Aeritalia G.222

ยท Aeritalia
Length
22.7 m
Flat Wing Span
28.7 m
Height
9.8 m
Flat Wing Aspect Ratio
9.15
Cruise Speed
439 km/h
Max Speed
540 km/h
Max Ceiling
7620 m
Number of Engines
2
First Flight
1970-07-18
Entry Into service
1978-04-01
Number Built
111
Maximum Take-Off Weight
28 t (paragliders: kg)
Total Fuel Capacity
12000
Maximum Range
1371 km

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Total Fuel Capacity Maximum Range (km)
Aeritalia G.222 28 12000 1371

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Northrop X-21 General Electric J79 22.94 28.51 Compare
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All data (28 fields)
Name
Aeritalia G.222
Manufacturer
Aeritalia
Description
The Aeritalia G.222 (formerly Fiat Aviazione, later Alenia Aeronautica) is a medium-sized STOL military transport aircraft.
ICAO Code
G222
First Flight
1970-07-18
Entry Into service
1978-04-01
Production End
1993-01-01
Service End
2012-01-01
Designer
Aeritalia
Type
Military transport aircraft
Length (m)
22.7
Height (m)
9.8
Cockpit Crew
3
Max Speed (km/h)
540
Cruise Speed (km/h)
439
Min Speed (km/h)
155
Max Ceiling (m)
7620
Rate of Climb (m/s)
8.667
Capacity Description
53 fully-equipped troops / 40 fully-equipped paratroops / 9000 kg max. payload
Number Built
111
Powerplant Description
2 × General Electric T64-GE-P4D turboprop engines, 2535 kW (3399 hp) each
Primary Users
Italian Air Force (historical), Nigerian Air Force , Argentine Army Aviation (historical)
Status
Retired
Wikipedia Article (URL)
en.wikipedia.org/wiki/Aeritalia_G.222
Flat Wing Span (m)
28.7
Flat Wing Aspect Ratio
9.15
Wake Category
M
Number of Engines
2