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]
PC-12NG · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Pilatus PC-12 |
|---|---|---|
| Type | Light aircraft[source] | Passenger and cargo aircraft[source] |
| Manufacturer | Cirrus Aircraft[source] | Pilatus Aircraft[source] |
| Number built | 2,084 (through 2025)[source] | 2,000 (as of May 2023 )[source] |
| Manufactured | 1999–present[source] | 1991–present[source] |
14.4 m (47 ft 3 in)[source]
PC-12NG · HSC, VFR Reserves
Single source3,417 km (2,123 mi, 1,845 nmi) (HSC, VFR 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]
PC-12NG · 1 × Pratt & Whitney Canada PT6A-67P turboprop engine 1,200 shp
Single source1 × Pratt & Whitney Canada PT6A-67P turboprop engine, 890 kW (1,200 shp)[source]
PC-12NG · Wing area
Single source25.81 m 2 (277.8 sq ft)[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] | 31 May 1991[source] |
|---|
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 6 to 9 passengers seats[source] |
|---|
| Propellers | 3-bladed[source] | 4-bladed Hartzell Propeller composite, 2.67 m (8 ft 9 in) diameter composite constant-speed fully-feathering reversible propeller[source] |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | 124 km/h (77 mph, 67 kn)[source] |
|---|
| National origin | United States[source] | Switzerland[source] |
|---|
| Status | — | In production[source] |
|---|
| Primary users | — | PlaneSense Royal Flying Doctor Service Tradewind Aviation United States Air Force[source] |
|---|
| Introduction date | — | 1994[source] |
|---|
| Variant | — | Pilatus U-28 Draco[source] |
|---|
| Airfoil | — | root : NASA LS(1)-0417MOD; tip : NASA LS(1)-0313[source] |
|---|
| Maximum landing weight | — | 4,500 kg (9,921 lb)[source] |
|---|
| Maximum zero fuel weight | — | 4,100 kg (9,039 lb)[source] |
|---|
| Fuel capacity | — | 1,226 kg (2,703 lb) / 1,521 L (402 US gal; 335 imp gal)[source] |
|---|
| Cabin | — | 5.16 metres (16.9 ft) long, 1.47 metres (4.8 ft) high, up to 1.52 metres (5.0 ft) wide[source] |
|---|
| Take-off distance over 50 ft (15 m) | — | 793 m (2,602 ft)[source] |
|---|
| Landing distance over 50 ft (15 m) | — | 661 m (2,169 ft)[source] |
|---|
| Fuel consumption | — | 250 L/h (66 gal/h; 55 imp gal/h) (915 km (569 mi; 494 nmi) trip, including climb, cruise and descent, 491 km/h (305 mph; 265 kn) average block speed)[source] |
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