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Basic Profile

Bell 214B

Overview

The Bell 214B is a helicopter aircraft manufactured by Bell, with the profile centered on its utility helicopter role. It first flew in 1970 and entered service in 1972. Production is recorded as ending in 1981. The listed crew requirement is 2. Power is provided by 1 Lycoming T5508D engine. Listed performance includes cruise speed 112 mph kt. Its ICAO type designator is B214. Figures shown here describe the listed type or configuration and may vary by sub-variant, certification basis, or operator fit.

Quick Facts

First Flight 1970
Crew 2
Range 220 nm
Cruise Speed 112 mph
Max Speed 140 kt

Specifications

ICAO Type CodeB214
First Flight1970
Introduction Date1972
Crew2
Length48 ft 8 in
Wingspan / Rotor Diameter48 ft rotor diameter
Height12 ft 11 in
Empty Weight7425 lb
Max Takeoff Weight15000 lb
Cruise Speed112 mph
Max Speed140 kt
Range220 nm
Service Ceiling15000 ft
Engine ManufacturerLycoming
Engine ModelT5508D
Engine Count1

Data verification status: Verified

Source: ICAO Aircraft Type Designators