Cessna 414
WIkipedia
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 Developments
The pressurized 414 was developed to appeal to owners of unpressurized, 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 prototype, registered N7170C, first flew on 1 November 1968, and production aircraft were available in a number of optional seating arrangements and avionics 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 redesigned and increased-span wing with integral fuel tanks and an extended nose to give more baggage space.
Controls
Just A normal Controls Nothing special on this
Some Pict's
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Specifications
General Characteristics
- Predecessor Cessna 414
- Created On Android
- Wingspan 64.2ft (19.6m)
- Length 50.2ft (15.3m)
- Height 17.3ft (5.3m)
- Empty Weight 18,692lbs (8,478kg)
- Loaded Weight 18,692lbs (8,478kg)
Performance
- Horse Power/Weight Ratio 0.213
- Wing Loading 89.1lbs/ft2 (434.8kg/m2)
- Wing Area 209.9ft2 (19.5m2)
- Drag Points 10200
Parts
- Number of Parts 285
- Control Surfaces 3
- Performance Cost 1,014
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