There are 6 images added between 29 September 2016 and 13 December 2018
Initial Operational Capability (IOC): 2019
Maiden Flight: 29 September 2016
Total Production: ?
Origin: Russia
Corporations: AS Yakovlev and IRKUT Corporation
Parent System: Yak-152
Initial Operational Capability (IOC): 2019
Maiden Flight: 29 September 2016
Total Production: ?
Family Members: L-7
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Description: The Irkut Corporation/Yakovlev Yak-152 is a twin-seat, turboprop aircraft designed to serve as primary/basic training airplane for the Russian Air Force. Russia's Irkut Corporation and Yakovlev and China's Hongdu Aviation Industry Group have been working together on the new trainer since 2004. The Russian Ministry of Defense announced on March 19, 2014, the development and completion of the new aircraft with the maiden flight planned for 2015 and the entry into service slated for November 2016. The People's Liberation Army Air Force (PLAAF) intended L-7 will provide basic training starting by the end of 2016 or later.

Russia's Irkut Corporation is meant to assemble four Yak-152 prototypes beginning in September 2014: two for flight trials, one for static tests and the fourth for fatigue testing. The prototypes will be delivered by the end of October 2015 and the trials program will complete by September 2016. The new trainer would be declared operational with the Russian Air Force by the end of November 2016. In addition to the Ministry of Defense, the new Yak-152 will serve with paramilitary sports organization DOSAAF and other civilian organizations. The Russian Air Force training program will start with MAI-223 Kityonok ultra-light aircraft, followed by the Yak-152 basic turboprop aircraft and finally pilots will transfer onto the Yak-130 advanced training jet. The Yak-152 will be provided with a retractable tricycle landing gear, powered by a German turboprop engine with the crew using SKS-94M ejection system.

Yak-152 Specifications

Crew: 2
Number of Engines: 1
Propeller Blades: 3
Service Life Flight Hours: 10,000
Max Maneuvering Load Factor: 9 g
Min Maneuvering Load Factor: -7 g
Ceiling: 4,000 meter (13,123 foot)
Landing Run Distance: 360 meter (1,181 foot)
Max Range: 1,400 kilometer (756 nautical mile)
Take Off Run Distance: 175 meter (574 foot)
Max Power at TakeOff: 360 hp
Stall Speed: 100 kph (54 knot)
Top Speed at High Altitude: 500 kph (270 KTAS)
Service Life: 30 year
Fuel Load: 200 kilogram (441 pound)
Max Takeoff Weight: 1,320 kilogram (2,910 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)
Shaft-Horse-Power (shp)

Yak-152 News

There is 1 news
on 29 Sep 2016
Thursday, September 29, 2016Yakovlev Yak-152 Initial Training Aircraft Performs Maiden Flight

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