Alenia G222
Alenia G222
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| Developing Nation: | Italy |
| Task: | Tactical Transporter |
| First Flight: |
- prototype: July 18th 1970 - first production airframe: December 23rd 1975 |
| First Delivery: | April 1978 |
| Crew: |
- 2 (flight-crew) - 1 (extra accommodation for loadmaster) |
| Accommodation: |
- Typical accommodation for 46 troops or 40 paratroops - capability 9000 kg payload incl. light vehicles and artillery |
| Wing Span: | 28,70 m |
| Wing Area: | 82,00 m² |
| Length: | 22,70 m |
| Height: | 10,57 m |
| Engine (s): |
General Electric T64-GE-P4D turboprops with 2535 kW power (2x) License built by Fiat. Powering 3 blade propellers |
| Weight: | 15700 kg |
| Max.Take off weight: | 28000 kg |
| Max. Speed: |
- 487 km/h top speed - 437 km/h long range cruise speed |
| Max. Range: |
- 4685 km - 1260 km with max payload |
| Ceiling: | 8560 m |
| Weapons: | none |
| Extra: | Production ended in 1999 |
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Operators of the G222 |
| Argentina |
| Italy (44) |
| Libya |
| Nigeria |
| Thailand |
| Tunisia |
| Venezuela |
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research M. v. Leeuwen



