AT-3 Tsu Chiang vs Beechcraft Baron
Overview
The AT-3 Tsu Chiang and the Beechcraft Baron are both Military Training Aircraft, manufactured by AIDC and Beechcraft respectively.
The AT-3 Tsu Chiang reaches 904 km/h β 2.4x the Beechcraft Baron's 370 km/h. The AT-3 Tsu Chiang has an operational range of 2,280 km vs 1,745 km for the Beechcraft Baron. The AT-3 Tsu Chiang operates at altitudes up to 14,650 m compared to 6,005 m for the Beechcraft Baron. At 7,940 kg MTOW, the AT-3 Tsu Chiang is 3.4x the Beechcraft Baron's 2,313 kg.
The AT-3 Tsu Chiang has been produced in 62 units vs 6,884 for the Beechcraft Baron. Unit cost is $4M for the AT-3 Tsu Chiang vs $1M for the Beechcraft Baron. The Beechcraft Baron first flew 20 years before the AT-3 Tsu Chiang (1960 vs 1980).
| Taiwanese advanced jet trainer, deployed in the 1980s, renowned for its service in the Republic of China Air Force. | |
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| Origin country | πΉπΌ Taiwan |
| Category | Military Training Aircraft |
| Manufacturer | AIDC |
| First flight | 16 September 1980 |
| Year introduced | 1984 |
| Number produced | 62 units |
| Average unit price | $4 million |
| 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 |
| Wing area | 21.9 mΒ² β |
| Wingspan | 10.5 m β |
| Height | 4.4 m β |
| Length | 12.9 m β |
| Maximum speed | 904 km/h β |
| Operational range | 2,280 km β |
| Service ceiling | 14,650 m β |
| Max. takeoff weight | 7,940 kg β |
| Empty weight | 3,856 kg β |
| Total thrust | 2 x 794 kgf β |
| 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 |
Performance Radar Chart
Detailed Comparison
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