The BELL 412EP is a medium size turbine powered helicopter using a 4-blade rotor system. The advanced rotor system design permits smooth and quiet operations with being able to fly at high speed.
The standard 412 is certified in accordance to FAA-FAR Part-29 Transport Category Rotorcraft, and it is qualified for day and night operation under visual flight conditions.
With cruising speed of 130 Knots and range of up to 402 NM, the BELL 412EP will be a desirable aircraft for transport mission providing a fast, reliable, efficient fuel consumption, and low direct operation cost. Thus, its purposes serve the design targets: High safety, Low Maintenance, High availability and Low Cost of Operation.
With more than 5,405 Pounds (2,452 Kilograms) internal use load capacity, a cabin with wide doors for easy loading, exceptional hot and high altitude operating characteristic, BELL 412EP is absolutely ideal for rough terrain operations and accessing remote areas.
|Take-off Gross Weight||:||11,900 Lbs|
|IGE Standard day||:||10,200 ft|
|Standard Day + 20oC||:||6,200 ft|
|Service Ceiling (OEI, 30 mnt power)||:||7,600 ft|
|Max. Continous Cruise TAS (SL)||:||122 Kts|
|Max. Continous Cruise TAS (5000 ft)||:||124 Kts|
|Long Range Cruise Speed||:||130 Kts|
|Range at LRC Speed, No Reserve (5000 ft)||:||402 NM|
|Fuel Capacity (usable)||:||330.5 Gal|
|Max. Endurance||:||3.7 Hrs|
Powered by PT6T-3D Twin Pac with 1,600 SHP each
The BELL 412EP helicopter has been designed for a wide range of applications as:
Since 2014, PTDI has an Industrial and Commercial Agreement (ICA) with Bell Helicopter Textron Incorporated (BHTI) for Production, Sales and Certified Maintenance Center (CMC) for Bell 412 Series and Bell Huey II components.