DHC-6 Twin Otter vs PC-6 Porter
Overview
The DHC-6 Twin Otter and the PC-6 Porter are both Military Transport Aircraft, manufactured by De Havilland Canada and Pilatus respectively.
Top speed is 315 km/h for the DHC-6 Twin Otter vs 244 km/h for the PC-6 Porter. The DHC-6 Twin Otter has an operational range of 1,480 km vs 730 km for the PC-6 Porter. The PC-6 Porter operates at altitudes up to 10,000 m compared to 7,620 m for the DHC-6 Twin Otter. At 5,670 kg MTOW, the DHC-6 Twin Otter is 2.0x the PC-6 Porter's 2,800 kg.
The DHC-6 Twin Otter has been produced in 985 units vs 604 for the PC-6 Porter. Unit cost is $7M for the DHC-6 Twin Otter vs $0.06M for the PC-6 Porter. The PC-6 Porter first flew 6 years before the DHC-6 Twin Otter (1959 vs 1965).
| Canadian utility aircraft, vital in civil and military operations worldwide since the 1960s, famous for its STOL capabilities. | |
|
|
| Origin country | 🇨🇦 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 |
| Swiss light utility aircraft, renowned for its versatility and ruggedness, extensively utilized in remote areas for cargo transport and search and rescue missions. | |
|
|
| Origin country | 🇨🇠Switzerland |
| Category | Military Transport Aircraft |
| Manufacturer | Pilatus |
| First flight | 4 May 1959 |
| Year introduced | 1960 |
| Number produced | 604 units |
| Average unit price | $60K |
| Wing area | 39.0 m² ◉ |
| Wingspan | 20.0 m â—‰ |
| Height | 6.0 m â—‰ |
| Length | 15.8 m â—‰ |
| Maximum speed | 315 km/h â—‰ |
| Operational range | 1,480 km â—‰ |
| Service ceiling | 7,620 m â—‰ |
| Max. takeoff weight | 5,670 kg â—‰ |
| Empty weight | 3,175 kg â—‰ |
| Total thrust | 2 x 205 kW â—‰ |
| Wing area | 30.2 m² ◉ |
| Wingspan | 15.9 m â—‰ |
| Height | 3.2 m â—‰ |
| Length | 10.9 m â—‰ |
| Maximum speed | 244 km/h â—‰ |
| Operational range | 730 km â—‰ |
| Service ceiling | 10,000 m â—‰ |
| Max. takeoff weight | 2,800 kg â—‰ |
| Empty weight | 1,260 kg â—‰ |
| Total thrust | 1 x 410 kW â—‰ |
Performance Radar Chart
Detailed Comparison
Generating comparison analysis...
Unable to generate comparison at this time.