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At a glance
Measured figures
1956 model 310 · Length
Single source27 ft 0 in (8.23 m)[source]
SR20-G3 · Length
Single sourceConfiguration
| Specification | Cessna 310 | Cirrus SR20 |
|---|---|---|
| Type | Twin-engine cabin monoplane[source] | Light aircraft[source] |
| Manufacturer | Cessna[source] | Cirrus Aircraft[source] |
| Primary user | United States Air Force[source] | — |
| Number built | 5,449 (310) 577 (320)[source] | 2,084 (through 2025)[source] |
26 ft 0 in (7.92 m)[source]
1956 model 310 · Range
Single source1,000 mi (1,600 km, 870 nmi)[source]
1956 model 310 · 2 × Continental O-470-B horizontally opposed piston engine each
Single source2 × Continental O-470-B horizontally opposed piston engine, 240 hp (180 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]
1956 model 310 · Wing area
Single source175 sq ft (16.3 m 2 )[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured |
|---|
1954–1980[source] |
1999–present[source] |
| Introduction date | 1954[source] | — |
|---|
| First flight | January 3, 1953[source] | 21 March 1995[source] |
|---|
| Developed into | Cessna 340 Cessna 411[source] | Cirrus SR22[source] |
|---|
| Capacity | four passengers[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Fuel capacity | 100 US gal (83 imp gal; 380 L)[source] | — |
|---|
| National origin | United States[source] | United States[source] |
|---|
| Propellers | — | 3-bladed[source] |
|---|
| Stall speed | — | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|