Flat Wing Aspect Ratio
9.15
Entry Into service
1978-04-01
Maximum Take-Off Weight
28 t (paragliders: kg)
Total Fuel Capacity
12000
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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 |
Similar airplanes
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