BELL 214 Civil Aircraft Model Details

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General Information of BELL 214

Developed From : Bell 204/205

Developed Into : Bell 214ST

First Flight : 1970

Introduction : 1972

Manufacturer : Bell Helicopter

Primary Users : Islamic Republic of Iran Army

Produced : 1970-1981

Role : Medium-lift helicopter

Status : In service

General characteristics of BELL 214

Capacity : 3,880 lb including 14 troops, or 6 stretchers, or equivalent cargo

Crew : 2

Empty Weight : 7,588 lb (3,442 kg)

Height : 12 ft 10 in (3.90 m)

Length : 48 ft 0 in (14.63 m))

Loaded_Weight : 13,800 lb (6,260 kg)

Max Takeoff Weight : 15,000 lb with slung load (6,805 kg)

Powerplant : 1 × Lycoming LTC4B-8D turboshaft, 2,930 shp (2,185 kW)

Rotor Diameter : 50 ft 0 in (15.24 m)

Performance of BELL 214

Cruise Speed : 140 knots (260 km/h, 161.5 mph)

Range : 255 mi (475 km)

Service Ceiling : 16,400 ft density altitude (5,000 m)

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