WEG MediaWiki

Bell 412EP American Utility Helicopter

tiers
false
false
true
false
categories
"WEG"
"Aircraft"
"Rotary Wing Aircraft"
"Utility Helicopter"
"United States"
"PRO_Algeria"
"PRO_Argentina"
"PRO_Australia"
"PRO_Azerbaijan"
"PRO_Bosnia and Herzegovina"
"PRO_Brazil"
"PRO_Cameroon"
"PRO_Canada"
"PRO_Chile"
"PRO_Colombia"
"PRO_Dominican Republic"
"PRO_El Salvador"
"PRO_Eritrea"
"PRO_Finland"
"PRO_Ghana"
"PRO_Guatemala"
"PRO_Guinea"
"PRO_Honduras"
"PRO_Indonesia"
"PRO_Iran (Islamic Republic of)"
"PRO_Italy"
"PRO_Jamaica"
"PRO_Lesotho"
"PRO_Mexico"
"PRO_Montenegro"
"PRO_Morocco"
"PRO_Nigeria"
"PRO_Norway"
"PRO_Pakistan"
"PRO_Panama"
"PRO_Peru"
"PRO_Philippines"
"PRO_Saudi Arabia"
"PRO_Slovenia"
"PRO_South Korea (Republic of Korea)"
"PRO_Sri Lanka"
"PRO_Thailand"
"PRO_Turkey"
"PRO_United Arab Emirates"
"PRO_United Kingdom of Great Britain and Northern Ireland"
"PRO_Uruguay"
"PRO_Venezuela (Bolivarian Republic of)"
"PRO_Yemen"
"PRO_Zimbabwe"
"Air"
"Tier3"
notes"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."
dateOfIntroduction1981
countryOfOrigin"United States"
proliferation"Algeria, Argentina, Australia, Azerbaijan, Bosnia and Herzegovina, Brazil, Cameroon, Canada, Chile, Colombia, Dominican Republic, El Salvador, Eritrea, Finland, Ghana, Guatemala, Guinea, Honduras, Indonesia, Iran (Islamic Republic of), Italy, Jamaica, Lesotho, Mexico, Montenegro, Morocco, Nigeria, Norway, Pakistan, Panama, Peru, Philippines, Saudi Arabia, Slovenia, South Korea (Republic of Korea), Sri Lanka, Thailand, Turkey, United Arab Emirates, United Kingdom of Great Britain and Northern Ireland, Uruguay, Venezuela (Bolivarian Republic of), Yemen, Zimbabwe"
selectedregions
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checkedregions
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checkedcountries
"Algeria"
"Argentina"
"Australia"
"Azerbaijan"
"Bosnia and Herzegovina"
"Brazil"
"Cameroon"
"Canada"
"Chile"
"Colombia"
"Dominican Republic"
"El Salvador"
"Eritrea"
"Finland"
"Ghana"
"Guatemala"
"Guinea"
"Honduras"
"Indonesia"
"Iran (Islamic Republic of)"
"Italy"
"Jamaica"
"Lesotho"
"Mexico"
"Montenegro"
"Morocco"
"Nigeria"
"Norway"
"Pakistan"
"Panama"
"Peru"
"Philippines"
"Saudi Arabia"
"Slovenia"
"South Korea (Republic of Korea)"
"Sri Lanka"
"Thailand"
"Turkey"
"United Arab Emirates"
"United Kingdom of Great Britain and Northern Ireland"
"Uruguay"
"Venezuela (Bolivarian Republic of)"
"Yemen"
"Zimbabwe"
dis
name"AGUSTA BELL 412"
string"01.02.225.091.012.001.000"
images
"Bell_412(A).jpg"
"Bell_412(BB).jpg"
"Bell_412(C).jpg"
sections
name"System"
properties
name"Alternative Designation"
value"Bell 412"
name"Type"
value"Utility Helicopter"
name"Crew"
value"1"
units"ea"
name"Blades, Main Rotor"
value"4"
units"ea"
name"Blades, Tail Rotor"
value"2"
units"ea"
name"Number of Engines"
value"1"
units"ea"
name"Number of Hard Points"
value"INA"
name"Dimensions"
properties
name"Length"
value"17.09 m"
name"Main Rotor Diameter"
value"14.02 m"
name"Main Rotor Area"
value"154.4 m2"
name"Height"
value"4.57 m"
name"Empty Weight"
value"3,079 kg"
name"Maximum Takeoff Weight"
value"5,398 kg"
name"Automotive"
properties
name"Engine Name"
value"1 × Pratt & Whitney Canada PT6T-3D Twin-Pac or PT6T-3DF Twin-Pac"
name"Engine Type"
value"Turboshaft"
name"Engine Power"
value"1,250 shp (930 kW)"
name"Maximum Speed"
value"260 km/h"
name"Cruise Speed"
value"226 km/h"
name"Range"
value"980 km"
name"Service Ceiling"
value"6,100 m"
name"Rate of Climb"
value"6.9 m/s"
name"Protection"
properties
name"Stealth Properties"
value"None"
name"Heat Signature Reduction"
value"No"
name"Add on Armor"
value"INA"
name"NBC Protection"
value"INA"
name"Counter Measures (Chaff/Flares)"
value"No"
type"WEG"
version1
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