Credit
Markus Eigenheer from Genève, Schweiz · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Citation Latitude · Length
Single source62 ft 3 in (18.97 m)[source]
SR20-G3 · Length
Configuration
| Specification | Cessna Citation Latitude | Cirrus SR20 |
|---|---|---|
| Type | Corporate jet[source] | Light aircraft[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Textron Aviation[source] | Cirrus Aircraft[source] |
| Status | In production[source] | — |
26 ft 0 in (7.92 m)[source]
Citation Latitude · 4 passenger
Single source2,700 nmi (3,100 mi, 5,000 km) 4 passenger[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]
Citation Latitude · 2 × Pratt Whitney Canada PW306D1 turbofan thrust each
Single source2 × Pratt Whitney Canada PW306D1 turbofan, 5,907 lbf (26.28 kN) thrust each[source]
Citation Latitude · Wing area
Single source543 sq ft (50.4 m 2 )[source]
Citation Latitude · Maximum payload
Single source2,544 lb (1,154 kg)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Number built |
|---|
400 by May 2024[source] |
2,084 (through 2025)[source] |
| Manufactured | 2014–present[source] | 1999–present[source] |
|---|
| First flight | 18 February 2014[source] | 21 March 1995[source] |
|---|
| Developed from | Cessna Citation Sovereign[source] | — |
|---|
| Developed into | Cessna Citation Longitude[source] | Cirrus SR22[source] |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Fuel capacity | 11,394 lb (5,168 kg)[source] | — |
|---|
| Aspect ratio | 9.64[source] | — |
|---|
| Airfoil | 16.3° sweep[source] | — |
|---|
| Cabin | 72 in (1.83 m) height × 77 in (1.96 m) width[source] | — |
|---|
| Never exceed speed | 460 kn (530 mph, 850 km/h) Mach .80[source] | — |
|---|
| Time to altitude | 16 min to FL370[source] | — |
|---|
| Wing loading | 56.7 lb/sq ft (277 kg/m 2 ) MTOW[source] | — |
|---|
| Thrust/weight | 0.38[source] | — |
|---|
| Takeoff | 3,580 ft (1,091 m)[source] | — |
|---|
| Landing | 2,480 ft (756 m)[source] | — |
|---|
| Propellers | — | 3-bladed[source] |
|---|
| Stall speed | — | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|