Beechcraft 390 Premier I vs PA-34 Seneca
Overview
The Beechcraft 390 Premier I and the PA-34 Seneca are both Military Transport Aircraft, manufactured by Beechcraft and Piper respectively.
The Beechcraft 390 Premier I reaches 841 km/h β 2.2x the PA-34 Seneca's 378 km/h. The Beechcraft 390 Premier I has an operational range of 2,519 km vs 1,611 km for the PA-34 Seneca. The Beechcraft 390 Premier I operates at altitudes up to 12,497 m compared to 7,620 m for the PA-34 Seneca. At 5,670 kg MTOW, the Beechcraft 390 Premier I is 2.6x the PA-34 Seneca's 2,155 kg.
The Beechcraft 390 Premier I has been produced in 292 units vs 5,037 for the PA-34 Seneca. The PA-34 Seneca first flew 31 years before the Beechcraft 390 Premier I (1967 vs 1998).
| American business jet, produced in the late 20th century, utilized globally primarily in aial ambulance and executive transport roles. | |
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| Origin country | πΊπΈ United States |
| Category | Military Transport Aircraft |
| Manufacturer | Beechcraft |
| First flight | 22 December 1998 |
| Year introduced | 2001 |
| Number produced | 292 units |
| Average unit price | $5 million |
| American twin-engined light aircraft, renowned for its versatility, extensively used for flight training and personal use since the 1970s. | |
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| Origin country | πΊπΈ United States |
| Category | Military Transport Aircraft |
| Manufacturer | Piper |
| First flight | 25 April 1967 |
| Year introduced | 1971 |
| Number produced | 5037 units |
| Average unit price | -- |
| Wing area | 23.0 mΒ² β |
| Wingspan | 13.6 m β |
| Height | 4.7 m β |
| Length | 14.0 m β |
| Maximum speed | 841 km/h β |
| Operational range | 2,519 km β |
| Service ceiling | 12,497 m β |
| Max. takeoff weight | 5,670 kg β |
| Empty weight | 3,627 kg β |
| Total thrust | 2 x 522 kgf β |
| Wing area | 19.4 mΒ² β |
| Wingspan | 11.9 m β |
| Height | 3.0 m β |
| Length | 8.7 m β |
| Maximum speed | 378 km/h β |
| Operational range | 1,611 km β |
| Service ceiling | 7,620 m β |
| Max. takeoff weight | 2,155 kg β |
| Empty weight | 1,457 kg β |
| Total thrust | 2 x 82 kW β |
Performance Radar Chart
Detailed Comparison
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