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]
Mi-10 · fuselage only
Single sourceConfiguration
| Specification | IAR 316 | Mil Mi-10 |
|---|---|---|
| Type | Light utility /training helicopter[source] | Aerial crane[source] |
| Manufacturer | Industria Aeronautică Română[source] | Mil Moscow Helicopter Plant[source] |
| Status | operational for training purposes[source] | Active as of 2014 (Mi-10K)[source] |
| Primary user | Romanian Air Force[source] | — |
| Number built | 250 |
Mi-10 · overall length, rotors turning
Single source32.86 m (107 ft 10 in) (fuselage only), 41.89 m (137 ft 5 in) (overall length, rotors turning)[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.
55[source] |
| Manufactured | 1971-1987[source] | 1964–69[source] |
|---|
| Introduction date | 1971[source] | 1963[source] |
|---|
| Developed from | Aérospatiale Alouette III[source] | Mil Mi-6[source] |
|---|
| Capacity | 5 passengers[source] | 28 passengers or 3 t (3,000 kg; 6,600 lb) internally up to 15 t (15,000 kg; 33,000 lb) payload on platform or 8 t (8,000 kg; 18,000 lb) max slung payload[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] | 962 m 2 (10,350 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 | — | 15 June 1960[source] |
|---|
| Ground clearance under fuselage | — | 3.75 m (12 ft 4 in)[source] |
|---|
| Hovering ceiling out of ground effect | — | 3,000 m (9,840 ft)[source] |
|---|
Gross; Mi-10 · Gross weight
Single sourceGross; Mi-10 · Mi-10K
Single sourceMaximum take-off; Mi-10 · Max takeoff weight
Single sourceMaximum take-off; Mi-10 · Mi-10K
Single source