Cessna Citation V/Ultra/Encore

Jet • twin engine • Low Wing • Retractable gear

Range Visualization

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Payload vs. Range

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Default: 190 lbs (FAA standard)

Default: 30 lbs

Passengers
lbs @ lbs / pax
0 lbs
Fuel on board
gal
+ 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.

Mission Profile

430
KTAS
Cruise Speed
8
Occupants
1960
nm
Max Range
3538
lbs
Wet Payload

Estimated Ownership Costs

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About the Cessna Citation V/Ultra/Encore

Citation V / Ultra / Encore (Model 560 series) is a light business jet produced by Cessna from 1989 to 2011. The base V was equipped with JT15D-5A engines; the Ultra uses JT15D-5D variants; the Encore upgrades to PW535A engines and further refinements. Typical cruise is in the 420-430 kt region (≈ Mach 0.73-0.75) under favorable conditions. Published weight & balance sources indicate useful load ~6,400 lb; typical passenger seating is 7-8 plus crew (though some arrangements permit a belted lav seat). The service ceiling is ~45,000 ft, and the wing span is about 54.1 ft. The available “Note-Taking Guide” for CE-560 suggests VMO (i.e. max operating) speeds of 262 kt up to 14,000 ft, and 292 kt above, with MMO = 0.755; these likely correspond to structural upper limits, suggesting a VNE near 292 kt, and a VNO somewhat lower (perhaps ~260-270 kt) — although official published VNO/VNE values in the AFM or type certificate were not located in open sources. Data is derived mostly from Cessna Citation Ultra / 560-series data; original V has slightly lower perf.

Technical Specifications

Dimensions

Wingspan
54.1 ft
Length
48.9 ft
Height
15.2 ft

Weights

Max Takeoff Weight
16,300 lbs
Max Landing Weight
15,200 lbs
Useful Load
6,426 lbs
Fuel Capacity
431 gal

Performance

Cruise Speed
430 KTAS
Range
1960 NM
Service Ceiling
45,000 ft
Rate of Climb
4230 fpm

Engines

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