Bell 412
The Bell 412 is a utility helicopter manufactured by Bell Helicopter. It is a development of the Bell 212 model, the major difference being the composite four-blade main rotor. The 412 model was followed by the 412SP (Special Performance) version featuring larger fuel capacity, higher takeoff weight and optional seating arrangements. In 1991, the 412HP (High Performance) variant with improved transmission replaced the SP version in production.
Aircraft Specification
| Aircraft Size | Metric | English |
| Length | 12.70 m | 41.67 ft |
| Rotor Diameter | 14.00 m | 45.93 ft |
| Height | 4.57 m | 15.00 ft |
| Bag. Capacity | 1 m³ | 28 ft³ |
Performance Specification
| Performance | Metric | English |
| Cruise Speed | 243 km/h | 131 KTAS |
| Certified Ceiling | 6,096 m | 20,000 ft |
| Rate of Climb | 411 m/m | 1,350 ft/m |
| Takeoff Distance | 15 m | 50 ft |
| Landing Distance | 15 m | 50 ft |