Bell 212 Twin Huey

Explore the Bell 212 Twin Huey in side view and top view to compare its silhouette and proportions.

Bell 212 Twin Huey, side profile
Bell 212 Twin Huey, side profile
17.46 m
Bell 212 Twin Huey, top view
Bell 212 Twin Huey, top view

From Wikipedia

The Bell 212 is a two-blade, twin-engine, medium helicopter that first flew in 1968. Originally manufactured by Bell Helicopter in Fort Worth, Texas, United States, production was moved to Mirabel, Quebec, Canada in 1988, along with all Bell commercial helicopter production after that plant opened in 1986.

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Summary of “Bell 212” from Wikipedia, the free encyclopedia, used under CC BY-SA 4.0. Retrieved 2026-10-11.

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Use these drawings for anything, commercial too, under Creative Commons Attribution 4.0 International. Credit us like this:

Drawing of the Bell 212 Twin Huey by AirwayControl Aircraft Library (https://aircraft.intelsystems.ai/aircraft/B212/), CC BY 4.0

Specifications

Length
17.46 m
Rotor diameter
14.63 m
Max take-off weight
5.08 t
Cruise speed
190 km/h
Max speed
259 km/h
Range
439 km
Ceiling
5,304 m
Engines
2× P&WC PT6T Twin-Pac (turboshaft)
Power
2× 900 hp
First flight
1968
In service
1968

From the AirwayControl spec register, curated from Wikipedia and manufacturer pages. Figures vary by variant.