Il-20 Coot-A vs King Air 90
Il-20 Coot-A vs King Air 90 at a glance — top speed 675 vs 494 km/h, range 6,200 vs 2,446 km, max takeoff weight 64,000 vs 5,352 kg.
Specifications
|
Il-20 Coot-A |
King Air 90 |
| Origin country |
🇷🇺 Ex-USSR |
🇺🇸 United States |
| Category |
Military Special Mission Aircraft |
Military Special Mission Aircraft |
| Manufacturer |
Ilyushin |
Beechcraft |
| First flight |
21 March 1968 |
1 January 1964 |
| Year introduced |
-- |
1964 |
| Number produced |
N/A |
3100 units |
| Average unit price |
-- |
-- |
| Wing area |
140.6 m² |
26.0 m² |
| Wingspan |
37.4 m |
13.8 m |
| Height |
10.2 m |
4.7 m |
| Length |
35.9 m |
11.9 m |
| Maximum speed |
675 km/h |
494 km/h |
| Operational range |
6,200 km |
2,446 km |
| Service ceiling |
10,000 m |
7,574 m |
| Max. takeoff weight |
64,000 kg |
5,352 kg |
| Empty weight |
33,760 kg |
3,217 kg |
| Total thrust |
4 x 3,169 kW
|
2 x 626 kW
|
Detailed Comparison
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Which is faster, the Il-20 Coot-A or King Air 90?
The Il-20 Coot-A is faster with a maximum speed of 675 km/h compared to the King Air 90's 494 km/h, a difference of 181 km/h.
Which has longer range, the Il-20 Coot-A or King Air 90?
The Il-20 Coot-A has a longer range at 6,200 km compared to the King Air 90's 2,446 km.
Which can fly higher, the Il-20 Coot-A or King Air 90?
The Il-20 Coot-A has a higher service ceiling at 10,000 meters (32,808 ft) compared to the King Air 90's 7,574 meters (24,849 ft).
Which is heavier, the Il-20 Coot-A or King Air 90?
The Il-20 Coot-A has a higher maximum takeoff weight at 64,000 kg compared to the King Air 90's 5,352 kg.
Which is larger, the Il-20 Coot-A or King Air 90?
The Il-20 Coot-A is longer at 35.9 meters compared to the King Air 90's 11.9 meters.
