Fiat G.91

Country of originItaly
ManufacturerFiat Aviazione
First flight9 August 1956
ProducedData is not available
Numbers built770
Unit costsData is not available
Max speed1,075 km/h (580 kn, 668 mph)
Max rangeRange: 1,150 km (621 nmi, 715 mi)
Service ceiling: 13,100 m (43,000 ft)
DimensionsLength: 10.3 m (33 ft 9 in)
Wingspan: 8.56 m (28 ft 1 in)
Height: 4.0 m (13 ft 1 in)
Wing area: 16.4 m² (177 ft²)
WeightEmpty weight: 3,100 kg (6,830 lb)
Loaded weight: 5,440 kg (11,990 lb)
Max. takeoff weight: 5,500 kg (12,100 lb)
Powerplant1 x Bristol Siddeley Orpheus 803 turbojet, 22.2 kN (5,000 lbf
4x 12.7 mm (0.50 in) M2 Browning machine guns; or
2x 30 mm (1.18 in) DEFA cannons (Luftwaffe G.91R/3 only)
Hardpoints : 4x under-wing pylon stations holding up to maximum of 1,814 kg/4,000 lb of payload for G.91Y, 680 kg/1,500 lb for G.91R/3 & R/4 and 500 kg/1,100 lb for G.91R/1
2x Matra rocket pods (each with 19× SNEB 68 mm rockets); or
18x Hispano SURA R80 80 mm rockets[35]
Bombs: A wide variety of air-to-ground ordnance including unguided iron bombs, gun pods in addition to auxiliary drop tanks for extended range
OperatorsFormer operators:
Germany, Greece (evaluation), Italy, Portugal, United States (evaluation)

Fiat G.91 videos

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