Cessna 414

Cessna 414
A Cessna 414 Chancellor at Amsterdam-Schiphol Airport, 1990
Role Six/eight-seat light transport
National origin United States
Manufacturer Cessna
First flight November 1, 1968
Produced 1968-1985
Number built 1070


The Cessna 414 is an American light, pressurized, twin-engine transport aircraft built by Cessna. It first flew in 1968 and an improved variant was introduced from 1978 as the 414A Chancellor.

Design and development

The pressurized 414 was developed to appeal to owners of un-pressurised 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 piston engines. The prototype, registered N7170C, first flew on 1 November 1968 and production aircraft were available in a number of optional seating arrangements and avionic packages. The name Chancellor 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.

Modifications

Many supplemental type certificates exist for the aircraft that allow upgrades to improve performance. Common are engine and aerodynamic modifications, including winglets.[1]

In 1974, American Jet Industries built a turboprop-powered conversion of the Cessna 414, named the Turbo Star Pressurized 414, using Allison 250-B17B engines.[2] Scenic Airlines of Las Vegas purchased the rights to the design in 1977.[3]

Thielert has offered engine conversions using their Centurion Engine.[4] This involves the installation of FADEC-controlled aviation diesel piston engines that run on commonly available jet fuel. Thielert claims increased power and improved fuel economy over other available conventional piston engines.

Variants

414
Initial production variant, 516 built
414A Chancellor
Improved 414 with narrower vertical tail, longer span bonded wet wing without tip tanks, a lengthened nose, re-designed landing gear and powered by two 310hp (231kW) TSIO-520-N engines, 554 built.
Riley Rocket 414
Conversion of Cessna 414 aircraft by fitting two 400hp Lycoming IO-720 engines.[5]

Operators

Military operators

 Bahamas
 Lebanon

Accidents and incidents

Specifications (414A Chancellor)

Data from Orbis[7]

General characteristics

Performance

See also


References

Notes
  1. "RAM Altitude Performance Enhancing Winglets". Ramaircraft.com. Retrieved 2012-08-30.
  2. Jane's All the World's Aircraft 1977–78, p.398
  3. Taylor 1989, 793
  4. Thielert AG (2007-09-28). "CENTURION ENGINES - Cessna 340, 414 & 421". Web.archive.org. Archived from the original on September 28, 2007. Retrieved 2012-08-30.
  5. Taylor 1982, pp. 454–455.
  6. "FTW82AA299". Web.archive.org. Archived from the original on September 29, 2007. Retrieved 2012-08-30.
  7. Orbis 1985, page 1119
Bibliography
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