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T-50 Golden Eagle

Crew

Two

Maiden Flight

August 2002

Entry into Service

April 2007

Numbers Built

60

Length

12.98m

Height

4,78m

Wingspan

9.11m

Wingspan Including Missiles

9.17m

Empty Weight

6,263kg

Maximum Take-Off Weight With External Payload

13,471kg

Type

1 x General Electric F404-102 turbofan

Engine Length

4,030mm

Engine Diameter

880mm

Engine Dry Weight

1,035kg

Take-Off Power Rating

78.7kN

Dry Thrust

53.07kN

Maximum Level Speed

1,837km per hour

Maximum Altitude

16,764m

Manoeuvrability

+8g to -3g

Range

1,851km

Service Life

Up to 10,000 hours

Number of Hardpoints

7

Guns

1 × A-50 3-barreled 20mm M197 Gatling gun

Rockets

Hydra 70, LOGIR

Air-to-Ground Missiles

AIM-9 Sidewinder, AIM-120 AMRAAM

Bombs

Mk 82, Mk 83 and Mk 84 general purpose bombs with SPICE, JDAM or JDAM-ER guidance kits; CBU-97 / 105 sensor fused weapons, laser-guided bombs

Manufacturer

Korean Aerospace Industries and Lockheed Martin Corporation

Operator

Republic of Korean Air Force

Engines

General Electric

Landing Gear

Messier Dowty

Fuel System

Argo-Tech

Power Systems

Hamilton Sundstrand

Three-barrel M61 Cannon

General Dynamics

Cockpit Ejection Seats

Martin Baker

VIR-130A integrated VOR / Instrument Landing System

Rockwell Collins

Avionics

Lockheed Martin

Head Up Displays

BAE Systems

Multifunctional Displays

Honeywell
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