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337 Super Skymaster
|Name||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.
|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|
(to 5000 ft)
|MACH Climb||Cruise||Initial Descent
|V2 (IAS)||kts||IAS||kts||IAS||kts||IAS||kts||MACH||TAS||125 kts||MACH||IAS||kts||IAS||kts||Vapp (IAS)||kts|
|Distance||400 m||ROC||ft/min||ROC||ft/min||ROC||ft/min||ROC||ft/min||MACH||ROD||ft/min||ROD||ft/min||MCS||kts||Distance||450 m|
|MTOW|| 22002,200 kg
2.2 tonnes kg
|WTC||L||Range|| 13501,350 nm
8,202,755.912 ft NM
Accidents & Serious Incidents involving C337
None on SKYbrary