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At a glance
Measured figures
Mi-8MT · Length
Single source18.4 m (60 ft 4 in)[source]
S-92 · Length
Single sourceConfiguration
| Specification | Mil Mi-8 | Sikorsky S-92 |
|---|---|---|
| Type | Transport helicopter (also several armed versions)[source] | Medium-lift transport/utility helicopter[source] |
| National origin | Soviet Union / Russia[source] | United States[source] |
| Manufacturer | Kazan Helicopter Plant Ulan-Ude Aviation Plant[source] | Sikorsky Aircraft[source] |
| Designer | Mil Moscow Helicopter Plant[source] | — |
68 ft 6 in (20.88 m)[source]
S-92 · fuselage
Single source17 ft 3 in (5.26 m) fuselage[source]
Empty; Mi-8MT · Empty weight
Single sourceGross; Mi-8MT · Gross weight
Single sourceMaximum take-off; Mi-8MT · Max takeoff weight
Single source7,100 kg (15,653 lb)[source]
11,100 kg (24,471 lb)[source]
13,000 kg (28,660 lb)[source]
Empty; S-92 · Empty weight
Single sourceGross; S-92 · Gross weight
Single sourceMi-8MT · 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]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status | In service[source] | In service[source] |
|---|
| Primary user | Soviet Union (historical) Russia Approx. 80 other countries, see Operators below[source] | — |
|---|
| Number built | >17,000 and production continues today; world's most-produced helicopter[source] | at least 300[source] |
|---|
| Manufactured | 1961–present[source] | 1998–present[source] |
|---|
| Introduction date | 1967[source] | 2004[source] |
|---|
| First flight | 7 July 1961[source] | December 23, 1998[source] |
|---|
| Variant | Mil Mi-8M/Mi-17[source] | — |
|---|
| Developed into | Mil Mi-14 Mil Mi-24[source] | — |
|---|
| Capacity | 24 passengers or 12 stretchers and seat for one medical attendant or 4,000 kg (8,800 lb) on internal/external hardpoints[source] | 19 passengers[source] |
|---|
| Fuel capacity | 3,700 L (980 US gal; 810 imp gal)[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] |
|---|
| Hardpoints | 4,000 kg (8,818 lb) of disposable stores on six hardpoints , including 57 mm S-5 rockets , bombs, or 9M17 Phalanga ATGMs and one or two side-mounted PK machine guns[source] | — |
|---|
| Former operator · Albania | Albania[source] | — |
|---|
| Former operator · Artsakh | Artsakh[source] | — |
|---|
| Former operator · Bangladesh | Bangladesh[source] | — |
|---|
| Former operator · Benin | Benin[source] | — |
|---|
| Former operator · Czechoslovakia | Czechoslovakia[source] | — |
|---|
| Former operator · Croatia | Croatia[source] | — |
|---|
| Role | family of medium twin-turbine helicopters , originally[source] | — |
|---|
| Source measurement | The prototype, which was named V-8, was designed in 1958 and based on the Mil Mi-4 with a larger cabin. Powered by an AI-24 2,010 kW (2,700 shp) Soloviev turboshaft engine, the single engined V-8 prototype had its maiden flight in June 1961 and was first shown on Soviet Aviation Day parade (Tushino Air Parade) in July 1961.[source]Mil Mi-8 · Design and development; only the objects and conditions stated in this passage Two months after the engines were completed by Isotov, the third prototype designated V-8A equipped with two 1,120 kW (1,500 shp) Isotov TV2 engines, made its first flight piloted by Nikolai Ilyushin on 2 August 1962, marking the first flight of any Soviet helicopter to fly with purpose built gas turbine engines. The aircraft completed its factory based testing in February 1963.[source]Mil Mi-8 · Design and development; only the objects and conditions stated in this passage There are numerous variants, including the Mi-8T , which, in addition to carrying 24 troops, is armed with rockets and anti-tank guided missiles . The Mil Mi-17 export version is employed by around 20 countries; its equivalent in Russian service in the Mi-8M series. The only visible differences between the Mi-8 and Mi-17 are A) the position of the tail rotor (Mi-8 right side, Mi-17 left side), B) the shape of the exhausts (Mi-8 circular, Mi-17 oval), and C) Dust shields in front of engine air intakes for the Mi-17. Also Mi-17 has some improved armour plating for its crew. The naval Mil Mi-14 version is also derived from the Mi-8.