Bell Model 212
United States (1968)
Where applicable, the appearance of U.S. Department of Defense (DoD), Russian Ministry of Defense, Chinese Ministry of Defense or British Ministry of Defence visual information does not imply or constitute endorsement of this website (www.MilitaryFactory.com). Images marked with "www.MilitaryFactory.com" or featuring the Military Factory logo are copyrighted works exclusive to this site and not for reuse in any form.
Produced from 1968 until 1998, the Bell Model 212 helicopter found homes in many inventories spanning several global operators.
Detailing the development and operational history of the Bell Model 212 Medium-Lift Utility / Transport Helicopter. Entry last updated on 6/22/2018. Authored by Staff Writer. Content ©www.MilitaryFactory.com
The Model 212 achieved first-flight in 1968 and was introduced that same year. Production then spanned from 1968 until 1998. Back in 1988, manufacture of the series moved from the United States to Canada (though still produced under the Bell Helicopter brand label).
In both form and function, the Model 212 was indicative of the whole Huey line. It featured its crew of one or two seated at front in a side-by-side arrangement. Automobile-style doors were granted to each crewman for easy entry-exit. The passenger cabin was designed to seat up to fourteen. Overall length of the aircraft was 57 feet with a rotor diameter of 48 feet and a height of 12.6 feet. Empty weight was 6,530lb against an MTOW of 11,200lb. Power was provided by a Pratt & Whitney Canada PT6T-3 (or PT6T-3B) turboshaft engine. This drove both the main rotor atop the cabin as well as the tail rotor (offset to portside) atop the vehicle tail fin. Output of this engine fit was 1,800 horsepower. Performance specifications included a maximum speed of 140 miles per hour and range was out to 240 nautical miles. Its service ceiling reached 17,400 feet with a rate-of-climb reaching 1,745 feet-per-minute.
The Model 412 was an offshoot of the Bell 212 line and incorporated a four-bladed main rotor as well as two engines in its make-up. Foreign (licensed) production of the Model 212 was taken up by Agusta-Bell of Italy (as the "AB212") and its Anti-Submarine Warfare (ASW) derivative became the "AB212 ASW". The Eagle 212 "Single" was a local Canadian development that substituted the PWC engine with the Lycoming T53-17 (or T53-BCV) turboshaft.
Model 212 helicopters continue to serve in several roles today despite their 1960s heritage - some with navy and coast guard services and others with police forces.
Any available statistics for the Bell Model 212 Medium-Lift Utility / Transport Helicopter are showcased in the areas immediately below. Categories include basic specifications covering country-of-origin, operational status, manufacture(s) and total quantitative production. Other qualities showcased are related to structural values (namely dimensions), installed power and standard day performance figures, installed or proposed armament and mission equipment (if any), global users (from A-to-Z) and series model variants (if any).
Our Data Modules allow for quick visual reference when comparing a single entry against contemporary designs. Areas covered include general ratings, speed assessments, and relative ranges based on distances between major cities.
Relative Maximum Speed Rating
This entry's maximum listed speed (140mph).
Graph average of 112.5 miles-per-hour.
Graph showcases the Bell Model 212's operational range (on internal fuel) when compared to distances between major cities.