Fuji T-7 vs Pilatus PC-21
Fuji T-7 vs Pilatus PC-21 at a glance — max takeoff weight 1,585 vs 4,250 kg, built 49 vs 211 units.
Specifications
|
Fuji T-7 |
Pilatus PC-21 |
| Origin country |
🇯🇵 Japan |
🇨🇭 Switzerland |
| Category |
Military Training Aircraft |
Military Training Aircraft |
| Manufacturer |
Fuji |
Pilatus |
| First flight |
1 January 2002 |
1 July 2002 |
| Year introduced |
2003 |
2008 |
| Number produced |
49 units |
211 units |
| Average unit price |
-- |
$9 million |
| Wing area |
16.5 m² |
15.2 m² |
| Wingspan |
10.0 m |
9.1 m |
| Height |
3.0 m |
3.8 m |
| Length |
8.6 m |
11.2 m |
| Maximum speed |
-- km/h |
685 km/h |
| Operational range |
-- km |
1,333 km |
| Service ceiling |
-- m |
11,580 m |
| Max. takeoff weight |
1,585 kg |
4,250 kg |
| Empty weight |
-- kg |
2,270 kg |
| Total thrust |
1 x 336 kW
|
1 x 1,193 kW
|
Detailed Comparison
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Which is heavier, the Fuji T-7 or Pilatus PC-21?
The Pilatus PC-21 has a higher maximum takeoff weight at 4,250 kg compared to the Fuji T-7's 1,585 kg.
Which is larger, the Fuji T-7 or Pilatus PC-21?
The Pilatus PC-21 is longer at 11.2 meters compared to the Fuji T-7's 8.6 meters.
Which entered service first, the Fuji T-7 or Pilatus PC-21?
The Fuji T-7 entered service first in 2003, 5 years before the Pilatus PC-21 which entered service in 2008.
Which has been built in greater numbers, the Fuji T-7 or Pilatus PC-21?
The Pilatus PC-21 has been produced in greater numbers with 211 units compared to 49 units of the Fuji T-7.
