C-17 Globemaster III vs PA-34 Seneca
Overview
The C-17 Globemaster III and the PA-34 Seneca are both Military Transport Aircraft, manufactured by McDonnell Douglas and Piper respectively.
The C-17 Globemaster III reaches 930 km/h β 2.5x the PA-34 Seneca's 378 km/h. The C-17 Globemaster III has an operational range of 4,480 km vs 1,611 km for the PA-34 Seneca. The C-17 Globemaster III operates at altitudes up to 13,715 m compared to 7,620 m for the PA-34 Seneca. At 259,460 kg MTOW, the C-17 Globemaster III is 120:1 the PA-34 Seneca's 2,155 kg.
The C-17 Globemaster III has been produced in 279 units vs 5,037 for the PA-34 Seneca. The PA-34 Seneca first flew 24 years before the C-17 Globemaster III (1967 vs 1991).
| American military transport aircraft, extensively deployed in global conflict zones since the 1990s for strategic airlift missions. | |
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| Origin country | πΊπΈ United States |
| Category | Military Transport Aircraft |
| Manufacturer | McDonnell Douglas |
| First flight | 15 September 1991 |
| Year introduced | 1993 |
| Number produced | 279 units |
| Average unit price | $340 million |
| American twin-engined light aircraft, renowned for its versatility, extensively used for flight training and personal use since the 1970s. | |
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| Origin country | πΊπΈ United States |
| Category | Military Transport Aircraft |
| Manufacturer | Piper |
| First flight | 25 April 1967 |
| Year introduced | 1971 |
| Number produced | 5037 units |
| Average unit price | -- |
| Wing area | 353.0 mΒ² β |
| Wingspan | 51.8 m β |
| Height | 16.8 m β |
| Length | 53.0 m β |
| Maximum speed | 930 km/h β |
| Operational range | 4,480 km β |
| Service ceiling | 13,715 m β |
| Max. takeoff weight | 259,460 kg β |
| Empty weight | 122,000 kg β |
| Total thrust | 4 x 4,727 kgf β |
| Wing area | 19.4 mΒ² β |
| Wingspan | 11.9 m β |
| Height | 3.0 m β |
| Length | 8.7 m β |
| Maximum speed | 378 km/h β |
| Operational range | 1,611 km β |
| Service ceiling | 7,620 m β |
| Max. takeoff weight | 2,155 kg β |
| Empty weight | 1,457 kg β |
| Total thrust | 2 x 82 kW β |
Performance Radar Chart
Detailed Comparison
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