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At a glance
Measured figures
Mi-14PL · Length
Single source18.38 m (60 ft 4 in)[source]
S-92 · Length
Single sourceConfiguration
| Specification | Mil Mi-14 | Sikorsky S-92 |
|---|---|---|
| Type | Anti-submarine helicopter[source] | Medium-lift transport/utility helicopter[source] |
| National origin | Soviet Union[source] | United States[source] |
| Manufacturer | Mil Moscow Helicopter Plant[source] | Sikorsky Aircraft[source] |
| Status | In service[source] | In service[source] |
68 ft 6 in (20.88 m)[source]
S-92 · fuselage
Single source17 ft 3 in (5.26 m) fuselage[source]
Mi-14PL · 2 × Klimov TV3-117MT turboshaft engines each
Single source2 × Klimov TV3-117MT turboshaft engines, 1,454 kW (1,950 hp) each[source]
S-92 · 2 × General Electric CT7-8A turboshaft engines, 2,520 shp ( ) each
Single source2 × General Electric CT7-8A turboshaft engines, 2,520 shp (1,880 kW) each[source]
Mi-14PL · with maximum fuel
Single source4 hours with maximum fuel[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | Soviet Navy Russian Navy Ukrainian Navy Polish Navy[source] | CHC Helicopter Petroleum Helicopters International Bristow Helicopters Cougar Helicopters[source] |
|---|
| Number built | 273[source] | at least 300[source] |
|---|
| Manufactured | 1969-1986[source] | 1998–present[source] |
|---|
| Introduction date | 1976[source] | 2004[source] |
|---|
| First flight | 1 August 1967[source] | December 23, 1998[source] |
|---|
| Developed from | Mil Mi-8[source] | Sikorsky S-70[source] |
|---|
| Main rotor area | 356 m 2 (3,830 sq ft)[source] | 2,492.3 sq ft (231.54 m 2 )[source] |
|---|
| Blade section | NACA 23012[source] | - root: Sikorsky SC2110; tip: Sikorsky SSC-A09[source] |
|---|
| Variants | — | Sikorsky CH-148 Cyclone Sikorsky VH-92[source] |
|---|
| Capacity | — | 19 passengers[source] |
|---|
| Cabin dimensions | — | 20 ft (6 m) long by 6.6 ft (2 m) tall[source] |
|---|
| Disk loading | — | 9.8 lb/sq ft (48 kg/m 2 )[source] |
|---|
| Power/mass | — | 0.23 hp/lb (0.38 kW/kg)[source] |
|---|
Maximum take-off; S-92 · Max takeoff weight
Single source