Korea Aerospace Industries · Korea, South · ICAO: T-50 · 1900–Present ·
$21 million (2008)

The KAI T-50 Golden Eagle is a series of South Korean supersonic advanced trainers and light combat aircraft designed and produced by Korea Aerospace Industries (KAI) together with Lockheed Martin. It is the first indigenous supersonic aircraft of South Korea and one of the few supersonic trainers in the world.

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Engine:
1× General Electric F404-102
Engine type:
Turbofan
Thrust:
17,700 lbf  ·  79 kN
Avionics:
Honeywell H-764
Wing Tips:
No winglets
Seats:
2
Exterior length:
43 ft 1 in · 13.14 m
Tail height:
16 ft 2 in · 4.94 m
Fuselage diameter:
ft 3 in · 1.00 m
Wing span / rotor:
31 ft 0 in · 9.45 m
Max takeoff weight:
27,100 lb  ·  12,300 kg
Max landing weight:
22,700 lb  ·  10,300 kg
Max Payload:
12,900 lb  ·  5,850 kg
Fuel capacity:
730 gal  ·  2,800 L  ·  2,200 kg  (Jet A)
Max cruise speed:
992 kt  ·  1,142 mph  ·  1,837 km/h
Approach speed (Vref):
130 kt  ·  150 mph  ·  241 km/h
Range:
999 nm  ·  1,150 mi  ·  1,850 km
Ceiling:
48,000 ft  ·  14,600 m
Rate of climb:
39,000 ft/min  ·  198 m/s
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The KAI T-50 program was initially planned to develop an original South Korean trainer aircraft capable of supersonic flight, to train and equip pilots for the General Dynamics KF-16 and McDonnell Douglas F-15K, and to replace previous Northrop T-38 and Cessna A-37 trainers in service with the Republic of Korea Air Force (ROKAF). Generally, the T-50 family of aircraft is almost the same as the KF-16 in the configuration.

In February 2000, the aircraft was officially named as the T-50 Golden Eagle. The final assembly of the first T-50 started from January 15 to September 14, 2011. In August 2002, the T-50 conducted its maiden flight. An initial operational assessment took place from July 28 to August 14, 2003. KAI is currently working with Lockheed Martin for an international joint marketing program of the T-50. In December 2003, the ROKAF placed a production contract for twenty-five aircraft, expected to be delivered from 2005 to 2009.

The T-50 Golden Eagle is equipped with digital fly-by-wire controls and hands-on throttle-and-stick. The cockpit of the T-50 includes two multifunction displays by Honeywell, instrumentation displays, and a head-up display from BAE Systems. Lockheed Martin developed the full authority digital flight control system and avionics. The flight equipment incorporates a navigation/attack system, a Honeywell H-764G embedded global positioning/inertial navigation system, and an HG9550 radar altimeter, Collins Aerospace VIR-130A/instrument landing system, and ARN-153V advanced digital TACAN receiver. The cockpit is equipped with an Onboard Oxygen Generating System (OBOGS) and ejection seats from Martin-Baker.

The aircraft has an exterior length of 13.14 meters, a height of 4.94 meters, and a fuselage diameter of 1 meter. It is equipped with retractable tricycle undercarriage from Messier Dowty. The wheelbase is 5.2 meters.

General Electric F404-102 turbofan engine powers the T-50. The engine has a maximum power of 17,700 lbf. The T-50 has a maximum cruise speed of 992 knots and a travel range of 999 nautical miles. The service ceiling is 48,000 feet and the rate of climb is 39,000 feet per minute.

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