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Military aircraft· Cold War· 1972

Mil Mi-24

attack helicopter family by Mil

The Mil Mi-24 (Russian: Миль Ми-24; NATO reporting name: Hind) is a large helicopter gunship, attack helicopter and low-capacity troop transport with room for eight passengers. It is produced by Mil Moscow Helicopter Plant and was introduced by the Soviet Air Force in 1972. As of 2026, the helicopter is used worldwide by 52 countries. In NATO circles, the export versions, Mi-25 and Mi-35, are denoted with a letter suffix as "Hind D" and "Hind E". Soviet pilots called the Mi-24 the "flying tank" (Russian: летающий танк, romanized: letayushchiy tank), a term used historically with the famous World War II Soviet Il-2 Shturmovik armored ground attack aircraft. Other common unofficial nicknames were "Galina" (or "Galya"), "Crocodile" (Russian: Крокодил, romanized: Krokodil), due to the helicopter's camouflage scheme, and "Drinking Glass" (Russian: Стакан, romanized: Stakan), because of the flat glass plates that surround earlier Mi-24 variants' cockpits.

== Development == During the early 1960s, it became apparent to Soviet designer Mikhail Mil that the trend towards ever-increasing battlefield mobility would result in the creation of flying infantry fighting vehicles, which could be used to perform both fire support and infantry transport missions. The first expression of this concept was a mock-up unveiled in 1966 in the experimental department of the Ministry of Aircraft's factory number 329, where Mil was head designer. The mock-up designated V-24 was based on another project, the V-22 utility helicopter, which never flew. The V-24 had a central infantry compartment that could hold eight troops sitting back to back, and a set of small wings positioned to the top rear of the passenger cabin, capable of holding up to six missiles or rockets and a twin-barreled GSh-23L cannon fixed to the landing skid.

Mil proposed the design to the heads of the Soviet armed forces. While he had the support of a number of strategists, he was opposed by several more senior members of the armed forces, who believed that conventional weapons were a better use of resources. Despite the opposition, Mil managed to persuade the defence minister's first deputy, Marshal Andrey A. Grechko, to convene an expert panel to look into the matter. While the panel's opinions were mixed, supporters of the project eventually held sway and a request for design proposals for a battlefield support helicopter was issued. The development and use of gunships and attack helicopters by the US Army during the Vietnam War convinced the Soviets of the advantages of armed helicopter ground support, and fostered support for the development of the Mi-24. Mil engineers prepared two basic designs: a 7-ton single-engine design and a 10.5-ton twin-engine design, both based on the 1,300 kW (1,700 hp) Izotov TV3-177A turboshaft. Later, three complete mock-ups were produced, along with five cockpit mock-ups to allow the pilot and weapon station operator positions to be fine-tuned. The Kamov design bureau suggested an army version of their Ka-25 ASW helicopter as a low-cost option. This was considered but later dropped in favor of the new Mil twin-engine design. A number of changes were made at the insistence of the military, including the replacement of the 23 mm cannon with a rapid-fire heavy machine gun mounted in a chin turret, and the use of the 9K114 Shturm (AT-6 Spiral) antitank missile. A directive was issued on 6 May 1968 to proceed with the development of the twin-engine design. Work proceeded under Mil until his death in 1970. Detailed design work began in August 1968 under the codename Yellow 24. A full-scale mock-up of the design was reviewed and approved in February 1969. Flight tests with a prototype began on 15 September 1969 with a tethered hover, and four days later the first free flight was conducted. A second prototype was built, followed by a test batch of ten helicopters.

