Cessna Citation VI

Turbofan twin engine • Low Wing • Retractable gear

Range Visualization

Origin:

nm at current load

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Payload vs. Range

Configure weights

Default: 190 lbs

Default: 30 lbs

Occupants
lbs lbs / pax

Fuel on board

Extra weight

Range

Available Range / nm
Mission capable. Aircraft can handle the current load with full fuel tanks.
Fuel tradeoff required. You'll need to leave gallons of fuel behind ( gal usable for nm range).
Over max gross weight. Reduce payload by lbs to safely operate this aircraft.
Extra weight is the additional payload available with your selected passengers.

Mission Profile

Endorsements & ratings:
  • • High-Altitude
  • • Pressurization
  • • Multi-Engine
  • • Instrument
468
KTAS
Cruise Speed
15
Occupants
2054
nm
Max Range
730
lbs
Wet Payload
• Used market

Estimated Ownership Costs

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About the Cessna Citation VI

Overview

The Cessna Citation VI (Model 650) is the economy-interior version of the Citation III, built on the same swept-wing airframe, T-tail, and Honeywell TFE731-3B-100S turbofans under the same FAA type certificate (A9NM, Section I). Cessna offered it in the early 1990s with a standardized interior and a simplified avionics package to lower acquisition cost while keeping the III’s 51,000 ft ceiling and high-altitude cruise. Only 39 were built before the line advanced to the more powerful Citation VII.

Key Features for GA Buyers

  • Citation III performance at a lower entry price. The VI matches the III’s airframe, engines, and 51,000 ft ceiling, so it cruises in the same high-altitude band at a lower acquisition cost.
  • Standardized cabin and systems. A single non-custom interior and avionics fit simplifies pre-buy evaluation and keeps parts commonality high across the small fleet.
  • Stand-up cabin. The Model 650 cabin carries the same dropped-aisle headroom and enclosed aft lavatory as the III.

Trade-offs

  • TFE731 maintenance economics. The same Honeywell TFE731-3B engines as the III carry midsize-jet overhaul and hot-section costs; budget engine reserve well above light-jet levels.
  • Thin production run. Only 39 VIs were built, so comparable sales, parts familiarity, and variant-specific support are scarcer than for the III or VII.
  • Two-pilot operation. The Model 650 is certificated for a minimum crew of two and is not single-pilot eligible.
  • Legacy avionics. The simplified early-1990s panel typically needs upgrades for current airspace compliance.

See Also

Technical Specifications

Dimensions & Weights

Wingspan 53.5 ft
Height
16.83 ft
Length
55.5 ft
Parking area (ft2)
3841.75 ft2
Max Takeoff Weight
22,000 lbs
Max Landing Weight
20,000 lbs
Useful Load
8,100 lbs
Fuel Capacity
1100 gal

Performance

Cruise Speed
468 KTAS
Never-Exceed (Vne)
Source: FAA Type Certificate Data Sheet 346 KIAS
Max Structural Cruise (Vno)
Source: FAA Type Certificate Data Sheet 305 KIAS
Approach Speed
115 KIAS
Stall, Clean (Vs1)
97 KIAS
Range
2054 NM
Service Ceiling
51,000 ft
Rate of Climb
3699 fpm
Takeoff over 50 ft obstacle
5,150 ft
Landing ground roll
2,900 ft

Engines

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Sources

Where the figures on this page come from. Cessna Citation VI specifications are traced to published references; estimated values are flagged inline next to the figure.

Similar to the Cessna Citation VI

Similar Turbofans

Cessna Citation III

Cruise
472 kts (higher than this aircraft)
Range
2348 nm (higher than this aircraft)
Seats
15
View details

Cessna Citation VII

Cruise
476 kts (higher than this aircraft)
Range
1798 nm (lower than this aircraft)
Seats
15
View details

Gulfstream G550

Cruise
488 kts (higher than this aircraft)
Range
6750 nm (higher than this aircraft)
Seats
19
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See how the Cessna Citation VI stacks up against similar aircraft

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