FORCETALLY
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At a glance
Measured figures
337D · Length
Single source29 ft 9 in (9.07 m)[source]
SR20-G3 · Length
Single sourceConfiguration
| Specification | Cessna Skymaster | Cirrus SR20 |
|---|---|---|
| Type | Personal use and air taxi aircraft[source] | Light aircraft[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Cessna Reims Aviation[source] | Cirrus Aircraft[source] |
| Number built | 2,993[source] |
26 ft 0 in (7.92 m)[source]
Cruise; 337D · at 10,000 ft (3,000 m) (econ cruise)
Single source199 mph (320 km/h, 173 kn) at sea level[source]Source text · numeric interpretation needs review
144 mph (232 km/h, 125 kn) at 10,000 ft (3,000 m) (econ cruise)[source]
Cruise; SR20-G3 · TAS
Single source155 kn (178 mph, 287 km/h) TAS[source]
337D · econ cruise, normal fuel
Single source965 mi (1,553 km, 839 nmi) (econ cruise, normal fuel)[source]
337D · 2 × Continental IO-360-C air-cooled flat-six piston engine each
Single source2 × Continental IO-360-C air-cooled flat-six piston engine, 210 hp (160 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]
337D · Wing area
Single source201 sq ft (18.7 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 | 1963–1982[source] | 1999–present[source] |
|---|
| Introduction date | 1962[source] | — |
|---|
| First flight | February 28, 1961[source] | 21 March 1995[source] |
|---|
| Variants | Cessna O-2 Skymaster Conroy Stolifter Spectrum SA-550[source] | — |
|---|
| Capacity | 5 passengers[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Aspect ratio | 7.18:1[source] | — |
|---|
| Airfoil | NACA 2412 at root, NACA 2409 at tip[source] | — |
|---|
| Fuel capacity | 92 US gal (77 imp gal; 350 L) normal, 128 US gal (107 imp gal; 480 L) with auxiliary tanks[source] | — |
|---|
| Propellers | 2-bladed McCauley fully-feathering, constant-speed propeller, 6 ft 4 in (1.93 m) diameter[source] | 3-bladed[source] |
|---|
| Stall speed | 69 mph (111 km/h, 60 kn) (flaps and undercarriage down)[source] | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|
| Takeoff distance to 50 ft (15m) | 1,545 ft (471 m)[source] | — |
|---|
| Landing distance from 50 ft (15m) | 1,650 ft (500 m)[source] | — |
|---|
| Developed into | — | Cirrus SR22[source] |
|---|