General Dynamics F-16A Block 15U

Modern Drawings/Air/Pakistan/Fighters/F-16-FightingFalcon/F-16A_Block15U.htm | Update: -

14 Sqn "Shaheens", 38th TW, PAF - This aircraft crashed on October 28th, 1991 in Attock, Pakistan after it suffered an engine failure.

Specifications F-16A

General

Type: Fighter-Bomber
Crew: 1
First flight: 2 February 1974
Introduction: 1979
Number built: 111 ordered 40 delivered 71 under embargo
(Pakistan)

Powerplant

1 x Pratt & Whitney F100-PW-229
Dry thrust: 79 kN
Thrust with afterburner: 106 kN

Dimensions/Masses

Length: 14.80 m | Wingspan: 9.80 m | Height: 4.80 m
Wing area: 27.87 m2
Empty weight: 8272 kg | Max takeoff weight: 16900 kg

Performances

Maximum speed: 2173 km/h (Mach 2,05)
Combat radius: 550 km | Ferry range: ? km
Service ceiling: 15200 m

Armament

Inside: 1 × 20 mm (0.787 in) M61A1 Vulcan
Outside: Air-to-air missiles Sidewinder, ASRAAM, Magic 2, AMRAAM, Sparrow, Air-to-ground missile Maverick, anti-radar missile HARM or bombs (some guided by laser), or rockets.