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]
PZL M28 · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | PZL M28 Skytruck |
|---|---|---|
| Type | Light aircraft[source] | STOL transport, patrol and maritime reconnaissance aircraft[source] |
| Manufacturer | Cirrus Aircraft[source] | PZL Mielec[source] |
| Number built | 2,084 (through 2025)[source] | 200+ (including PZL An-28)[source] |
| Manufactured | 1999–present[source] | 1984-1993 (PZL An-28) 1993- (PZL M28 Skytruck) |
13.1 m (43 ft 0 in)[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]
PZL M28 · 2 × Pratt & Whitney Canada PT6A-65B turboprop engines each
Single source2 × Pratt & Whitney Canada PT6A-65B turboprop engines, 820 kW (1,100 hp) each[source]
PZL M28 · Wing area
Single source39.72 m 2 (427.5 sq ft)[source]
PZL M28 · 3,000 m (10,000 ft)
Single sourcePZL M28 · reserve
Single source6.2 h (3,000 m (10,000 ft), 45 min reserve)[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] | 22 July 1984 (PZL An-28) 24 July 1993 (PZL M28 Skytruck)[source] |
|---|
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 19 passengers (17 paratroopers) or 2,300 kg (5,071 lb)[source] |
|---|
| Propellers | 3-bladed[source] | Hartzell HC-B5MP-3D10876ASK[source] |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | 120 km/h (75 mph, 65 kn)[source] |
|---|
| National origin | United States[source] | — |
|---|
| Designer | — | Antonov / PZL Mielec[source] |
|---|
| Status | — | In active service[source] |
|---|
| Primary users | — | Polish Air Force Polish Navy Venezuelan Army United States Air Force[source] |
|---|
| Developed from | — | Antonov An-28[source] |
|---|
| Fuel capacity | — | 1,766 kg (3,893 lb) / 2,278 L (602 US gal; 501 imp gal)[source] |
|---|
| Cabin length | — | 5.26 m (17 ft)[source] |
|---|
| Cabin width | — | 1.74 m (5 ft 9 in)[source] |
|---|
| Cabin height | — | 1.72 m (5 ft 8 in)[source] |
|---|
| Cabin volume | — | 13.73 m 2 (148 sq ft)[source] |
|---|
| Aspect ratio | — | 12.25[source] |
|---|
| Airfoil | — | TsAGI R-II-14 (14%)[source] |
|---|
| Minimum control speed | — | 153 km/h (95 mph, 83 kn) (V MCA )[source] |
|---|
| g limits | — | +3/-1[source] |
|---|
| Time to altitude | — | 3,000 m (9,800 ft) in 6 minutes with air bleed off (9 min with air bleed on)[source] |
|---|
| Take-off run | — | 494 m (1,620 ft)[source] |
|---|
| Landing run | — | 250 m (820 ft)[source] |
|---|
| Fuel consumption | — | 268 kg/h (591 lb/h)[source] |
|---|
| Alternative designation | — | M28 Skytruck[source] |
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| Country of origin | — | Poland[source] |
|---|