ARMSNET
Military Equipment Database
Initializing 0%

Bell 412EP American Utility Helicopter

Bell 412

Utility Helicopter
Spotted an error? Sign in to suggest an edit.
Basic Information
Name
Bell 412EP American Utility Helicopter
Designation
Bell 412
Alternate Designation
Bell 412
Equipment Type
Utility Helicopter
Manufacturer
Date of Introduction
1981
Description

The Bell 412 is a utility helicopter of the Huey family manufactured by Bell Helicopter. It is a development of the Bell 212, with the major difference being the composite four-blade main rotor. Development began in the late 1970s with two Bell 212s being converted into 412 prototypes. An advanced four-blade main rotor with a smaller diameter replaced the 212's two-blade rotor. A Bell 412 prototype first flew in August 1979. The initial model was certified in January 1981 with deliveries commencing in the same month. 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. The current production version, 412EP (Enhanced Performance), is equipped with a dual digital automatic flight control system. In 2013 Bell introduced the 412EPI which includes an electronic (Digital) engine control for a PT6T-9 engine upgrade, and a glass cockpit display system similar to the Bell model 429. Also featured is a Garmin touchscreen navigation system, and the BLR Strake and Fast Fin upgrades for improved hover performance. Over 700 Model 412s (including 260 by AgustaWestland) have been built.

Air & Air Defense Specifications
Crew 1
Engine Turboshaft (1250 hp)
Max Speed 260.0 km/h
Cruise Speed 226.0 km/h
Service Ceiling 6100 m
System
Alternative Designation Bell 412
Type Utility Helicopter
Crew 1 ea
Blades, Main Rotor 4 ea
Blades, Tail Rotor 2 ea
Number of Engines 1 ea
Number of Hard Points INA
Dimensions
Length 17.09 m
Main Rotor Diameter 14.02 m
Main Rotor Area 154.4 m2
Height 4.57 m
Empty Weight 3,079 kg
Maximum Takeoff Weight 5,398 kg
Automotive
Engine Name 1 × Pratt & Whitney Canada PT6T-3D Twin-Pac or PT6T-3DF Twin-Pac
Engine Type Turboshaft
Engine Power 1,250 shp (930 kW)
Maximum Speed 260 km/h
Cruise Speed 226 km/h
Range 980 km
Service Ceiling 6,100 m
Rate of Climb 6.9 m/s
Protection
Stealth Properties None
Heat Signature Reduction No
Add on Armor INA
NBC Protection INA
Counter Measures (Chaff/Flares) No
Details
Country of Origin United States
Category Utility Helicopter
Air > Utility Helicopter
Filter Label
B
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
17.09 m
Width
Height
4.57 m
Weight
5398 kg
Operators (44)
United Kingdom
Italy
South Korea
Turkey
Iran
Pakistan
Brazil
Algeria
Argentina
Australia
Azerbaijan
Bosnia and Herzegovina
Cameroon
Canada
Chile
Colombia
Dominican Republic
El Salvador
Eritrea
Finland
Ghana
Guatemala
Guinea
Honduras
Indonesia
Jamaica
Lesotho
Mexico
Montenegro
Morocco
Nigeria
Norway
Panama
Peru
Philippines
Saudi Arabia
Slovenia
Sri Lanka
Thailand
United Arab Emirates
Uruguay
Venezuela
Yemen
Zimbabwe
Something went wrong. Please reload the page. Reload