DHC-8 Dash 8 vs P180 Avanti
Overview
The DHC-8 Dash 8 and the P180 Avanti are both Military Training Aircraft, manufactured by De Havilland Canada and Piaggio respectively.
Top speed is 451 km/h for the DHC-8 Dash 8 vs 732 km/h for the P180 Avanti. The DHC-8 Dash 8 has an operational range of 1,600 km vs 2,800 km for the P180 Avanti. The P180 Avanti operates at altitudes up to 12,500 m compared to 9,144 m for the DHC-8 Dash 8. At 15,649 kg MTOW, the DHC-8 Dash 8 is 2.9x the P180 Avanti's 5,489 kg.
The DHC-8 Dash 8 has been produced in 1,258 units vs 246 for the P180 Avanti. Unit cost is $27M for the DHC-8 Dash 8 vs $7.7M for the P180 Avanti. The DHC-8 Dash 8 first flew 3 years before the P180 Avanti (1983 vs 1986).
| Canadian turboprop-powered regional airliner, widely adopted globally for short-haul commuter flights throughout the late 20th century. | |
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| Origin country | 🇨🇦 Canada |
| Category | Military Training Aircraft |
| Manufacturer | De Havilland Canada |
| First flight | 20 June 1983 |
| Year introduced | 1984 |
| Number produced | 1258 units |
| Average unit price | $27 million |
| Italian turboprop business aircraft, renowned for its unusual design, extensively utilized for executive transport since the 1980s. | |
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| Origin country | 🇮🇹 Italy |
| Category | Military Training Aircraft |
| Manufacturer | Piaggio |
| First flight | 26 September 1986 |
| Year introduced | 1990 |
| Number produced | 246 units |
| Average unit price | $7.7 million |
| Wing area | 54.4 m² ◉ |
| Wingspan | 26.0 m â—‰ |
| Height | 7.5 m â—‰ |
| Length | 22.0 m â—‰ |
| Maximum speed | 451 km/h â—‰ |
| Operational range | 1,600 km â—‰ |
| Service ceiling | 9,144 m â—‰ |
| Max. takeoff weight | 15,649 kg â—‰ |
| Empty weight | 14,787 kg â—‰ |
| Total thrust | 2 x 671 kW â—‰ |
| Wing area | 16.0 m² ◉ |
| Wingspan | 14.0 m â—‰ |
| Height | 4.0 m â—‰ |
| Length | 14.4 m â—‰ |
| Maximum speed | 732 km/h â—‰ |
| Operational range | 2,800 km â—‰ |
| Service ceiling | 12,500 m â—‰ |
| Max. takeoff weight | 5,489 kg â—‰ |
| Empty weight | 3,402 kg â—‰ |
| Total thrust | 2 x 317 kW â—‰ |
Performance Radar Chart
Detailed Comparison
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