Guizhou JL-9

Chinese Advanced trainer & light attack aircraft From Wikipedia, the free encyclopedia

Guizhou JL-9

The Guizhou JL-9, also known as the FTC-2000 Mountain Eagle (Chinese: 山鹰; pinyin: Shānyīng), is a family of two-seat transonic advanced jet trainer and light combat aircraft developed by the Guizhou Aviation Industry Import/Export Company (GAIEC) for the People's Liberation Army Air Force (PLAAF) and the People's Liberation Army Naval Air Force (PLANAF).[1]

Quick Facts JL-9, Role ...
Close

Development

Summarize
Perspective

The FTC-2000 started as a GAIEC private venture to develop an inexpensive trainer for fourth generation aircraft. The trainer was revealed at the 2001 China International Aviation & Aerospace Exhibition.[2] The aircraft are reported to be produced at a GAIC assembly line in Anshun, Guizhou.[3]

The FTC-2000, as the JL-9, competed with the Hongdu JL-10 to meet the advanced trainer requirements of the PLAAF and PLANAF. The JL-10 is more technologically advanced, but also more expensive, than the JL-9. In 2013, both had entered production.[4]

A carrier-landing trainer variant was revealed by Chinese state media in 2011.[4] Designated the JL-9G, it has strengthened undercarriage, enlarged wing and diverterless supersonic inlets, but has proved to be unsuitable for arrested landings and is limited to land-based operations.[5]

On 5 September 2018, Chinese state-run Xinhua News Agency reported that GAIC had begun mass production of the FTC-2000G variant.[6] On 28 September, it was reported that the first mass-produced FTC-2000G performed its maiden flight.[7][8] In April 2020, China reported that an unnamed South-East Asian country had placed an order for the FTC-2000G, with deliveries expected between 2021 and 2023.[9] Later it was confirmed that Myanmar had ordered those jets.[10]

Design

Thumb
A FTC-2000 at Zhuhai airshow 2016

The FTC-2000 is developed from the JJ-7/FT-7, the two seat trainer version of the Chengdu J-7; the Chengdu J-7 is a Chinese variant of the MiG-21. The FTC-2000 uses a new wing, a forward fuselage with side air intakes, and a glass cockpit; the engine, empennage, and mechanical controls of the JJ-7/FT-7 are retained.[2]

Operational history

Thumb
A PLAAF JL-9 releasing flare

In 2014, the PLANAF had a regiment of JL-9s.[11] However, it was not until October 18, 2015, that the PLAAF started using the JL-9 for training purposes.[12]

In April 2023, the Rapid Support Forces of Sudan launched an attack on Merowe Air Base, destroying one Sudanese FTC-2000 while capturing the base.[13] Satellite imagery has revealed that three more FTC-2000s were present at the base at the time.[13]

On January 16, 2024, a Myanmar Air Force FTC-2000G was shot down by a Kachin Independence Army FN-6 missile in Shan State. Both pilots were killed.[14]

Variants

Thumb
FTC-2000G in Zhuhai airshow 2024

Operators

Specifications (FTC-2000)

Data from Jane's All the World's Aircraft 2010-11 [1]

General characteristics

  • Crew: 2
  • Length: 14.555 m (47 ft 9 in) excluding nose-probe
  • Wingspan: 8.32 m (27 ft 4 in)
  • Height: 4.105 m (13 ft 6 in)
  • Wing area: 26.15 m2 (281.5 sq ft)
  • Gross weight: 7,800 kg (17,196 lb) clean
7,900 kg (17,417 lb) normal
  • Max takeoff weight: 9,800 kg (21,605 lb)
  • Fuel capacity: 2,000 kg (4,409 lb) internal + up to 1,302 kg (2,870 lb) in external tanks
  • Powerplant: 1 × Guizhou Liyang WP-13F (C) afterburning turbojet, 43.15 kN (9,700 lbf) thrust dry, 63.25 kN (14,220 lbf) with afterburner
    (1 × WP-14C Kunlun-3 for FTC-2000G, 53.89 kN (12,110 lbf) thrust dry and 76.53 kN (17,200 lbf) with afterburner.)

Performance

  • Maximum speed: 1,100 km/h (680 mph, 590 kn) / Mach 0.89
  • Unstick and touchdown speed: 260 km/h (160 mph; 140 kn)
  • Minimum flying speed: 210 km/h (130 mph; 110 kn)
  • Cruise speed: 870 km/h (540 mph, 470 kn) [19]
  • Stall speed: 125 km/h (78 mph, 67 kn) [19]
  • Range: 863 km (536 mi, 466 nmi) on internal fuel
  • Ferry range: 2,400 km (1,500 mi, 1,300 nmi) with maximum internal and external fuel
  • Endurance: 3 hours
  • Service ceiling: 16,000 m (52,000 ft)
  • g limits: +8 -3
  • Rate of climb: 150 m/s (30,000 ft/min) at sea level
  • Wing loading: 374.8 kg/m2 (76.8 lb/sq ft)
  • Thrust/weight: 0.00645 kN/kg (0.658 lbf/lb)
  • Take-off run: 400–500 m (1,300–1,600 ft)
  • Landing run: 700 m (2,300 ft)

Armament

  • Guns: 1x 23 mm cannon[12]
  • Hardpoints: 5 with a capacity of 2,000 kg (4,409 lb) maximum, with provisions to carry combinations of:
    • Other: up to 3 x fuel tanks[12]
  • Missiles: ** Short range air-to-air missile

Avionics

  • Pulse Doppler radar
  • comms
  • IFF
  • Transponder
  • EFIS
  • HOTAS
  • GPS / INS

See also

Related development

Aircraft of comparable role, configuration, and era

References

Loading related searches...

Wikiwand - on

Seamless Wikipedia browsing. On steroids.