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Northrop F-5A Freedom Fighter


The F-5 series of fighters was an attempt to produce a lightweight combat aircraft in face of the prevailing high weights and associated costs involved in fighter aircraft production. The initial production version was the F-5A which first flew in 1963 and the type was supplied to a number of countries under the Military Assistance Program including Greece, Jordan, Libya, Morocco, Turkey, Philippines, Thailand and Saudi Arabia. A reconnaissance version was the RF-5A (107 built) and the two seat trainer was the F-5B (293 built). Of the F-5A’s built, 164 were built by Canadair for the Canadian Armed Forces as the CF-5A (89) and the Netherlands Air Force (75 NF-5A’s). CASA in Spain also built 36 SF-5A’s and 34 SF-5B’s. The type was further developed as the F-5E Tiger 11 (1166 built) which first flew in 1972 powered by 2x 5000lb.s.t.(22.25kN) General Electrics and with a maximum take-off weight of 15,745lb (7142kg). The two seat trainer version was the F-5F (241 built). A small number of F-5A’s and F-5B’s are now flown in civil markings.

Northrop F-5A Freedom Fighter

N4416T                 c/n GG1001                    USA

Single seat fighter bomber first flown in 1959

Engines: 2x 4080lb.s.t.(18.15kN) GE J85-GE-13                                                                              Length: 47’2"(14.38m)                                                                                        Height: 13’2"(4.01m)Wingspan: 25’3"(7.7m)                                                                                                  No.built: 799 Range: 558miles(898km)                                                                Cruising speed: 600mph(965kmh) Empty weight: 8085lb(3667kg)                                           Maximum take-off weight: 13,663lb(6197kg)

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