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
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