The Cessna 414 Chancellor is the ideal private jet for short haul flights.
The pressurized 414 was developed to appeal to owners of un-pressurized twin-engined aircraft and was based on the fuselage of the Cessna 421 and used the wing design of the Cessna 401. The 414 is a low-wing cantilever monoplane with a conventional tail unit and a retractable tricycle landing gear. It is powered by two wing-mounted 310 hp (231 kW) Continental TSIO-520-J horizontally-opposed six cylinder engines. The name
was used for models marketed from 1976. An improved variant the
Cessna 414A Chancellor
was introduced in 1978 with the major change being a re-designed and increased-span wing with integral fuel tanks and an extended nose to give more baggage space.
The fuel system consists of two main tanks, two fuel selectors, emergency crossfeed shutoff valves and necessary components to complete the system. The main tanks are an integral portion of the sealed wet wing. Auxiliary fuel pumps are located outside of the tanks. A fuel flow gauge, fuel quantity gauge and a fuel low level warning light is located in the cockpit.
Powered by two six-cylinder engines, the Cessna 414 Chancellor (expanded to the Cessna 414A Chancellor) combines flexibility and economy. Six or even eight passenger seats are installed in the cabin, depending on the configuration. Production of the 414 Chancellor was discontinued in 1985. However, to this day, this aircraft is one of the most popular private jets for short-haul flights.
The airplane is powered by two horizontally opposed, six cylinder, direct drive, turbocharged, air cooled, fuel injected engines. The engines are Continental Model TSIO-520-NBs and are rated at 310 horsepower each.
Whether you are traveling alone or in a small group, the Cessna 414 Chancellor is the ideal private jet for short haul flights
Frequently Asked Questions about 414A
How long of a runway does a 414A need?
The aircraft 414A requires a takeoff distance of 0 m m and landing distance of 0 m m.
What category is a 414A ?
The 414A belongs to a Turbo prop category
what manufacture of engine model of the aircraft 414A ?
The 414A is powered by engines manufactured by TSIO-520-NB
What is maximum Baggage capacity in 414A ?
Baggage capacity in 414A is 0.87 m3
How many seats does a 414A have?
The 414A has typical seating for 8 pax passengers and 4 crew.
What is the aircraft cabin height on 414A ?
Cabin height on 414A is 1.3 m.
What is the length of the cabin in a 414A ?
The 414A cabin is 3.44 m. long from the cockpit bulkhead to the aft lavatory (excluding baggage).