AIRCRAFT:F-4E Phantom II

• TYPE:two seat all weather fighter
  
• MAKER:McDonnell Douglas Corporation
  
• SPAN:38 ft. 7.5 in. (11.7 m.)
  
• LENGTH:63 ft. (19.2 m.)
  
• HEIGHT:16 ft. 5.5 in. (5.02 m.)
  
• WING AREA:530 sq. ft. (49.2 m. sq.)
  
• WEIGHT:empty 30,328 lb. (13,757 kg.), maximum take-off 61,795 lb. (28,030 kg.)
  
• POWERPLANT:two 17,902 lb. (8,120 kg.) standard General Electric J79-GE-17A turbojets with afterburning
  
• PERFORMANCE:speed over 1,500 m.p.h. (2,414 k.p.h, mach 2.27), combat radius 786 miles (1,266 km.), ceiling 54,400 ft. (16,580 m.)
  
• ARMAMENT:one nose-mounted 20 m.m. M61A-1 rotary cannon, four under-fuselage mountings and four under-wing pylons capable of carrying 16,000 lb. (7,250 kg.) of weapons
  
• CREW:2

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