FORCETALLY
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At a glance
Measured figures
Conquest II · Length
Single source39 ft 0 in (11.89 m)[source]
SR20-G3 · Length
Single sourceConfiguration
| Specification | Cessna 441 Conquest II | Cirrus SR20 |
|---|---|---|
| Type | Utility aircraft[source] | Light aircraft[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Cessna[source] | Cirrus Aircraft[source] |
| Number built | 362[source] |
26 ft 0 in (7.92 m)[source]
Cruise; Conquest II · at 35,000 ft (10,700 m)
Single sourceMaximum; Conquest II · at 16,000 ft (4,875 m)
Single source340 mph (550 km/h, 300 kn) at 16,000 ft (4,875 m)[source]
298 mph (480 km/h, 259 kn) at 35,000 ft (10,700 m)[source]
Cruise; SR20-G3 · TAS
Single source155 kn (178 mph, 287 km/h) TAS[source]
Conquest II · at 35,000 ft (10,700 m)
Single source2,525 mi (4,064 km, 2,194 nmi) at 35,000 ft (10,700 m)[source]
Conquest II · 2 × Garrett TPE331 -8-403S turboprops, 636 shp ( ) each
Single source2 × Garrett TPE331 -8-403S turboprops, 636 shp (474 kW) each[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]
Conquest II · Wing area
Single source253.6 sq ft (23.56 m 2 )[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
2,084 (through 2025)[source]
| Manufactured | 1977–1986[source] | 1999–present[source] |
|---|
| First flight | August 26, 1975[source] | 21 March 1995[source] |
|---|
| Developed from | Cessna 404 Titan[source] | — |
|---|
| Capacity | Up to 10 passengers with one pilot; up to 9 passengers with two pilots[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Aspect ratio | 9.6:1[source] | — |
|---|
| Airfoil | NACA 23018 at root, NACA 23019 at tip[source] | — |
|---|
| Propellers | 3-bladed Hartzell or McCauley[source] | 3-bladed[source] |
|---|
| Stall speed | 86 mph (139 km/h, 75 kn) flaps and gear down[source] | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|
| Developed into | — | Cirrus SR22[source] |
|---|