AVIOCAR C-212 (CASA)
| Specifications | |
|---|---|
| Country of Origin | Spain |
| Builder | |
| Role | STOL, light-utility transport (18 equipped troops, light tactical vehicles), airdrop |
| Similar Aircraft | C-160 Transall, C-123 Provider, G.222 |
| Wing Span | 62 ft, 4 in (19.12 m) / 20,3 m (212-300) |
| Length | 49 ft, 9 in (15.18 m) / 16,1 m (212-300) |
| Height | 6,29 m |
| Weight |
4.200 Kg base weight 6.500 Kg Max. takeoff weight 8.100 Kg Max. takeoff weight (212-300) |
| Engine | Two turbo propeller engines supplying 715 HP each, at sea level
2 GARRETT turbo propeller engines, supplying a power of 925 HP each, at sea level (212-300) |
| Maximum speed | 370 Km/h |
| Cruising speed | 275 Km/h |
| Endurance | 05 Hr 40 min |
| Service Ceiling | 9,900 m |
| Distance of takeoff | 400 m / 895 m (212-300) |
| Landing distance | 300 m / 865 m (212-300) |
| Armament | Usually none |
| Crew | Two |
| Cost | |
| User Countries | Angola, Chad, Equatorial New Guinea, Ghana, Mexico, Nicaragua, Panama, Paraguay, Portugal, Saudi Arabia, Somalia, South Africa, Spain, Sudan, Venezuela |
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