CN-235 vs G.222
CN-235 vs G.222 at a glance — top speed 450 vs 540 km/h, range 4,355 vs 1,371 km, max takeoff weight 16,500 vs 28,000 kg, built 354 vs 111 units.
Specifications
|
CN-235 |
G.222 |
| Origin country |
🇪🇸 Spain🇮🇩 Indonesia |
🇮🇹 Italy |
| Category |
Military Transport Aircraft |
Military Transport Aircraft |
| Manufacturer |
CASA |
Aeritalia |
| First flight |
11 November 1983 |
18 July 1970 |
| Year introduced |
1988 |
1978 |
| Number produced |
354 units |
111 units |
| Average unit price |
$25 million |
-- |
| Wing area |
59.1 m² |
82.0 m² |
| Wingspan |
25.8 m |
28.7 m |
| Height |
8.2 m |
9.8 m |
| Length |
21.4 m |
22.7 m |
| Maximum speed |
450 km/h |
540 km/h |
| Operational range |
4,355 km |
1,371 km |
| Service ceiling |
9,144 m |
7,620 m |
| Max. takeoff weight |
16,500 kg |
28,000 kg |
| Empty weight |
8,800 kg |
15,400 kg |
| Total thrust |
2 x 1,305 kW
|
2 x 2,501 kW
|
Detailed Comparison
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Which is faster, the CN-235 or G.222?
The G.222 is faster with a maximum speed of 540 km/h compared to the CN-235's 450 km/h, a difference of 90 km/h.
Which has longer range, the CN-235 or G.222?
The CN-235 has a longer range at 4,355 km compared to the G.222's 1,371 km.
Which can fly higher, the CN-235 or G.222?
The CN-235 has a higher service ceiling at 9,144 meters (30,000 ft) compared to the G.222's 7,620 meters (25,000 ft).
Which is heavier, the CN-235 or G.222?
The G.222 has a higher maximum takeoff weight at 28,000 kg compared to the CN-235's 16,500 kg.
Which is larger, the CN-235 or G.222?
The G.222 is longer at 22.7 meters compared to the CN-235's 21.4 meters.
Which entered service first, the CN-235 or G.222?
The G.222 entered service first in 1978, 10 years before the CN-235 which entered service in 1988.
Which has been built in greater numbers, the CN-235 or G.222?
The CN-235 has been produced in greater numbers with 354 units compared to 111 units of the G.222.
