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Cessna 650 Citation VI

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Cessna 650 Citation VI

In 1990, Cessna announced the Citation VI aircraft, a simplified and more affordable version of the Citation III. The first aircraft rolled out of the assembly plant on January 2, 1991, with customer deliveries commencing in 1992.

Development and Design

The aircraft largely retained the Citation III’s airframe, featuring modified flaps and spoilers. The passenger cabin length was increased, though its height was simultaneously reduced, allowing it to accommodate up to ten passengers.

Several cabin layout options were available for customer selection. The Cessna Citation VI was also equipped with a high-lift wing and modified landing gear, enabling it to operate from unpaved airstrips.

Performance and Features

Powered by two Garrett TFE 731-3B-100 turbofan engines, the aircraft could achieve a cruising speed of 874 km/h (543 mph) at an altitude of 15545 m (51000 feet).

Production and Legacy

Despite its features, only 39 units of this model were produced. Manufacturing of the Cessna Citation VI ceased in May 1995.

Technical Specifications

Modification Citation VI
Wingspan, m 16.31
Aircraft length, m 16.92
Aircraft height, m 5.13
Wing area, m2 29.00
Empty weight 5851
Maximum takeoff weight 9979
Engine type 2 Turbofan Garrett TFE731-3B-100S
Thrust, kN 2 x 16.24
Maximum speed, km/h 905
Cruising speed, km/h 874
Practical range, km 4345
Service ceiling, m 15545
Crew 2
Payload 8-10 passengers

Image and diagram gallery of the Cessna 650 Citation VI

Cessna 650 Citation VI business jet
Cessna 650 Citation VI
Cessna 650 Citation VI business jet
Cessna 650 Citation VI
Cessna 650 Citation VI business jet
Cessna 650 Citation VI
Cessna 650 Citation VI business jet
Cessna 650 Citation VI. Photography: Roberto Bianchi
Cessna 650 Citation VI business jet
Cessna 650 Citation VI
Cessna 650 Citation VI business jet
Cessna 650 Citation VI
Cessna 650 Citation VI business jet
Cessna 650 Citation VI
Cessna 650 Citation VI business jet
Cessna 650 Citation VI

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Fuentes y Rigurosidad

La información presentada en esta ficha técnica ha sido compilada a partir de manuales de vuelo desclasificados, archivos históricos y bibliografía especializada. Aunque nos esforzamos por mantener la máxima precisión, algunos datos de rendimiento pueden variar según la variante específica o las condiciones operativas.

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