Helicopter • Bell • Bell 412EP, Bell 412EPi, Bell 412EPI (Improved), VH-71 Kestrel (Military variant)
| Manufacturer | Bell |
| Model | 412EP |
| Category | Helicopter |
| Variants | Bell 412EP, Bell 412EPi, Bell 412EPI (Improved), VH-71 Kestrel (Military variant) |
| Seating | 14, 15 seats |
| Typical TTAF | 4,200 hours |
| Markets | United States, Canada, Australia, Brazil, Mexico |
| Price Range | $2.5M – $8.5M |
The Bell 412EP is a twin-engine, medium-lift utility helicopter developed by Bell Helicopter as an enhanced variant of the original Bell 412. The "EP" designation stands for "Enhanced Performance," reflecting significant improvements in power, payload capacity, and operational efficiency introduced in the late 1990s. The aircraft features a four-bladed main rotor system and is powered by two Pratt & Whitney PT6T-3B Twin-Pac turboshaft engines, providing superior performance in hot-and-high environments compared to its predecessor.
The Bell 412EP is renowned for its versatility and reliability, making it a preferred choice for civil and military operators worldwide. Primary applications include emergency medical services (EMS), offshore transport, search and rescue, corporate transport, and law enforcement operations. The helicopter's spacious cabin accommodates up to 15 passengers or various cargo configurations, while maintaining excellent single-engine safety margins—a critical feature for operations over water and remote terrain.
Key distinguishing features include improved avionics packages, enhanced rotor blade technology for better efficiency, and increased maximum takeoff weight capabilities. The aircraft's proven track record, low maintenance requirements, and availability of experienced maintenance personnel have contributed to its sustained popularity across diverse operational environments globally.
Maximum speed: 287 km/h (174 mph)
Cruise speed: 259 km/h (161 mph)
Range: 685 km (426 miles)
Service ceiling: 5,486 meters (18,000 feet)
Maximum takeoff weight: 5,443 kg (12,000 lbs)
Engines: 2 × Pratt & Whitney PT6T-3B turboshafts
Fuel capacity: 1,814 liters (479 gallons)
Main rotor diameter: 14.73 meters (48.35 feet)