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BELL 212 Twin Huey

From SKYbrary Wiki

Name 212 Twin Huey
Manufacturer BELL
Wing Rotary
WTC Light
Type code H1T
Engine Turboshaft
Engine count Single
Mass group 2

Manufacturered as:

BELL Twin Two-Twelve
BELL 212
BELL 212 Twin Two-Twelve

BELL 212 Twin Huey

BELL 212 Twin Huey BELL 212 Twin Huey 3D


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.

Technical Data

Wing span 14.64 m48.031 ft <br />
Length 17.43 m57.185 ft <br />
Height 3.83 m12.566 ft <br />
Powerplant 1 x Pratt & Whitney Canada PT6T-3 or -3B turboshaft, 1,800 shp (1,342 kW).
Engine model Pratt & Whitney Canada PT6T

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
(to FL100)
Descent (FL100
& below)
V2 (IAS) kts IAS kts IAS kts IAS kts MACH TAS 100 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance m ROC ft/min ROC ft/min ROC ft/min ROC ft/min MACH ROD ft/min ROD ft/min MCS kts Distance m
MTOW 50805,080 kg <br />5.08 tonnes <br /> kg Ceiling FL174 ROD ft/min APC
WTC L Range 237237 nm <br />438,924 m <br />438.924 km <br />1,440,039.371 ft <br /> NM

Accidents & Serious Incidents involving B212

None on SKYbrary