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From SKYbrary Wiki
Name 337 Super Skymaster
Manufacturer CESSNA
Body Narrow
Wing Fixed Wing
WTC Light
Type code L2P
Engine Piston
Engine count Multi
Mass group UNK

Manufacturered as:

CESSNA O-2 Super Skymaster
CESSNA M337 Super Skymaster
CESSNA MC337 Super Skymaster
CESSNA Turbo Super Skymaster
CESSNA Super Skymaster
CESSNA T337D Turbo Super Skymaster
CESSNA T337H Turbo Super Skymaster
CESSNA T337E Turbo Super Skymaster
CESSNA T337C Turbo Super Skymaster
CESSNA T337B Turbo Super Skymaster
CESSNA T337F Turbo Super Skymaster
CESSNA 337 Super Skymaster
REIMS FT337E Turbo Super Skymaster
REIMS FT337F Turbo Super Skymaster
REIMS FTB337 Milirole
REIMS Milirole
REIMS Super Skymaster
REIMS Turbo Super Skymaster
REIMS F337 Super Skymaster
SUMMIT O2-337 Sentry

CESSNA 337 Super Skymaster

CESSNA 337 Super Skymaster


Light piston aircraft. In service since 1965 Member of Cessna's Centre line thrust. Layout with nose mounted tractor, rear fuselage mounted pusher engine and twin boom tail unit. Improved version of 336 Skymaster with retractable gear and more powerful engines. Pressurized version T337G. Cessna's production ended in 1980, continued by REIMS, France. US Air Force type: O-2.

Technical Data

Wing span 11.6 m38.058 ft
Length 9.1 m29.856 ft
Height 2.8 m9.186 ft
Powerplant 337: 2 x 210 HP Continental IO-360-C piston engines with two blade propellers.

T337: 2 x 225 HP Continental TSIO-360-C turbocharged piston engine with two blade propellers.

Engine model Continental O-360

Accidents & Serious Incidents involving C337

None on SKYbrary