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Cessna Citation VI

1991 – 1995

Key Facts

  • The Cessna Citation VI is a Medium jet manufactured by Cessna between 1991 and 1995.
  • The Cessna Citation VI is powered by two Honeywell TFE731-3BR-100S engines, resulting in an hourly fuel burn of 251 Gallons per Hour.
  • Capable of cruising at up to 459 knots, the Cessna Citation VI can fly non-stop for up to 2000 nautical miles.
  • The aircraft can carry up to 9 passengers.
  • The Cessna Citation VI has an estimated hourly charter price of $3250, with a new list price of $8.1 million at the time of manufacture.

Overview and History – A Version of the Citation III

The first flight of the VI took place in 1991 and was the successor to the Citation V aircraft.

The first Citation VI was delivered in April 1991.

However, despite following on from the Citation V, the VI is actually based on the Citation III, with the purpose of being a more economical version of the Citation III. 

The Citation VI is physically the same aircraft as the Citation III model. Despite this Cessna offered the VI at a lower purchase price thanks to a standardized avionics package and a generic cabin interior.

After just 39 aircraft were built production was discontinued in May 1995, and replaced the VI with the Citation VII.

Its inception marked a significant advancement in the aviation industry, combining cutting-edge technology with an unerring attention to detail. 

Cessna Citation VI Performance

The Cessna Citation VI is powered by two Honeywell TFE731-3BR-100S engines, each delivering a robust thrust output of 7,300 lbs (3,311 kg).

These engines provide the thrust necessary to achieve a high-speed cruise of 459 knots (850 km/h).

In order to achieve the maximum range the aircraft has a cruise speed of 418 knots (774 km/h).

The Citation VI flexes its muscles with a maximum altitude of 51,000 feet (15,545 m) and boasts a remarkable range of 2,000 nautical miles (3,704 km), allowing for non-stop flights over considerable distances.

The aircraft excels in ground performance as well, requiring a take-off distance of 4,850 feet (1,478 m) and a landing distance of 2,520 feet (768 m).

It’s important to note that these figures represent best-case scenarios.

Actual range and ground performance may vary based on a multitude of factors including weather conditions, payload, and fuel load, among others.

As always, it is crucial for pilots to make careful considerations and calculations before each flight. 

Cabin and Interior Features of the Citation VI

The cabin of the Citation VI is spacious and well-designed. However, it is important to note that VI aircraft came without the option of custom interiors.

The cabin dimensions come in at an ample 18.7 feet (5.7 meters) in length, 5.7 feet (1.7 meters) in width, and reaches a height of 5.8 feet (1.8 meters), providing passengers with plenty of room to move around and relax. 

This, therefore, results in the VI having a total cabin volume of 438 cubic feet.

The Citation VI offers a highly flexible seating arrangement, with configurations that can accommodate between six and nine passengers, though the typical setup comfortably seats seven.

Each seat is adjustable, ensuring maximum comfort during the flight, and is positioned near sturdy, convenient tables that sit between the seats, ideal for work or dining. 

Additionally, there is ample baggage space with the baggage compartment measuring 61 cubic feet.

The cabin environment maintains a pleasant atmosphere throughout the flight.

Utilizing a maximum differential pressure of 9.3 psi, the Citation VI is capable of maintaining a sea-level cabin altitude of up to 25,230 feet (7,690 meters) and sustains an 8,000-foot (2,438-meter) cabin altitude even at its maximum certified ceiling of 51,000 feet (15,545 meters).

This feature contributes significantly to passenger comfort during long-duration flights.

The Citation VI is not only comfortable but practical as well.

The aircraft comes standard with a well-equipped refreshment center and more insulation for better heat distribution and noise cancellation.

Safety is also a priority, with engine bleed air utilized for the anti-ice system of the engine inlets, wing leading edges, and the windshield.

Cockpit and Avionics Package

All Cessna Citation VI aircraft came as standard with the Honeywell digital SPZ-8000 flight control system.

Furthermore, it came equipped with a Honeywell PZ-650 A/P, a King KMD-850 multi-function display (MFD), Honeywell EDZ-600 EFIS, a Honeywell 8000 EGPWS, and a Sperry Primus 300SL color radar.

For communication and navigation, it uses dual Collins VHF-22C communication systems, dual Collins VIR-32 navigation systems, and dual Collins DME-42.

Additional features include a Collins ADF-60, dual Collins TDR-90, and dual King KHF-950.

To further complement its navigation capabilities, the suite incorporates dual Honeywell GNS-XLS and a Sperry SPZ-650 FDS. 

To ensure an enhanced level of safety and communication, the cockpit includes a King KMH-820 TCAS I and Mode S transponders as standard features with this Collins package. 

Charter Cost

Chartering a Cessna Citation VI in North America is estimated to cost around $3,250 per hour.

However, it’s important to know that this figure is not set in stone.

There are numerous factors that can influence this cost.

For instance, the final charter cost may vary depending on the distance and duration of the flight, the time of booking, and the current demand for charter flights.

Furthermore, additional services such as on-board catering or ground transportation can also play a role in the final price. 

Purchase and Operating Costs

The Cessna Citation VI, once valued at $8.1 million when new, can now be acquired on the pre-owned market at an average cost of $1.18 million.

However, it is always important to consider the annual operating costs and not just the acquisition cost.

For an owner flying approximately 200 hours per year, the estimated annual ownership cost would total around $840,000.

This estimated cost encompasses key factors such as maintenance, fuel, insurance, and other related expenses. 

 

 

Performance

Comfort

Weights

Range: 2,000 nm Number of Passengers: 9 Baggage Capacity: 61 Cubic Feet
Cruise Speed: 459 knots Cabin Pressure: 9.3 PSI Max Take-Off Weight: 22,000 lbs
Ceiling: 51,000 feet Cabin Altitude: 8,000 feet Max Landing Weight: 20,000 lbs
Take-Off Distance: 4,850 feet Production Start: 1991
Landing Distance: 2,520 feet Production End: 1995

 

Dimensions

Power

Exterior Length: 55.5 feet Engine Manufacturer: Honeywell
Exterior Height: 16.9 feet Engine Model: TFE731-3BR-100S
Wingspan: 53.5 feet Fuel Burn: 251 Gallons per Hour
Interior Length: 18.7 feet
Interior Width: 5.7 feet
Interior Height: 5.8 feet
Interior/Exterior Ratio: 34%