Acceptance testing for the design began in June 1970, continuing for 18 months. Changes made in the design addressed structural strength, fatigue problems and vibration levels. Also, a 12-degree anhedral was introduced to the wings to address the aircraft's tendency to Dutch roll at speeds in excess of 200 km/h (124 mph), and the Falanga missile pylons were moved from the fuselage to the wingtips. The tail rotor was moved from the right to the left side of the tail, and the rotation direction reversed. The tail rotor now rotated up on the side towards the front of the aircraft, into the downwash of the rotor, which increased its efficiency. A number of other design changes were made until the production version Mi-24A (izdeliye 245) entered production in 1970, obtaining its initial operating capability in 1971 and was officially accepted into the state arsenal in 1972. In 1972, following completion of the Mi-24, development began on a unique attack helicopter with transport capability. The new design had a reduced transport capability (three troops instead of eight) and was called the Mi-28, and that of the Ka-50 attack helicopter, which is smaller and more maneuverable and does not have the large cabin for carrying troops. In October 2007, the Russian Air Force announced it would replace its Mi-24 fleet with Mi-28Ns and Ka-52s by 2015. However, after the successful operation of the type in Syria it was decided to keep it in service and upgrade it with new electronics, sights, arms and night vision goggles.

Design

Overview

The core of the aircraft was derived from the Mil Mi-8 (NATO reporting name "Hip") with two top-mounted turboshaft engines driving a mid-mounted 17.3 m (57 ft) five-blade main rotor and a three-blade tail rotor. The engine configuration gave the aircraft its distinctive double air intake. Original versions have an angular greenhouse-style cockpit; Model D and later have a characteristic tandem cockpit with a "double bubble" canopy. Other airframe components came from the Mi-14 "Haze". Two mid-mounted stub wings provide weapon hardpoints, each offering three stations, in addition to providing lift. The loadout mix is mission dependent; Mi-24s can be tasked with close air support, antitank operations, or aerial combat. The Mi-24's titanium rotor blades are resistant to 12.7 mm (.50 caliber) rounds. The cockpit is protected by ballistic-resistant windscreens and a titanium-armored tub. The cockpit and crew compartment are overpressurized to protect the crew in NBC conditions.

Flight characteristics

Considerable attention was given to making the Mi-24 fast. The airframe was streamlined, and fitted with retractable tricycle undercarriage landing gear to reduce drag. At high speed, the wings provide considerable lift (up to a quarter of total lift). The main rotor was tilted 2.5° to the right from the fuselage to compensate for translating tendency at a hover. The landing gear was also tilted to the left so that the rotor would still be level when the aircraft was on the ground, making the rest of the airframe tilt to the left. The tail was also asymmetrical to give a side force at speed, thus unloading the tail rotor. A modified Mi-24B, named A-10, was used in several speed and time-to-climb world record attempts. The helicopter had been modified to reduce weight as much as possible—one measure was the removal of the stub wings. The previous official speed record was set on 13 August 1975 over a closed 1,000 km (620 mi) course of 332.65 km/h (206.70 mph); many of the female-specific records were set by the all-female crew of Galina Rastorguyeva and Lyudmila Polyanskaya. On 21 September 1978, the A-10 set the absolute speed record for helicopters with 368.4 km/h (228.9 mph) over a 15/25 km course. The record stood until 1986, when it was broken by the current official record holder, a modified British Westland Lynx.

Comparison to Western helicopters

As a combination of armoured gunship and troop transport, the Mi-24 has no direct NATO counterpart. While the UH-1 ("Huey") helicopters were used by the US in the Vietnam War either to ferry troops, or as gunships, they were not able to do both at the same time. Converting a UH-1 into a gunship meant stripping the entire passenger area to accommodate extra fuel and ammunition, and removing its troop transport capability. The Mi-24 was designed to do both, and this was greatly exploited by airborne units of the Soviet Army during the 1980–89 Soviet–Afghan War. The closest Western equivalent was the American Sikorsky S-67 Blackhawk, which used many of the same design principles and was also built as a high-speed, high-agility attack helicopter with limited troop transport capability using many components from the existing Sikorsky S-61. The S-67, however, was never adopted for service. Other Western equivalents are the Romanian Army's IAR 330, which is a licence-built armed version of the Aérospatiale SA 330 Puma, and the MH-60 Direct Action Penetrator, a special purpose armed variant of the Sikorsky UH-60 Black Hawk.

