General Dynamics F-16 Fighting Falcon
Flat Wing Area
27.8709 m²
Cruise Speed
933.4072 km/h
Entry Into service
1978-08-17
Maximum Take-Off Weight
19.187 t (paragliders: kg)
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All data (24 fields)
- Name
- General Dynamics F-16 Fighting Falcon
- Manufacturer
- General Dynamics
- Description
- The General Dynamics (now Lockheed Martin) F-16 Fighting Falcon is an American single-engine supersonic multirole fourth-generation fighter aircraft developed by General Dynamics and produced by multiple companies, including General Dynamics until 1993 and Lockheed Martin since.
- First Flight
- 1974-01-20
- Entry Into service
- 1978-08-17
- Designer
- General Dynamics
- Type
- Multirole fighter, , air superiority fighter
- Length (m)
- 14.9352
- Height (m)
- 4.8768
- Cockpit Crew
- 1
- Cruise Speed (km/h)
- 933.4072
- Max Ceiling (m)
- 15240
- Armament
- 1 × 20 mm (0.787 in) M61A1 Vulcan 6-barrel rotary cannon, 500 rounds; ; 8 × CBU-87 Combined Effects Munition; 8 × CBU-89 Gator mine; 8 × CBU-97 Sensor Fuzed Weapon; 4 × Mark 84 general-purpose bombs; 8 × Mark 83 GP bombs; 12 × Mark 82 GP bombs; 8 × GBU-39 Small Diameter Bomb (SDB); 4 × GBU-10 Paveway II; 6 × GBU-12 Paveway II; 4 × GBU-24 Paveway III; 4 × GBU-27 Paveway III; 4 × Joint Direct Attac…
- Max Mach (Mach)
- 2.05
- National Origin
- United States of America
- Number Built
- 4604
- Powerplant Description
- 1 × General Electric F110-GE-129 for Block 50 aircraft
- Primary Users
- United States Air Force, 25 other users , (see operators page)
- Status
- In service
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/General_Dynamics_F-16_Fighting_Falcon
- Flat Wing Span (m)
- 9.7536
- Flat Wing Area (m²)
- 27.8709
- Aircraft Engine
- General Electric F110
- Number of Engines
- 1