Mi-26T2 Initial Operational Capability (IOC): 2015 Maiden Flight: 17 February 2011 Total Production: 26 Also Known As:Mi-26T2V Origin:Russia Corporations: Mil Helicopter and Russian Helicopters* (*) lead contractor
Parent System:Mi-26 Initial Operational Capability (IOC): 1983 Total Production: 337 Family Members:Mi-26 and Mi-26T2VA
Reviews There are no reviews so far
Description: The Mi-26T2 is a modernized ultra-heavy version of the Mi-26 helicopter launched in 2010. The newest variant features modern avionics suite fully compliant with international standards, glass cockpit, new D-136-2 engines and other equipment. The helicopter is fitted with a modern BREO-26 avionics suite designed by Ramenskoye Design Company. The glass cockpit of the Mi-26T2 is equipped with five multi-functional LCDs that can display a colored image of external load, a new digital autopilot and a new navigation system supporting NAVSTAR/GLONASS. The new avionics and equipment have brought down the crew to only two from five in existing versions of the Mi-26 aircraft. A third crew member is necessary to work with the external sling load. As of August 2011, the Mi-26T2 was undergoing test flights.
The Mi-26T2 helicopter is also fitted with an additional Tranzas TSL-1600 light to visually control external sling load at night. It is capable both of standard and IR lighting to be used in combination with night vision goggles. The Mi-26T2 is fitted with a new BREO-26 avionics suite with five multi-functional LCD displays, as well as new digital autopilot with satellite navigation support. The helicopter also features modernised D-136-2 turboshaft engines with FADEC (full authority digital engine control) which can boost output by 250 hp during flight when at full throttle. The Mi-26T2 can fly missions anywhere in the world, and can significantly enhance the battle readiness of the Russian Armed Forces. The Mi-26T2V is standard for the Russian Air Force and will be introduced in 2018.
Number of Engines: 2
Troops: 82 Power Max Power at TakeOff: 23,300 hp (17,382 kW) Weight Max Takeoff Weight: 56,000 kilogram (123,457 pound)
Payload: 20,000 kilogram (44,092 pound)
CEP: Circular Error Probable
Meters (m) Kilometers (km) Nautic Miles (nm) Inch (in) Yard (yd) Foot (ft) Millimeter (mm)
Pound (lb) Kilogram (kg) kN (KiloNewton) Ton (t)
Meters per Second (mps) Kilometers per Hour (kph) Knot (kt) Miles per Hour (mph)
Liter (l) Galon (gl)
Year (yr) Minutes (min) Second (sec)
There are 9 news between 11 Aug 2011 and 4 Jul 2019