Bell 412EP

The Bell 412EP is a multi-purpose helicopter developed by the American firm Bell Helicopter Textron. This advanced aircraft represents a significant evolution within the Bell 412 family, building upon its robust design and proven performance.

Advanced Propulsion Systems

Equipped with new Pratt & Whitney Canada PT6T-3D Twin Pac gas turbine engines, delivering 1342 kW of power, the Bell 412EP offers enhanced capabilities. A key innovation includes its improved elastomeric rotor suspensions, contributing significantly to its operational efficiency and reliability.

Serial Production and Key Features

Serial production of the Bell 412EP commenced in 1996, establishing its presence in the market. Its design focuses on versatility, making it suitable for a wide range of missions.

Specialized Naval Operations Variant

A distinct modification, developed by Heli-Dyne of Dallas, equips the Bell 412EP for specialized naval operations. This variant includes advanced equipment such as radar, sonar, and other systems, enabling it to perform anti-submarine and anti-ship missions effectively.

Technical Specifications

Modification	Bell 412EP
Main rotor diameter, m	14.02
Tail rotor diameter, m	2.62
Length, m	12.70
Height, m	3.48
Width, m	2.80
Empty weight	3102
Maximum takeoff weight	5398
Internal fuel, l	1250
Engine type	1 Gas turbine engine Pratt Whitney Canada PT6T-3D Twin Pac
Power, kW	1 х 1342
Maximum speed, km/h	259
Cruising speed, km/h	230
Range, km	745
Flight endurance, h	3.70
Service ceiling, m	3110
Static ceiling, m	1585
Crew	2
Payload	13 passengers or 2296 kg of cargo

Image and diagram gallery of the Bell 412EP

Bell 412EP. Photograph: Westleigh Bushell	Bell 412EP. Photograph: Philip B Hosking
Bell 412EP. Photograph: T.S Spotter	Bell 412EP. Photograph: sae.org
Bell 412EP. Photograph: Bell Helicopter	Bell 412EP