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ForceTally · AI-generated illustration · Not a photograph · AI-generated · OpenAI output terms · Source ↗ · Modified
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At a glance
Measured figures
Length
Single source9 m (29 ft 6 in)[source]
IAR 316 · Length
Single sourceConfiguration
| Specification | HESA Shahed 274 | IAR 316 |
|---|---|---|
| Type | Light utility helicopter[source] | Light utility /training helicopter[source] |
| Manufacturer | Iran Aircraft Manufacturing Industrial Company[source] | Industria Aeronautică Română[source] |
| Designer | Institute of Industrial Research and Development of the IRGC[source] | — |
| Status | Unknown[source] | operational for training purposes[source] |
12.82 m (42 ft 1 in)[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.
| Primary user |
|---|
Islamic Revolutionary Guard Corps[source] |
Romanian Air Force[source] |
| Number built | At least 3[source] | 250[source] |
|---|
| Introduction date | 30 December 2000[source] | 1971[source] |
|---|
| First flight | 1997[source] | — |
|---|
| Capacity | 5 (including pilot)[source] | 5 passengers[source] |
|---|
| Propellers | 2-bladed main and tail[source] | — |
|---|
| National origin | Iran[source] | Romania[source] |
|---|
| Manufactured | — | 1971-1987[source] |
|---|
| Developed from | — | Aérospatiale Alouette III[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] |
|---|
| Country of origin | — | Romania[source] |
|---|