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Yak-130

Crew

2

Manufacturer

Irkut Corporation

Operator

Russian Air Force

Maiden Flight

April 1996

Entry into Service

July 2009

Length, Development Model

11.49m

Length, Production Model

11.245m

Height

4.76m

Wingspan

9.72m

Wing Area

23.52m²

Wing Aspect Ratio

4:1

Empty Weight

4,600kg

Typical Training Configuration Weight

5,700kg

Maximum Take-Off Weight

9,000kg

Weapon Payload

3,000kg

Internal Fuel

1,750kg

Type (Prototype)

2 x V-2S turbofan engines

Thrust (Prototype)

2,200kg each

Type (Production Aircraft)

2 x AI-222-25 turbofan engines

Thrust (Production Aircraft)

2,500kg each

Maximum Level Speed

1,060km/h

Service Ceiling

12,500m

Range With Internal Fuel

2,000km

Sustained G-limit at Mach 0.8

+4.8G

g-Limit

+8g to -3g

Landing Speed

190km/h

Landing Run

670m

Take-Off Speed

210km/h

Take-Off Run

380m

Service Life

30 years

Flight Hours

10,000 extendable to 15,000

Landings

20,000 landings

Voice Warning System

AAS Popov GZAS joint stock company
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