Fiat G.80

Airplanes

Length

12.93 m

Flat Wing Span

11.81 m

Height

4.08 m

Flat Wing Area

25.14 m²

Flat Wing Aspect Ratio

4.82

Max Speed

910 km/h

Max Ceiling

12500 m

Number of Engines

Aircraft Engine

First Flight

1951-12-09

Number Built

Maximum Take-Off Weight

7 t (paragliders: kg)

Total Fuel Capacity

1755

Maximum Range

1600 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Fiat G.80	7	1755	1600

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Hawker Sea Hawk		11.8872	11.8872	Compare
SNCAC NC 1080		12.87	12	Compare
Lockheed T-33		11.2776	11.5824	Compare
Nord 2200		13	12	Compare
Fokker S.14 Machtrainer	Rolls-Royce Derwent	13.3	12	Compare
Fairey Firefly		11.2776	12.4968	Compare

All data (21 fields)

Name: Fiat G.80
Manufacturer: Fiat Aviazione
Description: The Fiat G.80 was a military jet trainer designed and produced by the Italian aircraft manufacturer Fiat.
First Flight: 1951-12-09
Service End: 1955-01-01
Designer: Giuseppe Gabrielli
Length (m): 12.93
Height (m): 4.08
Max Speed (km/h): 910
Min Speed (km/h): 180
Max Ceiling (m): 12500
Armament: 2× fixed, forward-firing 12.7 mm (.5 in) Colt-Browning M3 machine guns; 2× 230 kg (500 lb); 8× HVAR
Number Built: 2
Powerplant Description: 1 × Rolls-Royce Nene 2/21 turbojet
Primary Users: Italian Air Force
Wikipedia Article (URL): en.wikipedia.org/wiki/Fiat_G.80
Flat Wing Span (m): 11.81
Flat Wing Area (m²): 25.14
Flat Wing Aspect Ratio: 4.82
Aircraft Engine: Rolls-Royce Nene
Number of Engines: 1