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
– prototype: July 18th 1970
– first production airframe: December 23rd 1975
– 2 (flight-crew)
– 1 (extra accommodation for loadmaster)
– Typical accommodation for 46 troops or 40 paratroops
– capability 9000 kg payload incl. light vehicles and artillery
General Electric T64-GE-P4D turboprops with 2535 kW power (2x) License built by Fiat.
Powering 3 blade propellers
– 487 km/h top speed
– 437 km/h long range cruise speed
– 4685 km
– 1260 km with max payload
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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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