Credit
Tomás Del Coro from Las Vegas, Nevada, USA · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
SR20-G3 · Length
Single source26 ft 0 in (7.92 m)[source]
Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Piper PA-31T Cheyenne |
|---|---|---|
| Type | Light aircraft[source] | Turboprop[source] |
| Manufacturer | Cirrus Aircraft[source] | Piper Aircraft[source] |
| Number built | 2,084 (through 2025)[source] | 823[source] |
| Manufactured | 1999–present[source] | 1974–1985 |
34 ft 8 in (10.57 m)[source]
Cruise; SR20-G3 · TAS
Single source155 kn (178 mph, 287 km/h) TAS[source]
econ. cruise, 45 min reserves
Single source1,702 mi (2,739 km, 1,479 nmi) (econ. cruise, 45 min reserves)[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]
2 × Pratt & Whitney Canada PT6 A-28 turboprops , 620 shp ( ) each
Single source2 × Pratt & Whitney Canada PT6 A-28 turboprops , 620 shp (460 kW) each[source]
Wing area
Single source229 sq ft (21.3 m 2 )[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| First flight | 21 March 1995[source] | 29 August 1969[source] |
|---|
| Developed into | Cirrus SR22[source] | Piper PA-42 Cheyenne[source] |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 4–6 passengers[source] |
|---|
| Propellers | 3-bladed[source] | 3-bladed Hartzell HC-BTN-3B constant-speed propellers , 7 ft 9 in (2.36 m) diameter[source] |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | 88 mph (142 km/h, 76 kn) (flaps down)[source] |
|---|
| National origin | United States[source] | — |
|---|
| Developed from | — | Piper PA-31 Navajo[source] |
|---|
| Airfoil | — | NACA 63 2 -415 at root, 63A212 at tip[source] |
|---|
| Fuel capacity | — | 382 US gal (318 imp gal; 1,450 L) usable fuel[source] |
|---|
| Takeoff run to 50 ft (15 m) | — | 1,980 ft (600 m)[source] |
|---|
| Landing run from 50 ft (15 m) | — | 1,860 ft (570 m)[source] |
|---|
| Country of origin | — | United States[source]Inventory Origin column; table 1, row 25, cell 2; revision 1370518079; retrieved 2026-09-30 |
|---|