MI-17 V5 Helicopter Specifications PDF

Mil Mi-17 (NATO Reporting Name: Hip)

The Mil Mi-17 is a Soviet-designed, Russian military helicopter family, produced at two factories in Kazan and Ulan-Ude. Known as the Mi-8M series in Russian service, it is widely used as a medium twin-turbine transport helicopter, with an armed gunship version also available.

Key Information

  • Size: 1 MB
  • Total Pages: 3
  • Language: English
  • Source: rhc.aero

Capabilities and Cargo

The Mi-17 is highly efficient for cargo transportation. It features a spacious 23 m³ cargo compartment, equipped with portside and starboard sliding doors and a rear ramp to ease loading and unloading.

  • Troop capacity: Up to 36 personnel in troop seats
  • Cargo: Supports long cargo loads and vehicles
  • Internal payload: 4 tons
  • External sling payload: Up to 4 tons — ideal for delivering bulky cargo to remote areas and performing assembly tasks
  • Firefighting: Can be equipped with a water drop system

Specifications

FeatureMi-17 V5
Maximum level-flight speed250 km/h
Cruise speed230 km/h
Service ceiling6000 m
Flight range675 km (main fuel tanks) / 1180 km (with 2 auxiliary tanks)
Maximum take-off weight13,000 kg
Maximum payload4,000 kg

Components and Equipment

  • Weather radar
  • Pilot’s cockpit
  • Nose landing gear
  • Searchlight
  • Portside sliding door frame
  • LPG-150 winch
  • SLG-300 winch
  • Cargo compartment
  • TV3-117VM or VK-2500-03 engine
  • Main gearbox
  • Main rotor hub and blades
  • Auxiliary power unit
  • Radio equipment compartment
  • Tail boom and tail rotor
  • Rear ramp
  • Main landing gear
  • Main fuel tank
  • Dust protection device

Armament

  • C-8 type unguided missile system
  • Additional fuel tanks
  • Gun armament
  • Exhaust suppression system
  • Light arms

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