| The original single Bristol Siddeley Orpheus-engined Fiat G91 was designed in accordance with NATO requirements for a standard lightweight tactical strike fighter to equip its forces. The first of three prototypes and 27 pre-production aircraft flew on 9 August 1956. Original production models included the G91R/1 photographic-reconnaissance version (three Vinten 70mm cameras) and similar R/3 and R/4 with armament changes; G91N modified aircraft to evaluate navigational aids; G91T/1 tandem two-seat version for advanced training at tran-sonic speeds, and similar T/3 and T/4 with equipment changes.
The G91Y is a twin-engined development of the G91 based upon the G91T version. Two prototypes were built (the first flying on 27 December 1966) followed by 20 pre-series G91Y for the Italian Air Force. Delivery of the initial series of 35 production aircraft to the Italian Air Force began in September 1971, as single-seat light tactical strike-reconnaissance fighters. Armament comprises two 30mm DEFA cannon and cameras in nose; four underwing attachment points for 450kg bombs, 340kg napalm tanks, 7 X 50mm rocket packs, 28 X 50mm rocket packs or 4 X 127mm rocket containers. G91 are in service with the air forces of the German Federal Republic (G91R/3 and G91T/3 - including R/3 licence-built in Germany), Italy (G91R/1, R/1A, R/1B, G91T/1 and G91Y) and Portugal (G91R/4).
CREW | 1 |
ENGINE | 1 x BS "Orpheus 803", 22.3kN |
WEIGHTS |
Take-off weight | 5200 kg | 11464 lb |
Empty weight | 3000 kg | 6614 lb |
DIMENSIONS |
Wingspan | 8.6 m | 28 ft 3 in |
Length | 11.1 m | 36 ft 5 in |
Height | 4.5 m | 15 ft 9 in |
Wing area | 16.4 m2 | 176.53 sq ft |
PERFORMANCE |
Max. speed | 1020 km/h | 634 mph |
Cruise speed | 407 km/h | 253 mph |
Ceiling | 12000 m | 39350 ft |
Range w/max.fuel | 2300 km | 1429 miles |
Range w/max payload | 700 km | 435 miles |
ARMAMENT | 4 x 12.7mm machine-guns or 2 x 30mm cannons |
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