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CESSNA 414 Chancellor

From SKYbrary Wiki
Name 414 Chancellor
Manufacturer CESSNA
Body Narrow
Wing Fixed Wing
WTC Light
Type code L2P
Engine Piston
Engine count Multi
Mass group 2

Manufacturered as:

CESSNA Chancellor
CESSNA 414 Chancellor
RILEY Rocket Power 414

CESSNA 414 Chancellor

CESSNA 414 Chancellor


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 12.5 m41.01 ft
Length 10.3 m33.793 ft
Height 3.6 m11.811 ft
Powerplant 2 x 310 HP Continental TSIO-520-NB turbocharged piston engines with 3 blade propellers.
Engine model Continental O-520

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
(to FL100)
Descent (FL100
& below)
V2 (IAS) kts IAS kts IAS kts IAS kts MACH TAS 225 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance 790 m ROC ft/min ROC ft/min ROC ft/min ROC ft/min MACH ROD ft/min ROD ft/min MCS kts Distance 718 m
MTOW 30003,000 kg
3 tonnes
Ceiling FL300 ROD ft/min APC B
WTC L Range 13101,310 nm
2,426,120 m
2,426.12 km
7,959,711.292 ft

Accidents & Serious Incidents involving C414

None on SKYbrary