Credit
Adrian Pingstone · Public domain · Resized · Public domain · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
Cessna Citation Ultra · Length
Single source48 ft 11 in (14.9 m)[source]
SR20-G3 · Length
Configuration
| Specification | Cessna Citation V | Cirrus SR20 |
|---|---|---|
| Type | Corporate jet[source] | Light aircraft[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Cessna[source] | Cirrus Aircraft[source] |
| Primary users | United States Army United States Marine Corps[source] | — |
26 ft 0 in (7.92 m)[source]
Cessna Citation Ultra · two pilots and six passengers, no wind
Single source1,960 nmi (2,260 mi, 3,630 km) two pilots and six passengers, no wind[source]
SR20-G3 · 1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine
Single source1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine , 200 hp (150 kW)[source]
Cessna Citation Ultra · 2 × Pratt & Whitney Canada JT15D -5D turbofans thrust each
Single source2 × Pratt & Whitney Canada JT15D -5D turbofans , 3,045 lbf (13.54 kN) thrust each[source]
Cessna Citation Ultra · Wing area
Single source342 sq ft (31.8 m 2 )[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Number built |
|---|
774 : 262 V, 279 Ultra, 168 Encore, 65 Encore+[source] |
2,084 (through 2025)[source] |
| Manufactured | 1989 (V) – 2011 (Encore+)[source] | 1999–present[source] |
|---|
| Introduction date | 1987 (Citation V), 1994 (Ultra), 1998 (Encore)[source] | — |
|---|
| First flight | August 1987[source] | 21 March 1995[source] |
|---|
| Developed from | Cessna Citation S/II[source] | — |
|---|
| Capacity | 7–11 passengers[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Fuel capacity | 5,771 lb (2,618 kg)[source] | — |
|---|
| Max. Payload | 2,275 lb (1,032 kg)[source] | — |
|---|
| Cabin length | 17.4 ft (5.3 m)[source] | — |
|---|
| Cabin height × width | 4.8 ft × 4.9 ft (1.5 × 1.5 m)[source] | — |
|---|
| Fuel consumption | 2.4 lb/mi (0.67 kg/km) at FL410, 433 kn (802 km/h)[source] | — |
|---|
| Cabin pressurization | 8.9 psi (0.61 bar)[source] | — |
|---|
| Developed into | — | Cirrus SR22[source] |
|---|
| Propellers | — | 3-bladed[source] |
|---|
| Stall speed | — | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|
| Reported operators |
| — |
|---|