Cessna 414 Chancellor

Twin Turboprops

ICAO aircraft code C414

Manufacturer Cessna

Country United States

New price USD .5 million (1981)

The Cessna 414 Chancellor is a light, pressurized, twin-engine transport aircraft with a pressurized cabin in service since 1969.

Specifications

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Cessna 414 Chancellor specifications

General

ICAO aircraft code

C414

Manufacturer

Cessna

Manufactured

1968 - 1985

Country

United States

New purchase price

USD .5 million (1981)

Aircraft performance

Engine:

2x Continental TSIO-520-NB
Piston

Power:

310 HP

Max Cruise Speed:

235 Kts
435 Km/h

Approach Speed (Vref):

68 Kts

Travel range:

1,328 Nm
2,459 Kilometers

Service Ceiling:

30,800 feet

Rate of Climb:

1520 feet / minute
7.72meter / second

Take Off Distance:

665 meter - 2,181.73 feet

Landing Distance:

718 meter - 2,355.61 feet

Weight & dimensions

Max Take Off Weight:

3,061 Kg
6,748 lbs

Max Landing Weight:

2,697 Kg
5,946 lbs

Max Payload:

802 Kg
1,768 lbs

Fuel Tank Capacity:

213 gallon
806 liter

Baggage Volume:

2.4 m3 / 85 ft3

Disclaimer: The information on this page may not be accurate or current. Never use it for flight planning or any other aircraft operation purposes. No warranty of fitness for any purpose is made or implied. Flight planning or any other aircraft operations should only be done using official technical information provided by the manufacture or official aviation authorities.

About the Cessna 414 Chancellor

The Cessna 414 Chancellor is a light, pressurized, twin-engine transport aircraft with a pressurized cabin in service since 1969. It is a less powerful and lighter evolution of the Cessna 421.