Brief History
Philippine Air Force acquisition if a twelve FA-50 is part of the Armed Forces of the Philippines Modernization Plan Horizon 1 which aim to enhance the Southeast Asian Country's defense capabilities.
FA-50 first maiden flight took place at Sancheon, South Korea on June 19, 2015. The first two FA-50 delivery that arrive in Clark Air Base was on November 18, 2015.
The Philippine Air Force F-5A freedom fighter retirement on 2005 made it no platform as dedicated air defense. A procurement program to replace the retired Philippine Air Force was under development for sometime which aim to equip with one squadron of twelve fighters.
It was initially planned that Philippine Air Force would acquire surplus US Air Force F-16 C/D multi-role fighter aircraft to meet this requirement. However, the cost was too high that eliminated this option.
In August 2012, the Philippine Air Force sent letter of intent to South Korea to buy the Korea Aerospace Industries FA-50 Advanced Trainer Aircraft.
In March 2014, the Philippine Air Force signed contracts to purchase 12 FA-50 from Korean Aerospace Industries. In addition to the requirements, it will install an advance radar system which enable to use medium range air to air missiles on four aircraft was revealed. This will give the capability of beyond visual range and it will enable the Philippine Air Force to undertake long range interception missions.
Conception of the FA-50 in Korea
Initially, the FA-50 was intended as new light combat aircraft for the Republic of Korea Air Force (ROKAF) and manufactured by the Korea Aerospace Industries (KAI). It is a supersonic light combat version of the T-50 Golden Eagle advance jet trainer and light attack aircraft.
In October 1997, the development of the FA-50 combat aircraft begun. There were six prototypes built during the development phase which concluded in January 2006. In October 2012, the FA-50 awarded military type certificate by the Korean Military Aircraft Airworthiness Committee (MAAC). It is the first locally made fighter-class military aircraft to received the MAAC certification
Features of the FA-50
The FA-50 is a combat aircraft that meets its intended requirements as a light fighter aircraft of Air Forces around the world. It's detection capability is similar to that of the KF-16 fighter because of the advanced radar installed.
The dimension of the FA-50 is measures 13.14 meters in length, 9.45 meters in width and 4.82 meters in height. The aircraft's empty weight is 6.47 tons and the maximum take-off weight of 12.3 tons.
FA-50 Cockpit an Avionics
The designed tandem glass cockpit of the FA-50 enables it to carry two crew members. The high mounted canopy provides the pilot with good visibility and has been tested to protect the canopy against four pound objects impacting at a speed of 400 knots. The applied stretched acrylic fiber has develop by Hankuk Fiber. The cockpit is equipped with the wide field of view head-up display (HUD), colored multi function displays (MFD), Hands On throttle and Sticks (HOTAS), digital engine instrumentation, zero zero ejection seat and integrated up-front controls.
The flight control systems includes active stick, digital fly-by-wire, digital break-by-wire, electrical emergency power power unit and triple redundant electrical system.
The cockpit has an on-board Night Vision Imaging System (NVIS) to ensure the aircraft a mission capability during day and night. Also it integrates an On-Board Oxygen Generation Systems (OBOGS).
The avionics system package consists of identification friend or foe (IFF), embedded Inertial Navigation System / Global Positioning System (INS/GPS), radar altimeter, integrated mission computer, UHF/VHF radio, data transfer and recording system, store management system, Counter Measure Dispensing System (CMDS) and Radar Warning Receiver (RWR).
Armament and Weapon System
The FA-50 fighter aircraft can carry an array of different weapons load of up to 4.5 tons. It can be armed from different variety of weapons from air-to-air to air-to-ground missiles. These includes with AIM-9 sidewinder short-range air-to-air heat seeking missiles, GBU-38/B Joint Direct Attack Munitions (JDAM), AGM-65 Maverick air-to-ground tactical missiles (AGM), Mark 82 Low Drag General Purpose (LDGP) bombs, CBU-105 Sensor Fused Weapons (SFW), and Cluster Bomb Units (CBUs). The FA-50 has an internal, three barrel 20 mm Gatling gun and LAU-3/A 19-tube 2.75 inch rocket launcher for firing Folding Fin Aerial Rockets (FFAR).
Engine and Performance
The FA-50 aircraft's power plant integrates a General Electric F404-GE-102 turbofan engine that develops 17,700 lbs of thrust with an afterburner. The engine has a three stage fans with seven axial stage arrangement. The dual channel Full Authority Digital Engine Control (FADEC) System controls the engine performance. The internal fuel tank capacity is 2,655 liters and an additional of 1,710 liters of fuel in the three external fuel tanks. The maximum altitude is 14,000 meters (48,000 feet) and the air frame is designed to last 8,000 hours of service. The maximum speed of Mach 1.5 or one and half times the speed of sound.