C337
CESSNA 337 Super Skymaster
CESSNA 337 Super Skymaster
Aircraft
Name
337 Super Skymaster
Manufacturer
Body
Narrow
Wing
Fixed Wing
WTC
L
APC
A
Type Code
L2P
Engine
Piston
Engine Count
Multi
Manufactured as
SUMMIT O2-337 Sentry
SUMMIT Sentry
REIMS F337 Super Skymaster
REIMS FT337E Turbo Super Skymaster
REIMS FT337F Turbo Super Skymaster
REIMS FTB337 Milirole
REIMS Milirole
REIMS Super Skymaster
REIMS Turbo Super Skymaster
CESSNA 337 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 M337 Super Skymaster
CESSNA O-2 Super Skymaster
AVIONES COLOMBIA 337
C337
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 (metric)
11.60 m
Length (metric)
9.10 m
Height (metric)
2.80 m
Powerplant
337: 2 x 210 HP Continental IO-360-C piston engines with two blade propellers.
Engine Model(s)
Continental O-360
Indicative Performance Data
Take-Off
V2
n/a
Distance
400 m
MTOW
2200 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
n/a
Initial Climb (to FL150)
IAS
n/a
ROC
n/a
Initial Climb (to FL240)
IAS
n/a
ROC
n/a
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
125 kts
MACH
n/a
Ceiling
173
Range
1350 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
n/a
ROD
n/a
Descent (FL100 & below)
IAS
n/a
MCS
n/a
ROD
n/a
Approach
Vapp (IAS)
n/a
Distance
450 m
