Beechcraft 390 Premier I vs Gulfstream G100
Overview
The Beechcraft 390 Premier I and the Gulfstream G100 are both Military Transport Aircraft, manufactured by Beechcraft and Gulfstream respectively.
Top speed is 841 km/h for the Beechcraft 390 Premier I vs 874 km/h for the Gulfstream G100. The Beechcraft 390 Premier I has an operational range of 2,519 km vs 5,462 km for the Gulfstream G100. The Gulfstream G100 operates at altitudes up to 13,716 m compared to 12,497 m for the Beechcraft 390 Premier I. At 11,500 kg MTOW, the Gulfstream G100 is 2.0x the Beechcraft 390 Premier I's 5,670 kg.
The Beechcraft 390 Premier I has been produced in 292 units vs 265 for the Gulfstream G100. Unit cost is $5M for the Beechcraft 390 Premier I vs $4.3M for the Gulfstream G100. The Gulfstream G100 first flew 14 years before the Beechcraft 390 Premier I (1984 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 | 🇺🇸 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 |
| Israeli-American mid-size business jet, recognized for transcontinental range, introduced in the late 20th century. | |
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| Origin country | 🇺🇸 United States |
| Category | Military Transport Aircraft |
| Manufacturer | Gulfstream |
| First flight | 1 January 1984 |
| Year introduced | 1985 |
| Number produced | 265 units |
| Average unit price | $4.3 million |
| Wing area | 23.0 m² ◉ |
| Wingspan | 13.6 m ◉ |
| Height | 4.7 m ◉ |
| Length | 14.0 m ◉ |
| Maximum speed | 841 km/h ◉ |
| Operational range | 2,519 km ◉ |
| Service ceiling | 12,497 m ◉ |
| Max. takeoff weight | 5,670 kg ◉ |
| Empty weight | 3,627 kg ◉ |
| Total thrust | 2 x 522 kgf ◉ |
| Wing area | 29.4 m² ◉ |
| Wingspan | 16.6 m ◉ |
| Height | 5.5 m ◉ |
| Length | 17.0 m ◉ |
| Maximum speed | 874 km/h ◉ |
| Operational range | 5,462 km ◉ |
| Service ceiling | 13,716 m ◉ |
| Max. takeoff weight | 11,500 kg ◉ |
| Empty weight | 6,531 kg ◉ |
| Total thrust | 2 x 964 kgf ◉ |
Performance Radar Chart
Detailed Comparison
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