Credit
Oleg Belyakov · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
An-32 · Length
Single source23.78 m (78 ft 0 in)[source]
SR20-G3 · Length
Single sourceConfiguration
| Specification | Antonov An-32 | Cirrus SR20 |
|---|---|---|
| Type | Military transport aircraft[source] | Light aircraft[source] |
| National origin | Soviet Union / Russia / Ukraine[source] | United States[source] |
| Manufacturer | Antonov Serial Production Plant[source] | Cirrus Aircraft[source] |
| Designer | Antonov[source] | — |
| Status |
26 ft 0 in (7.92 m)[source]
An-32 · with 3,700 kg (8,160 lb) payload, no reserves
Single source2,500 km (1,600 mi, 1,300 nmi) with 3,700 kg (8,160 lb) payload, no reserves[source]
An-32 · 2 × ZMKB Progress AI-20DM turboprop engines each
Single source2 × ZMKB Progress AI-20DM turboprop engines, 3,812 kW (5,112 hp) 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]
An-32 · Wing area
Single source75 m 2 (810 sq ft)[source]
SR20-G3 · 828 ft/min (
Single source828 ft/min (4.21 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
In service[source] |
| — |
| Primary users | Indian Air Force National Air Force of Angola Sri Lanka Air Force Ukrainian Air Force[source] | — |
|---|
| Number built | 373[source] | 2,084 (through 2025)[source] |
|---|
| Manufactured | 1982–2012[source] | 1999–present[source] |
|---|
| First flight | 9 July 1976[source] | 21 March 1995[source] |
|---|
| Developed from | Antonov An-26[source] | — |
|---|
| Developed into | Antonov/Taqnia An-132[source] | Cirrus SR22[source] |
|---|
| Capacity | 42 paratroopers/50 passengers/24 Casualties on stretcher with three medical personnel / 6,700 kg (14,771 lb) max payload[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Propellers | 4-bladed constant speed propellers[source] | 3-bladed[source] |
|---|
| Stall speed | — | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|