C-160 Transall vs CN-235
Overview
The C-160 Transall and the CN-235 are both Military Transport Aircraft, manufactured by Transall and CASA respectively.
Top speed is 513 km/h for the C-160 Transall vs 450 km/h for the CN-235. The C-160 Transall has an operational range of 1,853 km vs 4,355 km for the CN-235. The CN-235 operates at altitudes up to 9,144 m compared to 8,230 m for the C-160 Transall. At 51,000 kg MTOW, the C-160 Transall is 3.1x the CN-235's 16,500 kg.
The C-160 Transall has been produced in 214 units vs 354 for the CN-235. Unit cost is $12M for the C-160 Transall vs $25M for the CN-235. The C-160 Transall first flew 20 years before the CN-235 (1963 vs 1983).
| German-French transport plane, employed globally since the Cold War, essential for humanitarian aid, military logistical support, and troop transport. | |
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| Origin country | 🇩🇪 Germany 🇫🇷 France |
| Category | Military Transport Aircraft |
| Manufacturer | Transall |
| First flight | 25 February 1963 |
| Year introduced | 1967 |
| Number produced | 214 units |
| Average unit price | $12 million |
| Spanish-Indonesian transport aircraft, widespread use in the civil sector, military services, and humanitarian aid, developed during the late 20th century. | |
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| Origin country | 🇪🇸 Spain 🇮🇩 Indonesia |
| Category | Military Transport Aircraft |
| Manufacturer | CASA |
| First flight | 11 November 1983 |
| Year introduced | 1988 |
| Number produced | 354 units |
| Average unit price | $25 million |
| Wing area | 160.0 m² ◉ |
| Wingspan | 40.0 m â—‰ |
| Height | 11.7 m â—‰ |
| Length | 32.4 m â—‰ |
| Maximum speed | 513 km/h â—‰ |
| Operational range | 1,853 km â—‰ |
| Service ceiling | 8,230 m â—‰ |
| Max. takeoff weight | 51,000 kg â—‰ |
| Empty weight | 29,000 kg â—‰ |
| Total thrust | 2 x 2,275 kW â—‰ |
| Wing area | 59.1 m² ◉ |
| Wingspan | 25.8 m â—‰ |
| Height | 8.2 m â—‰ |
| Length | 21.4 m â—‰ |
| Maximum speed | 450 km/h â—‰ |
| Operational range | 4,355 km â—‰ |
| Service ceiling | 9,144 m â—‰ |
| Max. takeoff weight | 16,500 kg â—‰ |
| Empty weight | 8,800 kg â—‰ |
| Total thrust | 2 x 653 kW â—‰ |
Performance Radar Chart
Detailed Comparison
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Frequently Asked Questions
Which is faster, the C-160 Transall or CN-235?
The C-160 Transall is faster with a maximum speed of 513 km/h compared to the CN-235's 450 km/h, a difference of 63 km/h.
Which has longer range, the C-160 Transall or CN-235?
The CN-235 has a longer range at 4,355 km compared to the C-160 Transall's 1,853 km.
Which can fly higher, the C-160 Transall or CN-235?
The CN-235 has a higher service ceiling at 9,144 meters (30,000 ft) compared to the C-160 Transall's 8,230 meters (27,001 ft).
Which is heavier, the C-160 Transall or CN-235?
The C-160 Transall has a higher maximum takeoff weight at 51,000 kg compared to the CN-235's 16,500 kg.
Which is larger, the C-160 Transall or CN-235?
The C-160 Transall is longer at 32.4 meters compared to the CN-235's 21.4 meters.
Which is more expensive, the C-160 Transall or CN-235?
The CN-235 is more expensive at approximately $25 million per unit compared to the C-160 Transall at $12 million.
Which entered service first, the C-160 Transall or CN-235?
The C-160 Transall entered service first in 1967, 21 years before the CN-235 which entered service in 1988.
Which has been built in greater numbers, the C-160 Transall or CN-235?
The CN-235 has been produced in greater numbers with 354 units compared to 214 units of the C-160 Transall.