An-30 Clank vs DHC-6 Twin Otter
Overview
The An-30 Clank and the DHC-6 Twin Otter are both Military Transport Aircraft, manufactured by Antonov and De Havilland Canada respectively.
Top speed is 540 km/h for the An-30 Clank vs 315 km/h for the DHC-6 Twin Otter. The An-30 Clank has an operational range of 2,630 km vs 1,480 km for the DHC-6 Twin Otter. The An-30 Clank operates at altitudes up to 8,300 m compared to 7,620 m for the DHC-6 Twin Otter. At 23,000 kg MTOW, the An-30 Clank is 4.1x the DHC-6 Twin Otter's 5,670 kg.
The An-30 Clank has been produced in 123 units vs 985 for the DHC-6 Twin Otter. Unit cost is $7M for the An-30 Clank vs $7M for the DHC-6 Twin Otter. The DHC-6 Twin Otter first flew 2 years before the An-30 Clank (1965 vs 1967).
| Soviet photo-mapping aircraft, operational in Cold War-era, widely utilised for aerial cartography and surveillance roles. | |
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| Origin country | πΊπ¦ Ukraine |
| Category | Military Transport Aircraft |
| Manufacturer | Antonov |
| First flight | 27 August 1967 |
| Year introduced | 1968 |
| Number produced | 123 units |
| Average unit price | $7 million |
| Canadian utility aircraft, vital in civil and military operations worldwide since the 1960s, famous for its STOL capabilities. | |
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| Origin country | π¨π¦ Canada |
| Category | Military Transport Aircraft |
| Manufacturer | De Havilland Canada |
| First flight | 20 May 1965 |
| Year introduced | 1966 |
| Number produced | 985 units |
| Average unit price | $7 million |
| Wing area | 75.0 mΒ² β |
| Wingspan | 29.2 m β |
| Height | 8.3 m β |
| Length | 24.3 m β |
| Maximum speed | 540 km/h β |
| Operational range | 2,630 km β |
| Service ceiling | 8,300 m β |
| Max. takeoff weight | 23,000 kg β |
| Empty weight | 15,590 kg β |
| Total thrust | 2 x 1,037 kW β |
| Wing area | 39.0 mΒ² β |
| Wingspan | 20.0 m β |
| Height | 6.0 m β |
| Length | 15.8 m β |
| Maximum speed | 315 km/h β |
| Operational range | 1,480 km β |
| Service ceiling | 7,620 m β |
| Max. takeoff weight | 5,670 kg β |
| Empty weight | 3,175 kg β |
| Total thrust | 2 x 205 kW β |
Performance Radar Chart
Detailed Comparison
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