Bell 412 Civil Aircraft Model Details

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General Information of Bell 412

Developed From : Bell 212

Introduction : 1981

Manufacturer : Bell Helicopter

National Origin : United States / Canada

Number Built : over 869

Primary Users : Royal Air Force; See Operators for others

Produced : 1979–present

Role : Multipurpose Utility helicopter

Status : In service

Variants : Bell CH-146 Griffon

General characteristics of Bell 412

Capacity : up to 13 passengers, maximum external load of almost 6,614 lb (3,000 kg)[41]

Crew : 1-2 pilots

Disc Area : 1,662 ft² (154.4 m²)

Empty Weight : 6,789 lb (3,079 kg)

Height : 15 ft (4.6 m)

Length : 56 ft 1 in (17.1 m)

Max Takeoff Weight : 11,900 lb (5,397 kg)

Powerplant : 2 × Pratt & Whitney Canada PT6T-3BE Twin-Pac turboshafts, 900 shp (671 kW) each

Rotor Diameter : 46 ft (14.0 m)

Performance of Bell 412

Cruise Speed : 122 knots (140 mph, 226 km/h)

Maximum Speed : 140 knots (161 mph, 259 km/h)

Power/Mass : 0.2663 hp/lb (437 W/kg)

Range : 609 mi (up to 980km)

Rate Of Climb : 1,350 ft/min (6.86 m/s)

Service Ceiling : 20,000 ft (6,096 m)

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