[source]Mil Mi-8 · Design and development; only the objects and conditions stated in this passage The Finnish Defence Forces and the Finnish Border Guard began using Mi-8s in the 1970s, with the Finnish Air Force receiving its first, serialed HS-2, on 28 May 1973, and the second, HS-1, on 31 May 1973. Six Mi-8Ts were obtained at first, followed by further two Mi-8Ts and two Mi-8Ps. Three of the helicopters were handed over to the Border Guard Wing. One of these was lost after sinking through ice during a landing in April 1982. It was soon replaced by a new Mi-8.[source]Mil Mi-8 · Operational history / Finland; only the objects and conditions stated in this passage After their Border Guard service, the helicopters were transferred to the civil register, but shortly thereafter to the Finnish Air Force. In 1997 it was decided that all helicopters, including the remaining five Mi-8Ts and two Mi-8Ps, should be transferred to the Army Wing at Utti . All Mi-8s have now been retired. One Mi-8 is on display at the Finnish Aviation Museum in Vantaa , and one is at the Päijänne Tavastia Aviation Museum in Asikkala , near Lahti . One Mi-8T is on display in Tuulos. The two final Mi-8Ts were given to Hungary in August 2011 with all the remaining spare parts.[source]Mil Mi-8 · Operational history / Finland; only the objects and conditions stated in this passage On another occasions Abkhaz Mi-8MTVs were shot down by Georgian forces, by SA-14 in one case and by RPG-18 in a second case, both during 1993. In the final case, Georgian Mi-8MTV carrying civilian refugees was shot down, killing 25 people. Georgian Air Force and Police currently operate about 20 Mi-8T/MTVs.[source]Mil Mi-8 · Operational history / Georgia; only the objects and conditions stated in this passage The Indian Air Force inducted the Mi-8 in the 1970s as part of a growing rotary-wing fleet that evolved without centralised long-term planning. Acquired in the wake of geopolitical deals and stop-gap needs, the Mi-8 formed the backbone of medium-lift capability before being succeeded by the Mi-17.[source]Mil Mi-8 · Operational history / India; only the objects and conditions stated in this passage Between April and May 1986, Mi-8s were used in large numbers to drop radiation-absorbing materials into the No. 4 reactor of Chernobyl Nuclear Power Plant after the Chernobyl disaster , and the fire was extinguished by the combined effort of helicopters dropping over 5000 metric tons of sand, lead, clay, and neutron-absorbing boron onto the burning reactor and injecting liquid nitrogen into it. Most of the helicopters were severely irradiated and abandoned in a giant junkyard, the so-called "machines cemetery" near Chernobyl, with several disappearing from the site in later years. During the initial operation, one crashed near the power plant after hitting a construction crane cable with all the crew of four being killed in the crash. It is now known that virtually none of the neutron absorbers reached the core.[source]Mil Mi-8 · Operational history / Soviet Union; only the objects and conditions stated in this passage On 16 August 2013, the Ministry of Defense of Ukraine reported that one of its Mi-8MSB had set a world altitude record of 9,150 metres (30,020 ft) at the Kirovske military airfield on 15 August.[source]Mil Mi-8 · Operational history / Ukraine; only the objects and conditions stated in this passage The Ukrainian Armed Forces used Mi-8MSB along with Mi-24s in operations against separatists in Eastern Ukraine during the Russo-Ukrainian War . On 29 May 2014, a Ukrainian National Guard Mi-8 was brought down by Russian separatist forces in Donbas using a MANPADS near Slavyansk with 12 personnel, including an Army general, killed and one seriously injured. On 24 June 2014, a Ukrainian National Guard Mi-8 was shot down by separatist forces again using a MANPADS near Slavyansk with nine personnel killed. Ukrainian forces used Mi-8 helicopters to resupply forces during the Siege of Mariupol at Azovstal iron and steel works and bring in additional reinforcements for the Azov Regiment . Some 16 Mi-8s were used a number of times, two of which were shot down. Russia claimed on 5 April that it shot down two Ukrainian Mi-8s that it said were being used to evacuate commanders of the Azov Regiment . In late August 2023, it was reported that a Russian defector named Maksym Kuzminov handed over a Mi-8AMTSh to the Ukrainian forces in coordination with Ukrainian Intelligence agents.