Overview
The McDonnell Douglas F-4 Phantom II is a twin-engine supersonic fighter developed in the late 1950s. Designed initially for the U.S. Navy, it evolved into a multirole aircraft serving numerous air forces. The Phantom became one of the most widely produced Western jet fighters.
Live Fleet Activity (F4)
📡
Fetching live data…
Specifications
Units
- Engine
- 2 × General Electric J79-GE-17A Turbojets
- Engine type
- Jet
- Thrust
- 2 × 17,900 lbf · 80 kN
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 2
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- 63 ft 0 in · 19.20 m
- Tail height
- 16 ft 5 in · 5.00 m
- Fuselage diameter
- —
- Wing span
- 38 ft 5 in · 11.70 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 62,000 lb · 28,000 kg
- Max landing weight
- 36,800 lb · 16,700 kg
- Max payload
- 18,700 lb · 8,500 kg
- Fuel capacity
- 3,350 gal · 12,600 L · 10,100 kg (Jet A)
- Max cruise speed
- 1,280 kt · 1,473 mph · 2,371 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 1,520 nm · 1,750 mi · 2,820 km
- Fuel burn
- 0.42 nm/gal · 0.21 km/L
- Ceiling
- 62,000 ft · 18,900 m
- Rate of climb
- 41,300 ft/min · 210 m/s
- Takeoff distance
- 4,500 ft · 1,370 m
- Landing distance
- 3,650 ft · 1,120 m
Gallery
(/)
tap to zoom
(/)
Live fleet activity details
📡