Modern Drawings/Air/Israel/Fighters/F-16-FightingFalcon/F-16D_Block40J.htm | Update: 15-02-2018


 

105 tajeset "Scorpion", IDF/AF - Hatzor AB. May 2005.

 

Specifications F-16D
General

Type: 2-Seat Fighter-Trainer
Crew: 2
First flight: 7 December 1976
Introduction: early 1979
Entered production in: 1984
Number built: 243 for Israël (C/D)
Powerplant
1 × F110-GE-100 afterburning turbofan
Dry thrust: 76.3 kN
Thrust with afterburner: 127 kN
Dimensions/Masses
Length: 15.06 m | Wingspan: 9.96 m | Height: 4.88 m
Wing area: 27.87 m2
Empty weight: 8570 kg | Loaded weight: 12000 kg |
Max takeoff weight: 19200 kg
Performances
Maximum speed: 2120 km/h (Mach 2)
Combat radius: 550 km | Ferry range: 4220 km with drop tanks
Service ceiling: 15240 m
Armament

Inside: 1 × 20 mm (0.787 in) M61A1 Vulcan 6-barrel Gatling (511 rounds)
Outside: 2 × wing-tip Air-to-air missile launch rails, 6 × under-wing, and 3 × under-fuselage pylon (2 of 3 for sensors) stations with a capacity of Up to 7700 kg of stores

 

 

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