Operational history

=== Ogaden War (1977–1978) === The first combat use of the Mi-24 was with the Ethiopian forces during the Ogaden War against Somalia. The helicopters formed part of a massive airlift of military equipment from the Soviet Union, after the Soviets switched sides towards the end of 1977. The Mi-24s were flown by Soviet pilots and proved to be instrumental in the combined air and ground assault that allowed the Ethiopians to retake the Ogaden by the beginning of 1978. Cuban and East German aircrews reportedly also flew the helicopters during the war. They were used with great success in targeting Somali armor and artillery positions.

Chadian–Libyan conflict (1978–1987)

The Libyan air force used Mi-24A and Mi-25 units during their numerous interventions in Chad's civil war. The Mi-24s were first used in October 1980 in the battle of N'Djamena, where they helped the People's Armed Forces seize the capital. In March 1987, the Armed Forces of the North, which were backed by the US and France, captured a Libyan air force base at Ouadi-Doum in Northern Chad. Among the aircraft captured during this raid were three Mi-25s. These were supplied to France, which in turn sent one to the United Kingdom and one to the US.

Soviet war in Afghanistan (1979–1989)

The aircraft was operated extensively during the Soviet–Afghan War, mainly for bombing Mujahideen fighters. When the U.S. supplied heat-seeking Stinger missiles to the Mujahideen, the Soviet Mi-8 and Mi-24 helicopters proved to be favorite targets of the rebels. It is difficult to find the total number of Mi-24s used in Afghanistan. At the end of 1990, the whole Soviet Army had 1,420 Mi-24s. During the Afghan war, sources estimated the helicopter strength to be as much as 600 units, with up to 250 being Mi-24s, whereas a (formerly secret) 1987 Central Intelligence Agency (CIA) report says that the number of Mi-24s in theatre increased from 85 in 1980 to 120 in 1985.

==== First deployment and combat ==== In April 1979, Mi-24s were supplied to the Afghan government to deal with Mujahideen guerrillas. The Afghan pilots were well-trained and made effective use of their machines, but the Mujahideen were not easy targets. The first Mi-24 to be lost in action was shot down by guerrillas on 18 July 1979.

Despite facing strong resistance from Afghan rebels, the Mi-24 proved to be very destructive. The rebels called the Mi-24 "Shaitan-Arba (Satan's Chariot)". In one case, an Mi-24 pilot who was out of ammunition managed to rescue a company of infantry by maneuvering aggressively towards Mujahideen guerrillas and scaring them off. The Mi-24 was popular with ground troops, since it could stay on the battlefield and provide fire as needed, while "fast mover" strike jets could only stay for a short time before heading back to base to refuel. The Mi-24's favoured munition was the 80-millimetre (3.1 in) S-8 rocket, the 57 mm (2.2 in) S-5 having proven too light to be effective. The 23 mm (0.91 in) gun pod was also popular. Extra rounds of rocket ammunition were often carried internally so that the crew could land and self-reload in the field. The Mi-24 could carry ten 100-kilogram (220 lb) iron bombs for attacks on camps or strongpoints, while harder targets could be dealt with a load of four 250-kilogram (550 lb) or two 500-kilogram (1,100 lb) iron bombs. Some Mi-24 crews became experts at dropping bombs precisely on targets. Fuel-air explosive bombs were also used in a few instances, though crews initially underestimated the sheer blast force of such weapons and were caught by the shock waves. The 9K114 Shturm was used infrequently, largely due to a lack of targets early in the war that required the precision and range the missile offered and a need to keep stocks of antitank missiles in Europe. After the Mujahideen got access to more advanced antiaircraft weapons later in the war the Shturm was used more often by Mi-24 units. Combat experience quickly demonstrated the disadvantages of having an Mi-24 carrying troops. Gunship crews found the soldiers a concern and a distraction while being shot at, and preferred to fly lightly loaded anyway, especially given their operations from high ground altitudes in Afghanistan. Mi-24 troop compartment armour was often removed to reduce weight. Troops would be carried in Mi-8 helicopters while the Mi-24s provided fire support.

