Boeing (Hughes) AH-64 Apache vs Mil Mi-28 (Havoc) Comparison

Aviation | Utilities | Side-by-Side Comparison

Direct side-by-side comparison of two aircraft.

Your selected aircraft are compared in side-by-side arrangement below. You can always go back and Compare any two aircraft in our database. Some entries contain '0', 'not available', or an 'NA' value. This is more common with conceptual, experimental, and x-plane designs. Rotary-wing system (i.e. helicopters) values include main rotor diameter as part of width/wingspan measurement. UAV entries may display crew values as '0', not taking into account ground-based controllers.

Subjects

Boeing AH-64D Apache Longbow
Dedicated Two-Seat Attack Helicopter

Mil Mi-28N (Havoc)
Dedicated Twin-Seat, Twin-Engine Attack Helicopter

Basics

ORIGIN
United States

ORIGIN
Russia

YEAR
1986 [Diff.-23 yrs]

YEAR
2009 [Diff.+23 yrs]

CREW
2

PRODUCTION
2,268 units [Diff.+2,142]

PRODUCTION
126 units [Diff.-2,142]

Dimensions

LENGTH
58.2 ft (17.8 m) [Diff.+2.4 ft]

LENGTH
55.8 ft (17.0 m) [Diff.-2.4 ft]

WIDTH/SPAN
48.1 ft (14.7 m) [Diff.-8.4 ft]

WIDTH/SPAN
56.4 ft (17.2 m) [Diff.+8.4 ft]

HEIGHT
12.7 ft (3.9 m) [Diff.-2.7 ft]

HEIGHT
15.4 ft (4.7 m) [Diff.+2.7 ft]

Relative Size Comparison

Shapes below depict aircraft from wingtip-to-wingtip / nose-to-tail assuming aircraft are being viewed from overhead perspective (the nose pointing towards the top of the screen). Helicopter widths include main rotor diameter. If any dimensional values are "NA" in the database then the presented shapes may appear skewed.

Boeing AH-64D Apache Longbow

Mil Mi-28N (Havoc)

Weights

EMPTY WT.
11,799 lb (5,352 kg) [Diff.-7,161 lb]

EMPTY WT.
18,960 lb (8,600 kg) [Diff.+7,161 lb]

M.T.O.W.
22,282 lb (10,107 kg) [Diff.-3,071 lb]

M.T.O.W.
25,353 lb (11,500 kg) [Diff.+3,071 lb]

Installed Power

2 x General Electric T700-GE-701C turboshaft engines developing 1,890 shaft horsepower and driving four-bladed main and twin-bladed "double" tail rotor.

2 x Klimov TV3-117VMA turboshaft engines developing 2,200 horsepower each while driving a five-bladed main rotor and four-bladed tail rotor.

Performance

SPEED
183 mph (295 kph) [Diff.-16 mph]

SPEED
199 mph (320 kph) [Diff.+16 mph]

RANGE
298 miles (480 km) [Diff.-385 miles]

RANGE
684 miles (1,100 km) [Diff.+385 miles]

CEILING
20,997 ft (6,400 m) [Diff.+1,969 feet]

CEILING
19,029 ft (5,800 m) [Diff.-1,969 feet]

RATE-OF-CLIMB
2,415 ft/min [Diff.-265 feet]

RATE-OF-CLIMB
2,680 ft/min [Diff.+265 feet]

Armament

STANDARD:
1 x 30mm Hughes chain gun / automatic cannon in powered, traversing chin-mounted turret.

OPTIONAL:
Four underwing hardpoints and two wing stub endpoints for various mission-specific air-launched ordnance including:

16 x AGM-114 "Hellfire" Anti-Tank Guided Missiles (ATGMs).
4 x Hydra-70 2.75" 19-Shot FFAR (Folding-Fin Aerial Rocket) rocket pods.
2 x AIM-92 "Stinger" short-ranged, air-to-air missiles in ATAS twin missile mount launchers.
4 x Auxiliary Fuel Tanks.

TRIALED:
4 x AIM-9 "Sidewinder" air-to-air missiles.
4 x "Sidearm" anti-radiation missiles.

Up to 1,600lb of externally carried / launched ordnance.

STANDARD:
1 x 30mm Shipunov 2A42 cannon in powered traversing chin mounting.

OPTIONAL (Mission Specific):
4 hardpoints for 4,230 lb of externally-held ordnance including rocket pods, up to 16 x AT-6 "Spiral" anti-armor / anti-tank air-to-surface missiles, and gun pods / cannon pods as needed.

Going Further

View Entry
(Boeing (Hughes) AH-64 Apache)

View Entry
(Mil Mi-28 (Havoc))

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