Cessna 650 Citation VII

Advanced Development and Avionics

Announced in 1990, the Cessna 650 Citation VII was a development of the Citation VI, featuring SPZ-8000 based avionics. This evolution aimed to offer superior performance and technology within the executive jet segment.

Enhanced Power and Performance

It was equipped with AlliedSignal TFE731-4R-2S turbofan engines, each providing 18.41 kN of thrust. These engines significantly increased the aircraft’s cruising speed, rate of climb, and service ceiling.

With this improvement, the flight range with six passengers also saw an enhancement, extending to 4111 km, substantially boosting its operational capabilities for longer flights.

Production and Certification Milestones

The prototype conducted its first flight in February 1991. Official certification for the model was completed in January 1992, and just three months later, deliveries of the production aircraft began to customers, marking its entry into service.

Technical Specifications

Modification	Citation VII
Wingspan, m	16.31
Aircraft length, m	16.92
Aircraft height, m	5.13
Wing area, m2	29.00
Empty weight	5316
Maximum takeoff weight	10183
Engine type	2 AlliedSignal TFE731-4R-2S Turbofan engines
Thrust, kN	2 x 18.41
Maximum speed, km/h	910
Cruising speed, km/h	881
Practical range, km	4110
Service ceiling, m	15545
Crew, crew members	2
Payload	6-9 passengers

Image and diagram gallery of the Cessna 650 Citation VII

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Cessna 650 Citation VII