Fuji T-7 vs T-25 Universal
Fuji T-7 vs T-25 Universal at a glance — max takeoff weight 1,585 vs 1,700 kg, built 49 vs 189 units.
Specifications
|
Fuji T-7 |
T-25 Universal |
| Origin country |
🇯🇵 Japan |
🇧🇷 Brazil |
| Category |
Military Training Aircraft |
Military Training Aircraft |
| Manufacturer |
Fuji |
Neiva |
| First flight |
1 January 2002 |
29 April 1966 |
| Year introduced |
2003 |
1971 |
| Number produced |
49 units |
189 units |
| Average unit price |
-- |
-- |
| Wing area |
16.5 m² |
17.2 m² |
| Wingspan |
10.0 m |
11.0 m |
| Height |
3.0 m |
3.0 m |
| Length |
8.6 m |
8.6 m |
| Maximum speed |
-- km/h |
300 km/h |
| Operational range |
-- km |
1,500 km |
| Service ceiling |
-- m |
6,100 m |
| Max. takeoff weight |
1,585 kg |
1,700 kg |
| Empty weight |
-- kg |
1,150 kg |
| Total thrust |
1 x 336 kW
|
1 x 220 kW
|
Detailed Comparison
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Which is heavier, the Fuji T-7 or T-25 Universal?
The T-25 Universal has a higher maximum takeoff weight at 1,700 kg compared to the Fuji T-7's 1,585 kg.
Which is larger, the Fuji T-7 or T-25 Universal?
Both the Fuji T-7 and T-25 Universal are 8.6 meters long.
Which entered service first, the Fuji T-7 or T-25 Universal?
The T-25 Universal entered service first in 1971, 32 years before the Fuji T-7 which entered service in 2003.
Which has been built in greater numbers, the Fuji T-7 or T-25 Universal?
The T-25 Universal has been produced in greater numbers with 189 units compared to 49 units of the Fuji T-7.