Beechcraft Baron vs Soko G-4 Super Galeb
Overview
The Beechcraft Baron and the Soko G-4 Super Galeb are both Military Training Aircraft, manufactured by Beechcraft and SOKO respectively.
The Soko G-4 Super Galeb reaches 910 km/h β 2.5x the Beechcraft Baron's 370 km/h. The Beechcraft Baron has an operational range of 1,745 km vs 1,900 km for the Soko G-4 Super Galeb. The Soko G-4 Super Galeb operates at altitudes up to 12,850 m compared to 6,005 m for the Beechcraft Baron. At 6,330 kg MTOW, the Soko G-4 Super Galeb is 2.7x the Beechcraft Baron's 2,313 kg.
The Beechcraft Baron has been produced in 6,884 units vs 85 for the Soko G-4 Super Galeb. The Beechcraft Baron first flew 18 years before the Soko G-4 Super Galeb (1960 vs 1978).
| American light, twin-engined piston aircraft, utilized globally for business, personal, and flight training purposes since the mid-20th century. | |
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| Origin country | πΊπΈ United States |
| Category | Military Training Aircraft |
| Manufacturer | Beechcraft |
| First flight | 29 February 1960 |
| Year introduced | 1961 |
| Number produced | 6884 units |
| Average unit price | $1 million |
| Yugoslav single-engine advanced jet trainer and light ground-attack aircraft, developed in the 1970s and utilized for both pilot training and close air support missions. | |
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| Origin country | π³π± Ex-Yugoslavia |
| Category | Military Training Aircraft |
| Manufacturer | SOKO |
| First flight | 17 July 1978 |
| Year introduced | 1983 |
| Number produced | 85 units |
| Average unit price | -- |
| Wing area | 18.5 mΒ² β |
| Wingspan | 11.3 m β |
| Height | 3.0 m β |
| Length | 9.0 m β |
| Maximum speed | 370 km/h β |
| Operational range | 1,745 km β |
| Service ceiling | 6,005 m β |
| Max. takeoff weight | 2,313 kg β |
| Empty weight | 1,432 kg β |
| Total thrust | 2 x 97 kW β |
| Wing area | 19.5 mΒ² β |
| Wingspan | 9.9 m β |
| Height | 4.3 m β |
| Length | 12.3 m β |
| Maximum speed | 910 km/h β |
| Operational range | 1,900 km β |
| Service ceiling | 12,850 m β |
| Max. takeoff weight | 6,330 kg β |
| Empty weight | 3,250 kg β |
| Total thrust | 1 x 1,815 kgf β |
Performance Radar Chart
Detailed Comparison
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