Credit
Adrian Sultănoiu · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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Measured figures
IAR 316 · Length
Single source12.82 m (42 ft 1 in)[source]
Configuration
| Specification | IAR 316 | Kamov Ka-65 |
|---|---|---|
| Type | Light utility /training helicopter[source] | — |
| Manufacturer | Industria Aeronautică Română[source] | — |
| Status | operational for training purposes[source] | — |
| Primary user | Romanian Air Force[source] | — |
| Number built | 250[source] | — |
| Manufactured | 1971-1987[source] |
IAR 316 · 3 ×
Single source3 × 11.02 m (36 ft 2 in)[source]
IAR 316 · Height
Single source2.97 m (9 ft 9 in)[source]
IAR 316 · Range
Single source540 km (340 mi, 290 nmi)[source]
IAR 316 · 1 × Turbomeca Artouste IIIB turboshaft
Single source1 × Turbomeca Artouste IIIB turboshaft, 425 kW (570 hp)[source]
IAR 316 · Service ceiling
Single source3,200 m (10,500 ft)[source]
IAR 316 · 852 ft/min
Single source4.33 m/s (852 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Introduction date | 1971[source] | — |
|---|
| Developed from | Aérospatiale Alouette III[source] | — |
|---|
| Capacity | 5 passengers[source] | — |
|---|
| Fuel capacity | 550 kg (1,210 lb) maximum[source] | — |
|---|
| Fuselage width | 2.6 m (8 ft 6 in)[source] | — |
|---|
| Main rotor area | 95.4 m 2 (1,027 sq ft)[source] | — |
|---|
| Hardpoints | 2 hardpoints for anti-tank guided missiles[source] | — |
|---|
| National origin | Romania[source] | Russia[source] |
|---|
| Country of origin | Romania[source] | Russia[source]Inventory Origin column; table 6, row 10, cell 2; revision 1364906102; retrieved 2026-10-02 |
|---|
| First flight | — | 2025 (expected)[source] |
|---|
| Role | — | project for a new helicopter[source] |
|---|