Beechcraft 390 Premier I vs 737
Overview
The Beechcraft 390 Premier I and the 737 are both Military Transport Aircraft, manufactured by Beechcraft and Boeing respectively.
Top speed is 841 km/h for the Beechcraft 390 Premier I vs 904 km/h for the 737. The Beechcraft 390 Premier I has an operational range of 2,519 km vs 4,800 km for the 737. The Beechcraft 390 Premier I operates at altitudes up to 12,497 m compared to 11,278 m for the 737. At 52,163 kg MTOW, the 737 is 9.2x the Beechcraft 390 Premier I's 5,670 kg.
The Beechcraft 390 Premier I has been produced in 292 units vs 11,535 for the 737. Unit cost is $5M for the Beechcraft 390 Premier I vs $115M for the 737. The 737 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-engine narrow-body jet airliner, popularly deployed for commercial aviation since the late 1960s. | |
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| Origin country | πΊπΈ United States |
| Category | Military Transport Aircraft |
| Manufacturer | Boeing |
| First flight | 9 April 1967 |
| Year introduced | 1968 |
| Number produced | 11535 units |
| Average unit price | $115 million |
| 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 | 91.0 mΒ² β |
| Wingspan | 28.0 m β |
| Height | 11.0 m β |
| Length | 30.0 m β |
| Maximum speed | 904 km/h β |
| Operational range | 4,800 km β |
| Service ceiling | 11,278 m β |
| Max. takeoff weight | 52,163 kg β |
| Empty weight | 29,071 kg β |
| Total thrust | 2 x 3,289 kgf β |
Performance Radar Chart
Detailed Comparison
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