CESSNA 340
CESSNA 340
C340
Business aircraft. In service since 1971. Similar production to BEECHs Duke, slotting in between CESSNA 310 and CESSNA 414/421 with 414s wings and 310s undercarriage and tail unit. Introduction of a pressuration system. Production ended in 1984. CESSNA 335 unpressurized, light weight and lower cost development. Built from 1979 to 1980.
Technical Data
Wing span:
11.60 m
Length:
10.50 m
Height:
3.80 m
Powerplant:
2 x 285 HP Continental TSIO-520-K or
Engine Model:
Continental O-520
Indicative Performance Data
Take-Off
V2:
n/a
Distance:
535 m
MTOW:
2700 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:
170 kts
MACH:
n/a
Ceiling:
300
Range:
1170 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:
688 m