It proved useful to carry a technician in the Mi-24's crew compartment to handle a light machine gun in a window port. This gave the Mi-24 some ability to "watch its back" while leaving a target area. In some cases, a light machine gun was fitted on both sides to allow the technician to move from one side to the other without having to take the machine gun with him. This weapon configuration still left the gunship blind to the direct rear, and Mil experimented with fitting a machine gun in the back of the fuselage, accessible to the gunner through a narrow crawl-way. The experiment was highly unsuccessful, as the space was cramped, full of engine exhaust fumes, and otherwise unbearable. During a demonstration, an overweight Soviet Air Force general got stuck in the crawl-way. Operational Mi-24s were retrofitted with rear-view mirrors to help the pilot spot threats and take evasive action. Besides protecting helicopter troop assaults and supporting ground actions, the Mi-24 also protected convoys, using rockets with flechette warheads to drive off ambushes; performed strikes on predesignated targets; and engaged in "hunter-killer" sweeps. Hunter-killer Mi-24s operated at a minimum in pairs, but were more often in groups of four or eight, to provide mutual fire support. The Mujahideen learned to move mostly at night to avoid the gunships, and in response the Soviets trained their Mi-24 crews in night-fighting, dropping parachute flares to illuminate potential targets for attack. The Mujahideen quickly caught on and scattered as quickly as possible when Soviet target designation flares were lit nearby.

==== Attrition in Afghanistan ==== The war in Afghanistan brought with it losses by attrition. The environment itself, dusty and often hot, was rough on the machines; dusty conditions led to the development of the twin PZU ('PyleZashchitnoe Ustroystvo') air intake filters. The rebels' primary air-defence weapons early in the war were heavy machine guns and antiaircraft cannons, though anything smaller than a 23 millimetre shell generally did not do much damage to an Mi-24. The cockpit glass panels were resistant to 12.7 mm (.50 in calibre) rounds. The rebels also quickly began to use Soviet-made and US shoulder-launched, man-portable air-defense system (MANPADS) missiles such as the Strela and Redeye which had either been captured from the Soviets or their Afghan allies or were supplied from Western sources. Many of them came from stocks that the Israelis had captured during wars with Soviet backed states in the Middle East. Owing to a combination of the limited capabilities of these early types of missiles, poor training and poor material condition of the missiles, they were not particularly effective. Instead, the RPG-7, originally developed as an antitank weapon, was the first effective countermeasure to the Hind. The RPG-7, not designed for air defence, had inherent shortcomings in this role. When fired at the angles needed to hit aerial targets, the back-blast could easily wound the shooter, and the inevitable cloud of smoke and dust made it easy for gunners to spot the shooter's position. From 1986, the CIA began supplying the Afghan rebels with newer Stinger shoulder-launched, heat-seeking SAMs. These were a marked improvement over earlier weapons. Unlike the Redeye and SA-7, which locked on to only infrared emissions, the Stinger could lock onto both infrared and ultraviolet emissions. This enabled the operator to engage an aircraft from all angles rather than just the tail and made it significantly more resistant to countermeasures like flares. In addition the Mil helicopters, particularly the Mi-24, suffered from a design flaw in the configuration of their engines that made them highly vulnerable to the Stinger. The Mi-24, along with the related Mi-8 and Mi-17 helicopters, had its engines placed in an inline configuration in an attempt to streamline the helicopter to increase speed and minimize the aircraft's overall frontal profile to incoming fire in a head on attack. However this had the effect of leaking all the exhaust gasses from the Mi-24's engines directly out the side of the aircraft and away from the helicopter's rotor wash, creating two massive sources of heat and ultraviolet radiation for the Stinger to lock onto. The inline placement of the engines was seen as so problematic in this regard that Mil designers abandoned the configuration on the planned successor to the Mi-24, the Mil Mi-28, in favour of an engine placement more akin to Western attack helicopters which vents the exhaust gasses into the helicopter's main rotor wash to dissipate heat. Initially, the attack doctrine of the Mi-24 was to approach its target from high altitude and dive downwards. After the introduction of the Stinger, doctrine changed to "nap of the earth" flying, where they approached very low to the ground and engaged more laterally, popping up to only about 200 ft (61 m) in order to aim rockets or cannons. Countermeasure flares and missile warning systems would be installed in all Soviet Mil Mi-2, Mi-8, and Mi-24 helicopters, giving pilots a chance to evade missiles fired at them. Heat dissipation devices were also fitted to exhausts to decrease the Mi-24's heat signature. Tactical and doctrinal changes were introduced to make it harder for the enemy to deploy these weapons effectively. These reduced the Stinger threat, but did not eliminate it. Mi-24s were also used to shield jet transports flying in and out of Kabul from Stingers. The gunships carried flares to blind the heat-seeking missiles. The crews called themselves "Mandatory Matrosovs", after a Soviet hero of World War II who threw himself across a German machine gun to let his comrades break through. According to Russian sources, 74 helicopters were lost, including 27 shot down by Stinger and two by Redeye. In many cases, the helicopters with their armour and durable construction could withstand significant damage and able to return to base.

