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 |
 Cessna 650 Citation VI |
 Cessna 650 Citation VI |
 Cessna 650 Citation VI. Photography: Roberto Bianchi |
 Cessna 650 Citation VI |
 Cessna 650 Citation VI |
 Cessna 650 Citation VI |
 Cessna 650 Citation VI |
ArchivoAéreo Editorial Team
A group of aviation researchers and enthusiasts dedicated to documenting and preserving global aeronautical history. All articles are reviewed to ensure historical accuracy.
Sources & Accuracy
The information presented in this technical sheet has been compiled from declassified flight manuals, historical archives, and specialized literature. While we strive for maximum accuracy, some performance data may vary depending on the specific variant or operational conditions.