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Mi-28 Havoc

Russian attack helicopter, noted for operations in Chechnya, Syria, and Iraq, purposed for anti-armor, anti-aircraft, and combat roles. Key figures: top speed 324 km/h, range 1,100 km, service ceiling 5,700 m, max takeoff weight 12,000 kg, unit price $15M, built 126. In service with 5 air forces as of 2026 — Russia (113), Algeria (42), Iraq (17) and 2 others.

Mil Mi-28 Havoc military helicopters side profile drawing
Side profile · Mil Mi-28 Havoc · length 17.0 m
Mil Mi-28 Havoc military helicopters in flight
Max speed
324km/h
Range
1,100km
Produced
126units
Avg unit price
$15 million
Active worldwide
177+140 on order
Technical SpecificationsVersion: Mi-28N Havoc-B
Crew2 (pilot, WSO)
Length17.0 m (55.8 ft)
Wingspan17.2 m (56.4 ft)
Height4.7 m (15.4 ft)
Empty weight8,590 kg (18,938 lbs)
Max. takeoff weight12,000 kg (26,455 lbs)
Powerplant2 × turboshafts Klimov TV3-117VMA 1,641 kW each
PerformanceVersion: Mi-28N Havoc-B
Maximum speed324 km/h (201 mph)
Operational range1,100 km (684 mi)
Service ceiling5,700 m (18,701 ft)
Climb rate13.6 m/s (44.6 ft/s)
Operators — 2026
ActiveOn order
Live Losses TrackerUpdated daily

14 losses recorded here in the Russia-Ukraine War.

All Operators
🇩🇿 Algeria· 🇮🇷 Iran· 🇮🇶 Iraq· 🇷🇺 Russia· 🇺🇬 Uganda· 🇻🇪 Venezuela

Description

The Mil Mi-28 (NATO reporting name "Havoc") is a Soviet-designed heavy-weight, tandem-seat anti-armour attack helicopter produced by Mil and built at Rosvertol. Designed purely as an attack platform without secondary transport capabilities, the aircraft officially entered service with the Russian Air Force in October 2009. It is characterized by an under-nose cannon turret, stub-wing weapon pylons, and integrated heavy cockpit armor.

Development

Development began in 1972 as an anti-tank platform following the Mil Mi-24, with formal design work under Marat Tishchenko commencing in 1980. The first Mi-28 prototype flew on 10 November 1982, but the Soviet Air Force selected the Kamov Ka-50 in 1984, shifting the Mi-28 toward export development. Following the cancellation of the day-only Mi-28A variant in 1993, Mil developed the night-capable Mi-28N, which first flew on 14 November 1996. Serial production was approved at Rosvertol in Rostov-on-Don, with the first production Mi-28N delivered to the Russian military on 5 June 2006.

Design

The Mi-28 features a five-blade composite main rotor and a four-blade X-shaped biplane tail rotor. Power is provided by two top-mounted 2,200 hp Klimov VK-2500PS turboshaft engines fitted with downturned, infrared-suppressed exhausts. The fully armored tandem cockpit protects the two-person crew against 7.62 mm, 12.7 mm, and 14.5 mm armor-piercing rounds, while energy-absorbing seats and landing gear absorb vertical impacts up to 12 m/s. Target acquisition and flight navigation systems on the Mi-28N include a rotor-mast radar cover, thermal imaging, a television channel, a laser rangefinder, and a helmet-mounted target designator.

Armament

Fixed armament consists of an under-nose NPPU-28 turret containing a 30 mm Shipunov 2A42 autocannon with 250 rounds and a selectable rate of fire between 200 and 800 rounds per minute. Four pylons beneath the stub wings carry up to 16 9M120 Ataka-V anti-tank guided missiles using SACLOS guidance. Unguided ordnance options include 80 mm S-8 rockets in 20-round B8V-20 pods and 122 mm S-13 rockets in five-round B-13 pods. The aircraft can also carry R-73 air-to-air missiles, Kh-25 air-to-surface missiles, and up to 500 kg of aerial bombs.

Operational History

The Mi-28N made its combat debut during the Syrian civil war in March 2016, providing close air support during the Battle of Palmyra using Ataka missiles and S-8 rockets. Russian Mi-28 units deployed during the 2022 invasion of Ukraine, incurring confirmed aircraft losses from anti-aircraft missile systems, ground strikes, and mid-flight drone intercepts. Export deliveries include 15 Mi-28NE units to Iraq, where they saw combat usage starting in September 2014, and 42 units delivered to Algeria beginning in 2016.

Variants

  • Mi-28: Initial prototype version that conducted its maiden flight in 1982.
  • Mi-28A: Anti-tank production variant fitted with an X-shaped tail rotor and upgraded engines, cancelled in 1993 due to a lack of all-weather capability.
  • Mi-28N: All-weather day-night operational variant equipped with a mast-mounted radar, FLIR targeting system, and upgraded main gearbox.
  • Mi-28NE: Export derivative of the Mi-28N featuring directional infrared countermeasures, upgraded armor, and fire-resistant fuel systems.
  • Mi-28NM: Modernized variant fitted with VK-2500P engines, an H025 all-round radar, a redesigned nose, and integration for the LMUR missile.
Wikipedia (CC BY-SA) and other open sources. Illustrations generated by AI. Last updated on 30 August 2026. Suggest a change

Frequently Asked Questions

What type of aircraft is the Mi-28 Havoc?
The Mil Mi-28 Havoc is a military helicopters aircraft developed by Mil and entered service in 2006.
What is the maximum speed of the Mi-28 Havoc?
The Mil Mi-28 Havoc has a maximum speed of 324 km/h (201 mph).
What is the range of the Mi-28 Havoc?
The Mil Mi-28 Havoc has an operational range of 1,100 km (683 miles). This range can vary based on payload, altitude, and mission profile.
When did the Mi-28 Havoc first fly?
The Mil Mi-28 Havoc made its first flight on November 10, 1982. It entered operational service in 2006.
How many Mi-28 Havoc have been built?
Approximately 126 units of the Mil Mi-28 Havoc have been produced since it entered service in 2006.
Which countries operate the Mi-28 Havoc?
The Mil Mi-28 Havoc is operated by 5 countries with approximately 177 aircraft in active service. The largest operators include Russia, Algeria, and Iraq.
How much does a Mi-28 Havoc cost?
The Mil Mi-28 Havoc has an estimated unit cost of approximately $15.0 million. Actual prices vary based on configuration, quantity ordered, and included support packages.
What is the service ceiling of the Mi-28 Havoc?
The Mil Mi-28 Havoc has a service ceiling of 5,700 meters (18,700 feet). This is the maximum altitude at which the aircraft can maintain controlled flight.
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Latest Data Updates
  1. AUG 302026 Updated Range corrected to the ferry range with drop tanks
  2. AUG 62026 Updated Description updated
  3. AUG 52026 Updated Powerplant updated in a site-wide editorial pass
  4. JUL 232026 Updated Sources and cross-references refreshed
  5. APR 72026 Updated Sources and cross-references refreshed
  6. JAN 122026 Updated Range updated in a site-wide editorial pass