==== Mi-24 crews and end of Soviet involvement ==== Mi-24 crews carried AK-74 assault rifles and other hand-held weapons to give them a better chance of survival if forced down. Early in the war, Marat Tischenko, head of the Mil design bureau visited Afghanistan to see what the troops thought of his helicopters, and gunship crews put on several displays for him. They even demonstrated manoeuvres, such as barrel rolls, which design engineers considered impossible. An astounded Tischenko commented, "I thought I knew what my helicopters could do, now I'm not so sure!" The last Soviet Mi-24 shot down was during the night of 2 February 1989, with both crewmen killed. It was also the last Soviet helicopter lost during nearly 10 years of warfare.

Mi-24s in Afghanistan after Soviet withdrawal

Mi-24s passed on to Soviet-backed Afghan forces during the war remained in dwindling service in the grinding civil war that continued after the Soviet withdrawal. Afghan Air Force Mi-24s in the hands of the ascendant Taliban gradually became inoperable, but a few flown by the Northern Alliance, which had Russian assistance and access to spares, remained operational up to the US invasion of Afghanistan in late 2001. In 2008, the Afghan Air Force took delivery of six refurbished Mi-35 helicopters, purchased from the Czech Republic. The Afghan pilots were trained by India and began live firing exercises in May 2009 in order to escort Mi-17 transport helicopters on operations in restive parts of the country. India would also supply four upgraded Mil-35s to the Afghan Air Force in 2015.

=== Iran–Iraq War (1980–1988) === The Mi-25 saw considerable use by the Iraqi Army during the long war against Iran. Its heavy armament caused severe losses to Iranian ground forces during the war. However, the Mi-25 lacked an effective antitank capability, as it was only armed with obsolete 9M17 Skorpion missiles. This led the Iraqis to develop new gunship tactics, with help from East German advisors. The Mi-25s would form "hunter-killer" teams with French-built Aérospatiale Gazelles, with the Mi-25s leading the attack and using their massive firepower to suppress Iranian air defences, and the Gazelles using their HOT missiles to engage armoured fighting vehicles. These tactics proved effective in halting Iranian offensives, such as Operation Ramadan in July 1982.

