Bell Bell 430
Summary
| Category | Helicopter |
| Origin country | 🇺🇸 United States |
| First flight | 25 October 1994 |
| Year of introduction | 1995 |
| Number produced | 136 units |
Description
The Bell Bell 430 is a twin-engine, medium-sized military aircraft developed by the American company Bell Helicopter. Designed as a utility helicopter, it was primarily used for various missions such as troop transport, search and rescue, and reconnaissance. The aircraft features a spacious cabin with seating for up to 12 passengers and advanced avionics systems for enhanced situational awareness. Its twin-engine configuration provides increased reliability and performance capabilities, allowing it to operate in various weather conditions and terrains. The Bell 430 has been deployed by several military forces worldwide, showcasing its versatility and adaptability for different operational requirements.
Technical specifications
| Version: Bell 430 | |
|---|---|
| Crew | 1 pilot |
| Maximum speed | 278 km/h (173 mph) |
| Height | 3.8 m (12.3 ft) |
| Length | 15.3 m (50.2 ft) |
| Service ceiling | 6096 m (20000 ft) |
| Empty weight | 2406 kg (5304 lbs) |
| Max. takeoff weight | 4218 kg (9299 lbs) |
| Climb rate | 6.858 m/s (22.5 ft/s) |
| Powerplant | 2 × turbines Allison 250-C40B delivering 585 kW |
Current operating countries
| Country | Units | ||
|---|---|---|---|
|
Ecuador | 3 | |
|
Dominican Republic | 1 | |
Numbers in parentheses, e.g. '(+5)', indicate units ordered but not yet delivered.
All operators
Photo of Bell 430
Credits: Bell
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