C340
CESSNA 340
CESSNA 340
Aircraft
Name
340
Manufacturer
Body
Narrow
Wing
Fixed Wing
WTC
L
APC
A
Type Code
L2P
Engine
Piston
Engine Count
Multi
Manufactured as
RILEY Super 340
RILEY Rocket 340
CESSNA 340
AVIONES COLOMBIA 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 (metric)
11.60 m
Length (metric)
10.50 m
Height (metric)
3.80 m
Powerplant
2 x 285 HP Continental TSIO-520-K or
Engine Model(s)
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