[source]Mil Mi-8 · Operational history / Ukraine; only the objects and conditions stated in this passage During combat in the winter of 1991 in the Croatian war and in the spring of 1992 in the Bosnian War , the Yugoslav People's Army used the Mi-8 fleet for the evacuation of injured personnel, transport of cargo and search and rescue for the crews of aircraft forced down. As most flights were made behind the front, the Croatian forces were able to down just one helicopter, which was hit by small arms fire near Slavonski Brod on 4 October 1991.[source]Mil Mi-8 · Operational history / Yugoslavia; only the objects and conditions stated in this passage The North Macedonian Air Force bought two Mi-8MT helicopters in 2001 from Ukraine . They fly in the Transport Helicopter Squadron (ex 301. Transport Helicopter Squadron). One crashed, killing all 8 passengers and 3 crew members in an accident in January 2008 .[source]Mil Mi-8 · Operational history / Yugoslavia; only the objects and conditions stated in this passage During the Kosovo War of 1998 and 1999, the Federal Yugoslav Air Force used Mi-8s for transport of personnel and material to forces in otherwise-inaccessible mountain areas. Evacuation of injured personnel also occurred during the 1999 NATO bombing of Yugoslavia , flying at low altitude to avoid detection by NATO aircraft. In 1999, Yugoslav Mi-8s shot down at least one US Army Hunter UAV with the door gunner's 7.62 mm machine gun. Two Mi-17V helicopters secretly operated by the Special Operations Unit post-1997 were also active during the Kosovar conflict. After the unit disbanded in 2003, the helicopters were transferred to Serbia and Montenegro's air force .[source]Mil Mi-8 · Operational history / Yugoslavia; only the objects and conditions stated in this passage As of mid-2020, the Serbian Air Force , the successor of the Federal Yugoslav Air Force, operates a small amount of Mi-8T which are now being replaced by Mi-17 helicopters. There are 13 Mi-17 in the Serbian air force currently. They are in the 138th Mixed-Transport-Aviation Squadron of 204th Air Base and 119th Combined-Arms Helicopter Squadron (ex 199th regiment) of 98th Air Base .[source]Mil Mi-8 · Operational history / Yugoslavia; only the objects and conditions stated in this passage Vietnam- On 22 November 1992 a Vietnamese Mi-8 was sent from Hanoi carrying rescue workers for Flight 474 , but it crashed near Ô Kha mountain on the same day. All seven people aboard were killed[source]Mil Mi-8 · Operational history / Others; only the objects and conditions stated in this passage Prototype design, a modification of the existing Mil Mi-8. Two Mi-8s were extended by 0.9 meters (3 ft), the landing gear made retractable, and a sliding door added to the starboard side of the fuselage. The Mi-18s were used in the Soviet invasion of Afghanistan , and later used as static training airframes for pilots of the Mi-8/17.[source]Mil Mi-8 · Variants / Prototypes/experimental/low production rate; only the objects and conditions stated in this passage Version used as a gunship or direct air support platform. Airframe modifications add 2x external hard points for a total of 6, and mount a flexible 12.7 mm (0.5-inch) KV-4 machine gun in the nose. Armament of 57 mm S-5 rockets, six UV-32-57 rocket pods, 551-lb (250-kg) bombs, or four AT-2 Swatter ATGMs.[source]Mil Mi-8 · Variants / Basic military transport/airframe; only the objects and conditions stated in this passage Civilian and military utility transport version, with accommodation for 24 passengers, fitted with tip-up seats along the cabin walls, circular cabin windows and large rear clamshell doors with a sloping hinge line. The Mi-8T is powered by two 1,677 shp (1,251 kW) Klimov TV2-117A turboshaft engines, giving the helicopter a maximum speed of 155 mph (249 km/h) at sea level.