Beechcraft Baron vs C-101 Aviojet
Overview
The Beechcraft Baron and the C-101 Aviojet are both Military Training Aircraft, manufactured by Beechcraft and CASA respectively.
The C-101 Aviojet reaches 770 km/h β 2.1x the Beechcraft Baron's 370 km/h. The Beechcraft Baron has an operational range of 1,745 km vs 519 km for the C-101 Aviojet. The C-101 Aviojet operates at altitudes up to 12,500 m compared to 6,005 m for the Beechcraft Baron. At 6,300 kg MTOW, the C-101 Aviojet is 2.7x the Beechcraft Baron's 2,313 kg.
The Beechcraft Baron has been produced in 6,884 units vs 166 for the C-101 Aviojet. Unit cost is $1M for the Beechcraft Baron vs $8M for the C-101 Aviojet. The Beechcraft Baron first flew 17 years before the C-101 Aviojet (1960 vs 1977).
| 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 |
| Spanish jet trainer and light attack aircraft, deployed in the late 20th century, notably utilized by the Chilean and Spanish Air Forces. | |
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| Origin country | πͺπΈ Spain |
| Category | Military Training Aircraft |
| Manufacturer | CASA |
| First flight | 29 June 1977 |
| Year introduced | 1980 |
| Number produced | 166 units |
| Average unit price | $8 million |
| 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 | 20.0 mΒ² β |
| Wingspan | 10.6 m β |
| Height | 4.3 m β |
| Length | 12.5 m β |
| Maximum speed | 770 km/h β |
| Operational range | 519 km β |
| Service ceiling | 12,500 m β |
| Max. takeoff weight | 6,300 kg β |
| Empty weight | 2,800 kg β |
| Total thrust | 1 x 1,588 kgf β |
Performance Radar Chart
Detailed Comparison
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