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Designation: CM.170

Fouga Magister

Fouga CM.170 Magister

A picture of the Fouga CM.170 Magister

The Fouga Magister was designed in response to a French Air Force need for a jet trainer in the late 1940s.  An earlier trainer had proven to be underpowered and the new requirement called for more powerful engines to be fitted.  In 1950 Fouga enlarged the earlier design and added the Turbomeca Marbore engine.  The plane’s most distinctive feature its “V”-tail came from the glider that Fouga had fitted with a jet engine for testing.  The Magister first flew in 1952 and entered service with the French Air Force in 1956.  Its success resulted in large numbers of the aircraft being sold to other air forces around the world and eventually twenty-three nations would make use of the Magister.  In addition to being built in France Magisters were license built in West Germany, Finland, and Israel.  In all 929 were constructed.  After the Magister was retired several them found their way into civilian hands, particularly in the United States.

Wingspan 39 ft 10 in.

Wingspan

Length 33 ft

Length

Height 9 ft 2 in.

Height

Weight 6,280 lbs (loaded)

Weight

Max. Speed 444 MPH

Maximum Speed

Service Ceiling 36,080 ft

Service Ceiling

Range 575 miles

Range

Engines Two Turbomeca Marboré IIA turbojets with 880 pounds of thrust each

Engines

Crew 2

Crew


Manufacturer
Fouga

Markings
Michael W. Leverington, 2013

Designation
CM.170

Registration
N492FM

Serial Number
492

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