[source]Mil Mi-8 · Variants / Civil; only the objects and conditions stated in this passage Civilian passenger transport version, with accommodation for between 28 and 32 passengers, fitted with square cabin windows, small rear clamshell doors with a vertical hinge line and a horizontally split rear airstair door in between; powered by two 1,700 hp (1,300 kW) Klimov TV2-117A turboshaft engines.[source]Mil Mi-8 · Variants / Civil; only the objects and conditions stated in this passage Civilian VIP transport version, with accommodation for between 9 and 11 passengers, equipped with a galley and toilet.[source]Mil Mi-8 · Variants / Civil; only the objects and conditions stated in this passage Deluxe VIP transport version, with accommodation for between 7 and 9 passengers.[source]Mil Mi-8 · Variants / Civil; only the objects and conditions stated in this passage Capacity: 24 passengers or 12 stretchers and seat for one medical attendant or 4,000 kg (8,800 lb) on internal/external hardpoints[source]Mil Mi-8 · Specifications (Mi-8MT); only the objects and conditions stated in this passage Length: 18.4 m (60 ft 4 in)[source]Mil Mi-8 · Specifications (Mi-8MT); only the objects and conditions stated in this passage Height: 5.5 m (18 ft 1 in)[source]Mil Mi-8 · Specifications (Mi-8MT); only the objects and conditions stated in this passage Empty weight: 7,100 kg (15,653 lb)[source]Mil Mi-8 · Specifications (Mi-8MT); only the objects and conditions stated in this passage Gross weight: 11,100 kg (24,471 lb)[source]Mil Mi-8 · Specifications (Mi-8MT); only the objects and conditions stated in this passage Max takeoff weight: 13,000 kg (28,660 lb)[source]Mil Mi-8 · Specifications (Mi-8MT); only the objects and conditions stated in this passage Powerplant: 2 × Klimov TV3-117MT turboshaft engines, 1,454 kW (1,950 hp) each[source]Mil Mi-8 · Specifications (Mi-8MT); only the objects and conditions stated in this passage Main rotor diameter: 21.29 m (69 ft 10 in)[source]Mil Mi-8 · Specifications (Mi-8MT); only the objects and conditions stated in this passage Main rotor area: 356 m 2 (3,830 sq ft)[source]Mil Mi-8 · Specifications (Mi-8MT); only the objects and conditions stated in this passage Maximum speed: 250 km/h (160 mph, 130 kn)[source]Mil Mi-8 · Specifications (Mi-8MT); only the objects and conditions stated in this passage Cruise speed: 240 km/h (150 mph, 130 kn)[source]Mil Mi-8 · Specifications (Mi-8MT); only the objects and conditions stated in this passage Range: 495 km (308 mi, 267 nmi)[source]Mil Mi-8 · Specifications (Mi-8MT); only the objects and conditions stated in this passage Ferry range: 960 km (600 mi, 520 nmi)[source]Mil Mi-8 · Specifications (Mi-8MT); only the objects and conditions stated in this passage Service ceiling: 5,000 m (16,000 ft)[source]Mil Mi-8 · Specifications (Mi-8MT); only the objects and conditions stated in this passage | — |
|---|
| Origin reported by inventory | Russia[source]Inventory Origin column; table 1, row 10, cell 2; revision 1376912133; retrieved 2026-10-02 Russia[source]Inventory Origin column; table 1, row 16, cell 2; revision 1377030471; retrieved 2026-10-02 Soviet Union / Russia[source]Inventory Origin column; table 1, row 3, cell 2; revision 1375734230; retrieved 2026-10-02 Russia[source]Inventory Origin column; table 2, row 7, cell 3; revision 1376303113; retrieved 2026-10-01 Soviet Union[source]Inventory Origin column; table 6, row 4, cell 3; revision 1367424876; retrieved 2026-10-01 | — |
|---|
| Primary users | — | CHC Helicopter Petroleum Helicopters International Bristow Helicopters Cougar Helicopters[source] |
|---|
| Developed from | — | Sikorsky S-70[source] |
|---|
| Variants | — | Sikorsky CH-148 Cyclone Sikorsky VH-92[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] |
|---|
| Reported operators |
| — |
|---|
Maximum take-off; S-92 · Max takeoff weight
Single source