Fiat G.91

Airplanes

Length

10.3 m

Flat Wing Span

8.56 m

Height

4 m

Flat Wing Area

16.4 m²

Max Speed

1075 km/h

Max Ceiling

13100 m

Number of Engines

Aircraft Engine

First Flight

1956-08-09

Entry Into service

1958-01-01

Number Built

756

Maximum Take-Off Weight

5.5 t (paragliders: kg)

Maximum Range

1150 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Fiat G.91	5.5	1150

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Dassault Étendard VI	Bristol Siddeley Orpheus	10.85	8.3	Compare
SFCA Lignel 20	Renault 6Q	10	8.358	Compare
Focke-Wulf Project I		10.5	8.2	Compare
Lavochkin La-160		10.06	8.95	Compare
Nanchang J-12		10.644	7.192	Compare
Dufaux 4	Anzani 3-cylinder fan engines	9.5	8.5	Compare

All data (25 fields)

Name: Fiat G.91
Manufacturer: Aeritalia
Description: The Fiat G.91 is a jet fighter aircraft designed and built by the Italian aircraft manufacturer Fiat Aviazione, which later merged into Aeritalia.
First Flight: 1956-08-09
Entry Into service: 1958-01-01
Production End: 1977-01-01
Service End: 1995-01-01
Designer: Aeritalia
Type: Fighter-bomber
Length (m): 10.3
Height (m): 4
Cockpit Crew: 1
Max Speed (km/h): 1075
Max Ceiling (m): 13100
Rate of Climb (m/s): 30
Armament: 4× 12.7 mm (0.50 in) M3 Browning machine guns; or, 2× 30 mm (1.18 in) DEFA cannons (Luftwaffe G.91R/3 only); 4× under-wing pylon stations
Number Built: 756
Powerplant Description: 1 × Bristol Siddeley Orpheus 803 turbojet, 22.2 kN thrust each
Primary Users: Italian Air Force, German Air Force , Portuguese Air Force
Status: Retired
Wikipedia Article (URL): en.wikipedia.org/wiki/Fiat_G.91
Flat Wing Span (m): 8.56
Flat Wing Area (m²): 16.4
Aircraft Engine: Bristol Siddeley Orpheus
Number of Engines: 1