DHC-8 Dash 8 vs Gulfstream G550
Overview
The DHC-8 Dash 8 and the Gulfstream G550 are both Military Training Aircraft, manufactured by De Havilland Canada and Gulfstream respectively.
The Gulfstream G550 reaches 941 km/h β 2.1x the DHC-8 Dash 8's 451 km/h. The DHC-8 Dash 8 has an operational range of 1,600 km vs 12,500 km for the Gulfstream G550. The Gulfstream G550 operates at altitudes up to 15,545 m compared to 9,144 m for the DHC-8 Dash 8. At 41,050 kg MTOW, the Gulfstream G550 is 2.6x the DHC-8 Dash 8's 15,649 kg.
The DHC-8 Dash 8 has been produced in 1,258 units vs 600 for the Gulfstream G550. Unit cost is $27M for the DHC-8 Dash 8 vs $62M for the Gulfstream G550. The DHC-8 Dash 8 first flew 20 years before the Gulfstream G550 (1983 vs 2003).
| Canadian turboprop-powered regional airliner, widely adopted globally for short-haul commuter flights throughout the late 20th century. | |
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| Origin country | π¨π¦ 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 |
| American business jet, in service since the early 21st century, renowned for long-range capabilities and high-speed performance. | |
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| Origin country | πΊπΈ United States |
| Category | Military Training Aircraft |
| Manufacturer | Gulfstream |
| First flight | 1 January 2003 |
| Year introduced | 2004 |
| Number produced | 600 units |
| Average unit price | $62 million |
| Wing area | 54.4 mΒ² β |
| Wingspan | 26.0 m β |
| Height | 7.5 m β |
| Length | 22.0 m β |
| Maximum speed | 451 km/h β |
| Operational range | 1,600 km β |
| Service ceiling | 9,144 m β |
| Max. takeoff weight | 15,649 kg β |
| Empty weight | 14,787 kg β |
| Total thrust | 2 x 671 kW β |
| Wing area | 106.0 mΒ² β |
| Wingspan | 28.5 m β |
| Height | 7.7 m β |
| Length | 29.4 m β |
| Maximum speed | 941 km/h β |
| Operational range | 12,500 km β |
| Service ceiling | 15,545 m β |
| Max. takeoff weight | 41,050 kg β |
| Empty weight | 20,956 kg β |
| Total thrust | 2 x 3,345 kgf β |
Performance Radar Chart
Detailed Comparison
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