Credit
Adrian Sultănoiu · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
IAR 316 · Length
Single source12.82 m (42 ft 1 in)[source]
Length
Single sourceConfiguration
| Specification | IAR 316 | Kazan Ansat |
|---|---|---|
| Type | Light utility /training helicopter[source] | Multipurpose utility helicopter[source] |
| Manufacturer | Industria Aeronautică Română[source] | Kazan Helicopters[source] |
| Status | operational for training purposes[source] | In service[source] |
| Primary user | Romanian Air Force[source] | Russian Aerospace Forces[source] |
13.76 m (45 ft 2 in)[source]
Endurance
Single source3 hours 07 minutes[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Number built | 250[source] | — |
|---|
| Manufactured | 1971-1987[source] | 1998–present[source] |
|---|
| Introduction date | 1971[source] | 28 August 2013[source] |
|---|
| Developed from | Aérospatiale Alouette III[source] | — |
|---|
| Capacity | 5 passengers[source] | **7–8 passengers 2 stretchers and 3 attendants 1,235 kg (2,723 lb) internal[source] |
|---|
| Fuel capacity | 550 kg (1,210 lb) maximum[source] | 535 kg[source] |
|---|
| Fuselage width | 2.6 m (8 ft 6 in)[source] | — |
|---|
| Main rotor area | 95.4 m 2 (1,027 sq ft)[source] | 103.87 m 2 (1,118.0 sq ft)[source] |
|---|
| Hardpoints | 2 hardpoints for anti-tank guided missiles[source] | — |
|---|
| National origin | Romania[source] | Russia[source] |
|---|
| Country of origin | Romania[source] | — |
|---|
| First flight | — | 17 August 1999[source] |
|---|
| Never exceed speed | — | 275 km/h (171 mph, 148 kn)[source] |
|---|
| Hover ceiling OGE | — | 4,396 ft (1,340 m)[source] |
|---|