This war also saw the only confirmed air-to-air helicopter battles in history with the Iraqi Mi-25s flying against Iranian AH-1J SeaCobras (supplied by the United States before the Iranian Revolution) on several separate occasions. In November 1980, not long after Iraq's initial invasion of Iran, two Iranian SeaCobras engaged two Mi-25s with TOW wire-guided antitank missiles. One Mi-25 went down immediately, the other was badly damaged and crashed before reaching base. The Iranians repeated this accomplishment on 24 April 1981, destroying two Mi-25s without incurring losses to themselves. One Mi-25 was also downed by an IRIAF F-14A. The Iraqis hit back, claiming the destruction of a SeaCobra on 14 September 1983 (with YaKB machine gun), then three SeaCobras on 5 February 1984 and three more on 25 February 1984 (two with Falanga missiles, one with S-5 rockets). A 1982 news article published on the Iraqi Observer claimed an Iraqi Mi-24D shot down an Iranian F-4 Phantom II using its armaments, either antitank missiles, guns or S-5 unguided rockets. After a lull in helicopter losses, each side lost a gunship on 13 February 1986. Later, a Mi-25 claimed shooting down a SeaCobra with YaKB gun on 16 February, and a SeaCobra claimed downing a Mi-25 with rockets on 18 February. The last engagement between the two types was on 22 May 1986, when Mi-25s shot down a SeaCobra. The final claim tally was 10 SeaCobras and 6 Mi-25s destroyed. The relatively small numbers and the inevitable disputes over actual kill numbers makes it unclear if one gunship had a real technical superiority over the other. Iraqi Mi-25s also claimed 43 kills against other Iranian helicopters, such as Agusta-Bell UH-1 Hueys. In general, the Iraqi pilots liked the Mi-25, in particular for its high speed, long range, high versatility and large weapon load, but disliked the relatively ineffectual antitank guided weapons and lack of agility.

=== Nicaraguan civil war (1980–1988) === Mi-25s were also used by the Nicaraguan Army during the civil war of the 1980s. Nicaragua received 12 Mi-25s (some sources claim 18) in the mid-1980s to deal with "Contra" insurgents. The Mi-25s performed ground attacks on the Contras and were also fast enough to intercept light aircraft being used by the insurgents. The U.S. Reagan Administration regarded introduction of the Mi-25s as a major escalation of tensions in Central America. Two Mi-25s were shot down by Stingers fired by the Contras. A third Mi-25 was damaged while pursuing Contras near the Honduran border, when it was intercepted by Honduran F-86 Sabres and A-37 Dragonflies. A fourth was flown to Honduras by a defecting Sandinista pilot in December 1988.

=== Sri Lankan Civil War (1987–2009) === The Indian Peace Keeping Force (1987–90) in Sri Lanka used Mi-24s when an Indian Air Force detachment was deployed there in support of the Indian and Sri Lankan armed forces in their fight against various Tamil militant groups such as the Liberation Tigers of Tamil Eelam (LTTE). It is believed that Indian losses were considerably reduced by the heavy fire support from their Mi-24s. The Indians lost no Mi-24s in the operation, as the Tigers had no weapons capable of downing the gunship at the time. Since 14 November 1995, the Mi-24 has been used by the Sri Lanka Air Force in the war against the LTTE liberation group and has proved highly effective at providing close air support for ground forces. The Sri Lanka Air Force operates a mix of Mi-24/-35P and Mi-24V/-35 versions attached to its No. 9 Attack Helicopter Squadron. They have recently been upgraded with modern Israeli FLIR and electronic warfare systems. Five were upgraded to intercept aircraft by adding radar, fully functional helmet mounted target tracking systems, and AAMs. More than five Mi-24s have been lost to LTTE MANPADS, and another two lost in attacks on air bases, with one heavily damaged but later returned to service.

