried ordnance capacity Up to 6 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.