C414
CESSNA 414 Chancellor
CESSNA 414 Chancellor
Aircraft
Name
414 Chancellor
Manufacturer
Body
Narrow
Wing
Fixed Wing
WTC
L
APC
B
Type Code
L2P
Engine
Piston
Engine Count
Multi
Manufactured as
RILEY Rocket Power 414
CESSNA 414
CESSNA Chancellor
CESSNA 414 Chancellor
AVIONES COLOMBIA 414
C414
Utility twin aircraft. In service since 1969. Less powerful, light and low cost model of CESSNA 421 Golden Eagle. Features wing of CESSNA 402 and fuselage of CESSNA 421. Improved version CESSNA 414A Chancellor (appeared in 1978) with bonded wet wing, without tip tanks. Remained in production until 1985.
Technical Data
Wing span (metric)
12.50 m
Length (metric)
10.30 m
Height (metric)
3.60 m
Powerplant
2 x 310 HP Continental TSIO-520-NB turbocharged piston engines with 3 blade propellers.
Engine Model(s)
Continental O-520
Indicative Performance Data
Take-Off
V2
n/a
Distance
790 m
MTOW
3000 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
225 kts
MACH
n/a
Ceiling
300
Range
1310 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
718 m