Peruvian operations (1989–present)

The Peruvian Air Force received 12 Mi-25Ds and 2 Mi-25DU from the Soviets in 1983, 1984, and 1985 after ordering them in the aftermath of 1981 Paquisha conflict with Ecuador. Seven more second hand units (4 Mi-24D and 3 Mi-25D) were obtained from Nicaragua in 1992. These have been permanently based at the Vitor airbase near La Joya ever since, operated by the 2nd Air Group of the 211th Air Squadron. Their first deployment occurred in June 1989 during the war against Communist guerrillas in the Peruvian highlands, mainly against Shining Path. Despite the conflict continuing, it has decreased in scale and is now limited to the jungle areas of Valley of Rivers Apurímac, Ene and Mantaro (VRAEM). Peru also employed Mi-25s against Ecuadorian forces during the short Cenepa conflict in early 1995. The only loss occurred on 7 February, when a FAP Mi-25 was downed after being hit in quick succession by at least two, probably three, 9K38 Igla shoulder-fired missiles during a low-altitude mission over the Cenepa valley. The three crewmen were killed. By 2011 two Mi-35P were purchased from Russia to reinforce the 211th Air Squadron.

Persian Gulf War (1991)

The Mi-24 was also heavily employed by the Iraqi Army during their invasion of Kuwait, although most were withdrawn by Saddam Hussein when it became apparent that they would be needed to help retain his grip on power in the aftermath of the war. In the ensuing 1991 uprisings in Iraq, these helicopters were used against dissidents as well as fleeing civilian refugees.

=== Sierra Leone Civil War (1991–2002) === Three Mi-24Vs owned by Sierra Leone and flown by South African military contractors, including Neall Ellis, were used against RUF rebels. In 1995, they helped drive the RUF from the capital, Freetown. Neall Ellis also piloted a Mi-24 during the British-led Operation Barras against West Side Boys. Guinea also used its Mi-24s against the RUF on both sides of the border and was alleged to have provided air support to the LURD insurgency in northern Liberia in 2001–03.

=== Croatian War of Independence (1990s) === Twelve Mi-24s were delivered to Croatia in 1993, and were used effectively in 1995 by the Croatian Army in Operation Storm against the Army of Krajina. The Mi-24 was used to strike deep into enemy territory and disrupt Krajina army communications. One Croatian Mi-24 crashed near the city of Drvar, Bosnia and Herzegovina due to strong winds. Both the pilot and the operator survived. The Mi-24s used by Croatia were obtained from Ukraine. One Mi-24 was modified to carry Mark 46 torpedoes. The helicopters were withdrawn from service in 2004.

=== First and Second Wars in Chechnya (1990s–2000s) === During the First and Second Chechen Wars, beginning in 1994 and 1999 respectively, Mi-24s were employed by the Russian armed forces. In the first year of the Second Chechen War, 11 Mi-24s were lost by Russian forces, about half of which were lost as a result of enemy action.

Sudanese Civil War (1995–2005)

In 1995, the Sudanese Air Force acquired six Mi-24s for use in Southern Sudan and the Nuba Mountains to engage the SPLA. At least two aircraft were lost in non-combat situations within the first year of operation. A further twelve were bought in 2001, and used extensively in the oil fields of Southern Sudan. Mi-24s were also deployed to Darfur in 2004–05.

=== First and Second Congo Wars (1996–2003) === Three Mi-24s were used by Mobutu's army and were later acquired by the new Air Force of the Democratic Republic of the Congo. These were supplied to Zaire in 1997 as part of a French-Serbian contract. At least one was flown by Serbian mercenaries. One hit a power line and crashed on 27 March 1997, killing the three crew and four passengers. Zimbabwean Mi-24s were also operated in coordination with the Congolese Army. The United Nations peacekeeping mission employed Indian Air Force Mi-24/-35 helicopters to provide support during the Second Congo War. The IAF has been operating in the region since 2003.

=== Kosovo War (1998–1999) === Two second-hand Mi-24Vs procured from Ukraine earlier in the 1990s were used by the Yugoslav Special Operation Unit (JSO) against Kosovo Albanian rebels during the Kosovo War.

Insurgency in Macedonia (2001)

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