Bell 212

Data

ModelAB-212
IATABH2
ICAOB212
Manufacturer: Bell Helicopter
Introduced1968
StatusProduction completed
Wingspan14.64 m
Max Take-off Weight11,200 lb (5,080 kg)
Cruise speed100 knots (115 mph, 186 km/h)
Range237 nm (439 km)
Ceiling17,400 ft (5,305 m)
Engines2 x PT6T
Cockpit crew1
ICAO Mass Group2
Wake Turbulence GroupL
Type codeH2T

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Overview

The Bell 212 Twin Huey (also known as the Twin Two-Twelve) is a two-blade, twin-engine, medium helicopter that first flew in 1968. The 212 is marketed to civilian operators and has a fifteen-seat configuration, with one pilot and fourteen passengers.Based on the stretched fuselage Bell 205, the Bell 212 was originally developed for the Canadian Forces.

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Sources as credited. May also contain data from any of the following - Wikipedia